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BOMBARDIER Chalenger 604 Supplemental Maintenance Manual

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Highlights
Pages which have been added or revised are outlined below together with the highlights of the revision.
Remove and insert the affected pages as listed.
Chapter/Section and
All
CL-604 SUPPLEMENTAL MAINTENANCE MANUAL
TO: HOLDERS OF SUPPLEMENTAL MAINTENANCE MANUAL
(SMM) FOR CHALLENGER 604 AIRCRAFT SERIAL NUMBER 5596
Page No.
Due to the extent of the changes, the entire document has been revised and
reissued. Remove the old manual in its entirety and replace with the new one.
REVISION A DATED NOV 10/2006
HIGHLIGHTS
Description of Change
Highlights
Nov 10/2006
Page 1

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Summary of Contents for BOMBARDIER Chalenger 604

  • Page 1 Highlights CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TO: HOLDERS OF SUPPLEMENTAL MAINTENANCE MANUAL (SMM) FOR CHALLENGER 604 AIRCRAFT SERIAL NUMBER 5596 REVISION A DATED NOV 10/2006 HIGHLIGHTS Pages which have been added or revised are outlined below together with the highlights of the revision. Remove and insert the affected pages as listed.
  • Page 2 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK Highlights Page 2 Nov 10/2006...
  • Page 3 Cover Supplemental Maintenance Manual Aircraft S/N: 5596...
  • Page 4 It is understood that this documentation, comprising technical data and other information in any media shall not be reproduced or disclosed in whole or in part without Bombardier’s written authorization, is proprietary and confidential to Bombardier and that all rights to patent, copyright, trademark, trade secret and other intellectual property rights therein belong to Bombardier.
  • Page 5 Introduction CL-604 SUPPLEMENTAL MAINTENANCE MANUAL INTRODUCTION General This Supplemental Maintenance Manual (SMM) contains information describing custom installation(s) and modification(s) to this aircraft, and may include procedures for periodic maintenance. The SMM supplements the Aircraft Maintenance Manual (AMM) and should be used concurrently with the AMM for maintenance activities.
  • Page 6 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK Introduction EFFECTIVITY: 5596-SMM Page 2 Revision A Nov 10/2006...
  • Page 7 Revision Log CL-604 SUPPLEMENTAL MAINTENANCE MANUAL REVISION LOG REVISION NO. REVISION DATE DESCRIPTION OF CHANGE First Issue Jun 21/2005 Revision A Nov 10/2006 Completely revised and reissued Revision Log 5596-SMM Page 1 EFFECTIVITY: Revision A Nov 10/2006...
  • Page 8 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK Revision Log EFFECTIVITY: 5596-SMM Page 2 Revision A Nov 10/2006...
  • Page 9 CHAPTER 07 - LIFTING AND SHORING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 07 - LIFTING AND SHORING THIS SECTION INTENTIONALLY LEFT BLANK 5596-SMM Page 1 EFFECTIVITY: Revision A Nov 10/2006...
  • Page 10 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 Revision A Nov 10/2006...
  • Page 11 CHAPTER 09 - TOWING AND TAXIING List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 09 - TOWING AND TAXIING LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 09 - Effective Pages Nov 10/2006 Nov 10/2006 09 - Contents Nov 10/2006 Nov 10/2006 09-10-17...
  • Page 12 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 09 - Effective Pages Revision A Nov 10/2006...
  • Page 13 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 09 - TOWING AND TAXIING TABLE OF CONTENTS Subject Ch-Se-Su Page TOWBAR STORAGE 09-10-17 Description/Operation Description/Location EFFECTIVITY: 5596-SMM Page 1 09 - Contents Revision A Nov 10/2006...
  • Page 14 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 09 - Contents Revision A Nov 10/2006...
  • Page 15 TOWBAR STORAGE CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TOWBAR STORAGE - DESCRIPTION/OPERATION ESCRIPTION OCATION Mounting provisions for the towbar and towbar head have been installed in the forward equipment compartment at approximately FS185.70, BL0.0. The towbar and towbar head are supplied as loose equipment.
  • Page 16 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 09-10-17 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 17 CHAPTER 11 - PLACARDS AND MARKINGS List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 11 - PLACARDS AND MARKINGS LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 11 - Effective Pages Nov 10/2006 Nov 10/2006 11 - Contents Nov 10/2006 Nov 10/2006 11-00-00...
  • Page 18 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 11 - Effective Pages Revision A Nov 10/2006...

  • Page 19: Table Of Contents

    Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 11 - PLACARDS AND MARKINGS TABLE OF CONTENTS Subject Ch-Se-Su Page PLACARDS AND MARKINGS 11-00-00 Description/Operation Description/Location/Operation Removal/Installation Removal Installation Inspection/Check General Visual Inspection of the Cabin Placards - Internal Servicing Discard Self-Illuminated Exit Sign EFFECTIVITY: 5596-SMM Page 1 11 - Contents...
  • Page 20 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 11 - Contents Revision A Nov 10/2006...

  • Page 21: Placards And Markings

    For aircraft placard information, refer to Bombardier Completion Center drawing, Placard General Arrangement, drawing number 6041100006, revision (B), or the latest approved revision: For water system placard information, refer to the following Bombardier Completion Center drawings: • Plumbing Instl - Split Lav, drawing number TM433810-41, revision (G), or the latest approved revision •...
  • Page 22 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 11-00-00 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...

  • Page 23: Removal

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PLACARDS AND MARKINGS - REMOVAL/INSTALLATION EMOVAL To remove the self-illuminated exit sign: WARNING: RADIOACTIVE MATERIAL - THE RECEIPT, POSSESSION, USE, AND TRANSFER OF THIS DEVCE IS SUBJECT TO A GENERAL LICENSE OR THE EQUIVALENT, AND THE REGULATIONS OF THE U. S. NUCLEAR REGULATORY COMMISSION (NRC), OR A STATE WITH WHICH THE NRC HAS ENTERED INTO AN AGREEMENT FOR THE EXERCISE OF A REGULATORY AUTHORITY.
  • Page 24 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 11-00-01 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...

  • Page 25: General Visual Inspection Of The Cabin Placards - Internal

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PLACARDS AND MARKINGS - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE ABIN LACARDS NTERNAL Introduction Purpose TLMC Task 11-30-60-601 Reference Information REFERENCE DESIGNATION 6041100006 Placard General Arrangement TM411100-01 Placard Details English Procedure Inspect the cabin to make sure that the required placards are installed, and that the placards are legible.
  • Page 26 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 11-30-00 EFFECTIVITY: TE-55965000-SMM Page 602 Revision A Nov 10/2006...

  • Page 27: Discard Self-Illuminated Exit Sign

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PLACARDS AND MARKINGS - SERVICING ISCARD LLUMINATED Introduction Purpose TLMC Task 11-31-62-601 Procedure Remove the self-illuminated exit sign per REMOVAL/INSTALLATION. Obtain a new self-illuminated exit sign. Install the self-illuminated exit sign per REMOVAL/INSTALLATION. Job Completion Remove all tools, equipment, and unwanted materials from the work area. 11-31-00 TE-55965000-SMM Page 301...
  • Page 28 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 11-31-00 EFFECTIVITY: TE-55965000-SMM Page 302 Revision A Nov 10/2006...
  • Page 29 CHAPTER 20 - STAN- DARD PRACTICES - AIR FRAME CL-604 SUPPLEMENTAL MAINTENANCE MANUAL List of Effective Pages CHAPTER 20 - STANDARD PRACTICES - AIR FRAME LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 20 - Effective Pages Nov 10/2006 Nov 10/2006 20 - Contents Nov 10/2006...
  • Page 30 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 20 - Effective Pages Revision A Nov 10/2006...
  • Page 31 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 20 - STANDARD PRACTICES - AIR FRAME TABLE OF CONTENTS Subject Ch-Se-Su Page STANDARD PRACTICES - LIGHTING 20-12-00 Description/Operation Description Removal/Installation Removal/Installation EFFECTIVITY: 5596-SMM Page 1 20 - Contents Revision A Nov 10/2006...
  • Page 32 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 20 - Contents Revision A Nov 10/2006...
  • Page 33 STANDARD PRACTICES - LIGHTING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL STANDARD PRACTICES - LIGHTING - DESCRIPTION/OPERATION ESCRIPTION This section contains procedures to replace the interior lighting lamps installed by the completion center. For more information on these lights, see their individual lighting sections. Incandescent lamps can usually be replaced by removing a lens without removal of the light assembly.
  • Page 34 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Lighting Location Light Assembly Circuit Breakers Section Floor accent lights Vista incandescent 33-22-01 CBPG-1, GALLEY LAV ACCENT; CBPG-4, CABIN FLOOR Forward wardrobe dome light Whelen incandescent 33-10-00 CBPG-3, ENTRY AREA Galley work and effect lights Aerospace Lighting 33-26-00 CBPG-2, GALLEY WORK fluorescent Jumpseat light...
  • Page 35 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL STANDARD PRACTICES - LIGHTING - REMOVAL/INSTALLATION EMOVAL NSTALLATION Passenger Service Unit and Headliner Indirect Lights To remove a Passenger Service Unit (PSU) or headliner indirect lamp (Figure 401): Open and lock out associated circuit breaker(s) listed in Table If applicable, remove lens per 1.A.(2).
  • Page 36 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install a PSU or headliner indirect lamp (Figure 401): Install lamp into clips. Restore electrical connections to lamp. Install lens per 1.A.(4), if applicable. Restore power (AMM Task 24-00-00-861-801) and verify that lamp turns on. Remove all equipment used for these tasks and return aircraft to its initial condition.
  • Page 37 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EFFECT LIGHTS WORK LIGHTS (VIEW LOOKING FORWARD) GALLEY FLUORESCENT LIGHTS FIGURE 402 To install a galley work or effect lamp (Figure 402): Install lamp into clips. Restore electrical connections to lamp. Position lens and secure with fasteners. Restore power (AMM Task 24-00-00-861-801) and verify that lamp turns on.
  • Page 38 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LIGHT ASSEMBLY LENS LAMP GRIMES INCANDESCENT LIGHTS FIGURE 403 To install an incandescent lamp into a Grimes light assembly (Figure 403): NOTE: Do not touch the lamp directly with fingers during installation. If touched with bare fingers, wipe finger oil off of the lamp with a soft cloth and alcohol.
  • Page 39 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIRCRAFT STRUCTURE LENS PROTECTIVE GRILL LAMP COVER GRIMES FLUSH-MOUNTED INCANDESCENT LIGHTS FIGURE 404 To install an incandescent lamp into a Grimes flush-mounted light assembly (Figure 404): NOTE: Do not touch the lamp directly with fingers during installation. If touched with bare fingers, wipe finger oil off of the lamp with a soft cloth and alcohol.
  • Page 40 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL INNER RING LAMP INNER RING FASTENERS LENS WHELEN INCANDESCENT LIGHTS FIGURE 405 To install an incandescent lamp into a Whelen light assembly (Figure 405): NOTE: Do not touch the lamp directly with fingers during installation. If touched with bare fingers, wipe finger oil off of the lamp with a soft cloth and alcohol.
  • Page 41 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIRCRAFT STRUCTURE LIGHT ASSEMBLY BEZEL LAMP WEMAC INCANDESCENT LIGHTS FIGURE 406 To install an incandescent lamp into a Wemac light assembly (Figure 406): NOTE: Do not touch the lamp directly with fingers during installation. If touched with bare fingers, wipe finger oil off of the lamp with a soft cloth and alcohol.
  • Page 42 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LIGHT STRIP VISTA INCANDESCENT LIGHTS FIGURE 407 To install a Vista accent light strip (Figure 407): Restore electrical connections to light strip. Position light strip and secure with fasteners. Restore power (AMM Task 24-00-00-861-801) and verify that floor accent light turns Remove all equipment used for these tasks and return aircraft to its initial condition.
  • Page 43 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PANEL LAMP LIGHT ASSEMBLY CLIPS GRIMES INCANDESCENT ORDINANCE SIGN LIGHTS FIGURE 408 To install an incandescent lamp into a Grimes ordinance sign light assembly (Figure 408): NOTE: Do not touch the lamp directly with fingers during installation. If touched with bare fingers, wipe finger oil off of the lamp with a soft cloth and alcohol.
  • Page 44 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install a lavatory mirror fluorescent lamp: Install lamp into clips. Restore electrical connections to lamp. Position and secure mirror light lens with fasteners. Restore power (AMM Task 24-00-00-861-801) and verify that lamp turns on. Remove all equipment used for these tasks and return aircraft to its initial condition. 20-12-00 EFFECTIVITY: TE-55965000-SMM Page 410...
  • Page 45 CHAPTER 21 - AIR CON- DITIONING List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 21 - AIR CONDITIONING LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 21 - Effective Pages Nov 10/2006 Nov 10/2006 21 - Contents Nov 10/2006 Nov 10/2006 21-22-00...
  • Page 46 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 21 - Effective Pages Revision A Nov 10/2006...
  • Page 47 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 21 - AIR CONDITIONING TABLE OF CONTENTS Subject Ch-Se-Su Page PASSENGER COMPARTMENT AIR DISTRIBUTION 21-22-00 Description/Operation Ecs Return Air Distribution Conditioned Air Distribution Gasper Air Distribution Removal/Installation Removal Installation Adjustment/Test Introduction Test Set-up Test Test Completion ENTRY AREA HEAT...
  • Page 48 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 21 - Contents Revision A Nov 10/2006...

  • Page 49: Passenger Compartment Air Distribution

    PASSENGER COMPARTMENT AIR DISTRIBUTION CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER COMPARTMENT AIR DISTRIBUTION - DESCRIPTION/OPERATION ETURN ISTRIBUTION Description/Location Return air ducts and adapter assemblies have been added to the Environmental Control System (ECS) on the left and right sides of the cabin. Return air from the main cabin circulates through an opening between the Passenger Service Unit (PSU) and cabin headliner on each side of the cabin.
  • Page 50 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Operation The production-installed ECS equipment controls distribution of gasper air. Refer to the Gasper Air Distribution graphic for a layout of the gasper air modifications. LH HEADLINER RETURN AIR DUCTS 621.00 529.00 409.00 379.00 280.00 BAGGAGE COMPARTMENT RETURN AIR DUCTS 280.00 280.00...
  • Page 51 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL 555.00 353.00 542.00 621.00 GRILL IN BAGGAGE HEADLINER 97.50 73.50 RH MAIN AIR DUCT 555.00 621.00 589.00 542.00 353.00 97.50 73.50 LH MAIN AIR DUCT CONDITIONED AIR DISTRIBUTION 21-22-00 EFFECTIVITY: TE-55965000-SMM Page 3 Revision A Nov 10/2006...
  • Page 52 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LH CABIN LH MAIN GASPER PSU ASSY AIR DUCT 621.00 574.00 379.00 280.00 73.50 AVIONICS COOLING DUCT RH MAIN GASPER RH CABIN PSU ASSY AIR DUCT GALLEY 280.00 353.62 574.00 621.00 COOLING 73.50 GASPER AIR FOR PILOT, COPILOT, JUMPSEAT, AND GALLEY GASPER AIR DISTRIBUTION...

  • Page 53: Removal

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER COMPARTMENT AIR DISTRIBUTION - REMOVAL/INSTALLATION EMOVAL To remove the return air duct from the forward wardrobe: Remove contents from wardrobe. Remove air duct closeout (secured with hook-and-loop strips). Remove fasteners securing air duct to floor. Remove air duct.
  • Page 54 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 21-22-00 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...

  • Page 55: Introduction

    Prepare aircraft electrical, APU, and ECS systems for outside operations. Start APU and engage electrical and ECS systems. Engage utility buses. Perform integrity check of air distribution system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-131, revision (A), or the latest approved revision.
  • Page 56 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 21-22-00 EFFECTIVITY: TE-55965000-SMM Page 502 Revision A Nov 10/2006...

  • Page 57: Entry Area Heat

    ENTRY AREA HEAT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY AREA HEAT - DESCRIPTION/OPERATION ESCRIPTION OCATION An air heater has been installed to provide additional heat to the entry area through outlets in the galley kick panel and the jumpseat well risers. Table 1 lists the components and their locations.
  • Page 58 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL 28VDC - CABIN BUS 1 LIGHTS SYSTEM GALLEY GALLEY CABIN BAGGAGE CONF GALLEY ENTRY CONT FLOOR READ MIRROR CONTROL WORK AREA ACCENT WATER 28VDC - CABIN BUS 2 LIGHTS ENTERTAINMENT LH READ RH READ TOILET MGMT 1 MGMT 2 CONTROL TABLE...

  • Page 59: Introduction

    None Start APU or aircraft engines. Verify that system circuit breaker(s) are closed. Test the entry area heaters in accordance with Bombardier Completion Center Cabin Management System Ground Test Procedure, document number TE-GTP-251, revision (F), or the latest approved revision.
  • Page 60 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 21-40-03 EFFECTIVITY: TE-55965000-SMM Page 502 Revision A Nov 10/2006...

  • Page 61: Cabin Temperature Control

    CABIN TEMPERATURE CONTROL CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN TEMPERATURE CONTROL - DESCRIPTION/OPERATION ESCRIPTION OCATION The cabin environmental control system has been modified to allow the cockpit crew to transfer control of the cabin temperature to the cabin switch panels. Cabin switch panels with temperature control capabilities interface to the production cabin environmental control system through a potentiometer built into the cabin management system Cabin Control Module 1 (CCM 1) (23-90-00).
  • Page 62 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MODE CONTROL CALL ADJUST AIRSHOW CABIN AUDIO CABIN MODE VIDEO VIDEO UPWASH SELECT TEMP SELECT SELECT SELECT LIGHTS CABIN CABIN SPEAKER TONE MONITOR MONITOR FLOOR DNWASH ON/OFF ON/OFF ON/OFF LIGHTS LIGHTS VIP SWITCH PANEL SMOKE CABIN CALL COCKPIT CABIN...

  • Page 63: Removal

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN TEMPERATURE CONTROL - REMOVAL/INSTALLATION EMOVAL To remove the cabin temperature sensor box: Open and lock out circuit breaker(s) listed in Table Remove dado panel at FS478R (25-27-10). Disconnect electrical and air connections from sensor box. Remove fasteners securing sensor box to panel.
  • Page 64 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 21-61-18 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...

  • Page 65: Introduction

    Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Test the cabin temperature control system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-187, revision (B), or the latest approved revision.
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  • Page 67 CHAPTER AUTO FLIGHT List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 22 - AUTO FLIGHT LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 22 - Effective Pages Nov 10/2006 Nov 10/2006 22 - Contents Nov 10/2006 Nov 10/2006 22-30-00 Dec 3/03 Dec 3/03...
  • Page 68 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 22 - Effective Pages Revision A Nov 10/2006...
  • Page 69 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 22 - AUTO FLIGHT TABLE OF CONTENTS Subject Ch-Se-Su Page AUTO THROTTLE SYSTEM 22-30-00 Description/Operation Description Location Operation Removal/Installation Removal Installation Adjustment/Test Introduction Adjustment Completion Test Set-up Test Test Completion Inspection/Check Introduction Job Set-up Procedure Job Completion...
  • Page 70 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 22 - Contents Revision A Nov 10/2006...

  • Page 71: Auto Throttle System

    AUTO THROTTLE SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AUTO THROTTLE SYSTEM - DESCRIPTION/OPERATION ESCRIPTION The Safe Flight Instrument Corporation Enhanced Autopower Auto Throttle System (ATS) incorporates dual-servo control of the thrust levers to enable thrust and speed control for takeoff, climb, cruise, descent, landing, and go-around modes of operation.

  • Page 72: Operation

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM 250.00 244.40 COMPUTER 234.95 19.75 CLUTCH AND SERVO KIT 0.00 76.50 CLUTCH AND COMPUTER SERVO KIT AUTO THROTTLE EQUIPMENT LOCATION PERATION The ATS is controlled at the ATS CP, which incorporates an ATS system engage switch, and green LED engaged annunciators.
  • Page 73 ATS computer. Depress either ATS DISC push-button switch to confirm disengagement of the ATS and cancel the FAIL message. Do not engage the ATS. Refer to Bombardier Operating Manual Supplement Document for operational instructions pertaining to preflight, take-off, climb, cruise, descent, approach, and landing.
  • Page 74 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM FLIGHT CONTROL SPEED ATS MODE STATUS DISPLAY SWITCH ATS MODE STATUS DISPLAY PANEL KNOB MODETEXT MODETEXT N2 SYNC CAUTIONS CAUTIONS ATS CONTROL N2 SYNC PANEL SWITCH AUTO THROTTLE CONTROL AND DISPLAY INDICATORS 22-30-00 EFFECTIVITY: TE-22305001-SMM-2 Page 4 Dec 3/03...

  • Page 75: Removal

    AUTO THROTTLE SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AUTO THROTTLE SYSTEM - REMOVAL/INSTALLATION EMOVAL NOTE: Refer to Safe Flight Repair Procedure Document No. R-2830 for additional information pertaining to installation, repair, part replacement, and rigging. To remove the ATS computer: Open and lock out circuit breaker(s) listed in SMM 22-30-00, DESCRIPTION.
  • Page 76 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM Support the shaft between the servo drive and clutch assembly with safety wire attached to the support structure. Using the modified 3mm Allen wrench (see Safe Flight Repair Procedure R2830), remove the six screws and lock washers that attach the shaft connection to the servo drive. These screws are located on the opposite side of the support structure from the servo drive, between the clutch assembly and the servo support structure.
  • Page 77 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM Remove and discard cotter pin and retaining ring from one end of the pivot pin connecting the inner arm of the bell crank assembly to the control link. Remove pivot pin and allow control link to hang free. Disconnect outer arm of the bell crank assembly from the push pull engine cable (AMM Task 76-11-04-000-801).

  • Page 78: Installation

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM NSTALLATION To install the ATS computer: Verify protective covers have been removed from ATS computer. Position ATS computer on the mounting tray and slide into electrical connectors. Secure ATS computer with retaining knob. Restore power (AMM Task 24-00-00-861-801) and verify proper operation of auto throttle system in accordance with SMM 22-30-00, ADJUSTMENT/TEST.

  • Page 79: Adjustment/Test

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM To install the clutch pack assembly (Figure 401): NOTE: A rigging check and adjustment is required after replacement of the clutch pack assembly. NOTE: The shaft is a two-part assembly. Do not allow the two parts to become axially separated. Support the clutch pack assembly and position onto the stub shaft of the servo drive.
  • Page 80 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM To install a control rod (Figure 402): NOTE: A rigging check and adjustment is required after replacement of a control rod. NOTE: The left (pilot) and right (copilot) control rods are not interchangeable. Control rod 1135-105-1 is for the left side, and 1135-105-2 is for the right side.
  • Page 81 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM MOTOR COVER ELECTRICAL CONNECTOR PUSH PULL CABLE SERVO DRIVE CONNECTION SUB-ASSEMBLY BELL CRANK ASSEMBLY MOUNTING SCREWS (6) CONTROL LINK (TYPICAL - 2 PLACES) METRIC ALLEN-HEAD SCREWS (6) CLUTCH PACK ASSEMBLY METRIC ALLEN HEAD SCREWS (6) PIVOT PINS (TYPICAL - 6 PLACES) MOUNTING SCREWS (6)
  • Page 82 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM THRUST LEVER CONNECTION CONTROL ROD PIVOT PIN CLUTCH SERVO CONTROL LINK BELL CRANK INNER ARM PIVOT PIN RIG PIN (IDLE POSITION) CLUTCH PACK CLUTCH SERVO ASSEMBLY FORWARD VIEW A-A (LOOKING OUTBOARD LHS) CONTROL RODS AND LINKS FIGURE 402 22-30-00 EFFECTIVITY: TE-22305001-SMM-2...
  • Page 83 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM CONTROL ROD CLEVIS (PART OF PUSH PULL CABLE) BELL CRANK OUTER ARM RIG PIN (OPPOSITE, AT IDLE POSITION) VIEW B-B FORWARD (LOOKING INBOARD RHS) BELL CRANK ASSEMBLY FIGURE 403 22-30-00 EFFECTIVITY: TE-22305001-SMM-2 Page 409 Dec 3/03...
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  • Page 85: Introduction

    • GSE 71-00-32 Power Plant Rigging Kit Facilities • External power Reference Documents • Bombardier Completion Center Drawing TM4332230-10, Autothrottle Clutch and Servo Install - Enhanced • CL-604 AMM • Safe Flight Repair Procedure, R2830 Adjustment Set-up Prior to proceeding with adjustment of the auto throttle system, obtain the required tolerances for throttle split and throttle cushion at maximum power, idle, and shutoff.

  • Page 86: Adjustment Completion

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM Set cable assembly swivel fittings to provide equal adjustment forward and aft, and tighten jam nuts. Release aft and forward most clamps on forward fuel control cable assembly. Ensure fuel control lever on the engine is in the idle position (15 - 18 ) using the protractor supplied in the Power Plant Rigging Kit, GSE 71-00-32.

  • Page 87: Test Set-Up

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM Configure aircraft in standard configuration for maintenance. Operational Test of the Throttle Controls Perform CL-604 AMM Task 76-10-00-710-801, Operational Test. NOTE: If the throttle controls fail to meet any of the requirements of the operational test of the throttle controls, perform CL-604 AMM Task 76-10-00-720-801, Functional Test of the Throttle Controls.
  • Page 88 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM they shall be made to the cable ends that attach to the ATS assembly, not to the control rods between the throttle quadrant and the ATS assembly. Configuration Procedure Configure aircraft in standard configuration for maintenance. Connect external power to the aircraft.
  • Page 89 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM LAMP TEST CLIMB ENG PB ALT CAP DISC PB ALT HOLD VERT TO DIMMING AP #1 SEL AP ENG OVERSPD N2 SYNC PB Place the IND LTS switch on the miscellaneous lights overhead panel to the DIM position, and then press and hold the ATS and N2 SYNC push-button switches.
  • Page 90 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM ALT CAP DESCEND ALT HOLD Approximately 3 seconds later, note the AFCS transition to Altitude Hold mode. The state of the following parameters should be indicated on the PC monitor: NOTE: Repeat steps 8 and 9 as necessary to note transition below. ALT CAP ALT HOLD (10) Set the Altitude Preselector to an altitude above the current aircraft altitude.
  • Page 91 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM (17) Move the left-hand thrust lever to the MAX POWER position and then to the SHUTOFF position. Ensure that the thrust lever moves freely and smoothly. (18) Repeat steps 3.B.(12) through 3.B.(17) for the right-hand thrust reverser. (19) Hold the LAMP TEST toggle switch on the miscellaneous test panel in position 1.
  • Page 92 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM 300 ± 3 KTS L N2 Same as ED ± 0.2% 328 ± 2 KTS R N2 Same as ED ± 0.2% REF MACH Same as PFD ± 0.002 M MACH Same as PFD ± 0.002 M (24) Set the airspeed to 340 knots (overspeed).
  • Page 93 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM Self-Test Place the thrust levers approximately in the middle of travel, and the IND LTS toggle switch on the miscellaneous lights overhead panel to the BRT position. Hold the LAMP TEST toggle switch on the miscellaneous test panel in position 1. The SELFTEST message shall scroll across the top and bottom of the MSDs.
  • Page 94 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM Momentarily press the ATS DISC switch on the right-hand thrust lever. The MSDs shall indicate a flashing amber DISENG’D message, the ATS control panel annunciators shall extinguish, and the ATS shall cease driving the thrust levers. Momentarily press the ATS DISC switch on the left-hand thrust lever.

  • Page 95: Test Completion

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM (20) Momentarily press the ATS switch on the ATS control panel. The MSDs shall indicate a green SPEED message and the green ATS annunciators shall be illuminated. (21) Place IRU 1 in OFF mode. Observe that 10 seconds after IRU 1 completes shutdown, the ATS shall disengage, the green ATS control panel annunciators shall extinguish, and the MSDs shall display a flashing amber FAIL message.
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  • Page 97: Introduction

    AUTO THROTTLE SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AUTO THROTTLE SYSTEM - INSPECTION/CHECK NTRODUCTION Purpose Verify that the thrust reverser diodes have not opened or shorted. NOTE: The following procedure requires qualified operators using approved aircraft operational procedures. NOTE: Perform the following procedures per the Supplemental Time Limits and Maintenance Checks Manual, and whenever the thrust reverser diodes are replaced.

  • Page 98: Job Completion

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM Pull LH PDU main brake-release knob and install the brake-release block tool. Ensure that the ATS disengages. Ensure that L TR UNLOCKED message is displayed on Primary EICAS display. Remove the brake-release block tool and ensure that the main brake-release knob retracts fully.
  • Page 99 Page 1 of 14 R-2830 REPAIR PROCEDURE ENHANCED AUTOPOWER® DUAL SERVOMOTOR GEARBOX AND CLUTCH PACK ASSEMBLY BOMBARDIER CHALLENGER CL-604...
  • Page 100 Page 2 R-2830 REVISION NOTICE PAGES & PARAGRAPHS CHECKED APPROVED MADE ADDED, REVISED OR DELETED B.Carr Orig. Total pages: 14 L.Ostergren J.Gordon 12/1102 12/11/02 12/13/02...
  • Page 101 Page 3 Sym R-2830 TABLE OF CONTENTS Para. Title Page None Title Page........................1 None Revision Page....................... 2 None Table of Contents ......................3 Introduction ........................4 Removal/Replacement Procedures................4 Motor Assembly (1135-114) ..................5 Servo Drive Subassembly (1135-102) ................. 6 Clutch Pack Assembly (1135-123) ................

  • Page 102: Introduction

    Page 4 Sym R-2830 INTRODUCTION User repairs are limited to removal and replacement of major assemblies. Removed assemblies should be returned to SFIC for repair, overhaul or replacement, as applicable. Flight operations may or may not be possible, with the Enhanced AutoPower® not activated, with an assembly removed.

  • Page 103: Motor Assembly (1135-114)

    Page 5 Sym R-2830 Motor Assembly (1135-114) 2.1.1 Tools #0 Phillips screw driver 5/32-inch Allen head wrench 2.1.2 Removal Looking up at the Enhanced AutoPower assembly (1135-2) one servo drive (1135-102) will be seen, extending about six inches on the mechanic’s left and another on the mechanic’s right.

  • Page 104: Servo Drive Subassembly (1135-102)

    Page 6 Sym R-2830 Servo Drive Subassembly (1135-102) 2.2.1 Tools 7/64 inch Allen head wrench #0 Phillips screwdriver 3/16 inch hex wrench 3 mm Allen head wrench (see paragraph 4.1) 2.2.2 Removal The location of the two servo drive subassemblies (1135-102) is described in paragraph 2.1.2.

  • Page 105: Clutch Pack Assembly (1135-123)

    Page 7 Sym R-2830 Clutch Pack Assembly (1135-123) 2.3.1 Tools Diagonal cutters Needle nose pliers 7/64 inch Allen head wrench 3 mm Allen head wrench (see paragraph 4.1) Retaining ring tool (see paragraph 4.2) 2.3.2 Removal Remove four pivot pins (1135-232, see section 3.0) located at the two clutch cranks. Two of these pins connect to (gold colored) links (1135-110);...

  • Page 106: Bell Crank Assembly (1135-103-1 & -2)

    Page 8 Sym R-2830 Bell Crank Assembly (1135-103-1 & -2) 2.4.1 Engine Cable Before removing the bell crank, the engine (push-pull) cable must be disconnected from the bell crank, on the side to be replaced. This connection is the same one ordinarily used on CL-604 with or without Enhanced AutoPower.

  • Page 107: Actuator Rod (1135-105-1 & -2)

    Page 9 Sym R-2830 Actuator Rod (1135-105-1 & -2) 2.5.1 Thrust Lever The actuator rod to be replaced must be disconnected from the thrust lever, located in the pedestal. This connection is the same one ordinarily used on CL-604 with or without Enhanced AutoPower.

  • Page 108: Replacement Of Bell Crank Bolts

    Page 10 Sym R-2830 Replacement of Bell Crank Bolts Before replacing the bolts it is advisable to read paragraph 2.4.3, Removal of Bell Crank Assembly. Consult this paragraph and Figures 1, 2 and 3 to locate the bell cranks (1135-103- 1 and 1135-103-2).

  • Page 109: Figure 1 Right Bell Crank

    Page 11 Sym R-2830 Figure 1 Right Bell Crank (1135-103-2) Left is opposite hand (1135-103-1)

  • Page 110: Pivot Pin (1135-232) Removal

    Page 12 Sym R-2830 PIVOT PIN (1135-232) REMOVAL The removal and replacement tasks of paragraphs 2.3, 2.4 and 2.5 require the removal and replacement of pivot pins, which are used to connect the moving parts of the Enhanced AutoPower assembly. Removal of the pins from the internal link to bell crank joint can be done in either direction (i.e.

  • Page 111: Figure 2 − Top View

    Page 13 Sym R-2830...

  • Page 112: Figure 3 − Side View

    Page 14 Sym R-2830...
  • Page 113 CHAPTER 23 - COMMUNI- CATIONS List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 23 - COMMUNICATIONS LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 23 - Effective Pages Nov 10/2006 23-31-00 Nov 10/2006 Nov 10/2006 Nov 10/2006 23 - Contents Nov 10/2006 23-31-00...
  • Page 114 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Ch-Se-Su Page Date Ch-Se-Su Page Date 23-50-12 Nov 10/2006 Nov 10/2006 23-50-12 Nov 10/2006 Nov 10/2006 23-50-12 Nov 10/2006 Nov 10/2006 23-90-00 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 23-90-00 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006...
  • Page 115 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 23 - COMMUNICATIONS TABLE OF CONTENTS Subject Ch-Se-Su Page SATELLITE COMMUNICATION SYSTEM 23-15-00 Description/Operation Description Location Operation Removal/Installation Removal Installation Adjustment/Test Introduction Test Set-up Test Test Completion IRIDIUM COMMUNICATIONS SYSTEM 23-16-00 Description/Operation Description Location Operation...
  • Page 116 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page CABIN PAGING/PUBLIC ADDRESS 23-31-00 Description/Operation Description/Location Operation Removal/Installation Removal Installation Adjustment/Test Introduction Test Set-up Test Test Completion CABIN CALL SYSTEM 23-31-50 Description/Operation Description/Location Operation Adjustment/Test Introduction Test Set-up Test Test Completion AUDIO ENTERTAINMENT SYSTEM 23-32-00 Description/Operation Description/Location...
  • Page 117 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page PASSENGER INFORMATION SYSTEM 23-34-00 Description/Operation Description/Location Operation Adjustment/Test Introduction Test Set-up Test Test Completion JUMPSEAT AUDIO MODIFICATION 23-50-12 Description/Operation Description/Location Operation Removal/Installation Removal Installation Adjustment/Test Introduction Test Set-up Test Test Completion CABIN MANAGEMENT SYSTEM 23-90-00 Description/Operation Description...
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  • Page 119 SATELLITE COMMUNICATION SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SATELLITE COMMUNICATION SYSTEM - DESCRIPTION/OPERATION ESCRIPTION A Rockwell/Collins SATCOM 6100 Satellite Communication (SATCOM) system is installed in the aircraft to provide extended-range communication. It is a satellite-based system that will provide global coverage over approximately 75% of the earth’s surface. The system consists of an SRT-2100-3 Satellite Receiver-Transmitter (SRT), an antenna driver, an LNA/diplexer, and an EMS Technologies AMT-50 High Gain Antenna.
  • Page 120 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PERATION The INMARSAT organization provides a fleet of geosynchronous communication satellites and ground-based earth stations. The Rockwell/Collins SATCOM 6100 is designed to communicate with these satellites and ground stations. The aircraft system communicates with the satellites in the L-band radio spectrum.
  • Page 121 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SATELLITE COMMUNICATION SYSTEM - REMOVAL/INSTALLATION EMOVAL To remove the antenna, LNA/diplexer, and/or antenna driver (Figure 401): WARNING: DO NOT APPROACH FINCAP UNTIL THE SATELLITE COMMUNICATIONS (SATCOM) SYSTEM IS DEACTIVATED AND ELECTRICAL POWER HAS BEEN REMOVED. Open and lock out associated circuit breaker(s) listed in Table Remove fincap as detailed in 1.A.(3) through 1.A.(10).
  • Page 122 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To remove the Satellite Receiver/Transmitter (SRT) (Figure 402): Open and lock out associated circuit breaker(s) listed in Table Gain access to SRT in aft equipment bay. Loosen hold-down clamp securing SRT to rack. Slide SRT forward out of rack. If SRT requires repair or troubleshooting, proceed as follows: •...
  • Page 123 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ANTENNA ASSEMBLY LNA/DIPLEXER ANTENNA DRIVER VERTICAL STABILIZER FINCAP SATELLITE COMMUNICATION SYSTEM - REMOVAL/INSTALLATION FIGURE 401 23-15-00 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
  • Page 124 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CAPTIVE THUMBSCREWS AFT EQUIPMENT BAY SATCOM SHELF (VIEW LOOKING DOWN) SATELLITE COMMUNICATION SYSTEM - REMOVAL/INSTALLATION FIGURE 402 23-15-00 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 125 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the SATCOM in accordance with Bombardier Completion Center Ground Test Procedure, document number D-GT23905006, revision (-), or the latest approved revision.
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  • Page 127 IRIDIUM COMMUNICATIONS SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL IRIDIUM COMMUNICATIONS SYSTEM - DESCRIPTION/OPERATION ESCRIPTION An International Communications Group (ICG) ICS-200 Iridium Satellite Communications (SATCOM) system is installed on the aircraft. The ICG ICS-200 is a telecommunications system which uses the Iridium satellite system for worldwide coverage.
  • Page 128 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Air-to-Ground Calling The ICS-200 is capable of supporting two main dialing formats: the North American standard or the European standard. The ICS-200 will automatically add, strip, or change digits to accommodate the Iridium network. The caller dials a single format and does not need to change dialing formats required by disparate communications transceivers.
  • Page 129 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AEROCOM 1000 CTU BASE UNITS TRANSCEIVER COCKPIT HANDSET ANTENNA FILTER CORDLESS HANDSETS IRIDIUM COMMUNICATIONS SYSTEM - COMPONENT LOCATION 23-16-00 EFFECTIVITY: TE-55965000-SMM Page 3 Revision A Nov 10/2006...
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  • Page 131 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL IRIDIUM COMMUNICATIONS SYSTEM - REMOVAL/INSTALLATION EMOVAL To remove a cabin base unit (Figure 401): Open and lock out circuit breaker(s) listed in Table Slide single seats inboard to access dado panel. Remove dado panel (25-27-10). Remove fasteners securing base unit to mounting bracket. Remove base unit.
  • Page 132 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION To install a cabin base unit (Figure 401): Position base unit on mounting bracket and secure with fasteners. Perform test in accordance with ADJUSTMENT/TEST. Install dado panel (25-27-10). Remove all equipment used for these tasks and return aircraft to its initial condition. To install the cockpit handset and cord reel (Figure 401):...
  • Page 133 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AEROCOM 1000 CTU BASE UNITS TRANSCEIVER COCKPIT HANDSET FILTER ANTENNA CORDLESS HANDSETS IRIDIUM COMMUNICATIONS SYSTEM - REMOVAL/INSTALLATION FIGURE 401 23-16-00 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 135 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the airborne telephone system in accordance with Bombardier Completion Center Ground Test Plan, document number D-GT23905005, the latest approved revision.
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  • Page 137 OFFICE EQUIPMENT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL OFFICE EQUIPMENT - DESCRIPTION/OPERATION ESCRIPTION An Aerorouter 700 Local Area Network (LAN) server, two High Speed Transmitters (HST), RJ-45 PC jacks, and RJ-45 LAN jacks allow multiple computers to connect to a high-speed satellite data connection and send data to one another.
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  • Page 139 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL OFFICE EQUIPMENT - REMOVAL/INSTALLATION EMOVAL To remove the Aerorouter 700 Local Area Network (LAN) server (Figure 401): Open and lock out circuit breaker(s) listed in Table Gain access to the Aerorouter server through the right-hand baggage compartment closeout panel.
  • Page 140 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Tighten captive thumbscrew to secure router to mounting tray. Restore power (AMM Task 24-00-00-861-801). Perform test in accordance with ADJUSTMENT/TEST. Remove all equipment used for these tasks and return aircraft to its initial condition. To install an HST (Figure 402): Slide HST carefully into rack to ensure proper electrical connection.
  • Page 141 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CAPTIVE THUMBSCREWS AFT EQUIPMENT BAY SATCOM SHELF (VIEW LOOKING DOWN) OFFICE EQUIPMENT - REMOVAL/INSTALLATION FIGURE 402 23-23-00 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 143 Energize all aircraft electrical buses. Test the Aerorouter 700 cabin LAN system with HST in accordance with Bombardier Completion Center Ground Test Procedure, document number D-GT23905008, the latest approved revision.
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  • Page 145 CABIN PAGING/PUBLIC ADDRESS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN PAGING/PUBLIC ADDRESS - DESCRIPTION/OPERATION ESCRIPTION OCATION The production-installed cabin paging/public address system has been modified by the addition of a preamp and two utility speakers. These components interface to the cabin audio entertainment system and the cabin management system Entertainment Control Module (ECM) and stereo amplifier.
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  • Page 147 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN PAGING/PUBLIC ADDRESS - REMOVAL/INSTALLATION EMOVAL To remove the entry area headliner speaker (Figure 401): Open and lock out circuit breaker(s) listed in Table Remove headliner (25-15-01). Disconnect wiring to speaker. Remove fasteners securing speaker to aircraft structure. Remove speaker.
  • Page 148 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LAV SIDE PANEL LAV SPEAKER SPEAKER ATTACH POINTS (TYPICAL) (VIEW LOOKING FORWARD) NUTPLATE WASHER SCREW SPEAKER (VIEW LOOKING DOWN) CABIN PAGING/PUBLIC ADDRESS - REMOVAL/INSTALLATION FIGURE 401 23-31-00 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 149 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the cabin paging/public address system in accordance with Bombardier Completion Center Ground Test Procedure, document number D-GT23315000, revision (A), or the latest approved revision.
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  • Page 151 CABIN CALL SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN CALL SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION The cabin call system allows the passengers to notify the cockpit crew and the cabin attendant when in need of assistance. Aural and visual notification is provided by a chime and lighted annunciators. The system consists of call switches in the cabin and lavatory, and a call reset annunciator/switch in the cockpit (31-60-10).
  • Page 152 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CALL CALL SWITCH PANEL CONTROL MODE CALL ADJUST AIRSHOW CABIN AUDIO CABIN MODE VIDEO VIDEO UPWASH SELECT TEMP SELECT SELECT SELECT LIGHTS CABIN CABIN SPEAKER TONE MONITOR MONITOR FLOOR DNWASH ON/OFF ON/OFF ON/OFF LIGHTS LIGHTS VIP SWITCH PANEL SMOKE CABIN CALL...
  • Page 153 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the cabin call system in accordance with Bombardier Completion Center Ground Test Procedure, document number D-GT23315000, revision (A), or the latest approved revision.
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  • Page 155 AUDIO ENTERTAINMENT SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AUDIO ENTERTAINMENT SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION An audio entertainment system has been installed in the aircraft to provide stereo quality audio. Table 1 lists components and their locations. Audio selections are available through cabin speakers or through headphone jacks located on the passenger switch panels.
  • Page 156 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL The cabin management system provides control of the ECM and other audio components. See 23-90-00 for more detailed information on the cabin management system, ECM, data bus, remote control, and switch panels. Headphone Control The Passenger Switch Panels, located adjacent to the seats, control headphone audio source selection, AUDIO SELECT, and headphone volume control, VOLUME and VOLUME .
  • Page 157 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MODE CONTROL CALL ADJUST AIRSHOW CABIN AUDIO CABIN MODE VIDEO VIDEO UPWASH SELECT TEMP SELECT SELECT SELECT LIGHTS CABIN CABIN SPEAKER TONE MONITOR MONITOR FLOOR DNWASH ON/OFF ON/OFF ON/OFF LIGHTS LIGHTS VIP SWITCH PANEL REMOTE CONTROL WITH HOME MENU DISPLAYED 23-32-00 EFFECTIVITY: TE-55965000-SMM Page 3...
  • Page 158 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SWITCH PANEL ENTERTAINMENT SWITCH PANEL MULTI-DISC CD PLAYER VIDEO CASSETTE PLAYER DVD PLAYER 115VAC/60HZ UTILITY OUTLET DIVAN AFT END CABINET MID-RANGE SPEAKERS SUBWOOFER (6 PLACES) 350.25 560.31 586.92 SUBWOOFER AUDIO ENTERTAINMENT COMPONENTS 23-32-00 EFFECTIVITY: TE-55965000-SMM Page 4 Revision A Nov 10/2006...
  • Page 159 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AUDIO ENTERTAINMENT SYSTEM - REMOVAL/INSTALLATION EMOVAL To remove a mid-range speaker (Figure 401): Open and lock out circuit breaker(s) listed in Table Remove PSU cover in speaker area (25-26-20). Remove fasteners securing speaker. Disconnect wiring from speaker. Remove speaker.
  • Page 160 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Remove fasteners securing entertainment component to insert assembly. Remove entertainment component. To remove the entertainment control module (Figure 402): Open and lock out circuit breaker(s) listed in Table Remove contents (printer/fax machine, if installed) and drawer from forward section of divan aft end cabinet.
  • Page 161 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install the entertainment source equipment (Figure 402): Position entertainment component onto insert assembly and secure with fasteners. Position insert assembly inboard of divan aft end cabinet and restore electrical connections to entertainment components. Slide insert assembly into place and secure with fasteners to divan aft end cabinet. Install front panel.
  • Page 162 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MID-RANGE SPEAKERS (6 PLACES) 350.25 560.31 586.92 SUBWOOFER CABIN AUDIO ENTERTAINMENT - REMOVAL/INSTALLATION FIGURE 401 23-32-00 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 163 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL COOLING FAN (BEHIND CD PLAYER) SWITCH PANEL ENTERTAINMENT SWITCH PANEL MULTI-DISC CD PLAYER VIDEO CASSETTE PLAYER DVD PLAYER 115VAC/60HZ OUTLET REMOVABLE ACCESS PANEL (ENTERTAINMENT CONTROLLER MHE BEHIND) DIVAN AFT END CABINET CABIN AUDIO ENTERTAINMENT - REMOVAL/INSTALLATION FIGURE 402 23-32-00 EFFECTIVITY: TE-55965000-SMM...
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  • Page 165 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the audio entertainment system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-251, revision (F), or the latest approved revision.
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  • Page 167 VIDEO ENTERTAINMENT SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL VIDEO ENTERTAINMENT SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION Table 1 lists the video entertainment system components and their locations. Video selections are available on two LCD monitors in the forward and aft cabin bulkheads. The video system receives passenger input from switch panels, the remote control, and controls located on the video source units.
  • Page 168 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Cabin Video Control Cabin video is controlled at the Entertainment Switch Panel and VIP Switch Panel, the video source units, or the remote control. To operate the IR remote control, point the control toward either of the bulkhead monitors to allow the IR sensor, mounted adjacent to the monitors, to receive the signal.
  • Page 169 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL REMOTE CONTROL WITH HOME MENU DISPLAYED 23-33-00 EFFECTIVITY: TE-55965000-SMM Page 3 Revision A Nov 10/2006...
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  • Page 171 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL VIDEO ENTERTAINMENT SYSTEM - REMOVAL/INSTALLATION EMOVAL NOTE: See 23-32-00 for removal of the entertainment source equipment. To remove the forward monitor: Open and lock out circuit breaker(s) listed in Table Remove door jamb from bulkhead. Remove fasteners securing monitor. Slide monitor inboard enough to reach wiring.
  • Page 172 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION NOTE: See 23-32-00 for installation of the entertainment source equipment. To install the forward monitor: Restore electrical connections to monitor. Slide monitor into position and secure with fasteners. Install door jamb. Restore power (AMM Task 24-00-00-861-801) Perform test in accordance with ADJUSTMENT/TEST.
  • Page 173 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the video entertainment system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-251 revision (F), or the latest approved revision.
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  • Page 175 PASSENGER INFORMATION SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER INFORMATION SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION The Airshow 400 passenger information system displays a moving map with a symbol representing the aircraft to show the relative position of the aircraft during flight. It can also display other map and flight data on the video monitors.
  • Page 176 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL The operational software checks the system resources and initializes the system databases, navigation and air data interfaces, and the preset lines of information to be displayed. This software boot-up sequence takes 1-2 minutes to complete. During this time, only the Airshow 400 copyright page is displayed.
  • Page 177 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SCROLL SELECT FLIGHT DECK CONTROLLER 23-34-00 EFFECTIVITY: TE-55965000-SMM Page 3 Revision A Nov 10/2006...
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  • Page 179 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the Airshow passenger information system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-208, revision (C), or the latest approved revision.
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  • Page 181 JUMPSEAT AUDIO MODIFICATION CL-604 SUPPLEMENTAL MAINTENANCE MANUAL JUMPSEAT AUDIO MODIFICATION - DESCRIPTION/OPERATION ESCRIPTION OCATION An audio panel and mic/phone jack panel have been installed to provide communication capability to the jumpseat occupant. The existing Audio Electronic Control Unit (AECU) has been removed and replaced with a control unit that provides an interface to the added jumpseat audio control panel and mic/phone jack panel.
  • Page 182 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL OBSERVER MIC AND HEADPHONE JACKS OBSERVER AUDIO HDPH BOOM HAND OBSERVER MIC/PHONE JACK PANEL OBSERVER AUDIO CONTROL PANEL EQUIPMENT LOCATION 23-50-12 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 183 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL JUMPSEAT AUDIO MODIFICATION - REMOVAL/INSTALLATION EMOVAL To remove the CVR audio mixer: Open and lock out circuit breaker(s) listed in Table Remove fasteners securing the copilot’s side console closeout panel. Slide the closeout panel inboard enough to access the audio mixer. Disconnect wiring to audio mixer.
  • Page 184 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install the audio control panel: Connect the control panel electrical connection. Position the control panel in the mounting box. Rotate Dzus fasteners to the closed position. Close circuit breaker(s) listed in Table Restore power and check for proper operation. Stow the jumpseat.
  • Page 185 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the observer audio panel in accordance with Bombardier Completion Center Ground Test Plan, document number D-GT23515002 revision (-), or the latest approved revision.
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  • Page 187 CABIN MANAGEMENT SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN MANAGEMENT SYSTEM - DESCRIPTION/OPERATION ESCRIPTION A Honeywell/Baker Cabin Management System (CMS) has been installed in the aircraft to manage several cabin systems and components. These systems and components include cabin lights, galley lights, lavatory lights, cabin audio and video entertainment systems, cabin temperature, galley equipment, and water system.
  • Page 188 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL The PCUs are Honeywell/Baker MHS series switch panels. These units communicate with the other units on the RS-485 bidirectional bus and allow the passengers to control headphone audio selection, headphone volume, reading lights, and table lights. A headset jack provides access to stereo audio. An alphanumeric display indicates the selected audio source.
  • Page 189 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PERATION The Honeywell/Baker MH cabin management system utilizes a bidirectional data bus and discrete outputs to control switching functions. In addition, the entertainment remote control interfaces with this system through the remote IR sensors. Actuation of a push-button control switch sends a data word to the bidirectional data bus. Each data word is addressed to a particular device.
  • Page 190 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DOME LIGHT MIRROR LIGHTS FLOOR LIGHTS BAGGAGE LIGHTS LCU SWITCH PANEL GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR UPWASH LIGHTS LIGHTS LIGHTS LIGHTS CABIN CABIN COFFEE FLOOR FLOOR DNWASH ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER PURGE...
  • Page 191 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN MANAGEMENT SYSTEM - REMOVAL/INSTALLATION EMOVAL To remove a passenger switch panel: Open and lock out circuit breaker(s) listed in Table Open and lock out circuit breaker(s) associated with each switch’s respective electrical system. Gently lift out on edges of switch panel. Disconnect wiring from switch panel.
  • Page 192 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To remove a component outboard of a dado panel: Open and lock out circuit breaker(s) listed in Table Remove appropriate dado panel (25-27-10). Disconnect wiring from component. Remove fasteners securing component. Remove component. To remove the forward IR sensor: Open and lock out circuit breaker(s) listed in Table Remove forward bulkhead left-hand aft partition (25-23-37).
  • Page 193 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install the entertainment control module (Figure 401): Position unit and secure with fasteners to divan aft end cabinet removable panel. Position removable panel and restore electrical connections to unit. Secure removable panel with fasteners to the divan aft end cabinet. Install drawer and contents (printer/fax machine, if installed) into aft section of divan aft end cabinet.
  • Page 194 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Restore electrical connections to IR sensor. Install monitor (23-33-00). Perform test in accordance with ADJUSTMENT/TEST. Remove all equipment used for these tasks and return aircraft to its initial condition. To install the aft IR sensor: Position IR sensor mounting bracket. Install fasteners securing mounting bracket to bulkhead.
  • Page 195 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL REMOVABLE PANEL (DIVAN AFT END CABINET) ENTERTAINMENT CONTROL MODULE - REMOVAL/INSTALLATION FIGURE 401 23-90-00 EFFECTIVITY: TE-55965000-SMM Page 405 Revision A Nov 10/2006...
  • Page 196 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UPPER EQUIPMENT TRAY GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR LIGHTS LIGHTS LIGHTS LIGHTS COFFEE CABIN CABIN O N/OFF FLOOR FLOOR LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER DISP HEATER HEATER PURGE FULL RESET TEST MICROWAVE 115 VAC 60 Hz...
  • Page 197 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Test the cabin management system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-251, revision (F), or the latest approved revision.
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  • Page 199 CHAPTER 24 - ELECTRI- CAL POWER List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 24 - ELECTRICAL POWER LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 24 - Effective Pages Nov 10/2006 Nov 10/2006 24 - Contents Nov 10/2006 Nov 10/2006 24-03-20...
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  • Page 201 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 24 - ELECTRICAL POWER TABLE OF CONTENTS Subject Ch-Se-Su Page CIRCUIT BREAKER PANELS 24-03-20 Description/Operation Description/Location 60HZ POWER SYSTEM 24-25-00 Description/Operation Description/Location Operation Adjustment/Test Introduction Test Set-up Test Test Completion Inspection/Check Operational Test of the Ground Fault Interrupters LOAD SHEDDING 24-70-00 Description/Operation...
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  • Page 203 CIRCUIT BREAKER PANELS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CIRCUIT BREAKER PANELS - DESCRIPTION/OPERATION ESCRIPTION OCATION The aircraft has five production circuit breaker panels. A sixth circuit breaker panel has been added in the galley. They are as follows: • Circuit Breaker Panel 1 (CBP1) - on the forward side of the bulkhead at FS280L •...
  • Page 204 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TCAS CIRCUIT BREAKER PANEL 3 (CBP3) DATA LOAD CIRCUIT BREAKER PANEL 4 (CBP4) 24-03-20 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 205 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL POWER MUST BE OFF BEFORE OPENING PANEL CBP-1 115VAC BUS 1 115VAC BUS 1 28VDC CABIN BUS 1 CABIN BUS 1 GPWS FEED 115VAC BUS 1 28VDC BUS 1 WEATHER RADAR CABIN CONT1 CONT2 115VAC BUS 1 115VAC UTILITY BUS 1 28VDC BATTERY BUS 1 CABIN...
  • Page 206 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL POWER MUST BE OFF BEFORE OPENING PANEL CBP-2 115VAC BUS 2 28VDC CABIN BUS 2 115VAC BUS 2 CABIN BUS 2 SATCOM FEED AIRSHOW 28VDC BUS 2 115VAC BUS 2 SMOKE 26VAC 115VAC CABIN 28VDC BUS 2 115VAC BUS 2 115VAC UTILITY BUS 2 BUS 2...
  • Page 207 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL - A - - B - WATER SYSTEM BOARD SERVICE CIRCUIT BREAKER PANEL JB5 (CBP5) 24-03-20 EFFECTIVITY: TE-55965000-SMM Page 7 Revision A Nov 10/2006...
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  • Page 209 60HZ POWER SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL 60HZ POWER SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION A power converter has been installed to provide 115VAC/60Hz power for conventionally powered equipment on board the aircraft. This converter supplies power to the 115VAC/60Hz bus on the galley circuit breaker panel.
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  • Page 211 Apply external power to the aircraft. Cabin/galley utility power is required for this test. Verify that applicable circuit breakers are closed. Test the 60Hz power system in accordance with Bombardier Completion Center Ground Test Procedure, document number D-GT24255000, revision (B), or the latest approved revision.
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  • Page 213 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL 60HZ POWER SYSTEM - INSPECTION/CHECK PERATIONAL EST OF THE ROUND AULT NTERRUPTERS Introduction Purpose TLMC Task 24-25-60-601 Job Set-up CAUTION: THIS TEST PROCEDURE REQUIRES QUALIFIED OPERATORS USING APPROVED AIRCRAFT OPERATIONAL PROCEDURES. Obey all the electrical/electronic safety precautions (AMM Task 24-00-00-910-801). Make sure the UTILITY OUTLETS circuit breaker on the Galley Circuit Breaker Panel (GCBP) is closed.
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  • Page 215 LOAD SHEDDING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LOAD SHEDDING - DESCRIPTION/OPERATION ESCRIPTION OCATION A system to disconnect electrical power from the cabin electrical equipment has been installed. The system consists of a CABIN BUS/OFF Annunciator/Switch, AC contactors, DC contactors, a relay, and circuit breakers.
  • Page 216 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL cabin bus contactors to circuit breakers on CBPG and specific circuit breakers on CBP1 and CBP2. Pressing the switch to illuminate OFF opens the ground, de-energizing all four cabin bus contactors, thus removing power from the circuit breakers. In the OFF position, the ground circuit is opened to the 60Hz converter off/on control relay coil.
  • Page 217 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LOAD SHEDDING - REMOVAL/INSTALLATION EMOVAL To remove a contactor (Figure 401): CAUTION: AIRCRAFT BUS POWER FEEDERS ARE WIRED DIRECTLY TO THE CONTACTORS. ENSURE THAT AIRCRAFT POWER IS OFF AND DISPLAY A SIGN IN THE AIRCRAFT STATING THAT AIRCRAFT POWER IS TO REMAIN OFF UNTIL CABIN BUS POWER CONTACTOR WORK IS COMPLETED.
  • Page 218 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION To install a contactor (Figure 401): Position contactor and secure in place with fasteners. Restore electrical connections to contactor. Install closeout panel and secure with fasteners. Perform test in accordance with ADJUSTMENT/TEST. Remove all equipment used for these tasks and return aircraft to its initial condition. To install the galley circuit breaker panel (Figure 402):...
  • Page 219 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CONTACTOR (4 PLACES) CONTACTORS - REMOVAL/INSTALLATION FIGURE 401 24-70-00 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
  • Page 220 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CIRCUIT BREAKER PANEL CIRCUIT BREAKER PANEL COVER PLATE TRIM PIECE GALLEY CIRCUIT BREAKER PANEL - REMOVAL/INSTALLATION FIGURE 402 24-70-00 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 221 Verify that all circuit breakers are closed on all circuit breaker panels except those necessary for ground safety. Test the load shedding system in accordance with Bombardier Completion Center Ground Test Procedure, document number D-GT24035000, revision (B), or the latest approved revision.
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  • Page 223 CHAPTER 25 - EQUIPMENT/ FURNISHINGS List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 25 - EQUIPMENT/FURNISHINGS LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 25 - Effective Pages Nov 10/2006 25-18-01 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 25-20-10...
  • Page 224 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Ch-Se-Su Page Date Ch-Se-Su Page Date 25-21-30 Nov 10/2006 25-24-30 Nov 10/2006 Nov 10/2006 Nov 10/2006 25-23-37 Nov 10/2006 25-24-30 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 25-23-37 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 25-26-10 Nov 10/2006 Nov 10/2006...
  • Page 225 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Ch-Se-Su Page Date Ch-Se-Su Page Date 25-29-00 Nov 10/2006 25-49-00 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 25-29-00 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 25-30-10 Nov 10/2006 Nov 10/2006 25-49-00 Nov 10/2006 Nov 10/2006 25-30-10 Nov 10/2006...
  • Page 226 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Ch-Se-Su Page Date Ch-Se-Su Page Date 25-61-01 Nov 10/2006 Nov 10/2006 25-61-01 Nov 10/2006 Nov 10/2006 25-61-01 Nov 10/2006 Nov 10/2006 25-62-00 Dec 14/01 Dec 14/01 Dec 14/01 Dec 14/01 25-62-00 Dec 14/01 Dec 14/01 25-62-00 Dec 14/01 Dec 14/01 25-62-00...
  • Page 227 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 25 - EQUIPMENT/FURNISHINGS TABLE OF CONTENTS Subject Ch-Se-Su Page COCKPIT MISCELLANEOUS INSTALLATIONS 25-11-00 Description/Operation Description/Location Removal/Installation Removal Installation ENTRY AREA HEADLINER 25-15-01 Description/Operation Description/Location Removal/Installation Removal Installation ENTRY AREA CURTAINS 25-15-05 Description/Operation Description/Location Removal/Installation Removal...
  • Page 228 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page SEATING 25-21-00 Adjustment/Test Operational Test of the Passenger Seat Inertia Reels Operational Test of the Passenger Seat Tracking and Locking Mechanisms Inspection/Check General Visual Inspection of the Passenger Seat Restraints PASSENGER SINGLE SEATS 25-21-10 Description/Operation Description...
  • Page 229 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page DIVANS 25-21-30 Description/Operation Description/Location Servicing Introduction Job Set-up Procedure Job Completion Removal/Installation Removal Installation Inspection/Check Introduction Job Set-up Procedure Job Completion FORWARD CABIN BULKHEADS 25-23-37 Description/Operation Description/Location Removal/Installation Removal Installation MID CABIN BULKHEADS 25-23-55 Description/Operation Description/Location/Operation...
  • Page 230 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page STORAGE CABINETS 25-24-20 Description/Operation Description/Location/Operation Removal/Installation Removal Installation DIVAN END CABINETS 25-24-30 Description/Operation Description/Location Operation Removal/Installation Removal Installation CABIN SIDE PANELS 25-26-10 Description/Operation Description/Location Removal/Installation Removal Installation CABIN PASSENGER SERVICE UNIT 25-26-20 Description/Operation Description/Location Removal/Installation Removal...
  • Page 231 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page ADJUSTABLE-HEIGHT TABLES 25-27-35 Description/Operation Description/Location Operation Removal/Installation Removal Installation FLOOR COVERING 25-29-00 Description/Operation Description/Location Removal/Installation Removal Installation GALLEY ELECTRICAL OUTLETS 25-30-10 Description/Operation Description/Location/Operation Adjustment/Test General GALLEY 25-35-01 Description/Operation Description/Location Removal/Installation Removal Installation Inspection/Check General Visual Inspection of the Galley Waste Container GALLEY EQUIPMENT 25-35-05...
  • Page 232 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page AFT LAVATORY 25-49-00 Description/Operation Description/Location Removal/Installation Removal Installation Inspection/Check General Visual Inspection of the Lavatory Waste Container AFT LAVATORY HEADLINER 25-49-03 Description/Operation Description/Location Removal/Installation Removal Installation AFT LAVATORY SIDE PANELS 25-49-05 Description/Operation Description/Location Removal/Installation Removal Installation...
  • Page 233 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page LIFE RAFTS 25-61-01 Description/Operation Description/Location Maintenance Practices Introduction Job Set-up Procedure Job Completion Servicing Restore the Life Raft Inspection/Check General Visual Inspection of the Life Raft 406MHz ELT 25-62-00 Description Location Operation Removal/Installation Removal Installation Adjustment/Test...
  • Page 234 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page THERMAL/ACOUSTIC INSULATION 25-80-10 Description/Operation Description/Location Maintenance Practices Removal/Installation Inspection/Check Repairs EFFECTIVITY: 5596-SMM Page 8 25 - Contents Revision A Nov 10/2006...
  • Page 235 COCKPIT MISCELLANEOUS INSTALLATIONS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL COCKPIT MISCELLANEOUS INSTALLATIONS - DESCRIPTION/OPERATION ESCRIPTION OCATION The following miscellaneous equipment has been installed in the cockpit. Headliner A preformed, three-piece headliner is installed in the cockpit. The headliner is secured to existing attach points, some of which are shared with the sunvisor track.
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  • Page 237: Removal

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL COCKPIT MISCELLANEOUS INSTALLATIONS - REMOVAL/INSTALLATION EMOVAL To remove the cockpit headliner (Figure 401): Remove sunvisor track (1.C.). Remove fasteners securing headliner to remaining attaching mounts. Tip headliner down to clear overhead console. Continue to pull headliner together at aft ends. Disconnect drain tubes from fittings at FS274.
  • Page 238 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Secure fasteners through headliner into mounting brackets. Install sunvisor track (2.C.). Remove all equipment used for these tasks and return aircraft to its initial condition. To install a sunvisor (Figure 402): Position sunvisor. Rotate knob to tighten sunvisor clamp into place. To install the sunvisor track (Figure 402):...
  • Page 239 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL HEADLINER KNOB CLAMP SCREW RAIL ASSEMBLY SUNVISOR SUNVISORS - REMOVAL/INSTALLATION FIGURE 402 25-11-00 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 241 ENTRY AREA HEADLINER CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY AREA HEADLINER - DESCRIPTION/OPERATION ESCRIPTION OCATION A one-piece headliner is installed in the entry area. The right side of the headliner is fastened to brackets which slide over the galley. The aft edge of the headliner is secured to the cabin headliner with a hinge pin .
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  • Page 243 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY AREA HEADLINER - REMOVAL/INSTALLATION EMOVAL To remove the entry area headliner (Figure 401 Figure 402): Open and lock out applicable lighting circuit breakers (33-10-00, 33-45-00, and 33-51-00). Remove forward left-hand wardrobe switch panels (23-90-00). Remove FS350/FS354.75 closeout cap. Remove hinge pin securing entry headliner to main cabin headliner.
  • Page 244 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY HEADLINER HINGE HEADLINER ISOLATOR (TYPICAL) BRACKET PANEL CURTAIN TRACK HEADLINER GALLEY ENTRY AREA HEADLINER - REMOVAL/INSTALLATION FIGURE 401 25-15-01 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 245 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FORWARD WARDROBE CLOSEOUT ISOLATOR (TYPICAL) HEADLINER HINGE HEADER CURTAIN TRACK ENTRY AREA HEADLINER - REMOVAL/INSTALLATION FIGURE 402 25-15-01 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 247 ENTRY AREA CURTAINS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY AREA CURTAINS - DESCRIPTION/OPERATION ESCRIPTION OCATION Acoustic Curtain An acoustic curtain for noise reduction and temperature insulation has been provided to close off the main entry/airstair during flight. The curtain is suspended from a flush-mounted track recessed in the entry headliner and stowed on the forward side of the main entry in an alcove in the wardrobe.
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  • Page 249 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY AREA CURTAINS - REMOVAL/INSTALLATION EMOVAL To remove a curtain (Figure 401): Remove fasteners securing overhead track. Remove track. Slide curtain from end of track. Remove curtain. NSTALLATION To install a curtain (Figure 401): Slide curtain into track. Position track and secure with fasteners.
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  • Page 251 JUMPSEAT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL JUMPSEAT - DESCRIPTION/OPERATION ESCRIPTION OCATION A forward-facing, stowable jumpseat is approved for occupancy during takeoff and landing, and can be used as a cockpit observer’s seat. A restraint system for the jumpseat includes a shoulder harness with inertia reel.
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  • Page 253 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL JUMPSEAT - REMOVAL/INSTALLATION EMOVAL To remove the jumpseat (Figure 401): Open and lock out observer audio circuit breaker, CBP2 H-8. Pull handle to release jumpseat mechanism. Slide seat assembly toward center of aircraft until mount is fully extended. Disconnect electrical connections to observer audio control panel.
  • Page 254 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MOUNTING BOLTS (TYPICAL) JUMPSEAT - REMOVAL/INSTALLATION FIGURE 401 25-18-01 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...

  • Page 255: Introduction

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL JUMPSEAT - ADJUSTMENT/TEST PERATIONAL EST OF THE UMPSEAT NERTIA EELS Introduction Purpose TLMC Task 25-18-60-602 Test Set-up Deploy the jumpseat according to placarded instructions. Procedure Perform an operational test of the jumpseat inertia reels as follows: Pull lightly on the shoulder straps.
  • Page 256 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PERATIONAL EST OF THE UMPSEAT RACKING AND OCKING ECHANISMS Introduction Purpose TLMC Task 25-18-60-603 Procedure Perform an operational test of the jumpseat as follows: Deploy the seat assembly and confirm the following: • Seat moves freely along its tracks •...
  • Page 257 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL JUMPSEAT - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE UMPSEAT ESTRAINTS Introduction Purpose TLMC Task 25-18-60-601 Job Set-up Deploy the jumpseat according to placarded instructions. Procedure Perform a general visual inspection of the jumpseat safety restraints as follows: Examine the full length of each restraint strap for deterioration, safety of installation, and damage.
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  • Page 259 PASSENGER COMPARTMENT ELECTRICAL OUTLETS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER COMPARTMENT ELECTRICAL OUTLETS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Outlets for 115VAC/60Hz are located in the cabin as follows: • One single outlet in dado panel at left-hand seat 2 • One single outlet in dado panel at left-hand seat 4 •...
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  • Page 261 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER COMPARTMENT ELECTRICAL OUTLETS - ADJUSTMENT/TEST ENERAL Refer to 24-25-00, 60HZ POWER SYSTEM, ADJUSTMENT/TEST, for test procedures. 25-20-10 TE-55965000-SMM Page 501 EFFECTIVITY: Revision A Nov 10/2006...
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  • Page 263 SEATING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SEATING - ADJUSTMENT/TEST PERATIONAL EST OF THE ASSENGER NERTIA EELS Introduction Purpose TLMC Task 25-21-60-602 Reference SMM sections: • 25-21-10 • 25-21-20 • 25-21-30 Procedure Perform an operational test of each passenger seat inertia reels as follows: Pull lightly on the shoulder straps.
  • Page 264 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PERATIONAL EST OF THE ASSENGER RACKING AND OCKING ECHANISMS Introduction Purpose TLMC Task 25-21-60-603 Reference SMM sections: • 25-21-10 • 25-21-20 Procedure Test the fixed base passenger seats as follows: Configure the seat in the takeoff and landing position. Confirm full seat travel and that the seat locks in position.
  • Page 265 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SEATING - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE ASSENGER ESTRAINTS Introduction Purpose TLMC Task 25-21-60-601 Reference SMM sections: • 25-21-10 • 25-21-20 • 25-21-30 Job Set-up Remove the seat cushions (secured with hook-and-loop fasteners), as required. Procedure Perform the general visual inspection of the restraints as follows: Examine the full length of each restraint strap for deterioration, security of installation,...
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  • Page 267 PASSENGER SINGLE SEATS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER SINGLE SEATS - DESCRIPTION/OPERATION ESCRIPTION Four passenger single seats are installed in the aircraft. Each seat is fastened to seat tracks using four stud-and-nut assemblies. All single seats are equipped with lap belts. They can track 9" forward and aft, and 5"...
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  • Page 269: Introduction

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER SINGLE SEATS - SERVICING NTRODUCTION Purpose The following procedure gives instructions for replacing the passenger seat belts. Equipment and Facilities Required Equipment • Standard tool kit Facilities • None Position seat back in its full recline position. Remove seat cushion to access belt attachment points.
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  • Page 271 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER SINGLE SEATS - REMOVAL/INSTALLATION EMOVAL CAUTION: PRIOR TO REMOVAL AND/OR INSTALLATION OF PASSENGER SEATING, ENSURE THAT ALL CABIN EQUIPMENT AND FURNISHINGS ARE PROPERLY PROTECTED. USE CARE NOT TO DAMAGE OR SOIL UPHOLSTERY COVERINGS. NOTE: Removal or installation procedures for forward- and aft-facing seats are identical. For a detailed description, refer to the seat manufacturer’s documentation.
  • Page 272 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DOUBLE LUG SEAT SHEAR WASHER RETAINER SPACER SEAT TRACK PASSENGER SEATS - REMOVAL/INSTALLATION FIGURE 401 25-21-10 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 273 PASSENGER DOUBLE SEATS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER DOUBLE SEATS - DESCRIPTION/OPERATION ESCRIPTION Two double passenger seats have been installed in the aircraft. The seats are equipped with lap belts. They can track 9" forward and aft, and 2.5” to 4.5" laterally on their bases, and recline 90°. Each double seat is fastened to seat tracks using four stud-and-nut assemblies.
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  • Page 275 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER DOUBLE SEATS - SERVICING NTRODUCTION Purpose The following procedure gives instructions for replacing the passenger seat belts. Equipment and Facilities Required Equipment • Standard tool kit Facilities • None Push and hold seat-recline button and push against seat-back to recline. Release button to lock seat-back in position.
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  • Page 277 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER DOUBLE SEATS - REMOVAL/INSTALLATION EMOVAL CAUTION: PRIOR TO REMOVAL AND/OR INSTALLATION OF PASSENGER SEATING, ENSURE THAT ALL CABIN EQUIPMENT AND FURNISHINGS ARE PROPERLY PROTECTED. USE CARE NOT TO DAMAGE OR SOIL UPHOLSTERY COVERINGS. NOTE: Removal or installation procedures for forward and aft-facing seats are identical. For a detailed description, refer to the chair manufacturer’s documentation.
  • Page 278 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Restore power (AMM Task 24-00-00-861-801) and verify proper operation of installed components, including:. • Cabin Management System, 23-90-00, ADJUSTMENT/TEST • Emergency escape path lighting system Refer to component maintenance manual for details on inspection, adjustment, and testing. (10) When maintenance procedures have been completed, return aircraft to its initial condition.
  • Page 279 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL STUD SEAT LOCKNUT WASHER STUD RETAINER SPACER (IF INSTALLED) SEAT TRACK PASSENGER DOUBLE SEATS - REMOVAL/INSTALLATION FIGURE 401 25-21-20 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 281 DIVANS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DIVANS - DESCRIPTION/OPERATION ESCRIPTION OCATION A three-seat full-berthing divan, belted for three, is located in the main cabin (see Cabin Passenger Seating). The divan is attached to the divan aft end cabinet with fasteners accessed from inside the divan, and to the production seat tracks with double lug studs.
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  • Page 283 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DIVANS - SERVICING NTRODUCTION Purpose The following procedure gives instructions for replacing the divan seat belts. NOTE: Includes replacement of entire seat-belt assembly Equipment and Facilities Required Equipment • Standard tool kit Facilities • None Removals as needed to access component Remove plug-in armrests.
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  • Page 285 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DIVANS - REMOVAL/INSTALLATION EMOVAL CAUTION: PRIOR TO REMOVAL AND/OR INSTALLATION OF DIVAN, ENSURE THAT ALL CABIN EQUIPMENT AND FURNISHINGS ARE PROPERLY PROTECTED. To remove the divan (Figure 401): Remove power from emergency escape path lighting system. Remove plug-in armrests.
  • Page 286 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Install seat cushions. Install plug-in armrests. (10) Restore power (AMM Task 24-00-00-861-801) and verify proper operation of emergency escape path lighting. (11) Remove all equipment used for these tasks and return aircraft to its initial condition. 25-21-30 EFFECTIVITY: TE-55965000-SMM Page 402...
  • Page 287 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DOUBLE LUG SEAT STUDS (TYPICAL) DIVAN FRAME LOCK DIVAN LOCK FRAME WASHER WASHER DIVAN FRAME FOOT SPACER FOOT SPACER DOUBLE LUG SEAT DOUBLE LUG SEAT TRACK FITTINGS TRACK FITTING SEAT TRACK SEAT TRACK DIVANS - REMOVAL/INSTALLATION FIGURE 401 25-21-30 EFFECTIVITY: TE-55965000-SMM...
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  • Page 289 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DIVANS - INSPECTION/CHECK NTRODUCTION Purpose The following procedure gives instructions for examining the divan structure and seat belts. Equipment and Facilities Required Equipment • Flashlight Facilities • None Perform removals as needed to access components for inspection. Open cabinets under divan.
  • Page 290 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Perform an operational test of the divan seat belts. Verify that seat-belt latches connect and release properly. Verify that belt adjustment holds its position and releases properly. Perform a general visual inspection of the storage doors under the divan. Verify that each door is in correct alignment when closed.
  • Page 291 FORWARD CABIN BULKHEADS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FORWARD CABIN BULKHEADS - DESCRIPTION/OPERATION ESCRIPTION OCATION Bulkhead FS350 Bulkhead FS350 is located directly aft of the entry door and galley. The left-hand bulkhead is a two-piece assembly composed of a forward and aft partition, and houses a video monitor for entertainment and information services.
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  • Page 293 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FORWARD CABIN BULKHEADS - REMOVAL/INSTALLATION EMOVAL To remove the pocket door lock spring: Remove right-hand bulkhead aft partition (1.B.). Slide door to closed position. Remove door lock spring. To remove the right-hand bulkhead aft partition (Figure 401): Remove passenger seat as necessary to prevent damage (25-21-10).
  • Page 294 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Remove fasteners securing aft partition to floor channel bracket. Depress spring-loaded pin assembly and slide partition inboard. Move aft partition inboard to release from clip brackets. Disconnect any remaining electrical or air connections. (10) Remove aft partition. To remove the left-hand bulkhead forward partition (Figure 402):...
  • Page 295 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install the right-hand bulkhead forward partition (Figure 402): Position forward partition and secure with fasteners to galley. Install sliding door and check for proper operation, if removed. Install drawers and contents into galley. Install aft partition (2.B.). Remove all equipment used for these tasks and return aircraft to its initial condition.
  • Page 296 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL RH BULKHEAD FORWARD PARTITION LH BULKHEAD FORWARD RH BULKHEAD PARTITION AFT PARTITION SPRING-LOADED PIN ASSEMBLY LH BULKHEAD AFT PARTITION CLIP BRACKETS (TYPICAL) RH AFT PARTITION ATTACH POINTS LH AFT PARTITION ATTACH POINTS (TYPICAL) LH FORWARD PARTITION ATTACH POINTS (TYPICAL) BULKHEAD FS350 - REMOVAL/INSTALLATION...
  • Page 297 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LH BULKHEAD AFT PARTITION SPRING-LOADED PIN ASSEMBLY RH BULKHEAD FORWARD LH BULKHEAD PARTITION FORWARD PARTITION RH BULKHEAD AFT PARTITION DOOR JAMB ATTACH POINTS (TYPICAL) GALLEY ATTACH POINTS (TYPICAL) BULKHEAD FS350 - REMOVAL/INSTALLATION FIGURE 402 25-23-37 EFFECTIVITY: TE-55965000-SMM Page 405 Revision A Nov 10/2006...
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  • Page 299 MID CABIN BULKHEADS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MID CABIN BULKHEADS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Bulkhead FS560 Bulkhead FS560 is located directly forward of the lavatory. The right-hand bulkhead houses a video monitor for entertainment and information services. A door header has been installed between the left-hand and right-hand bulkheads.
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  • Page 301 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MID CABIN BULKHEADS - REMOVAL/INSTALLATION EMOVAL To remove the left-hand bulkhead (Figure 401 Figure 402): Remove contents from vanity cabinet as necessary to access fasteners securing bulkhead to vanity cabinet. Remove door (1.C.). Remove door header: Remove inboard fasteners on slide pins.
  • Page 302 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Remove divan aft end cabinet (25-24-30). If installed, remove fasteners securing bulkhead to sideledge angle bracket. Remove fasteners securing bulkhead to toilet shroud/storage cabinet assembly. Remove fasteners securing pin-bracket assemblies to bulkhead. (10) Remove fasteners securing floor angle brackets to floor and seat tracks. (11) Slide bulkhead inboard and remove from aircraft.
  • Page 303 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL (11) Remove all equipment used for these tasks and return aircraft to its initial condition. To install the right-hand bulkhead (Figure 401 Figure 402): Slide bulkhead into position. Install fasteners securing bulkhead to sideledge angle bracket, if applicable. Install fasteners securing pin-bracket assemblies to bulkhead.
  • Page 304 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PIN-BRACKET DOOR HINGES ASSEMBLIES RH BULKHEAD HEADER PIN-BRACKET ASSEMBLIES LH BULKHEAD DIVAN AFT END CABINET ATTACH POINTS (TYPICAL) FLOOR ANGLE BRACKETS (TYPICAL) AFT LH STORAGE FLOOR ANGLE CABINET ATTACH BRACKETS POINTS (TYPICAL) (TYPICAL) BULKHEAD FS560 - REMOVAL/INSTALLATION FIGURE 401 25-23-55 EFFECTIVITY: TE-55965000-SMM...
  • Page 305 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PIN-BRACKET ASSEMBLIES DOOR HINGES HEADER RH BULKHEAD PIN-BRACKET ASSEMBLIES LH BULKHEAD TOILET SHROUD AND STORAGE CABINET ATTACH POINTS (TYPICAL) VANITY AND CURIO CABINET ATTACH POINTS (TYPICAL) BULKHEAD FS560 - REMOVAL/INSTALLATION FIGURE 402 25-23-55 EFFECTIVITY: TE-55965000-SMM Page 405 Revision A Nov 10/2006...
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  • Page 307 AFT CABIN BULKHEADS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT CABIN BULKHEADS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Bulkhead FS587 Bulkhead FS587 is located forward of the baggage area. A door header has been installed between the left-hand and right-hand bulkheads. The door header is secured to the left-hand and right-hand bulkheads with slide pins.
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  • Page 309 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT CABIN BULKHEADS - REMOVAL/INSTALLATION EMOVAL NOTE: Baggage and/or lavatory headliner may need to be removed before removing the bulkheads. To remove the left-hand bulkhead (Figure 401 Figure 402): Shut off aircraft power. Remove door (1.C.). Remove door header: Remove inboard fasteners on slide pins.
  • Page 310 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Remove contents from lavatory storage cabinet. Remove toilet shroud cover. Remove fasteners securing floor angle bracket to floor and seat tracks. Remove fasteners securing bulkhead to toilet shroud/storage cabinet assembly. (10) Slide bulkhead inboard and remove from aircraft. To remove the baggage compartment bulkhead door: NOTE: For proper fit and operation of the door, mark the bushings, hinge block assemblies, and veneer filler pieces with their location as they are removed.
  • Page 311 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install the right-hand bulkhead (Figure 401 Figure 402): Slide bulkhead into position. Install fasteners securing bulkhead to toilet shroud/storage cabinet assembly (25-49-00). Install fasteners securing floor angle bracket to floor and seat tracks. Install baggage compartment water tank compartment closeout. Install electrical components mounted to water tank closeout access panels and restore electrical connections.
  • Page 312 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHANNEL HEADER DOOR HINGES RH BULKHEAD CHANNEL VANITY CABINET AND CURIO CABINET ATTACH POINTS (TYPICAL) TOILET SHROUD/ STORAGE CABINET ATTACH POINTS (TYPICAL) LH BULKHEAD BULKHEAD FS587 - REMOVAL/INSTALLATION FIGURE 401 25-23-73 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 313 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL HEADER CHANNEL DOOR HINGES P-SEAL RH BULKHEAD CHANNEL LH BULKHEAD FLOOR ATTACH ANGLE BRACKET FLOOR ATTACH ANGLE BRACKET BULKHEAD FS587 - REMOVAL/INSTALLATION FIGURE 402 25-23-73 EFFECTIVITY: TE-55965000-SMM Page 405 Revision A Nov 10/2006...
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  • Page 315 WARDROBES CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WARDROBES - DESCRIPTION/OPERATION ESCRIPTION OCATION Forward Wardrobe The forward wardrobe is located on the left side of the aircraft just forward of the main cabin door at FS280 to FS310. The wardrobe assembly is secured to the aircraft floor with fasteners and angle brackets at the base of the forward and aft partitions.
  • Page 316 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SWITCH PANELS EMERGENCY EQUIPMENT MISC STORAGE PLACARD JUMPSEAT LIGHT SWITCH OXYGEN MASK AUDIO PANEL MASK CREW PBE FLASHLIGHT FIRE EXTINGUISHER PORTABLE OXYGEN EMERGENCY MEDICAL KIT BOTTLE AND MASK FIRST AID KIT FORWARD WARDROBE 25-24-10 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 317 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WARDROBES - REMOVAL/INSTALLATION EMOVAL CAUTION: TO PREVENT CONTAMINATION, INSTALL PROTECTIVE COVERS ON ALL OXYGEN LINES IMMEDIATELY AFTER DISCONNECTING. DO NOT REMOVE PROTECTIVE COVERS UNTIL IMMEDIATELY BEFORE CONNECTING. OBSERVE INSTALLATION AND TORQUING PROCEDURES FOR OXYGEN FITTINGS AND LINES IN CHAPTER 20 OF THE CANADAIR AIRCRAFT MAINTENANCE MANUAL FOR INSTALLATIONS AND REMOVALS IN THIS SECTION.
  • Page 318 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL While depressing spring-loaded pin assembly, slide wardrobe cabinet into correct location until pin assembly inserts into intercostal. Install fasteners securing angle brackets to floor. Restore electrical connections to jumpseat light bright/dim controller (33-10-00). Restore any remaining electrical connections. Restore oxygen connection.
  • Page 319 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PIN-BRACKET ASSEMBLY FLOOR ATTACH ANGLE BRACKETS FORWARD WARDROBE (TYPICAL) - REMOVAL/INSTALLATION FIGURE 401 25-24-10 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 321 STORAGE CABINETS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL STORAGE CABINETS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Aft Storage Cabinet A storage cabinet is located in the aft section of the cabin on the left side. It provides miscellaneous storage, and storage for two fire extinguishers. The aft storage cabinet is secured to the forward side of left-hand bulkhead FS560 (25-23-55), to the sideledge with a plate, to the floor, and to the seat track with a fastener and seat track insert.
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  • Page 323 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL STORAGE CABINETS - REMOVAL/INSTALLATION EMOVAL To remove the aft left-hand storage cabinet (Figure 401 Figure 402): Remove contents from storage cabinet. Remove drawers. Remove closeout panel. Remove fasteners securing storage cabinet to bulkhead. Remove fasteners securing storage cabinet to seat track and floor. Remove fasteners securing sideledge attach plate to storage cabinet.
  • Page 324 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SIDELEDGE ATTACH PLATE BULKHEAD ATTACH POINTS (TYPICAL) CLOSEOUT PANEL SEAT TRACK ATTACH POINT FLOOR ATTACH POINTS AFT STORAGE CABINET - REMOVAL/INSTALLATION FIGURE 401 25-24-20 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 325 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BOLT SPACER WASHER BUSHING INSERT CABINET BUSHING SEAT TRACK FITTING SEAT TRACK BOLT WASHER SPACER BUSHING INSERT CABINET BUSHING FLOOR AFT STORAGE CABINET - REMOVAL/INSTALLATION FIGURE 402 25-24-20 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 327 DIVAN END CABINETS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DIVAN END CABINETS - DESCRIPTION/OPERATION ESCRIPTION OCATION Divan Aft End Cabinet An end cabinet is located aft of the divan. The end cabinet is secured to the forward side of right-hand bulkhead FS560 (25-23-55), to the sideledge with brackets, to the divan frame, and to the floor seat tracks with fasteners and seat track inserts.
  • Page 328 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CD PLAYER SWITCH PANELS VIDEO CASSETTE PLAYER DVD PLAYER PRINTER/FAX MACHINE PROVISIONS DIVAN AFT END CABINET 25-24-30 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 329 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DIVAN END CABINETS - REMOVAL/INSTALLATION EMOVAL NOTE: Open and lock out applicable circuit breakers as needed before removing cabinet: (23-32-00, 23-33-00, 23-90-00, 24-25-00, and 33-21-08). To remove the divan aft end cabinet (Figure 401 Figure 402): Remove power from emergency escape path lighting system.
  • Page 330 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Install entertainment equipment (23-32-00 and 23-33-00). (10) Install contents into end cabinet. (11) Install dado panel (25-27-10), if removed. (12) Install divan (25-21-30), if removed. (13) Verify proper operation of installed components, including: • 60Hz Power System, 24-25-00, ADJUSTMENT/TEST •...
  • Page 331 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BULKHEAD ATTACH POINTS (TYPICAL) SIDELEDGE ATTACH OUTBOARD BRACKETS (TYPICAL) ACCESS PANEL SEAT TRACK ATTACH POINTS (TYPICAL) DIVAN FRAME ATTACH POINTS DIVAN END CABINET - REMOVAL/INSTALLATION FIGURE 401 25-24-30 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
  • Page 332 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BOLT WASHER SPACER BUSHING INSERT CABINET BUSHING SEAT TRACK WASHER FITTING SEAT TRACK CABINET WASHER DIVAN FRAME RING BUSHING SPACER WASHER BOLT DIVAN END CABINET - REMOVAL/INSTALLATION FIGURE 402 25-24-30 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 333 CABIN SIDE PANELS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN SIDE PANELS - DESCRIPTION/OPERATION ESCRIPTION OCATION Each side of the aircraft contains a two-piece side panel. Each outer side panel extends from the top of the sideledge to the headliner. Each inner side panel extends from the top of the sideledge to just below the Passenger Service Unit (PSU).
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  • Page 335 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN SIDE PANELS - REMOVAL/INSTALLATION EMOVAL NOTE: Remove seats (25-21-10) before performing these steps. Remove left-hand bulkhead FS350 (25-23-37) before performing these steps if side panels will be removed from aircraft. To remove an inner side panel (Figure 401): If applicable, remove emergency escape door.
  • Page 336 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install an outer side panel (Figure 401): Lower outer side panel into place. Install fasteners securing outer side panel to brackets. Install PSU (25-26-20). Install inner side panel (2.A.). Remove all equipment used for these tasks and return aircraft to its initial condition. OUTER SIDE PANEL ATTACH POINTS...
  • Page 337 CABIN PASSENGER SERVICE UNIT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN PASSENGER SERVICE UNIT - DESCRIPTION/OPERATION ESCRIPTION OCATION The Passenger Service Units (PSU) extend along the left and right sides of the cabin, between the side panels and the headliner panel. The PSU contains: •...
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  • Page 339 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN PASSENGER SERVICE UNIT - REMOVAL/INSTALLATION EMOVAL To remove a PSU cover: Open and lock out applicable circuit breaker(s), (33-22-20). Pull down at bottom/outboard edge of cover to release from ball catches. Pull down at top/inboard edge of cover to release from remaining ball catches. Disconnect wiring to reading and/or table lights.
  • Page 340 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Restore power (AMM Task 24-00-00-861-801) and verify proper operation of installed components, including: • Emergency Lights, 33-51-00, ADJUSTMENT/TEST • Passenger Compartment Air Distribution, 21-22-00, ADJUSTMENT/TEST • Reading and table lights Remove all equipment used for these tasks and return aircraft to its initial condition. To install a PSU (Figure 401):...
  • Page 341 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PSU ATTACH POINTS PSU COVERS PSU INDIRECT LIGHT (TYPICAL) AIR GASPER (FEEDER) CABIN PSU - REMOVAL/INSTALLATION FIGURE 401 25-26-20 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 343 CABIN HEADLINER CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN HEADLINER - DESCRIPTION/OPERATION ESCRIPTION OCATION A one-piece headliner panel is installed in the main cabin from the forward bulkhead to bulkhead FS560. The headliner contains return air ducts and indirect fluorescent lighting. The cabin headliner is secured with a hinge to the entry headliner, and with fasteners to brackets hidden behind the Passenger Service Units (PSU).
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  • Page 345 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CABIN HEADLINER - REMOVAL/INSTALLATION EMOVAL To remove the headliner (Figure 401): Open and lock out applicable lighting circuit breaker(s) (33-21-02). Remove entry headliner (25-15-01). Remove left-hand bulkhead FS350 (25-23-37), as necessary. Remove left-hand and right-hand PSU (25-26-20). Remove left-hand inner and outer side panels, all left-hand windows, and shades.
  • Page 346 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL HEADLINER INDIRECT LIGHT (TYPICAL) HEADLINER ATTACH POINT (TYPICAL) CABIN HEADLINER CABIN HEADLINER - REMOVAL/INSTALLATION FIGURE 401 25-26-30 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 347 SIDELEDGE/DADO PANELS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SIDELEDGE/DADO PANELS - DESCRIPTION/OPERATION ESCRIPTION OCATION Sideledges are installed on the left and right sides of the cabin, below the side panels, from the forward bulkhead to bulkhead FS560. The sideledges are secured outboard to brackets, which are secured to the airframe.
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  • Page 349 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SIDELEDGE/DADO PANELS - REMOVAL/INSTALLATION EMOVAL NOTE: Open and lock out applicable circuit breaker(s) as needed before removing dado panels or sideledges (21-61-18, 23-16-00, 23-90-00, and 25-20-10). To remove a dado panel (Figure 401 Figure 402): Shut off therapeutic oxygen supply, if applicable. Remove seats (25-21-10 and/or 25-21-20), divan (25-21-30), divan end cabinet (25-24-30), or other obstructions, as necessary.
  • Page 350 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION To install a dado panel (Figure 401 Figure 402): Position dado panel and restore any electrical, air, or oxygen connections. If applicable, restore therapeutic oxygen supply and perform leak check per 35-20-02, ADJUSTMENT/TEST. Push dado panel back against hook-and loop attach points. If applicable, install fasteners securing dado panel to sideledge pullout tables and/or storage boxes.
  • Page 351 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL (10) Restore power (AMM Task 24-00-00-861-801) and verify proper operation of applicable installed components, including: • Iridium Communication System, 23-16-00, ADJUSTMENT/TEST • Cabin Management System, 23-90-00, ADJUSTMENT/TEST • Cabin Temperature Control, 21-61-18, ADJUSTMENT/TEST (11) Remove all equipment used for these tasks and return aircraft to its initial condition. SIDELEDGE HOOK-AND-LOOP SIDELEDGE...
  • Page 352 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DADO PANEL ATTACH POINTS (TYPICAL) DADO PANEL ATTACH POINTS (TYPICAL) (DADO PANEL AT STORAGE BOX) (DADO PANEL AT PULLOUT TABLE) SIDELEDGE/DADO PANELS - REMOVAL/INSTALLATION FIGURE 402 25-27-10 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 353 PULLOUT TABLES CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PULLOUT TABLES - DESCRIPTION/OPERATION ESCRIPTION OCATION Pullout tables are installed into the sideledges. The pullout table assemblies are secured to brackets on the conditioned air ducts and sideledges. PERATION To open a pullout table: Open access panel in top of sideledge.
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  • Page 355 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PULLOUT TABLES - REMOVAL/INSTALLATION EMOVAL To remove a tabletop (Figure 401): Deploy table mechanism. Do not unfold table top. While supporting tabletop, remove fasteners securing tabletop to table mechanism. Remove tabletop. To remove a pullout table assembly (Figure 402): Remove dado panel (25-27-10).
  • Page 356 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TABLETOP ATTACH POINTS (TYPICAL) LEAF HANDLE/SUPPORTS (VIEW LOOKING DOWN) PULLOUT TABLES - REMOVAL/INSTALLATION FIGURE 401 25-27-30 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 357 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TABLETOP ATTACH POINTS (TYPICAL) TABLETOP PULLOUT TABLE MECHANISM ATTACH POINTS PULLOUT TABLE ASSEMBLY PULLOUT TABLE MECHANISM ATTACH POINTS PULLOUT TABLES - REMOVAL/INSTALLATION FIGURE 402 25-27-30 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 359 ADJUSTABLE-HEIGHT TABLES CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ADJUSTABLE-HEIGHT TABLES - DESCRIPTION/OPERATION ESCRIPTION OCATION A mechanical, two-position pedestal conference/dining table is located between the double seats in the cabin. The table incorporates fold-out padded leaves and drink holders. The table can accommodate four meal trays.
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  • Page 361 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ADJUSTABLE-HEIGHT TABLES - REMOVAL/INSTALLATION EMOVAL To remove the adjustable-height table assembly (Figure 401): Fold table leaves to stowed position and install securing straps. Remove fasteners securing table base to floor seat tracks. Remove table assembly. NSTALLATION To install the adjustable-height table assembly (Figure 401):...
  • Page 362 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SEAT TRACK ATTACH POINTS (6 PLACES) BOLT WASHER TABLE BASE SEAT TRACK SEAT TRACK FITTING ADJUSTABLE-HEIGHT TABLE (TYPICAL) - REMOVAL/INSTALLATION FIGURE 401 25-27-35 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 363 FLOOR COVERING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FLOOR COVERING - DESCRIPTION/OPERATION ESCRIPTION OCATION The padded carpet extends from the FS280 bulkhead to the aft pressure bulkhead. It is preshrunk and incorporates a fire-retardant latex and anti-static backing. The carpet may be attached with hook-and-loop strips at the outboard and bulkhead areas.
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  • Page 365 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FLOOR COVERING - REMOVAL/INSTALLATION EMOVAL To remove the cabin carpet: NOTE: Carpet may be secured with hook-and-loop strips along edges. Loosen carpet at lavatory and baggage area and fold to center of lavatory compartment. Fold forward into main cabin area, forward of bulkhead FS560. Loosen and fold entry area carpet into cabin.
  • Page 366 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Position carpet immediately aft of bulkhead FS350. Position carpet down center line of aircraft and unfold. Unfold and position lavatory and baggage compartment carpet. Unfold and position entry area carpet. Secure carpet by pressing down all hook-and-loop strip areas. To install carpet underlay: Position carpet underlay immediately aft of bulkhead FS350.
  • Page 367 GALLEY ELECTRICAL OUTLETS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY ELECTRICAL OUTLETS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Outlets for 115VAC/60Hz are located in the galley as follows: • One dual GFI-type outlet in upper galley In order for the outlets to operate, the cabin bus disconnect switch (24-70-00) must be active and the 60Hz converter (24-25-00) must be energized, and the cabin bus (24-70-00) must be engaged.
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  • Page 369 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY ELECTRICAL OUTLETS - ADJUSTMENT/TEST ENERAL Refer to 24-25-00, 60HZ POWER SYSTEM, ADJUSTMENT/TEST, for test procedures. 25-30-10 TE-55965000-SMM Page 501 EFFECTIVITY: Revision A Nov 10/2006...
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  • Page 371 GALLEY CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY - DESCRIPTION/OPERATION ESCRIPTION OCATION A galley is located in the entryway between FS280 and FS350 on the right-hand side of the aircraft. The galley consists of three major sections: an upper assembly, a lower assembly, and a countertop. The upper galley assembly is fastened to the lower galley and bulkhead FS350.
  • Page 372 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UPPER EQUIPMENT TRAY GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR LIGHTS LIGHTS LIGHTS LIGHTS COFFEE FLOOR CABIN FLOOR CABIN ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER DISP H EATER WATER HEATER WATER PURGE FULL RESET TEST MICROWAVE 115 VAC 60 Hz...
  • Page 373 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MICROWAVE OVEN DUAL GFI (PROVISIONS) RECEPTACLE COFFEE MAKER CIRCUIT BREAKER SWITCH PANEL CRYSTAL PANEL STORAGE HIGH-TEMPERATURE OVEN HOT WATER DISPENSER FLATWARE MISC STORAGE MISC COLD PLATTER STORAGE ICE DRAWER WASTE CONTAINER STORAGE ICE DRAWER JUMPSEAT MINI LIQUOR CHINA STORAGE STORAGE WATER...
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  • Page 375 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY - REMOVAL/INSTALLATION EMOVAL To remove the galley (Figure 401, Figure 402, and Figure 403): WARNING: USE EXTREME CARE WHEN WORKING WITH THE INSTANT HOT WATER DISPENSER (WATER HEATED TO 180° F) AND THE GALLEY WATER HEATER (WATER HEATED TO 125°...
  • Page 376 Load Shedding, 24-70-00, ADJUSTMENT/TEST • Passenger Compartment Air Distribution, 21-22-00, ADJUSTMENT/TEST • Water system per Bombardier Completion Center Ground Test Procedure, document number TE-GTP-243, revision (G), or the latest approved revision • Emergency escape path lighting system (15) Install all loose equipment, drawers, and doors.
  • Page 377 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UPPER GALLEY TO LOWER GALLEY ATTACH POINTS (TYPCIAL) FLOOR ATTACH POINTS (TYPICAL) GALLEY - REMOVAL/INSTALLATION FIGURE 401 25-35-01 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
  • Page 378 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SHEAR PLATE ATTACH POINTS (TYPICAL) GALLEY - REMOVAL/INSTALLATION FIGURE 402 25-35-01 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 379 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SCREW WASHER SPACER BUSHING INSERT GALLEY BUSHING WASHER INSERT AIRCRAFT FLOOR GALLEY SCREW SHEAR PLATES WASHER SPACER BUSHING AIRFRAME GALLEY - REMOVAL/INSTALLATION FIGURE 403 25-35-01 EFFECTIVITY: TE-55965000-SMM Page 405 Revision A Nov 10/2006...
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  • Page 381 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE ALLEY ASTE ONTAINER Introduction Purpose TLMC Task 25-35-60-601 Procedure Perform a detailed visual inspection of the waste container as follows: Inspect the condition of the door assembly for evidence of deterioration, wear, or damage.
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  • Page 383 GALLEY EQUIPMENT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY EQUIPMENT - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION The following equipment has been installed in the galley: Coffee Maker A coffee maker is located in the upper galley. Controls for operating the coffee maker are on the unit.
  • Page 384 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL high-temperature oven if the tambour door is not fully open. Table 3 lists the high-temperature oven components. The high-temperature oven is powered by 115VAC 400Hz - CABIN BUS 1. Relay K8MF is powered by 28VDC - CABIN BUS 1. Component (Qty) Location Relay K8MF...
  • Page 385 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Water Heater A water heater is installed in the galley (38-10-40). GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR UPWASH LIGHTS LIGHTS LIGHTS LIGHTS CABIN CABIN COFFEE FLOOR FLOOR DNWASH ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER PURGE...
  • Page 386 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MICROWAVE OVEN DUAL GFI (PROVISIONS) RECEPTACLE COFFEE MAKER CIRCUIT BREAKER SWITCH PANEL CRYSTAL PANEL STORAGE HIGH-TEMPERATURE OVEN HOT WATER DISPENSER FLATWARE MISC STORAGE MISC COLD PLATTER STORAGE ICE DRAWER WASTE CONTAINER ICE DRAWER STORAGE JUMPSEAT MINI LIQUOR CHINA STORAGE STORAGE WATER...
  • Page 387 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UPPER EQUIPMENT TRAY GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR LIGHTS LIGHTS LIGHTS LIGHTS COFFEE CABIN FLOOR FLOOR CABIN ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER DISP H EATER WATER HEATER WATER PURGE FULL RESET TEST MICROWAVE 115 VAC 60 Hz...
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  • Page 389 Restore electrical and water connections. Restore power (AMM Task 24-00-00-861-801). Perform applicable ground test(s) per Bombardier Completion Center Ground Test Procedure, document number TE-GTP-243, revision (G), or the latest approved revision. Remove all equipment used for these tasks and return aircraft to its initial condition.
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  • Page 391 LAVATORY ELECTRICAL OUTLETS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LAVATORY ELECTRICAL OUTLETS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Outlets for 115VAC/60Hz are located in the lavatory as follows: • One single outlet in vanity cabinet under sink In order for the outlets to operate, the cabin bus disconnect switch (24-70-00) must be active and the 60Hz converter (24-25-00) must be energized, and the cabin bus (24-70-00) must be engaged.
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  • Page 393 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LAVATORY ELECTRICAL OUTLETS - ADJUSTMENT/TEST ENERAL Refer to 24-25-00, 60HZ POWER SYSTEM, ADJUSTMENT/TEST, for test procedures. 25-40-10 TE-55965000-SMM Page 501 EFFECTIVITY: Revision A Nov 10/2006...
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  • Page 395 AFT LAVATORY CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY - DESCRIPTION/OPERATION ESCRIPTION OCATION The aft lavatory consists of a vanity cabinet, countertop, and curio cabinet assembly with mirror cabinet on the left side; and a toilet and toilet shroud/storage cabinet assembly on the right side. It is located between bulkheads FS560 and FS587.
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  • Page 397 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY - REMOVAL/INSTALLATION EMOVAL To remove the curio cabinet assembly mirror cabinet: Shut off aircraft power. Remove contents and shelves from mirror cabinet, as necessary. Remove mirror lamps (20-12-00), as necessary. Remove fasteners securing mirror cabinet to curio cabinet assembly. Move mirror cabinet inboard and disconnect electrical wiring.
  • Page 398 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Remove vanity curio cabinet assembly (1.B.). Drain water system and relieve water system pressure. Disconnect switch panels (23-90-00). Remove doors and drawer. Remove closeout panels. Disconnect drain lines to sink. Disconnect all electrical and air connections. (10) Remove middle baggage compartment headliner (25-55-03).
  • Page 399 Restore power (AMM Task 24-00-00-861-801) and verify proper operation of the water system per: • Bombardier Completion Center Ground Test Procedure, document number TE-GTP-243, revision (G), or the latest approved revision Remove all equipment used for these tasks and return aircraft to its initial condition.
  • Page 400 (11) Install vanity curio cabinet assembly (2.B.). (12) Restore power (AMM Task 24-00-00-861-801) and verify proper operation of installed components, including: • Cabin management system per Bombardier Completion Center Ground Test Procedure, document number TE-GTP-251, revision (E), or the latest approved revision •...
  • Page 401 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BULKHEAD FS560 ATTACH POINTS (TYPICAL) BULKHEAD FS587 MIRROR CABINET ATTACH POINTS ATTACH POINTS (TYPICAL) (TYPICAL) FLOOR ANGLE BRACKET LAVATORY VANITY CABINET - REMOVAL/INSTALLATION FIGURE 401 25-49-00 EFFECTIVITY: TE-55965000-SMM Page 405 Revision A Nov 10/2006...
  • Page 402 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BULKHEAD FS560 ATTACH POINTS (TYPICAL) FLOOR ANGLE BRACKETS (TYPICAL) BULKHEAD FS587 ATTACH POINTS (TYPICAL) LAVATORY TOILET SHROUD/STORAGE CABINET ASSEMBLY - REMOVAL/INSTALLATION FIGURE 402 25-49-00 EFFECTIVITY: TE-55965000-SMM Page 406 Revision A Nov 10/2006...
  • Page 403 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE AVATORY ASTE ONTAINER Introduction Purpose TLMC Task 25-49-60-601 Procedure Perform a detailed visual inspection of the waste container as follows: Inspect the condition of the door assembly for evidence of deterioration, wear, or damage.
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  • Page 405 AFT LAVATORY HEADLINER CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY HEADLINER - DESCRIPTION/OPERATION ESCRIPTION OCATION The lavatory headliner is a one-piece assembly covered with customer-approved material. The headliner contains three dome lights and a smoke detector. The sides of the headliner are secured to brackets by fasteners hidden behind the inner side panels. 25-49-03 TE-55965000-SMM Page 1...
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  • Page 407 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY HEADLINER - REMOVAL/INSTALLATION EMOVAL To remove the headliner (Figure 401): Open and lock out applicable circuit breakers (26-10-01, 33-25-50, 33-45-00, and 33-51-00). Remove trim strips (secured with hook-and-loop strips). Remove inner and outer side panels (25-49-05). Remove fasteners securing headliner to brackets.
  • Page 408 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL HEADLINER HEADLINER ATTACH POINTS (TYPICAL) OUTER SIDE PANEL TRIM STRIP INNER SIDE PANEL (VIEW LOOKING FORWARD, LEFT SIDE) HEADLINER HEADLINER ATTACH POINTS (TYPICAL) OUTER SIDE TRIM STRIP PANEL INNER SIDE PANEL (VIEW LOOKING FORWARD, RIGHT SIDE) LAVATORY HEADLINER - REMOVAL/INSTALLATION FIGURE 401 25-49-03...
  • Page 409 AFT LAVATORY SIDE PANELS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY SIDE PANELS - DESCRIPTION/OPERATION ESCRIPTION OCATION The lavatory side panels consist of inner and outer panels. Each side panel extends from the top of a lavatory cabinet to the headliner. The left-hand inner side panel contains an air gasper and an ordinance sign.
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  • Page 411 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY SIDE PANELS - REMOVAL/INSTALLATION EMOVAL To remove the right-hand inner side panel (Figure 401): Shut off oxygen supply to masks. Shut off aircraft power. Remove trim strip to reveal fasteners (trim strip secured with hook-and loop). Remove fasteners securing side panel to headliner.
  • Page 412 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION To install the right-hand inner side panel (Figure 401): NOTE: The outer side panel must be installed first. Position right-hand inner side panel and restore electrical and oxygen connections, and air return connection. Secure outboard edge of side panel in clip at cabinet. Install fasteners securing side panel to headliner.
  • Page 413 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL INNER SIDE PANEL ATTACH POINTS OUTER SIDE PANEL ATTACH POINTS TRIM STRIP INNER SIDE PANEL OUTER SIDE PANEL CLIPS (TYPICAL) (VIEW LOOKING FORWARD, LEFT SIDE) INNER SIDE PANEL ATTACH POINTS OUTER SIDE PANEL ATTACH POINTS TRIM STRIP AIR RETURN OUTER SIDE DIFFUSER...
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  • Page 415 BAGGAGE COMPARTMENT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BAGGAGE COMPARTMENT - DESCRIPTION/OPERATION ESCRIPTION OCATION The baggage compartment is located aft of bulkhead FS587 and extends to the aft pressure bulkhead at FS621. The following features are included in the baggage compartment: • Upholstered bulkheads, door, and headliner/side panels •...
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  • Page 417 BAGGAGE COMPARTMENT HEADLINER CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BAGGAGE COMPARTMENT HEADLINER - DESCRIPTION/OPERATION ESCRIPTION OCATION The baggage compartment headliner extends from FS587 to the aft pressure bulkhead and consists of three sections: right-hand, middle, and left-hand. The right-hand headliner outboard end is secured in an angle bracket at the top of the water compartment closeout.
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  • Page 419 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BAGGAGE COMPARTMENT HEADLINER - REMOVAL/INSTALLATION EMOVAL NOTE: The baggage compartment headliner consists of three sections: right-hand, middle, and left-hand. To remove the right-hand headliner (Figure 401): Open and lock out applicable lighting circuit breakers (33-33-00). Remove fasteners securing headliner to channel assembly. Rotate headliner down and inboard to disengage outboard edge from water compartment closeout angle bracket and to release hook-and-loop strips.
  • Page 420 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION To install the right-hand headliner (Figure 401): Restore electrical connections then position headliner into water compartment closeout angle bracket. Install air return duct connection. Apply pressure to hook-and-loop-attached areas. Install fasteners securing headliner to channel assembly. Restore power (AMM Task 24-00-00-861-801) and verify proper operation of headliner dome light.
  • Page 421 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHANNEL WATER TANK CHANNEL SMOKE CHANNEL SUPPORT CLOSEOUT ASSEMBLY DETECTOR ASSEMBLY FS610 ATTACH RH HEADLINER MIDDLE LH HEADLINER POINTS HEADLINER (VIEW LOOKING DOWN) BAGGAGE COMPARTMENT HEADLINER - REMOVAL/INSTALLATION FIGURE 401 25-55-03 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 423 EMERGENCY EQUIPMENT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EMERGENCY EQUIPMENT - DESCRIPTION/OPERATION ESCRIPTION OCATION The following emergency equipment has been installed in the aircraft. See Emergency Equipment Locations for a floor plan layout. Crash Axe The crash axe is located behind the pilot’s seat on bulkhead FS280L. Smoke Goggles Three pairs of smoke goggles, for use with the oxygen masks, are supplied in the cockpit on bulkhead FS280.
  • Page 424 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CREW LIFE VEST CREW LIFE VEST SMOKE HOOD SMOKE HOOD CRASH AXE HALON FIRE EXTINGUISHER FLASHLIGHT FLASHLIGHT SMOKE GOGGLES SMOKE GOGGLES (2) FIRST-AID KIT FLASHLIGHT CREW PBE CREW LIFE VEST HALON FIRE EXTINGUISHER PORTABLE OXYGEN BOTTLE & MASK BRIEFING CARDS WATER FIRE EXTINGUISHER LIFE VEST...
  • Page 425 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EMERGENCY EQUIPMENT - SERVICING ESTORE THE Introduction Purpose TLMC Task 25-60-60-602 Reference Information REFERENCE DESIGNATION Air Cruisers Company 25-64-02 P/N 63600-Series Component Maintenance Manual Job Set-up Obtain the life vests from all installed locations in the aircraft. Procedure Restore the life vests per manufacturer Component Maintenance Manual (Air Cruisers Company 25-64-02).
  • Page 426 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ESTORE THE MOKE Introduction Purpose TLMC Task 25-60-60-604 Reference Information REFERENCE DESIGNATION Essex PB&R Corp. Technical Essex PB&R Pilot Unit Technical Manual Manual Job Set-up Obtain the smoke hoods from all installed locations in the aircraft. Procedure Restore the PBE per manufacturer Manual (Essex PB&R Corp.
  • Page 427 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EMERGENCY EQUIPMENT - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE Introduction Purpose TLMC Task 25-60-60-601 Job Set-up Obtain the life vests from all installed locations in the aircraft. Procedure Perform a general visual inspection of each life vest as follows: Check the expiration date.
  • Page 428 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENERAL ISUAL NSPECTION OF THE MOKE Introduction Purpose TLMC Task 25-60-60-603 Job Set-up Obtain the smoke hoods from all installed locations in the aircraft. Procedure Perform a general visual inspection of each smoke hood as follows: Check the expiration date.
  • Page 429 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENERAL ISUAL NSPECTION OF THE IRST EDICAL PEN IF EALED Introduction Purpose TLMC Task 25-60-60-605 Job Set-up Obtain the first-aid/medical kit(s) from the forward wardrobe and any other locations. Procedure If sealed, check for expiration date and replace or recondition in accordance with manufacturer’s recommendations (if applicable).
  • Page 430 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENERAL ISUAL NSPECTION OF THE MERGENCY Introduction Purpose TLMC Task 25-60-60-606 Job Set-up Remove the over-wing emergency exit ditching line from its storage area. Procedure Do the general visual inspection of the line as follows: Examine the full length of each line for deterioration, safety of installation, and damage.
  • Page 431 LIFE RAFTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LIFE RAFTS - DESCRIPTION/OPERATION ESCRIPTION OCATION Two life rafts, each containing its own Emergency Locator Transmitter (ELT), are carried on the aircraft. Both are stored under the divan. Instructions for using the life rafts and ELT units are found on the rafts. 25-61-01 TE-55965000-SMM Page 1...
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  • Page 433 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LIFE RAFTS - MAINTENANCE PRACTICES NTRODUCTION Purpose The following procedure gives instructions for preparing the life rafts for return to the manufacturer or an approved facility and for installing the life rafts. Equipment and Facilities Required Equipment •...
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  • Page 435 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LIFE RAFTS - SERVICING ESTORE THE Introduction Purpose TLMC Task 25-61-60-602 Reference Information REFERENCE DESIGNATION Air Cruisers Company 25-62-28 P/N 64413-Series Component Maintenance Manual Job Set-up Obtain the life rafts from all installed locations in the aircraft. Procedure Restore the life rafts per manufacturer CMM (Air Cruisers Company 25-62-28).
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  • Page 437 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LIFE RAFTS - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE Introduction Purpose TLMC Task 25-61-60-601 Job Set-up Obtain the life rafts from all installed locations in the aircraft. Procedure Perform a general visual inspection of each life raft as follows: Check the expiration date.
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  • Page 439 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM 406MHZ ELT ESCRIPTION The Artex 406MHz is a triple frequency ELT transmitter. It has simultaneous transmission capabilities on 121.5MHz, 243MHz, and 406MHz. The manufacturer encodes the ELT serial number, an ID code, and country code on the 406MHz transmission. This data enables the authorities to quickly contact the owner/operator of the ELT.
  • Page 440 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM NAV INTERFACE REMOTE SWITCH ANTENNA (TYPICAL) EQUIPMENT LOCATION 25-62-00 BAS-63010055-SMM-5 (Rev. A) Page 2 Dec 14/01...
  • Page 441 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM REMOTE SWITCH COCKPIT EQUIPMENT LOCATION (TYPICAL) 25-62-00 BAS-63010055-SMM-5 (Rev. A) Page 3 Dec 14/01...
  • Page 442 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM THIS PAGE INTENTIONALLY LEFT BLANK 25-62-00 BAS-63010055-SMM-5 (Rev. A) Page 4 Dec 14/01...
  • Page 443 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM 406MHZ ELT - REMOVAL/INSTALLATION EMOVAL CAUTION: BEFORE ATTEMPTING TO REMOVE OR INSTALL ANY UNITS, TURN ELECTRICAL POWER OFF. To remove the ELT, buzzer, and/or NAV interface unit: Locate unit in aft equipment room. Remove hardware securing unit to mounting bracket. Disconnect antenna lead and remove unit.
  • Page 444 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM To install the antenna: Clean antenna and aircraft mating surfaces in accordance with procedures outlined in CL600-1A11/2A12/2B16 Structural Repair Manual. CAUTION: DO NOT REMOVE CONDUCTIVE FINISH FROM ANTENNA BASE PLATE. Remove any sealant from base plate connector and holes. Ensure that antenna base plate and aircraft mating surface are clean and bright.
  • Page 445 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM 406MHZ ELT - ADJUSTMENT/TEST NTRODUCTION Purpose The following procedure provides instructions for verifying the proper operation of the Artex 406MHz ELT for Canadair CL-600 1A11/2A12/2B16 aircraft. NOTE: The following test procedure requires qualified operators using approved aircraft operating pro- cedures.
  • Page 446 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM In the cockpit, momentarily actuate the ELT switch from the ARM position to the ON position. Verify that the cockpit mounted indicator light flashes. Verify that the buzzer in the tail cone sounds. Verify that a sweeping signal is heard in both the AM radio and the aircraft radio. After approximately three sweeps, return the switch to the ARM position.
  • Page 447 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM 406MHZ ELT - INSPECTION/CHECK 11. I NTRODUCTION NOTE: Refer applicable vendor manual servicing, cleaning, operational checkouts/adjustments or any repair of the equipment that is required. The information in this section is presented to help personnel perform the necessary tasks. As much information as deemed necessary to achieve the described tasks has been given.
  • Page 448 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-602355-NM Visually inspect ELT antenna penetrations. Penetration types are: • Fastener holes filled with expanding fasteners • Open holes used for mounting antennas • Antenna connector routing holes Any evidence of cracking and corrosion is grounds for rejection. •...
  • Page 449 PROTECTIVE BREATHING EQUIPMENT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PROTECTIVE BREATHING EQUIPMENT - DESCRIPTION/OPERATION ESCRIPTION OCATION A crew member Protective Breathing Equipment (PBE) is located in the forward left-hand wardrobe. The PBE consists of a heat-resistant hood with neck seal, two attached 18-liter oxygen bottles, and a carbon dioxide control device.
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  • Page 451 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PROTECTIVE BREATHING EQUIPMENT - SERVICING ESTORE THE Introduction Purpose TLMC Task 25-63-60-602 Reference Information REFERENCE DESIGNATION Essex PB&R Corp. PMR-01 User Reference and Procedures Manual Job Set-up Obtain the Protective Breathing Equipment (PBE) from all installed locations in the aircraft. Procedure Restore the PBE per manufacturer Manual (Essex PB&R Corp.
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  • Page 453 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PROTECTIVE BREATHING EQUIPMENT - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE Introduction Purpose TLMC Task 25-63-60-601 Job Set-up Obtain the PBE from all installed locations in the aircraft. Procedure Perform a general visual inspection of each PBE as follows: Check the expiration date.
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  • Page 455 AFT EQUIPMENT COMPARTMENT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT EQUIPMENT COMPARTMENT - DESCRIPTION/OPERATION ESCRIPTION OCATION Floor/Catwalk Assembly A floor/catwalk assembly has been installed forward of the equipment compartment access door. Right Side Shelf Assembly A shelf assembly is located on the right side in the aft equipment compartment. It is located at approximately FS682, RBL15.
  • Page 456 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PRESSURE BULKHEAD RH SHELF 621.00 700.00 ASSEMBLY LADDER STORAGE (PROVISIONS) AFT EQUIPMENT COMPARTMENT FLOOR/CATWALK DOOR ASSEMBLY STORAGE BOX MAIN WHEEL/TIRE STORAGE (PROVISIONS) SPARE APU ECU (PROVISIONS) AFT EQUIPMENT COMPARTMENT MODIFICATIONS 25-75-00 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 457 THERMAL/ACOUSTIC INSULATION CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THERMAL/ACOUSTIC INSULATION - DESCRIPTION/OPERATION ESCRIPTION OCATION A sophisticated soundproofing and thermal insulation package has been installed in the aircraft. It has been optimized to provide a suitable passenger environment at a minimum weight. The package on this aircraft consists of the following: Fuselage Skin in the Cabin Area (including doors) Individual blankets, consisting of layers of fiberglass insulation and layers of polyimide foam...
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  • Page 459 Inspect blankets for physical damage and moisture retention. Damaged blankets must be repaired or replaced, depending on condition. Blankets which are retaining moisture shall be replaced and should be reported to the Bombardier Completion Center engineering department. Further inspection for corrosion of adjacent structure must be performed if any insulation is found to be retaining moisture.
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  • Page 461 CHAPTER 26 - FIRE PROTEC- TION List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 26 - FIRE PROTECTION LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 26 - Effective Pages Nov 10/2006 Nov 10/2006 26 - Contents Nov 10/2006 Nov 10/2006 26-10-01...
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  • Page 463 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 26 - FIRE PROTECTION TABLE OF CONTENTS Subject Ch-Se-Su Page SMOKE DETECTORS 26-10-01 Description/Operation Description/Location Operation Servicing Restore the Smoke Detectors Removal/Installation Removal Installation Adjustment/Test Introduction Test Set-up Test Test Completion FIRE EXTINGUISHERS 26-20-01 Description/Operation Description/Location/Operation...
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  • Page 465 SMOKE DETECTORS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SMOKE DETECTORS - DESCRIPTION/OPERATION ESCRIPTION OCATION A smoke detector has been installed in the lavatory headliner. The production-installed smoke detector located in the baggage compartment headliner has been replaced with the same Walter Kidde smoke detector part number as installed in the lavatory.
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  • Page 467 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SMOKE DETECTORS - SERVICING ESTORE THE MOKE ETECTORS Introduction Purpose TLMC Task 26-10-60-601 Reference Information REFERENCE DESIGNATION Kidde Aerospace Smoke Detector Component Maintenance Manual Assembly 473597-2 26-10-69 Procedure Remove the smoke detector(s) per Removal/Installation. Clean the smoke detector(s) per the manufacturer CMM (Kidde Aerospace 473597-2 26-10-69).
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  • Page 469 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SMOKE DETECTORS - REMOVAL/INSTALLATION EMOVAL To remove a lavatory smoke detector: Open and lock out associated circuit breaker(s) listed in DESCRIPTION/LOCATION. Remove aft lavatory headliner panel (25-49-03). Remove fasteners securing the smoke detector closeout to the headliner panel. Remove smoke detector closeout.
  • Page 470 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install a baggage compartment smoke detector: Connect wiring to smoke detector. Position smoke detector and secure with fasteners. Restore power (AMM Task 24-00-00-861-801) and check for proper operation per ADJUSTMENT/TEST. Remove all equipment used for these tasks and return aircraft to its initial condition. 26-10-01 EFFECTIVITY: TE-55965000-SMM Page 402...
  • Page 471 Test the baggage compartment smoke detector in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-291, revision (C), or the latest approved revision. Test the lavatory smoke detector, if installed, in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-292, revision (B), or the latest approved revision.
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  • Page 473 FIRE EXTINGUISHERS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FIRE EXTINGUISHERS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Five portable fire extinguishers are located in the aircraft. Table 1 lists the components and their locations. See vendor documentation and instructions on bottle for operation instructions. Component (Qty) Location Halon fire extinguisher...
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  • Page 475 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FIRE EXTINGUISHERS - SERVICING ESTORE THE ORTABLE XTINGUISHER Introduction Purpose TLMC Task 26-20-60-604 Reference Information REFERENCE DESIGNATION Flag Fire Equipment Component Maintenance Manual (3.5 lbs. HAL-035-AVH extinguisher) Kidde Aerospace 466090 Component Maintenance Manual (9 lbs. 26-21-39 extinguisher) Kidde Aerospace 892480 Component Maintenance Manual (7 lbs.
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  • Page 477 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FIRE EXTINGUISHERS - INSPECTION/CHECK UNCTIONAL EST OF THE ORTABLE XTINGUISHER Introduction Purpose TLMC Task 26-20-60-603 Reference Information REFERENCE DESIGNATION Flag Fire Equipment Component Maintenance Manual (3.5 lbs. HAL-035-AVH extinguisher) Kidde Aerospace 466090 Component Maintenance Manual (9 lbs. 26-21-39 extinguisher) Kidde Aerospace 892480...
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  • Page 479 CHAPTER 28 - FUEL List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 28 - FUEL LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 28 - Effective Pages Nov 10/2006 Nov 10/2006 28 - Contents Nov 10/2006 Nov 10/2006 28-41-00 Nov 10/2006 Nov 10/2006...
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  • Page 481 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 28 - FUEL TABLE OF CONTENTS Subject Ch-Se-Su Page FUELING PANEL 28-41-00 Description/Operation Description/Location/Operation Adjustment/Test Introduction Test Set-up Test Test Completion EFFECTIVITY: 5596-SMM Page 1 28 - Contents Revision A Nov 10/2006...
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  • Page 483 FUELING PANEL CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FUELING PANEL - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION A refuel/defuel panel has been installed in the cockpit at FS280R. Refer to the Challenger Aircraft Maintenance Manual for operation, maintenance instructions, and removal/installation instructions. For Ground Test Procedures for the fueling panel system refer to ADJUSTMENT/TEST.
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  • Page 485 Verify that all circuit breakers are in on all circuit breaker panels, except those necessary for ground safety. Test fueling panel system per Aircraft Maintenance Manual section 28-25 (Same as Wing Refuel/Defuel Panel) in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-283, revision (A), or the latest approved revision. OMPLETION Remove external power unless needed for further tests.
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  • Page 487 CHAPTER 30 - ICE AND RAIN PROTECTION List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 30 - ICE AND RAIN PROTECTION LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 30 - Effective Pages Nov 10/2006 Nov 10/2006 30 - Contents Nov 10/2006 Nov 10/2006...
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  • Page 489 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 30 - ICE AND RAIN PROTECTION TABLE OF CONTENTS Subject Ch-Se-Su Page WATER SYSTEM FREEZE PROTECTION 30-75-00 Description/Operation Description/Location Operation Removal/Installation Removal Installation EFFECTIVITY: 5596-SMM Page 1 30 - Contents Revision A Nov 10/2006...
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  • Page 491 WATER SYSTEM FREEZE PROTECTION CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WATER SYSTEM FREEZE PROTECTION - DESCRIPTION/OPERATION ESCRIPTION OCATION Ribbon heaters prevent water from freezing in the supply and drain lines. Additional system components include, a production-installed drain mast heater, water tank heaters and circuit breakers. The ribbon heaters are installed spirally around the water lines.
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  • Page 493 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WATER SYSTEM FREEZE PROTECTION - REMOVAL/INSTALLATION EMOVAL To remove a water line ribbon heater (Figure 401): Open and lock out associated circuit breaker listed in Table Remove necessary panels/cabinets so that the ribbon-heated line is accessible. Purge line of water.
  • Page 494 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Install panels/cabinets removed for access to ribbon-heated line. Remove all equipment used for these tasks and return aircraft to its initial condition. To install a water tank blanket heater (Figure 402): Position blanket heater and tighten laces. Reconnect electrical connections.
  • Page 495 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WATER TANK HEATER LACES BLANKET HEATERS WATER TANK BLANKET HEATER (TYPICAL) - REMOVAL/INSTALLATION FIGURE 402 30-75-00 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
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  • Page 497 CHAPTER 31 - INDICATING AND RECORDING SYSTEMS List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 31 - INDICATING AND RECORDING SYSTEMS LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 31 - Effective Pages Nov 10/2006 Nov 10/2006 31 - Contents Nov 10/2006 Nov 10/2006...
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  • Page 499 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 31 - INDICATING AND RECORDING SYSTEMS TABLE OF CONTENTS Subject Ch-Se-Su Page COCKPIT ANNUNCIATOR/SWITCH PANELS 31-60-10 Description/Operation Description Location Operation Adjustment/Test Introduction Test Set-up Test Test Completion EFFECTIVITY: 5596-SMM Page 1 31 - Contents Revision A Nov 10/2006...
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  • Page 501 COCKPIT ANNUNCIATOR/SWITCH PANELS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL COCKPIT ANNUNCIATOR/SWITCH PANELS - DESCRIPTION/OPERATION ESCRIPTION The production auxiliary annunciator panel has been replaced with a new panel which adds the following new switches: • CABIN TEMP - COCKPIT/CABIN • CALL RESET - CABIN/LAV •...
  • Page 502 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SMOKE CABIN CALL COCKPIT CABIN CABIN TEST TEMP RESET ENTRY LIGHTS AUXILIARY ANNUNCIATOR PANEL MISC LTS OVHD BOARD CABIN NORM ON/OFF EXTERNAL LTS BEACON LOGO WING INSP MISCELLANEOUS LIGHTS PANEL 31-60-10 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 503 External power Apply external power to the aircraft. Close all circuit breakers applicable to annunciator operation. Test auxiliary annunciator system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-238, revision (A), or the latest approved revision. OMPLETION Remove external power unless needed for further tests.
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  • Page 505 CHAPTER 33 - LIGHTING List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 33 - LIGHTING LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 33 - Effective Pages Nov 10/2006 33-24-00 Nov 10/2006 Nov 10/2006 Nov 10/2006 33 - Contents Nov 10/2006 33-24-00 Nov 10/2006...
  • Page 506 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Ch-Se-Su Page Date Ch-Se-Su Page Date 33-45-00 Nov 10/2006 Nov 10/2006 33-46-01 Nov 10/2006 Nov 10/2006 33-46-01 Nov 10/2006 Nov 10/2006 Nov 10/2006 Nov 10/2006 33-51-00 Nov 10/2006 Nov 10/2006 33-51-00 Nov 10/2006 Nov 10/2006 33-51-00 Nov 10/2006 Nov 10/2006 Nov 10/2006...
  • Page 507 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 33 - LIGHTING TABLE OF CONTENTS Subject Ch-Se-Su Page COCKPIT LIGHTING 33-05-00 Description/Operation Description/Location Operation Removal/Installation Removal Installation ENTRY LIGHTING 33-10-00 Description/Operation Description/Location Operation Removal/Installation Removal Installation INDIRECT LIGHTS 33-21-02 Description/Operation Description/Location Operation Removal/Installation Removal...
  • Page 508 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page ORDINANCE SIGNS 33-24-00 Description/Operation Description/Location Operation Removal/Installation Removal Installation Adjustment/Test Operational Test of the Ordinance Signs AFT LAVATORY LIGHTING 33-25-50 Description/Operation Description/Location Operation Removal/Installation Removal Installation GALLEY LIGHTING 33-26-00 Description/Operation Description/Location Operation Removal/Installation Removal Installation PYLON LIGHTS...
  • Page 509 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page LANDING/TAXI LIGHTS 33-41-00 Description/Operation Description/Location/Operation AIRSTAIR/BOARDING LIGHTS 33-45-00 Description/Operation Description/Location Operation Adjustment/Test Introduction Test Set-up Test Test Completion BEACON LIGHTS 33-46-01 Description/Operation Description/Location Operation Removal/Installation Removal Installation EMERGENCY LIGHTING 33-51-00 Description/Operation Description Location Operation Removal/Installation Removal...
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  • Page 511: Operation

    Two chart holders have been installed on the pilot and copilot side walls. Table 1 lists the components and their locations. Component (Qty) Location Bombardier lighted chart holders (2) Pilot and copilot side walls Rheostat controls (2) Pilot and copilot side walls CHRT HLDR circuit breaker CBP1 G-11...
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  • Page 513: Removal

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL COCKPIT LIGHTING - REMOVAL/INSTALLATION EMOVAL To remove a map light power supply (Figure 401): Open and lock out circuit breaker(s) listed in Table Remove access panel. Disconnect wiring from power supply. Remove fasteners securing power supply to bulkhead. Remove power supply.
  • Page 514 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL POWER SUPPLIES BULKHEAD FS280 COCKPIT MAP LIGHTS - REMOVAL/INSTALLATION FIGURE 401 33-05-00 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 515 ENTRY LIGHTING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY LIGHTING - DESCRIPTION/OPERATION ESCRIPTION OCATION Entry Headliner Lights Two dome-light assemblies have been installed to provide general lighting for the entry area. An Entry Lights ON/OFF switch has been added to provide additional control of the entry lights from the cockpit.
  • Page 516 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Forward Wardrobe Light A dome-light assembly containing has been installed to provide light in the forward wardrobe. Table 3 lists the components and their locations. Component Location Incandescent lamp In forward wardrobe at top of main storage compartment WARD ROBE LIGHT switch Forward Wardrobe Switch Panel ENTRY AREA circuit breaker...
  • Page 517 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WARD AIRSTAIR DOME ROBE LIGHT LIGHT LIGHT FORWARD WARDROBE SWITCH PANEL JUMPSEAT LIGHT JUMPSEAT LIGHT SWITCH 33-10-00 EFFECTIVITY: TE-55965000-SMM Page 3 Revision A Nov 10/2006...
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  • Page 519 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTRY LIGHTING - REMOVAL/INSTALLATION EMOVAL NOTE: See 20-12-00 for lamp replacement instructions. To remove jumpseat light bright/dim controller WCU4: Open and lock out circuit breaker(s) listed in Table Remove forward wardrobe outboard closeouts. Disconnect wiring from controller. Remove fasteners securing controller to wardrobe.
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  • Page 521: Operation

    INDIRECT LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL INDIRECT LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION Fluorescent upwash and downwash lighting is installed in the headliner and the Passenger Service Units (PSU) to provide indirect cabin lighting. Control of the components listed in Table 1 is managed by the cabin management system Cabin Control Module 1 (CCM 1) (23-90-00).
  • Page 522 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR UPWASH LIGHTS LIGHTS LIGHTS LIGHTS CABIN CABIN COFFEE FLOOR FLOOR DNWASH ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER PURGE DISP HEATER HEATER FULL GALLEY SWITCH PANEL CONTROL MODE CALL ADJUST...
  • Page 523 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UPWASH LIGHTS 560.31 355.45 DOWNWASH LIGHTS INDIRECT LIGHTING 33-21-02 EFFECTIVITY: TE-55965000-SMM Page 3 Revision A Nov 10/2006...
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  • Page 525: Removal

    CL-604 SUPPLEMENTAL MAINTENANCE MANUAL INDIRECT LIGHTS - REMOVAL/INSTALLATION EMOVAL NOTE: See 20-12-00 for lamp replacement instructions. To remove a power supply: Open and lock out circuit breaker(s) listed in Table Remove PSU covers in power supply area (25-26-20). Disconnect wiring from power supply. Remove fasteners securing power supply.
  • Page 526 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install a dimming module (Figure 401): Position module and secure with fasteners. Restore electrical connections. Perform test in accordance with ADJUSTMENT/TEST. Install drawers. Remove all equipment used for these tasks and return aircraft to its initial condition. UPPER EQUIPMENT TRAY G ALLEY...
  • Page 527 Table 1, and all cabin management circuit breakers are closed. Test the indirect lights in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-251, revision (F), or the latest approved revision. OMPLETION Remove power from aircraft if it is no longer required.
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  • Page 529: Entertainment Equipment Lighting

    ENTERTAINMENT EQUIPMENT LIGHTING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ENTERTAINMENT EQUIPMENT LIGHTING - DESCRIPTION/OPERATION ESCRIPTION OCATION A lighting strip has been installed in the aft divan end cabinet to provide light for the entertainment equipment controls. Table 1 lists the components and their locations. Component (Qty) Location Door switch...
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  • Page 531: Operation

    FLOOR ACCENT LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FLOOR ACCENT LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION NOTE: See 20-12-00 for light strip replacement instructions. Lighting strips have been installed to provide floor accent lighting in the main cabin, entry area, and aft lavatory.
  • Page 532 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR UPWASH LIGHTS LIGHTS LIGHTS LIGHTS CABIN CABIN COFFEE FLOOR FLOOR DNWASH ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER PURGE DISP HEATER HEATER FULL GALLEY SWITCH PANEL CONTROL MODE CALL ADJUST...
  • Page 533 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL FLOOR LIGHTS FLOOR LIGHTS FLOOR LIGHTS FLOOR ACCENT LIGHTS FLOORPLAN LAYOUT 33-22-01 EFFECTIVITY: TE-55965000-SMM Page 3 Revision A Nov 10/2006...
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  • Page 535: Reading/Table Lights

    READING/TABLE LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL READING/TABLE LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION NOTE: See 20-12-00 for lamp replacement instructions. Reading and table lights have been installed in the Passenger Service Units (PSU) to provide individual lighting for the passengers. Switch panels in the sideledges, on the aft divan end cabinet, and in the inboard conference seat armrests control the lights.
  • Page 536 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-22-20 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 537 ORDINANCE SIGNS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ORDINANCE SIGNS - DESCRIPTION/OPERATION ESCRIPTION OCATION Ordinance signs have been added in the cabin to display instructions to the passengers. These graphic ordinance signs are interfaced to the production-installed ordinance sign system, and the cabin paging and public address systems (23-31-00).
  • Page 538 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-24-00 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 539 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ORDINANCE SIGNS - REMOVAL/INSTALLATION EMOVAL NOTE: See 20-12-00 for lamp replacement instructions. To remove a cabin or lavatory ordinance sign: Open and lock out circuit breaker(s) listed in Table Grasp ordinance sign with fingers and pull out far enough to reach wiring. Disconnect electrical connection.
  • Page 540 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-24-00 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 541 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ORDINANCE SIGNS - ADJUSTMENT/TEST PERATIONAL EST OF THE RDINANCE IGNS Introduction Purpose TLMC Task 33-24-60-601 Test Set-up Obey all the electrical/electronic safety precautions (AMM Task 24-00-00-910-801). Connect electrical power to the aircraft (AMM Task 24-00-00-861-801). Make sure the circuit breakers that follow are closed: LOCATION CB NO.
  • Page 542 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL In the flight compartment, set the PASS SIGNS/EMER LIGHTS control panel NO SMKG switch to OFF. In the flight compartment, set the PASS SIGNS/EMER LIGHTS control panel SEAT BLTS switch to OFF. Make sure the following ordinance signs are off: •...
  • Page 543 AFT LAVATORY LIGHTING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY LIGHTING - DESCRIPTION/OPERATION ESCRIPTION OCATION Mirror Lights Lighting has been installed to provide light for the lavatory mirror. Table 1 lists the components and their locations. Control of the components listed in Table 1 is managed by the cabin management system Cabin Control Module 2 (CCM 2) (23-90-00).
  • Page 544 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Headliner Dome Light Press the LAV DOME LIGHT switch to energize a relay in the switch panel, sending power to the center lamp. Pressing the LAV DOME LIGHT switch also energizes relay K1LY, sending power to the left- and right-hand lamps.
  • Page 545 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT LAVATORY LIGHTING - REMOVAL/INSTALLATION EMOVAL NOTE: See 20-12-00 for lamp replacement instructions. To remove the mirror lighting power supply: Open and lock out circuit breaker(s) listed in Table Remove mirror cabinet assembly (25-49-00). Disconnect wiring from power supply. Remove fasteners securing power supply.
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  • Page 547 GALLEY LIGHTING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY LIGHTING - DESCRIPTION/OPERATION ESCRIPTION OCATION Work Lights Lighting has been installed to provide light for the galley countertop area, and is managed by the cabin management system Cabin Control Module 1 (CCM 1) (23-90-00). Table 1 lists the components and their locations.
  • Page 548 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PERATION Work Lights Press the GALLEY WORK LIGHTS switch to send a signal via the cabin data bus to CCM 1, which sends power to the lamps, turning them on at high intensity. Press the switch a second time to energize relay K200LR, switching in a resistor on the dim sense line of the dimming unit, changing the intensity of the lamps to low intensity.
  • Page 549 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY LIGHTING - REMOVAL/INSTALLATION EMOVAL To remove a work lighting power supply (Figure 401): Open and lock out circuit breaker(s) listed in Table Remove galley appliance(s) inboard of upper equipment tray. Disconnect wiring from power supply. Remove fasteners securing power supply to equipment tray.
  • Page 550 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION To install a work lighting power supply (Figure 401): Restore electrical connections to power supply. Position power supply on upper equipment tray and secure with fasteners. Install galley appliance(s). Restore power (AMM Task 24-00-00-861-801) and verify proper operation of galley work lights.
  • Page 551 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UPPER EQUIPMENT TRAY GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR LIGHTS LIGHTS LIGHTS LIGHTS COFFEE FLOOR CABIN FLOOR CABIN ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER W ATER PURGE DISP HEATER HEATER FULL RESET TEST MICROWAVE 115 VAC 60 Hz...
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  • Page 553 PYLON LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PYLON LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION Microswitches have been installed to turn on the pylon lights when a No. 3 hydraulic pump service door is opened. A rocker switch has been installed to provide operation of the left-hand pylon light from the baggage compartment area.
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  • Page 555 BAGGAGE COMPARTMENT LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BAGGAGE COMPARTMENT LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION NOTE: See 20-12-00 for headliner lamp replacement instructions. Overhead dome-light assemblies have been installed to provide general lighting for the baggage compartment area. Each dome-light assembly contains two lamps. Flush-mounted light assemblies have been installed in the baggage compartment door header to provide additional lighting in the door area.
  • Page 556 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DOME LIGHT MIRROR LIGHTS FLOOR LIGHTS BAGGAGE LIGHTS LAVATORY SWITCH PANEL 33-33-00 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 557 EXTERIOR COMPARTMENT LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EXTERIOR COMPARTMENT LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION Two post lights have been installed to provide light for the exterior refuel/defuel control panel. A floodlight has also been installed to provide light for the fuel port compartment. The production microswitches and circuit breaker have been retained.
  • Page 558 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-37-01 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 559 AVIONICS COMPARTMENT LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AVIONICS COMPARTMENT LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION An additional service light has been installed to supplement the existing main avionics compartment lighting system. This new service light is operated by the existing service light switch, which has been relocated.
  • Page 560 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-37-03 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 561 AFT EQUIPMENT COMPARTMENT DOOR SWITCH CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AFT EQUIPMENT COMPARTMENT DOOR SWITCH - DESCRIPTION/OPERATION ESCRIPTION OCATION A microswitch and additional service light have been installed to supplement the aft equipment compartment lighting system. The microswitch allows the service lights to be turned on only when the access door is open.
  • Page 562 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-37-07 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 563 LANDING/TAXI LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LANDING/TAXI LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION The production-installed left and right landing light switches on the Landing Lights Panel in the cockpit have been removed and replaced to allow the lights to operate in a pulse mode. The new light switches have a center PLS position.
  • Page 564 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-41-00 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 565 AIRSTAIR/BOARDING LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIRSTAIR/BOARDING LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION NOTE: See 20-12-00 for lamp replacement instructions. The production-installed airstair/boarding light system has been supplemented by the addition of boarding lights for the main cabin and switches to control the lighting system. Table 1 lists the components and their locations.
  • Page 566 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL MISC LTS OVHD BOARD CABIN NORM ON/OFF EXTERNAL LTS LOGO BEACON WING INSP MISCELLANEOUS LIGHTS PANEL AIRSTAIR STEP NUMBER 5 STAIR LIGHTS SWITCH STAIR LIGHTS SWITCH 33-45-00 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 567 Apply external power to the aircraft. Verify that boarding lights and cabin management circuit breakers are closed. Test the airstair/boarding lights system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-251, revision (F), or the latest approved revision.
  • Page 568 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-45-00 EFFECTIVITY: TE-55965000-SMM Page 502 Revision A Nov 10/2006...
  • Page 569 BEACON LIGHTS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BEACON LIGHTS - DESCRIPTION/OPERATION ESCRIPTION OCATION A strobe-type beacon system utilizing red lenses has been installed. Table 1 lists the components and their locations. Component (Qty) Location BEACON OFF/ON switch Miscellaneous Lights Panel on cockpit overhead panel Lower beacon light assembly FS567 Power supply PS1LS...
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  • Page 571 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL BEACON LIGHTS - REMOVAL/INSTALLATION EMOVAL To remove the upper beacon light assembly: Open and lock out circuit breaker(s) listed in Table Remove fasteners securing lens and remove lens. Carefully remove sealant from around light assembly base. Remove fasteners securing beacon assembly.
  • Page 572 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL NSTALLATION To install the upper beacon light assembly: NOTE: Do not touch lamp directly with fingers. If touched with bare fingers, wipe finger oil off of lamp with a soft cloth and alcohol. Finger oil will cause momentary smoking and premature lamp failure when lamp is energized.
  • Page 573 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL To install the power supply (Figure 401): Position power supply and secure with fasteners. Restore electrical connections. Replace appropriate floorboard. Replace carpet and Protex-5 floor covering (25-29-00). Remove all equipment used for these tasks and return aircraft to its initial condition. Restore power and verify lights turns on when BEACON OFF/ON switch is toggled to ON.
  • Page 574 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 33-46-01 EFFECTIVITY: TE-55965000-SMM Page 404 Revision A Nov 10/2006...
  • Page 575 EMERGENCY LIGHTING CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EMERGENCY LIGHTING - DESCRIPTION/OPERATION ESCRIPTION NOTE: Refer to STC No. SA6011NM for the Emergency Escape Path Lighting System. The emergency light system consists of the production-installed emergency light system and the added components listed in Table The EICAS has an EMER LTS OFF caution indication when the emergency lights switch on the cockpit overhead panel is selected to OFF.
  • Page 576 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL When power is applied to the aircraft and the EMER LTS switch is set to ARM, the emergency lights do not operate, but the power supplies charge and are armed. If power is removed from the ESS DC or ESS AC bus, the emergency lights come on automatically and get their power from the power supplies.
  • Page 577 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EMERGENCY LIGHTING - REMOVAL/INSTALLATION EMOVAL To remove a cabin emergency lighting power supply (Figure 401): Open and lock out production-installed circuit breaker(s). Remove appropriate floorboard or dado panel. Disconnect wiring from power supply. Remove fasteners securing power supply. Remove power supply.
  • Page 578 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EMERGENCY LIGHTS (TYPICAL) POWER POWER SUPPLY NO. 1 SUPPLY NO. 2 EMERGENCY LIGHTING - REMOVAL/INSTALLATION FIGURE 401 33-51-00 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 579 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EMERGENCY LIGHTING - ADJUSTMENT/TEST PERATIONAL EST OF THE NTERIOR MERGENCY IGHTS Introduction Purpose TLMC Task 33-51-60-601 Test Set-up Obey all the electrical/electronic safety precautions (AMM Task 24-00-00-910-801). Ensure that on the PASS SIGNS/EMER LIGHTS control panel, the EMER LTS switch is set to OFF.
  • Page 580 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL In the flight compartment, on the PASS SIGNS/EMER LIGHTS control panel, set the EMER LTS switch to OFF. Make sure the emergency lights go off. In the flight compartment, on the EICAS primary page, make sure the EMER LIGHTS OFF caution message comes on.
  • Page 581 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PERATIONAL EST OF THE NTERIOR MERGENCY IGHTS ATTERY ACKS Introduction Purpose TLMC Task 33-51-60-602 Equipment and Materials REFERENCE DESIGNATION Commercially Available Digital Voltmeter Commercially Available Battery charger, adjustable constant current, 28VDC 2 amps minimum Commercially Available Three resistors, 25-ohm 50 Watt, Dale RH-50 25 (Newark P/N 01F9923) Commercially Available...
  • Page 582 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Remove charger 28VDC from unit connector pins A and E. Voltmeter should indicate greater than 24VDC. Remove charger 28VDC from unit connector pin C. Charger should now not be connected to unit. After one hour, voltmeter should indicate greater than 18.5VDC. This indicates batteries meet minimum capacity specifications.
  • Page 583 CHAPTER 34 - NAVIGATION CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 34 - NAVIGATION THIS SECTION INTENTIONALLY LEFT BLANK 5596-SMM Page 1 EFFECTIVITY: Revision A Nov 10/2006...
  • Page 584 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK EFFECTIVITY: 5596-SMM Page 2 Revision A Nov 10/2006...
  • Page 585 CHAPTER 35 - OXYGEN List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 35 - OXYGEN LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 35 - Effective Pages Nov 10/2006 35-20-02 Nov 10/2006 Nov 10/2006 Nov 10/2006 35 - Contents Nov 10/2006 35-30-00 Nov 10/2006...
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  • Page 587 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 35 - OXYGEN TABLE OF CONTENTS Subject Ch-Se-Su Page OXYGEN SYSTEM 35-00-00 Description/Operation Description/Location THIRD CREW MEMBER OXYGEN SYSTEM 35-10-05 Description/Operation Description/Location Operation Maintenance Practices Restore the Crew Oxygen Mask Modifications Servicing Introduction Job Set-up Procedure...
  • Page 588 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page PORTABLE OXYGEN BOTTLE 35-30-00 Description/Operation Description/Location/Operation Maintenance Practices Introduction Job Set-up Procedure Job Completion Adjustment/Test Restore the Portable Oxygen Bottle and Regulator Inspection/Check General Visual Inspection of the Portable Oxygen Bottle Mask EFFECTIVITY: 5596-SMM Page 2 35 - Contents Revision A...
  • Page 589 OXYGEN SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL OXYGEN SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION The aircraft is equipped with a gaseous emergency oxygen system consisting of supply and delivery for the crew and passengers, a therapeutic oxygen outlet, and a separate portable oxygen bottle. The system is supplied by two pressurized 115-cu.-ft.
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  • Page 591 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL 202.75 OVERBOARD OVERBOARD ACCESS DOOR, LOW PRESSURE HIGH PRESSURE FILLER VALVE AND TO P.A. & CHIME CIRCUIT AS WELL PRESSURE DISCHARGE DISCHARGE QUANTITY GAUGE AS CABIN STANDBY LIGHT CIRCUIT 280.00 621.00 BULKHEAD INDICATOR AND ORDINANCE SIGN CIRCUIT INDICATOR LOW SUPPLY PRESSURE BULKHEAD...
  • Page 592 THIRD CREW MEMBER OXYGEN SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIRD CREW MEMBER OXYGEN SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION An EROS MF10-03-03 full-face oxygen mask and stowage box have been installed in the forward wardrobe for the jumpseat occupant. The unit includes an attached regulator that provides NORMAL, 100%, and EMERGENCY operating positions, and an inflatable harness to facilitate quick donning.
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  • Page 594 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIRD CREW MEMBER OXYGEN SYSTEM - MAINTENANCE PRACTICES ESTORE THE XYGEN ODIFICATIONS Introduction Purpose TLMC Task 35-10-60-602 Reference Information REFERENCE DESIGNATION EROS/Zodiac Operating and Maintenance Instructions 4NUT0046A/35-13-61 for Quick Donning Mask-Regulator MF10 Series/Component Maintenance Manual With Illustrated Parts List Job Set-up Obtain the crew oxygen masks from the aircraft.
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  • Page 596 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIRD CREW MEMBER OXYGEN SYSTEM - SERVICING NTRODUCTION Purpose • The following procedure is used to clean and sanitize the face piece. Equipment and Facilities Required Equipment • EROS SAN 50 disinfectant swabs Facilities • None Remove mask from stowage box.
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  • Page 598 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THIRD CREW MEMBER OXYGEN SYSTEM - ADJUSTMENT/TEST PERATIONAL EST OF THE XYGEN ODIFICATIONS Introduction Purpose TLMC Task 35-10-60-601 Test Set-up CAUTION: MAKE SURE THAT THE PRESSURE OF THE OXYGEN CYLINDER IS NOT LESS THAN 50 PSI (340 KPA). IF THE PRESSURE IS LESS THAN 50 PSI (340 KPA), CONTAMINATION CAN GO INTO THE OXYGEN CYLINDER.
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  • Page 600 PASSENGER OXYGEN SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER OXYGEN SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION The passenger emergency oxygen system provides emergency oxygen to the passengers, crew members, jumpseat occupant, and lavatory. The passenger oxygen is supplied by two pressurized, 115-cu.-ft.
  • Page 601 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Passenger Oxygen Deployment One headliner-mounted, one side panel-mounted, and nine Passenger Service Unit-mounted (PSU) deployment containers have been installed in the aircraft as shown in the Passenger Oxygen System Distribution graphic. All of the deployment containers are dual-mask assemblies. The masks, when deployed, are presented in proximity to all cabin seat positions, the jumpseat, and the lavatory.
  • Page 602 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL LANYARD CORD AND RING PASSENGER MASK DOOR ACTIVATOR OXYGEN SHUT-OFF VALVE LANYARD CORD TO OPPOSITE SIDE AND RING MANIFOLD OXYGEN SUPPLY LANYARD TO MASK OXYGEN LINE CONNECTION INSTRUCTION LABEL DEPLOYMENT PASSENGER OXYGEN DEPLOYMENT BOX (TYPICAL) (LANYARD AND PIN ARE NOT INSTALLED IN LAVATORY DEPLOYMENT BOX) 35-20-00 EFFECTIVITY: TE-55965000-SMM Page 3...
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  • Page 604 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER OXYGEN SYSTEM - SERVICING ESTORE THE ASSENGER XYGEN ONTROL ANEL Introduction Purpose TLMC Task 35-20-60-603 Procedure Remove the passenger oxygen control panel. Send the passenger oxygen control panel to the manufacturer for restoration. Install the passenger oxygen control panel. Verify proper operation per Adjustment/Test.
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  • Page 606 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER OXYGEN SYSTEM - REMOVAL/INSTALLATION EMOVAL CAUTION: TO PREVENT CONTAMINATION, INSTALL PROTECTIVE COVERS ON ALL LINES, OPEN PORTS, ELECTRICAL PLUGS, AND RECEPTACLES IMMEDIATELY AFTER DISCONNECTING. DO NOT REMOVE PROTECTIVE COVERS UNTIL IMMEDIATELY BEFORE CONNECTING. OBSERVE INSTALLATION AND TORQUING PROCEDURES FOR OXYGEN FITTINGS AND LINES IN CHAPTER 20 OF THE CANADAIR AIRCRAFT MAINTENANCE MANUAL FOR INSTALLATIONS AND REMOVALS IN THIS SECTION.
  • Page 607 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Coil oxygen tubing under mask. (10) Connect oxygen tubing to supply line at lanyard valve. WARNING: MAKE SURE LANYARD PIN IS INSERTED INTO CORRECT LANYARD PIN RECEPTACLE. CROSS-CONNECTED PINS WILL RESULT IN PASSENGERS PULLING LANYARD CORDS ONLY TO INITIATE OXYGEN FLOW TO ANOTHER MASK.
  • Page 608 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PASSENGER OXYGEN SYSTEM - ADJUSTMENT/TEST PERATIONAL EST OF THE ASSENGER XYGEN YSTEM Introduction Purpose TLMC Task 35-20-60-601 Test Set-up CAUTION: MAKE SURE THAT THE PRESSURE OF THE OXYGEN CYLINDER IS NOT LESS THAN 50 PSI (340 KPA). IF THE PRESSURE IS LESS THAN 50 PSI (340 KPA), CONTAMINATION CAN GO INTO THE OXYGEN CYLINDER.
  • Page 609 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Select the THERAPEUTIC OXYGEN annunciator/switch on the PASSENGER OXYGEN control panel, to ON position. Make sure oxygen flows to therapeutic oxygen mask. Make sure the THERAPEUTIC OXYGEN annunciator/switch illuminates. Make sure the therapeutic oxygen mask functions properly (35-20-02). Deselect the THERAPEUTIC OXYGEN annunciator/switch.
  • Page 610 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UNCTIONAL EST OF THE ASSENGER XYGEN YSTEM Introduction Purpose TLMC Task 35-20-60-602 Tools and Equipment REFERENCE DESIGNATION Commercially available Electrical outlet tester GSE 35-20-02 Pressure-Tester, Passenger Oxygen Station GSE 34-10-01 Air Data Test Set Test Set-up CAUTION: MAKE SURE THAT THE PRESSURE OF THE OXYGEN CYLINDER IS NOT LESS THAN 50 PSI (340 KPA).
  • Page 611 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Remove the cap from the valve test receptacle on the PASSENGER OXYGEN control panel. Connect the air data test set to the test port on the PASSENGER OXYGEN control panel. (10) Connect the passenger-oxygen-station pressure-tester to the end of the passenger-oxygen supply line at the rear of the passenger compartment.
  • Page 612 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Initiate oxygen flow at all passenger oxygen masks by pulling down on the lanyards until the corresponding pins are released from the lanyard valves. Make sure that you get a free flow of oxygen from each mask. Make sure the passenger-oxygen-station pressure-tester decreases to 22 psig, +4/-0 psig.
  • Page 613 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Test Completion Disconnect the test equipment. Make sure that all oxygen line connections are put back to their initial positions. Put the cap on the valve test receptacle on the PASSENGER OXYGEN control panel. Insert the lanyard pins into the corresponding lanyard valves at all passenger oxygen masks.
  • Page 614 THERAPEUTIC OXYGEN SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THERAPEUTIC OXYGEN SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION One therapeutic oxygen outlet is located on the right-hand dado panel forward of the overwing emergency exit by right-hand seat 2. Two 12-foot oxygen hoses and masks (provided as loose equipment) are stowed in their respective pouches in the aft divan end cabinet.
  • Page 615 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL OXYGEN MASK ECONOMIZER BAG QUICK-DISCONNECT VALVE NEBULIZER HOSE BAYONET PLUG REGULATOR CONTROL KNOB ADAPTER NEBULIZER REGULATOR NEBULIZER ASSEMBLY THERAPEUTIC MASK AND NEBULIZER (LOOSE EQUIPMENT) 35-20-02 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A Nov 10/2006...
  • Page 616 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL THERAPEUTIC OXYGEN SYSTEM - SERVICING NTRODUCTION Purpose The following procedure gives instructions for servicing the therapeutic oxygen mask and nebulizer kit. Equipment and Facilities Required Equipment • Zephiran Chloride solution, Scott Aviation P/N 00-2572 Facilities • None Obey all the oxygen safety precautions (AMM Task 35-00-00-910-801).
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  • Page 618 Verify that all equipment necessary for test is installed in aircraft before proceeding. Test the therapeutic oxygen system in accordance with Bombardier Completion Center Ground Test Procedure, document number D-GT35205000, revision (A), or the latest approved revision. OMPLETION Remove power from aircraft if it is no longer required.
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  • Page 620 PORTABLE OXYGEN BOTTLE CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PORTABLE OXYGEN BOTTLE - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION An 11-cu.-ft. portable oxygen bottle is located in the forward wardrobe. It is equipped with two outlets, one for an Eros mask and one for the wide-screen mask that is provided. The wide-screen mask is a full-face oxygen mask, providing 100% forward visibility and full 180°...
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  • Page 622 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PORTABLE OXYGEN BOTTLE - MAINTENANCE PRACTICES NTRODUCTION Purpose The following procedure gives instructions for maintaining the portable oxygen bottle. Equipment and Facilities Required Equipment • None Facilities • None No special set-up is required. ROCEDURE Check pressure gauge for sufficient pressure prior to each flight. Check bottle weekly for leakage, corrosion, gouges, distortion, and integrity of mounting hardware.
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  • Page 624 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PORTABLE OXYGEN BOTTLE - ADJUSTMENT/TEST ESTORE THE ORTABLE XYGEN OTTLE AND EGULATOR Introduction Purpose TLMC Task 35-30-60-601 Reference Information REFERENCE DESIGNATION Scott Aviation 35-32-18 5500 Series and 5600 Series Portable Cylinder Assembly Component Maintenance Manual Test Set-up Obtain the portable oxygen bottle from the forward wardrobe.
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  • Page 626 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PORTABLE OXYGEN BOTTLE - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE ORTABLE XYGEN OTTLE Introduction Purpose TLMC Task 35-30-60-602 Job Set-up Obtain the portable oxygen bottle mask from the forward wardrobe. Procedure Perform a general visual inspection of the oxygen mask (used with the portable oxygen bottle) as follows: Check the oxygen mask and straps for evidence of damage or deterioration (stretch all rubber parts and pay particular attention to seams when inspecting for damage or...
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  • Page 628 CHAPTER WATER/ WASTE List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 38 - WATER/WASTE LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 38 - Effective Pages Nov 10/2006 38-30-00 Nov 10/2006 Nov 10/2006 Nov 10/2006 38 - Contents Nov 10/2006 38-31-00 Nov 10/2006...
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  • Page 630 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 38 - WATER/WASTE TABLE OF CONTENTS Subject Ch-Se-Su Page POTABLE WATER SYSTEM 38-10-00 Description/Operation Description Location Operation Maintenance Practices Restore the Potable Water Filter Cartridge Restore the Potable Water System Servicing Introduction Job Set-up Procedure Job Completion...
  • Page 631 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Subject Ch-Se-Su Page TOILETS 38-31-00 Description/Operation Description/Location Operation Servicing Introduction Job Set-up Procedure Job Completion Removal/Installation Removal Installation Adjustment/Test Introduction Test Set-up Test Test Completion Inspection/Check Introduction Job Set-up Procedure Job Completion AIR SUPPLY 38-40-00 Description/Operation Description/Location Operation Servicing...
  • Page 632 POTABLE WATER SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL POTABLE WATER SYSTEM - DESCRIPTION/OPERATION ESCRIPTION The aircraft is equipped with a pressurized potable water system. For water to flow, the system must be pressurized (38-40-00). Water Tank The water tank is a pressurized water tank with a capacity of 10 US gallons (38 liters). Water Level Indication Water level is sensed by a water quantity probe in the water tank interfaced to a control unit.
  • Page 633 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL The automatic water purge system consists of a two-way solenoid purge valve and a purge activation switch on the galley switch panel. The system is interfaced to empty tank sensor MT700MJ, relay K702MJ, and the cabin management system to turn off the water heaters and the hot water dispenser heater (if installed), and to end the purge cycle when empty.
  • Page 634 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Component (Qty) Location Associated Circuit Breaker Water fill overflow valve Water system components tray below CBP5 A-8, WATER SYSTEM V702MJ water tank Water fill relays K703MJ, Water system components tray above CBP5 A-8, WATER SYSTEM K704MJ, and K705MW water tank Water fill valve V703MJ Water system components tray below...
  • Page 635 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL to relay K705MW to de-energize the water fill valve. Water is then routed to the drain mast through the overflow valve. When water flows out the drain mast, select the water fill switch to OFF. Time-delay relay K703MJ will then close the overflow valve after the preset time delay. The water level indicators in the water fill service panel and Galley Switch Panel should show FULL.
  • Page 636 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL PLUNGER INSTANT HOT WATER AIR PRESSURE REGULATOR GALLEY PLUMBING AND PRESSURE GAUGE (20-22 PSI) SINK STRAINER RELIEF VALVE AIR PRESSURE, VENT/MUFFLER DRAIN VALVE 3-WAY MANUAL 10th STAGE CHECK VALVE BLEED AIR VALVE DRAWER DRAWER MECHANICAL PLUNGER RELIEF VALVE AIR FILTER OVERFLOW, 2-WAY...
  • Page 637 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL POTABLE WATER SYSTEM - MAINTENANCE PRACTICES ESTORE THE OTABLE ATER ILTER ARTRIDGE Introduction Purpose TLMC Task 38-10-60-601 Procedure Replace the potable water filter cartridge per SERVICING. Job Completion Remove all tools, equipment, and unwanted materials from the work area. 38-10-00 TE-55965000-SMM Page 201...
  • Page 638 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ESTORE THE OTABLE ATER YSTEM Introduction Purpose TLMC Task 38-10-60-602 Procedure Restore (sanitize) the potable water system per SERVICING. Job Completion Remove all tools, equipment, and unwanted materials from the work area. 38-10-00 EFFECTIVITY: TE-55965000-SMM Page 202 Revision A Nov 10/2006...
  • Page 639 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL POTABLE WATER SYSTEM - SERVICING NTRODUCTION Purpose The following procedure provides instructions for servicing components of the potable water system. Equipment and Facilities Required Equipment • Equipment and supplies specific to task Facilities • External power Apply electrical power to galley CB panel.
  • Page 640 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL Automatic Purge Procedure (Figure 301) WARNING: USE EXTREME CARE IN THE USE OF HIGH-PRESSURE NITROGEN. DO NOT OVER-PRESSURIZE SYSTEM. NOTE: Instructions for purging water system are also indicated on water system purging placard. In the case of a discrepancy between placard and these instructions, follow placard instructions.
  • Page 641 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR UPWASH LIGHTS LIGHTS LIGHTS LIGHTS CABIN CABIN COFFEE FLOOR FLOOR DNWASH ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER PURGE DISP HEATER HEATER FULL GALLEY SWITCH PANEL FIGURE 301 Manual Purge Procedure (Figure 302)
  • Page 642 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL (10) Repeat steps 3.C.(8) and 3.C.(9) for lavatory valves. NOTE: If vanity and/or galley faucet control switches are installed in the aircraft, verify pressure switch activation. (11) Shut off bleed air or nitrogen supply. (12) Close manual purge valve. (13) Remove all equipment used for these tasks and return aircraft to its initial condition.
  • Page 643 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL Close galley and lavatory faucets. Remove baggage compartment shelves and water tank closeouts. WARNING: USE EXTREME CARE IN THE USE OF HIGH-PRESSURE NITROGEN. DO NOT OVER-PRESSURIZE SYSTEM. Pressurize system with aircraft bleed air or nitrogen (38-40-00). Do not use shop air. Actuate air pressure manual three-way valve to LINE PURGE position.
  • Page 644 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL Refill water system in accordance with 3.A. above. With galley and lavatory faucets closed and electrical power available, pressurize system with aircraft bleed air or nitrogen (38-40-00). Do not use shop air. (10) Check for leaks. Correct as necessary. (11) Turn on galley and lavatory faucets and allow water to run for a minimum of 3 minutes.
  • Page 645 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL Sterilizing Main Water Tank and Lines NOTE: The water tank should be sterilized every 6 months. The water filter cartridge should be removed before sterilizing the system. To avoid the possibility of damage to tank and water lines, the following procedure should be used to sterilize the water system.
  • Page 646 BD-100 SUPPLEMENTAL MAINTENANCE MANUAL (18) Fill water filter canister with potable water. (19) Replace water filter cover and nut handle. (20) Fill water system with clean potable water in accordance with 3.A. above. (21) Flow water through lavatory and galley hot and cold faucets until it runs clear. (22) Momentarily press bleed air filter drain valve (Figure 302) to remove any water or...
  • Page 647 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL POTABLE WATER SYSTEM - REMOVAL/INSTALLATION EMOVAL To remove the potable water tank (Figure 401): Remove baggage compartment right-hand headliner (25-55-03). Remove baggage compartment shelf and water tank closeouts. Purge water in accordance with SERVICING (Procedure 3.B. or 3.C.). Ensure that aircraft power is off.
  • Page 648 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WATER TANK ATTACH POINTS POTABLE WATER SYSTEM - REMOVAL/INSTALLATION FIGURE 401 38-10-00 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 649 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Test the potable water system in accordance with Bombardier Completion Center Water System Ground Test Procedure, document number TE-GTP-243, revision (G), or the latest approved revision.
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  • Page 651 WATER HEATERS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WATER HEATERS - DESCRIPTION/OPERATION ESCRIPTION OCATION Two water heaters supply hot potable water to the galley and lavatory. The galley hot water dispenser is discussed in 25-35-05. Table 1 lists the water heater components, their locations, and if applicable, the associated circuit breaker(s).
  • Page 652 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR UPWASH LIGHTS LIGHTS LIGHTS LIGHTS CABIN CABIN COFFEE FLOOR FLOOR DNWASH ON/OFF LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER PURGE DISP HEATER HEATER FULL GALLEY SWITCH PANEL 38-10-40 EFFECTIVITY: TE-55965000-SMM Page 2 Revision A...
  • Page 653 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WATER HEATERS - REMOVAL/INSTALLATION EMOVAL To remove the galley water heater (Figure 401): WARNING: USE EXTREME CARE WHEN WORKING WITH THE INSTANT HOT WATER DISPENSER (WATER HEATED TO 180º F) AND THE GALLEY WATER HEATER (WATER HEATED TO 125º F). Open and lock out associated circuit breakers in Table Run water from hot water tap until cool.
  • Page 654 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL (10) Remove water heater mounting straps. (11) Remove water heater. To remove relay K901HR or K902HR (Figure 402): Open and lock out associated circuit breakers in Table Remove applicable drawers and contents from lower galley. Remove relay. NSTALLATION To install the galley water heater (Figure...
  • Page 655 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL ON LIGHT ON/OFF TOGGLE SWITCH WATER OUT MOUNTING FASTENING BRACKETS STRAPS CONNECTOR PRESSURE RELIEF VALVE 3-POSITION TOGGLE SWITCH (BEHIND) WATER IN WATER HEATERS - REMOVAL/INSTALLATION FIGURE 401 38-10-40 EFFECTIVITY: TE-55965000-SMM Page 403 Revision A Nov 10/2006...
  • Page 656 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL UPPER EQUIPMENT TRAY GALLEY GALLEY GALLEY CABIN WORK EFFECT FLOOR LIGHTS LIGHTS LIGHTS LIGHTS COFFEE CABIN CABIN ON/OFF FLOOR FLOOR LIGHTS LIGHTS LIGHTS GALLEY WATER WATER WATER WATER PURGE DISP HEATER HEATER FULL RESET TEST MICROWAVE 115 VAC 60 Hz COFFEE POT...
  • Page 657 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WATER HEATERS - ADJUSTMENT/TEST UNCTIONAL EST OF THE ATER EATER RESSURE ELIEF ALVE Introduction Purpose TLMC Task 38-10-60-603 Reference Information REFERENCE DESIGNATION BF Goodrich 38-10-01 Component Maintenance Manual Job Set-up Remove the water heaters per Removal/Installation. Procedure Do the pressure relief valve test of the water heaters per manufacturers CMM (BF Goodrich 38-10-01).
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  • Page 659 WASTE DISPOSAL CL-604 SUPPLEMENTAL MAINTENANCE MANUAL WASTE DISPOSAL - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Waste water from the lavatory sink, galley sink, and ice drawers is discharged overboard through the production drain mast. The drain lines and drain mast are electrically heated by 115VAC heaters to prevent freezing (30-75-00).
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  • Page 661 No special set-up is required. WARNING: USE EXTREME CARE WITH HIGH-PRESSURE NITROGEN. DO NOT OVER-PRESSURIZE SYSTEM. Perform leak check of drain system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-243, revision (G), or the latest approved revision. OMPLETION Remove power from aircraft if it is no longer required.
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  • Page 663 TOILETS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TOILETS - DESCRIPTION/OPERATION ESCRIPTION OCATION A self-contained, electrically operated flush toilet is located in the aft lavatory. The toilet is plumbed to be serviced from outside the aircraft, using a standard sanitary service cart. Table 1 lists the components and their locations.
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  • Page 665 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TOILETS - SERVICING NTRODUCTION Purpose The following procedure gives instructions for draining, rinsing, and recharging the toilet system. Equipment and Facilities Required Equipment • Lavatory service cart • Rubber gloves WARNING: WEAR RUBBER GLOVES WHEN SERVICING THE TOILET SYSTEM. IF THE WASTE FLUID GETS ON YOUR HANDS OR SKIN, INFECTION CAN OCCUR.
  • Page 666 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Turn water off and open drain valve to empty water from tank. Close drain valve. Charge empty tank through bowl or through service panel flush fitting with approximately 2 US gallons (7.5 liters) of water and 3 ounces (90 milliliters) of Monogram DG-19 Toilet Chemical as indicated on toilet placard or in manufacturer’s component maintenance manual.
  • Page 667 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TOILETS - REMOVAL/INSTALLATION EMOVAL WARNING: WASTE WATER CAN CAUSE INFECTIONS. WEAR RUBBER GLOVES AND EYE PROTECTION WHEN SERVICING OR REPAIRING THE TOILET SYSTEM. To remove the toilet (Figure 401): Service and drain toilet per SERVICING instructions. Open and lock out associated circuit breaker listed in Table Remove toilet shroud assembly (25-49-00).
  • Page 668 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL DRAIN VALVE TOILET AND TANK ASSEMBLY TIMER ASSEMBLY MOTOR, PUMP & FILTER ASSEMBLY DRAIN VALVE CABLE INLET CHECK VALVE VENT FITTING MOUNTING FRAME HOLD-DOWN RODS (TYPICAL) TOILET - REMOVAL/INSTALLATION FIGURE 401 38-31-00 EFFECTIVITY: TE-55965000-SMM Page 402 Revision A Nov 10/2006...
  • Page 669 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Test the waste disposal system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-292, revision (B), or the latest approved revision.
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  • Page 671 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL TOILETS - INSPECTION/CHECK NTRODUCTION Purpose The following procedure gives instructions for inspecting the flush cycle. Equipment and Facilities Required Equipment • Water Facilities • External power Apply electrical power to the aircraft. Ensure that toilet circuit breaker is closed. ROCEDURE Fill tank with approximately 2 US gallons (7.5 liters) of clear water.
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  • Page 673 AIR SUPPLY CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIR SUPPLY - DESCRIPTION/OPERATION ESCRIPTION OCATION The pressure for the water system is obtained from the 10th stage bleed air. The bleed air line is tapped at the manifold in the aft equipment compartment. The bleed air regulator reduces the air pressure from the tapped line in the aft equipment compartment.
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  • Page 675 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIR SUPPLY - SERVICING EPLACE THE LEED ILTER Introduction Purpose TLMC Task 38-40-60-602 Procedure Replace the bleed air filter per REMOVAL/INSTALLATION. Job Completion Remove all tools, equipment, and unwanted materials from the work area. 38-40-00 TE-55965000-SMM Page 301 EFFECTIVITY: Revision A...
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  • Page 677 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIR SUPPLY - REMOVAL/INSTALLATION EMOVAL To remove the bleed air filter (Figure 401 Figure 402): Shut off bleed air supply. Remove baggage compartment shelves and water tank closeouts. Open bleed air filter drain valve to vent pressure from bleed air line. Unscrew bowl.
  • Page 678 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Loosen swage connectors securing inlet line of three-way manual valve. Loosen swage connectors securing inlet line of overflow two-way solenoid valve at tee connector. (10) Loosen swage connectors securing inlet and outlet lines of bleed air line check valve, and remove check valve.
  • Page 679 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Tighten swage connector on tee fitting a quarter-turn with appropriate tool. Tighten swage connectors on inlet line of three-way manual valve a quarter-turn with appropriate tool. Close manual purge valve. Test air supply system in accordance with ADJUSTMENT/TEST. Install baggage compartment shelf and water tank closeouts.
  • Page 680 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIR PRESSURE THREE-WAY MANUAL VALVE (LINE PURGE) BLEED AIR (BLEED AIR SHUT-OFF VALVE) OVERFLOW CHECK VALVE TWO-WAY SOLENOID VALVE BLEED AIR FILTER DRAIN VALVE BLEED AIR PRESSURE REGULATOR MANUAL TANK BLEED AIR PURGE VALVE FILTER OUTLET LINE BLEED AIR FILTER...
  • Page 681 Verify that all equipment necessary for the test is installed in the aircraft before proceeding. Energize all aircraft electrical buses. Perform leak check of supply system in accordance with Bombardier Completion Center Ground Test Procedure, document number TE-GTP-243, revision (G), or the latest approved revision.
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  • Page 683 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIR SUPPLY - INSPECTION/CHECK ENERAL ISUAL NSPECTION OF THE RESSURE EGULATOR AUGE Introduction Purpose TLMC Task 38-40-60-601 Job Set-up Open the access panel to view the pressure gauge. Pressurize the water system. Procedure Perform a general visual inspection of the air pressure regulator gauge as follows: Observe the pressure gauge on the air supply regulator during system operation.
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  • Page 685 CHAPTER 49 - AIRBORNE AUXILIARY POWER List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 49 - AIRBORNE AUXILIARY POWER LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 49 - Effective Pages Nov 10/2006 Nov 10/2006 49 - Contents Nov 10/2006 Nov 10/2006 49-60-10...
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  • Page 687 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 49 - AIRBORNE AUXILIARY POWER TABLE OF CONTENTS Subject Ch-Se-Su Page AUXILIARY POWER UNIT/ELECTRONIC CONTROL UNIT 49-60-10 Description/Operation Description/Location AUXILIARY POWER UNIT HOUR METER 49-70-10 Description/Operation Description/Location Operation Removal/Installation Removal Installation Adjustment/Test Introduction Test Set-up Test...
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  • Page 689 AUXILIARY POWER UNIT/ELECTRONIC CONTROL UNIT CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AUXILIARY POWER UNIT/ELECTRONIC CONTROL UNIT - DESCRIPTION/OPERATION ESCRIPTION OCATION A spare Auxiliary Power Unit (APU) Electronic Control Unit (ECU) has been installed adjacent to the production ECU. This modification has been designed to allow easy disconnection and reconnection of the wire harness to the spare unit.
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  • Page 691 AUXILIARY POWER UNIT HOUR METER CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AUXILIARY POWER UNIT HOUR METER - DESCRIPTION/OPERATION ESCRIPTION OCATION An additional Auxiliary Power Unit (APU) hour meter with LCD display has been installed in the existing APU fault panel. The meter shows hours of operation and operates in parallel with the production meter. PERATION The operation of the hour meter is controlled by the APU control system and no crew input is required.
  • Page 692 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM THIS PAGE INTENTIONALLY LEFT BLANK 49-70-10 EFFECTIVITY: TE-49735000-SMM-1 Page 2 Revision FI Sep 25/2002...
  • Page 693 AUXILIARY POWER UNIT HOUR METER CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AUXILIARY POWER UNIT HOUR METER - REMOVAL/INSTALLATION EMOVAL CAUTION: BEFORE ATTEMPTING TO INSTALL OR REMOVE ANY UNITS, TURN ELECTRICAL POWER OFF. NOTE: The following procedures require qualified personnel using approved aircraft maintenance procedures.
  • Page 694 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM ATTACHING APU HOUR HARDWARE METER (2 PLACES) AUXILIARY POWER UNIT HOUR METER - REMOVAL/INSTALLATION FIGURE 401 49-70-10 EFFECTIVITY: TE-49735000-SMM-1 Page 402 Revision FI Sep 25/2002...
  • Page 695 AUXILIARY POWER UNIT HOUR METER CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AUXILIARY POWER UNIT HOUR METER - ADJUSTMENT/TEST NTRODUCTION Purpose The following procedure provides instructions for verifying the proper operation of the additional APU hour meter in CL-604 aircraft. NOTE: The following test procedure requires qualified operators using approved aircraft operational procedures.
  • Page 696 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM OMPLETION Remove all equipment used for testing and clear area of debris. If any unit fails any test, remove and proceed as follows: • Return unit to manufacturer or an authorized repair facility for troubleshooting and repair.
  • Page 697 CHAPTER 52 - DOORS List of Effective Pages CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 52 - DOORS LIST OF EFFECTIVE PAGES Ch-Se-Su Page Date Ch-Se-Su Page Date 52 - Effective Pages Nov 10/2006 Nov 10/2006 52 - Contents Nov 10/2006 Nov 10/2006 52-11-00 Nov 10/2006 Nov 10/2006...
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  • Page 699 Table of Contents CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 52 - DOORS TABLE OF CONTENTS Subject Ch-Se-Su Page AIRSTAIR DOOR 52-11-00 Description/Operation Description/Location Operation Maintenance Practices Handrail Rigging Instructions AFT EQUIPMENT BAY DOOR 52-41-00 Description/Operation Description/Location Adjustment/Test Introduction Test Set-up Test Test Completion EXTERIOR DOORS LOCKING PACKAGE 52-44-00...
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  • Page 701 AIRSTAIR DOOR CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIRSTAIR DOOR - DESCRIPTION/OPERATION ESCRIPTION OCATION The production-installed airstair door has been modified to increase compatibility with the entryway interior. This modification consists of two modified handrail assemblies, relocation of two mounting brackets, and adjustments to pushrod assemblies. Table 1 lists the airstair components and their locations.
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  • Page 703 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL AIRSTAIR DOOR - MAINTENANCE PRACTICES ANDRAIL IGGING NSTRUCTIONS The door handrail (Figure 201) has been modified and handrail pushrods have been re-rigged in accordance with drawing TM432517-02 to provide additional clearance between the handrail and the interior trim when the door is closed.
  • Page 704 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL HANDRAIL ASSEMBLY HANDRAIL ACTUATING PUSHROD ASSEMBLY DOOR FOOT PUSHROD ASSEMBLY BRACKET AIRSTAIR DOOR - MAINTENANCE PRACTICES FIGURE 201 52-11-00 EFFECTIVITY: TE-55965000-SMM Page 202 Revision A Nov 10/2006...
  • Page 705 AFT EQUIPMENT BAY DOOR CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AFT EQUIPMENT BAY DOOR - DESCRIPTION/OPERATION ESCRIPTION OCATION A stair assembly has been installed for the aft equipment bay door. The assembly consists of three step assemblies and two struts. The stair deploys from the aft, down and forward. It is locked in place by the struts, which fold to allow the stair to be stowed.
  • Page 706 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM THIS PAGE INTENTIONALLY LEFT BLANK 52-41-00 EFFECTIVITY: TE-3034e-SMM Page 2 Revision A Aug 9/2000...
  • Page 707 AFT EQUIPMENT BAY DOOR CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM AFT EQUIPMENT BAY DOOR - ADJUSTMENT/TEST NTRODUCTION Purpose The following procedure provides instructions for properly adjusting the strut rod ends. NOTE: The following test procedure requires qualified operators using approved aircraft operational procedures.
  • Page 708 CL-604 SUPPLEMENTAL MAINTENANCE MANUAL Prepared by DAS-605786-NM THIS PAGE INTENTIONALLY LEFT BLANK 52-41-00 EFFECTIVITY: TE-3034e-SMM Page 502 Revision A Aug 9/2000...
  • Page 709 EXTERIOR DOORS LOCKING PACKAGE CL-604 SUPPLEMENTAL MAINTENANCE MANUAL EXTERIOR DOORS LOCKING PACKAGE - DESCRIPTION/OPERATION ESCRIPTION OCATION PERATION Several doors and panels on the exterior of the aircraft are equipped with high-security Illinois locks. The locks are operated with a common key. Table 1 lists the components and their locations.
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  • Page 711 SERVICE DOOR INDICATOR SYSTEM CL-604 SUPPLEMENTAL MAINTENANCE MANUAL SERVICE DOOR INDICATOR SYSTEM - DESCRIPTION/OPERATION ESCRIPTION OCATION The production-installed service door open indication system has been modified by the addition of a dedicated annunciator and several service door switches. This annunciator panel lists the service doors monitored by the system and indicates when a door is open.
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  • Page 713 CHAPTER 56 - WINDOWS CL-604 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 56 - WINDOWS THIS SECTION INTENTIONALLY LEFT BLANK 5596-SMM Page 1 EFFECTIVITY: Revision A Nov 10/2006...
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This manual is also suitable for:

Cl-600-2b16