Saab 340B Operation Manual

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AIRCRAFT OPERATIONS MANUAL

The content of this document is proprietary and confidential to Saab AB

and may not:

a) be used for any purpose other than those for which it was supplied;

b) be copied or reproduced in whole or in part without the prior written

consent of Saab AB; nor

c) be disclosed to any third party without the prior written consent of

Saab AB

SE−581 88 Linköping

Sweden

Doc. No: 340LKS042109

Ref. No: SAAB 340B AOM

Part 1

Telephone: int+46 13 18 00 00

Initial Issue: JUN 15/89

Revision 59: Dec 01/20

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Summary of Contents for Saab 340B

Page 1 AIRCRAFT OPERATIONS MANUAL Part 1 The content of this document is proprietary and confidential to Saab AB and may not: a) be used for any purpose other than those for which it was supplied; b) be copied or reproduced in whole or in part without the prior written consent of Saab AB;...
Page 2 THIS PAGE INTENTIONALLY LEFT BLANK !
Page 3 Aircraft Operations Manual LETTER OF TRANSMITTAL REVISION No. 59, Dec 01/20 To: All holders of SAAB 340B EXTENDED WINGTIPS AIRCRAFT OPERATIONS MANUAL. FILING INSTRUCTIONS Before inserting this revision, ensure that Revision No. 58, Jun 01/20 is incorporated. Update the manual according to the revised ”List of Effective Pages”.
Page 4 EXTENDED WINGTIPS Aircraft Operations Manual THIS PAGE INTENTIONALLY LEFT BLANK ! PAGE Dec 01/20...
Page 5 EXTENDED WINGTIPS Aircraft Operations Manual RECORD OF REVISIONS Rev. Rev. Rev. Revision date Revision date Revision date Mar 20/98 Jun 01/16 Nov 06/98 Dec 01/16 Jun 24/99 Jun 01/17 Oct 15/99 Dec 01/17 Feb 02/01 Jun 01/18 Oct 05/01 Jun 01/19 Dec 03/01 Sep 30/19 Sep 06/02...
Page 6 EXTENDED WINGTIPS Aircraft Operations Manual THIS PAGE INTENTIONALLY LEFT BLANK ! PAGE Dec 01/20...
Page 7 EXTENDED WINGTIPS Aircraft Operations Manual HIGHLIGHTS REVISION No. 59, Dec 01/20 AOM BOOK I SE/CH/SU PAGES CODE REASON FOR CHANGE Title Part 1 Date and revision number changed to reflect this revision. Part 1 Revised to reflect this revision. Part 2 −”−.
Page 8 EXTENDED WINGTIPS Aircraft Operations Manual HIGHLIGHTS REVISION No. 59, Dec 01/20 AOM BOOK II SE/CH/SU PAGES CODE REASON FOR CHANGE Title Part 2 Date and revision number changed to reflect this revision. 1−2 Date changed to reflect this revision. No new or cancelled alert operations bulletin.
Page 9 EXTENDED WINGTIPS Aircraft Operations Manual SE/CH/SU PAGES CODE REASON FOR CHANGE 32/2.1 19−20 New pages with new tables for all engines climb gradient (metric). 32/2.2 19−20 New pages with new tables for all engines climb gradient (impe- rial). 37/3.5 E4−1 Text added to highlight who controls the aircraft after pitch discon- nect.
Page 10 EXTENDED WINGTIPS Aircraft Operations Manual THIS PAGE INTENTIONALLY LEFT BLANK ! PAGE Dec 01/20...
Page 11 Aircraft Operations Manual To: Saab AB MANUAL USER COMMENTS Support and Services on omissions, procedures, etc. Publication Engineering SE−581 88 Linköping SWEDEN Aircraft Operations Manual Phone: +46−13 18 00 00 Email: customer.support.publications@saabgroup.com From: Date: Phone/Fax/Email: Manual: Topic: Chap/Sect/Page: Page Date: Comments: Please forward this form, when completed, to the above address.
Page 12 Aircraft Operations Manual THIS PAGE INTENTIONALLY LEFT BLANK ! Manual User Comments PAGE Jun 01/17...
Page 13 FOREWORD Fuel Hydraulics The SAAB 340B AIRCRAFT OPERATIONS MANU- AL (AOM) is the property of Saab AB. It is supplied Ice and Rain Protection in confidence of commercial security. It shall not be Instruments and Recorders used for any purpose other than that for which it is...
Page 14 Aircraft Operations Manual INTRODUCTION Example: Special Range Prefix Performance Supplements Subchapter Line Checks Chapter Section Appendices Supplements Each section in Part 2 contains one or more chap- 15/4.1 ters. Page 1 The chapter can if necessary be separated in sub- chapters.
Page 15 Aircraft Operations Manual INTRODUCTION Appendices REVISIONS Supplements Revisions will be issued as necessary. They will be distributed together with a List of Effective Pages Each section in Part 2 Extended Wingtips contains (LEP) which shall be checked and filed under the one or more chapters.
Page 16 Aircraft Operations Manual INTRODUCTION THIS PAGE INTENTIONALLY LEFT BLANK ! INTRO PAGE Dec 01/16...
Page 17 Aircraft Operations Manual LIST OF EFFECTIVE PAGES REVISION 59 DATE: Dec 01/20 N, R or D, indicates pages which are New, Revised or Deleted respectively. Remove and insert the affected pages. AOM PART 1 CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE...
Page 18 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Jun 01/18 1/2.1 Jun 30/15 Jun 01/18 Jun 30/15 Jun 01/18 Jun 30/15 Jun 01/20 Jun 30/15 Jun 01/18 Jun 01/20 Jun 01/20 Jun 30/15 Jun 01/18 Jun 30/15...
Page 19 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 3.1 Cont’d Jun 01/20 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/20 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15...
Page 20 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 4/2.1 Cont’d Dec 01/15 Apr 01/15 Dec 01/15 Apr 01/15 Dec 01/15 Apr 01/15 Dec 01/15 Dec 01/15 4/2.2 Apr 01/15 Dec 01/15 Apr 01/15 Apr 01/15 4/4.2...
Page 21 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 5.1 Cont’d 6/1.1 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 6/2.1 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Jun 01/19...
Page 22 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 6/7.1 Cont’d Apr 01/15 Apr 01/15 Dec 01/20 Apr 01/15 Dec 01/20 Apr 01/15 Dec 01/20 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 6/8.1 Apr 01/15 Apr 01/15...
Page 23 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Jun 01/17 9/2.0 Apr 01/15 Jun 01/17 Apr 01/15 Jun 01/17 9/2.1 Apr 01/15 Jun 01/17 Apr 01/15 Jun 01/17 Apr 01/15 Jun 01/17 Apr 01/15 Jun 01/17 Jun 01/17...
Page 24 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 11.2 Cont’d Apr 01/15 Jun 01/19 Apr 01/15 Apr 01/15 TAB DIV. 12 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 12/1.1 Apr 01/15...
Page 25 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 13.1 Cont’d Jun 01/20 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Jun 01/20 Apr 01/15 Jun 01/20 Apr 01/15 Apr 01/15 Apr 01/15...
Page 26 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 15/1.1 Cont’d Jun 01/17 Jun 01/18 Jun 01/17 Jun 01/18 Jun 01/17 Jun 01/18 Jun 01/17 Jun 01/18 Jun 01/17 Jun 01/18 Jun 01/17 Jun 01/18 Jun 01/17 Jun 01/18...
Page 27 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 15/3.2 Cont’d Apr 01/15 Jun 01/20 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Jun 01/20...
Page 28 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 15/5.2 Cont’d 15/6.2 Sep 30/19 Apr 01/15 Sep 30/19 Apr 01/15 Sep 30/19 Apr 01/15 Sep 30/19 Apr 01/15 Sep 30/19 Apr 01/15 Sep 30/19 Apr 01/15 Sep 30/19...
Page 29 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 15/8.2 Cont’d Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Jun 01/20 Apr 01/15 TAB DIV. 16 Apr 01/15 Apr 01/15 15/9.1 Dec 01/16 Apr 01/15 Dec 01/16 Jun 01/20...
Page 30 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 17.1 Cont’d Jun 01/19 Jun 30/15 Jun 01/19 Jun 30/15 Jun 01/19 Jun 30/15 Jun 01/19 Jun 30/15 Jun 01/19 Jun 30/15 Jun 01/19 Jun 30/15 Jun 01/19 Jun 30/15...
Page 31 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Apr 01/15 19/1.2 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 19/2.1 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 19/5.2 Jun 01/20 Apr 01/15 Apr 01/15...
Page 32 Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 19/6.2 Cont’d 19/7.2 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Jun 01/20 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15...
Page 33 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES AOM PART 2 REVISION 59 DATE: Dec 01/20 THE FOLLOWING LEP PAGES ARE REFLECTING AIRCRAFT WITH EXTENDED WINGTIPS CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Sep 30/19 TAB DIV. 20 Sep 30/19 Sep 30/19 See list of Effective and Cancelled Alert Opera-...
Page 34 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 23/2 Cont’d A2−11 Jun 01/20 A0−3 Sep 30/19 A2−12 exp Jun 01/19 A0−3 exp Sep 30/19 A2−12 Jun 01/19 A0−3 Sep 30/19 A2−13 exp Jun 01/19 A0−3 exp...
Page 35 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 23/2 Cont’d A7−4 Jun 01/16 A5−6 Jun 01/17 A7−5 exp Jun 01/16 A5−7 exp Jun 01/17 A7−5 Jun 01/16 A5−7 Jun 01/17 A7−5 exp Jun 01/16 A5−8 exp...
Page 36 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 23/2 Cont’d A18−1 exp Sep 30/19 A9−0 Jun 01/16 A18−1 Sep 30/19 A9−1 exp Jun 01/16 A18−1 exp Sep 30/19 A9−1 Jun 01/16 A18−1 Sep 30/19...
Page 37 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 24/2 Cont’d E3−6 exp Jun 01/20 E1−7 exp Jun 01/19 E3−6 Jun 01/20 E1−7 Jun 01/19 E3−7 exp Jun 01/20 E1−8 exp Jun 01/19 E3−7 Jun 01/20...
Page 38 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 24/2 Cont’d Jun 01/20 E7−8 Jun 01/19 Jun 01/19 E7−9 exp Jun 01/19 Jun 01/19 E7−9 Jun 01/19 Jun 01/19 E7−10 exp Jun 01/19 25/2 Dec 01/16...
Page 39 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 25/10 Cont’d Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 26/5 Apr 01/15 25/11 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15...
Page 40 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 27/1.2 Cont’d Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Jun 01/19 Apr 01/15 Apr 01/15 27/2.1...
Page 41 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 28/4.1 Cont’d Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15...
Page 42 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Dec 01/15 28/6.2 Dec 01/20 Dec 01/20 29/4.2 Dec 01/15 Jun 01/20 Dec 01/15 Jun 01/20 Dec 01/15 Dec 01/15 TAB DIV. 29 Dec 01/15 Dec 01/15 Apr 01/15...
Page 43 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Apr 01/15 30/4.2 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 31/2.1 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 31/2.2 Apr 01/15 Apr 01/15 Apr 01/15...
Page 44 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 32/2.1 Cont’d 32/4.2 Apr 01/15 N 19 Dec 01/20 Apr 01/15 N 20 Dec 01/20 Apr 01/15 32/2.2 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15...
Page 45 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 33/2.1 Cont’d Apr 01/15 Dec01/15 Apr 01/15 Dec01/15 Apr 01/15 Dec01/15 Apr 01/15 Dec01/15 Apr 01/15 Dec01/15 Apr 01/15 Dec01/15 Apr 01/15 Dec01/15 Apr 01/15 Dec01/15...
Page 46 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 33/3.1Cont’d TAB DIV. 36 Apr 01/15 Apr 01/15 33/3.2 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 36/1.1 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15...
Page 47 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Jun 01/18 36/7.1 Apr 01/15 Jun 01/18 Apr 01/15 Jun 01/18 Apr 01/15 Jun 01/18 Apr 01/15 Jun 01/20 36/8.1 Apr 01/15 Jun 01/18 Apr 01/15 Jun 01/18...
Page 48 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE 37/2Cont’d A6−11 exp Jun 01/16 Apr 01/15 A6−11 Jun 01/16 A6−12 exp Jun 01/16 37/3 Apr 01/15 A6−12 Jun 01/16 Apr 01/15 A8−0 Jun 01/18 37/3.1...
Page 49 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE Apr 01/15 37/3.7 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 Apr 01/15 37/3.11 Jun 30/15 Apr 01/15 Jun 30/15 Apr 01/15 Jun 30/15 Apr 01/15...
Page 50 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF EFFECTIVE PAGES CHAPTER/ CHAPTER/ SECT/SUB PREFIX PAGE DATE SECT/SUB PREFIX PAGE DATE THIS PAGE INTENTIONALLY LEFT BLANK ! PAGE Dec 01/20...
Page 51 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF OPTIONS AND MODIFICATIONS QUOTED IN THIS MANUAL Mod. No. Service Bulletin No. Prod. Eff. Item 1149 26−005 Fire Protection − Installation of Extra fire Extin- guisher in Cargo Compartment. 1198 53−005 Fuselage − Ditching capability 1345 −...
Page 52 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF OPTIONS AND MODIFICATIONS QUOTED IN THIS MANUAL (Cont’d) Mod. No. Service Bulletin No. Prod. Eff. Item 2417 24−021 Engine start procedure 2418 24−020 Engine start control − change of pwr supply 2514 24−023 Electrical power −...
Page 53 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF OPTIONS AND MODIFICATIONS QUOTED IN THIS MANUAL (Cont’d) Mod. No. Service Bulletin No. Prod. Eff. Item 3112 25−274, 25−275 Air Precision ELT with 406 MHz transmission capability. 3121 21−050 Guarded cabin/flight deck temperature select switches.
Page 54 EXTENDED WINGTIPS Aircraft Operations Manual LIST OF OPTIONS AND MODIFICATIONS QUOTED IN THIS MANUAL (Cont’d) Mod. No. Service Bulletin No. Prod. Eff. Item 3543 24−052 Installation of Electronic Flight Bag (EFB) Arm holder knob and USB Power outlets (modified charger compared to Mod. No. 3453). 3564 34−256 FMS operation on battery power.
Page 55 Aircraft Operations Manual AIRCRAFT GENERAL CONTENTS Aircraft Data 1/1.0 Highlights − not applicable 1/1.1 Description 1/1.2 Operation Cockpit 1/2.0 Highlights − not applicable 1/2.1 Description 1/2.2 Operation − not applicable −CONTENTS PAGE Apr 01/15...
Page 56 Aircraft Operations Manual AIRCRAFT GENERAL THIS PAGE INTENTIONALLY LEFT BLANK ! −CONTENTS PAGE Apr 01/15...
Page 57 Saab Aircraft AB, Linköping, Sweden operating crew members and one observer. The This manual reflects SAAB 340B with A/C S/N from aircraft is certificated to carry up to 37 passengers. 160 and up. The aircraft is a Regional Airliner de-...
Page 58 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description THREE VIEW DRAWING A9898 Fig. 1 Three view drawing (without extended wingtips) 1/1.1 PAGE Apr 01/15...
Page 59 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description MINIMUM TURNING RADIUS WING TIP SWEEP 104 ft (32 m), WITHOUT EXTENDED WING TIPS WING TIP SWEEP 108 ft (33.3 m), WITH EXTENDED WING TIPS TURN CENTER 58 ft (18 m) MINIMUM PAVEMENT WIDTH (TIRE SLIPPAGE IS NOT CONSIDERED) A15474 Fig.
Page 60 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description CABIN CROSS SECTION 85.0 2.16 72.0 1.83 16.3 0.41 17.0 0.43 67.0 1.70 91.0 2.31 A11574 Fig. 3 Cabin cross section 1/1.1 PAGE Apr 01/15...
Page 61 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description ANTENNA ARRANGEMENT VOR/LOC COLLINS DUAL ADF ANTENNA ADF 1 + ADF 2 (OPTION) ADF 2 KING (OPTION) HF ANT (OPTION) VHF COM 1 GLIDE SLOPE ADF 1 KING VLF OMEGA (OPTION) MARKER BEACON DME 1 ATC 2 (OPTION) RADIO ALT...
Page 62 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/1.1 A/C 106−219 PAGE Apr 01/15...
Page 63 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description ANTENNA ARRANGEMENT VOR/LOC HF (option) COLLINS DUAL ANTENNA ADF 1 + ADF (option) TCAS (option) KING ADF 2 ATC 2 TCAS ATC 1 (option) (option) TCAS KING ADF 2 (option) (option) VHF 1 GLIDE SLOPE RNAV−VLF/OMEGA (option)
Page 64 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/1.1 A/C 220−UP or TCAS Mod for a/c 160−219 except for MARKER and PAGE VHF 2 Apr 01/15...
Page 65 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description (0.802 kg/L) A9986 Fig. 5 Ground service connections 1/1.1 PAGE Apr 01/15...
Page 66 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/1.1 PAGE Apr 01/15...
Page 67 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Operation LIMITATION SERVICEABILITY − The aircraft is certificated in the Transport Category for the following types of operation provided the appropriate instruments and equipment required are installed and in operable condition according to the Master Minimum Equipment List, MMEL.
Page 68 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Operation (Cont’d) − Maximum operating altitude and environmental envelope. PRESSURE ALTITUDE x 1000 FT Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï...
Page 69 Operation NORMAL OPERATION The Saab 340 is designed for a regional airline operation where a standard mission profile includes take− off, climb (to cruise altitude), cruise, descent and landing. A typical flight cycle is assumed to be carried out with duration and at altitudes associated with such operation. Significant and recurring deviations from the standard mission profile may be outside certified limits and shall be brought to Saab’s attention since a...
Page 70 Aircraft Operations Manual AIRCRAFT GENERAL, AIRCRAFT DATA Operation THIS PAGE INTENTIONALLY LEFT BLANK ! 1/1.2 PAGE Apr 01/15...
Page 71 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description COCKPIT GENERAL Accommodation etc. The cockpit has accommodation for two pilots and one observer. The observer seat is of a folding type and can be removed when not in use. It is provided with an in- ertia reel shoulder harness.
Page 72 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description PILOT SEATS The shoulder harness is of a reel type which can be locked by a handle or by inertia. The pilot seats have controls for forward/aft and If optional ACARS installed up/down movement. In addition, seat back recline, arm rests angle and lumbar support can be ad- With ACARS installed the center pedestal is ex- justed.
Page 73 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description EYE POSITION INDICATOR A11949 Fig. 3 Eye position indicator 1/2.1 PAGE Jun 30/15...
Page 74 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description PEDALS The rudder pedals can be adjusted in forward/aft direction. By pulling the lever, the pedal lock is re- leased and the pedals are free to be repositioned. When unlocked, the pedals are springloaded to- wards aft position.
Page 75 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description COCKPIT PANEL Sun−visor. Should never be parked in a position blocking the handgrips Overhead panel Handgrip Handgrip Glareshield panel Center instrument panel Right headset holder Left headset holder Right pilot Left pilot instrument panel instrument panel Left circuit Right circuit...
Page 76 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 77 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description Valid for a/c with Mod.no. 3529 for 340 B / 3530 for 340 WT. (Improved stall warning system for icing condition). A30788 Fig. 6 Standard instrument panel. King avionics shown. (Highest modification standard shown.) 1/2.1 PAGE Jun 30/15...
Page 78 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 79 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description Valid for a/c with Mod.no.3529 for 340 B / 3530 for 340 WT. (Improved stall warning system for icing condition). A30789 Fig. 7 Standard instrument panel. Collins avionics shown. (Highest modification standard shown.) 1/2.1 PAGE Jun 30/15...
Page 80 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 81 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description A9875 Fig. 8 Standard side panels and control wheels. (Highest modification standard shown.) 1/2.1 PAGE Jun 30/15...
Page 82 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 83 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description A9876 Fig. 9 Max option side panels and controls wheels. (Highest modification standard shown.) 1/2.1 PAGE Jun 30/15...
Page 84 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 85 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description A10750 Fig. 10 Standard overhead panel and pedestal. King avionics shown. (Highest modification standard shown.) 1/2.1 PAGE Jun 30/15...
Page 86 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 87 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description A10729 Fig. 11 Max option overhead panel and pedestal. Collins avionics shown. (Highest modification standard shown) 1/2.1 PAGE Jun 30/15...
Page 88 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 89 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description COCKPIT DOOR To open the cockpit door from the cabin, the rounded knob on the cockpit door is turned and the door pulled open. The door can be latched in the fully open position by pressing it against a door catcher located on the cover panel to the avionic rack.
Page 90 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description FLIGHT COMPARTMENT DOOR Door jamb Latch lever Used to latch the door in locked position. Rounded knob Door stop Used to engage the pintle latch lever. Prevents the door from beeing opened inwards. Blowout panel In case of a rapid decompression, the door has a pressure equalization...
Page 91 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 92 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 93 To meet new requirements for protection of cockpit viewing of cockpit from cabin side of door and cockpit crew from intrusion by unauthorized personnel, Saab 340 aircraft have been fitted with a Normal Operation reinforced cockpit door. In addition to a complete...
Page 94 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description d. Remove the abutment angle. e. Release the pintle latch by lifting up on the rounded knob, and slide the pintle latch lever in- board. f. Pull the door inwards. NOTE Easy or full opening of the door may be obstruc- ted by the observer’s smoke mask assembly, jumpseat harness buckle holder, etc.
Page 95 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description Observation window and window cover Used to observe the passenger cabin. Rotate the cover to either right or left to uncover the window. FLIGHT COMPARTMENT DOOR Pintle latch lever Used to latch the door in closed posi- tion.
Page 96 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description THIS PAGE INTENTIONALLY LEFT BLANK ! 1/2.1 PAGE Jun 30/15...
Page 97 AIRCRAFT GENERAL, COCKPIT Description ELECTRONIC FLIGHT BAG (EFB) General These optional SAAB modifications, Mod. Nos. 3453 or 3543, include the structural attachment in the aircraft and the electrical installation designed to support tablets (e.g. iPAD). The linkage from the structural attachment is not included in the modification and is assumed to be an off the shelf equipment.
Page 98 Aircraft Operations Manual AIRCRAFT GENERAL, COCKPIT Description Left side shown A31199 Fig. 13 Typical EFB support by RAM Mounting System, Inc. L/H side USB R/H side USB connector connector A31949 Fig. 14 Location of electrical USB connector on side panels (Mod. No. 3543 shown). 1/2.1 PAGE Jun 30/15...
Page 99 Aircraft Operations Manual AIR CONDITIONING & PRESSURIZATION CONTENTS Air Conditioning & Pressurization Highlights − not applicable Description Operation −CONTENTS PAGE Apr 01/15...
Page 100 Aircraft Operations Manual AIR CONDITIONING & PRESSURIZATION THIS PAGE INTENTIONALLY LEFT BLANK ! −CONTENTS PAGE Apr 01/15...
Page 101 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description GENERAL The manually controlled system is an all pneumatic system. The pilot operates the pneumatic second- Air conditioning ary outflow valve by adjusting the control valve set- ting while watching the cabin pressure instruments. Air conditioning is furnished by two packs located under the cabin floor in the wing fairing.
Page 102 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description towards open, the pack valve is moved towards Air Filter. The air is blown over the filter to prevent a closed and vice versa. This allows a temperature moisture build up in the filter. regulation of the air leaving the pack.
Page 103 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description exceeds the ram air pressure keeping the ground A temperature below freezing is indicated by snow connection check valve closed. Should the remain- blowing through the gaspers or frost freezing in the ing ACP fail, ram air pressure opens the check gasper nozzles.
Page 104 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description The heaters are powered from the UTILITY BUS For emergency pressure relief, the electro−pneu- and are individually controlled by an ON−OFF matical outflow valve can be opened by an emer- switch on each side panel. gency pressure dump switch.
Page 105 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description sec. a timer will give a control command driving − Cruise mode When the aircraft reaches its cruis- the valve to fully open position. ing level and the altitude change is less than 200 ft per minute the system transfers to cruise With Mod.
Page 106 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description Manual operation Pressure indication When the AUTO/MAN switch is set to MAN, system The pressure system has the following indications: pressurization is manually controlled. − Differential pressure. − Cabin altitude. A rotary knob on the pressure control panel is used to set the pneumatic outflow valve in desired posi- −...
Page 107 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description (For R side, temperature signals are received from sensors in cockpit and duct.) A12060 Fig. 1 Air conditioning pack − schematic (L−side shown) PAGE Jun 01/18...
Page 108 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description A12061 Fig. 2 Flow path through air conditioning pack PAGE Jun 01/18...
Page 109 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description A26903 Fig. 3 Air conditioning distribution system − schematic This page is Applicable to aircraft without Mod no 1991 installed PAGE Jun 01/18...
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Page 111 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description A12063 Fig. 4 Cabin pressurization system − schematic This page is applicable to aircraft without Mod no 1994 installed PAGE Jun 01/18...
Page 112 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description THIS PAGE INTENTIONALLY LEFT BLANK ! This page is applicable to aircraft without Mod no 1994 installed PAGE Jun 01/18...
Page 113 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description A26864 Fig. 3 Air conditioning distribution system − schematic This page is applicable to aircraft with Mod no 1991 installed PAGE Jun 01/18...
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Page 115 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description BELOW T/O PWR A26863 Fig. 4 Cabin pressurization system − schematic This page is applicable to aircraft with Mod no 1994 installed PAGE Jun 01/18...
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Page 117 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description CONTROLS AND INDICATORS L/R DUCT OV TEMP light (amber). Comes on together with associated master cau- tion for a: − ACP Compressor discharge overtemp. − Distribution duct overtemp. Corresponding Bleed Valve will automatically close.
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Page 119 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description CONTROLS AND INDICATORS L/R DUCT OV TEMP light (amber). Comes on together with associated master cau- tion for a: − ACP Compressor discharge overtemp. − Distribution duct overtemp. Corresponding Bleed Valve will automatically close.
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Page 121 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description CABIN PRESSURIZATION INDICATION DIFF PRESS indicator. Displays cabin differential pressure. Shows 8.8 when LAMP TEST switch on test panel is held in LWR position. A negative diff pressure is indi- cated by ...
Page 122 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description FAULT light (amber). − Illuminates to advise of a system failure. − Illuminates for 3 seconds when system self− Cabin rate set knob. test is performed. If no fault is detected light Used to set cabin vertical speeds from 50 to goes off.
Page 123 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description PILOT FOOTWARMER PANELS MOD NO 1345 LH SIDE FOOTWARMER TEMP HIGH TEST 2 PANEL TEST 2 PROP OVSP L GEN R Air flow Regulator. ENG OVSP Heater switch. AIR DATA EMER PWR AHRS Controls the amount Three position...
Page 124 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description CENTRAL WARNING PANEL CABIN PRESS light (red). L ENG AVIONIC R ENG FIRE SMOKE SMOKE FIRE Comes on if cabin altitude climbs above 10 000 L ENG CARGO CABIN R ENG OIL PRESS SMOKE PRESS OIL PRESS...
Page 125 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description Heater element location COCKPIT FLOOR HEATERS MOD NO 2293 Heater switch. Two position heater element ON−OFF switch. A10800 Fig. 10 Air conditioning and pressurization − cockpit floor heaters PAGE Jun 01/18...
Page 126 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description CARGO HEATER AIR CONDITIONING PANEL CARGO HEATER ON/OFF switch Used to control the optional cargo heater. TEMP IND switch Used to select either CABIN, CARGO or L DUCT temperature to be displayed on the temp indicator.
Page 127 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description A15969 Fig. 12 Optional cargo heater installation PAGE Dec 01/20...
Page 128 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Description ELECTRICAL POWER SUPPLY Air conditioning Cockpit temperature control ....L MAIN BUS H−15 F DECK TEMP Cabin temperature control ....R MAIN BUS P−14 CABIN TEMP...
Page 129 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation LIMITATIONS Unit Norm OPERATING LIMITS Cabin differential pressure − In flight ..........−...
Page 130 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation NORMAL OPERATION CARGO COMPARTMENT TEMPERATURE V.S. FLYING TIME, FL AND OAT Cargo compartment temperature varies with OAT at the departure airport, cruising level OAT, FL and duration of flight. In general, as can be seen in below graphs there is a slight temperature increase in the cargo compartment How to use the charts Establish a REFERENCE TEMPERATURE: when OAT at departure airport and at cruising level deviates...
Page 131 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation (Cont’d) CARGO COMPART- FL 150 MENT TEMPERATURE ( C ) REFERENCE TEMPERATURE = ISA REFERENCE TEMPERATURE = ISA −10 C REFERENCE TEMPERATURE = ISA −15 C −10 FLYING TIME−MINUTES CARGO COMPARTMENT TEMPERATURE FL 200 ( C ) REFERENCE = ISA...
Page 132 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation (Cont’d) CARGO COMPARTMENT TEMPERATURE FL 250 ( C ) REFERENCE TEMP.= ISA +5 C REFERENCE TEMP. = ISA REFERENCE TEMP. = ISA −5 C REFERENCE TEMP. = ISA −10 C REFERENCE TEMP. = ISA −15 C −10 FLYING TIME−MINUTES A10251...
Page 133 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Temperature control knobs ..... . . SET AS DESIRED After engine start Air conditioning panel...
Page 134 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) RECIRC fans ........Reset power and operate the propeller brake in accordance with AOM 17.2.
Page 135 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) TEMP SELECT switch for desired system ..COLD − Hold the switch in COLD position for 3 sec., thereby setting the valve in middle position.
Page 136 Aircraft Operations Manual AIR CONDITIONING AND PRESSURIZATION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Cabin pressurization panel ..... . . − Set barometric knob to actual QNH for landing airfield. −...
Page 137: Table Of Contents
Aircraft Operations Manual AUTOFLIGHT CONTENTS Autoflight, CAT I (STANDARD) Highlights Description Operation Autoflight, CAT II (OPTION) Highlights Description Operation −CONTENTS PAGE Apr 01/15...
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Page 139: Highlights
Aircraft Operations Manual AUTOFLIGHT, CAT I Highlights MODIFICATION STANDARD The system in this chapter assumes a certain modi- fication standard of the aircraft. If a modification is not installed, the following applies as a complement to what is stated in this chapter. DESCRIPTION / OPERATION Flight Director comparator caution Without Mod.
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Page 141: Description
Aircraft Operations Manual AUTOFLIGHT, CAT I Description GENERAL Autopilot with yaw damper, AP/YD The AP function controls the aircraft in pitch and roll Flight Guidance & Autopilot System maneuvering axes on commands from the FD. The (FGAS) YD function is a part of the AP rudder steer channel and provides directional stability.
Page 142 Aircraft Operations Manual AUTOFLIGHT, CAT I Description − Combined modes − by selecting GA (L/R Power lever button).  APPR − by operating the pitch trim switches. (AP disengage only.)  GA (FD mode only; selectable on the power levers). The Stall warning computers will automatically dis- engage the AP/YD if a stall situation should occur.
Page 143 Aircraft Operations Manual AUTOFLIGHT, CAT I Description if the pitch knob is moved out of its detent ex- − Selectable by ALT mode button. cept in GS ”CAP” or ALTS mode. − Selection of ALT clears any previously selected vertical mode except ALTS and GS ”CAP”. −...
Page 144 Aircraft Operations Manual AUTOFLIGHT, CAT I Description pointer. When in VNAV mode the letters VNV will LATERAL MODES be indicated above the deviation scale. HDG, Heading mode − The FCC gives commands to turn to and hold the NOTE heading indicated by the heading bug on the The deviation scale can also display GS (Glide EHSI.
Page 145 Aircraft Operations Manual AUTOFLIGHT, CAT I Description − NAV mode is cleared by selecting HDG or APPR. Vertical profile has to be flown by pilot inputs. c. VOR: Operation is similar to NAV except tighter 1/2 BANK, Half bank mode (If installed) gains, VOR ”CAP”...
Page 146 Aircraft Operations Manual AUTOFLIGHT, CAT I Description MAIN COMPONENTS AND SUBSYSTEMS Vertical Navigation Indicator (VNI) (if installed) Flight Control Computer (FCC) The Vertical Navigation Indicator/computer (VNI) The FD/AP computer is the heart of the flight con- serves as a vertical speed indicator. In addition it trol system.
Page 147 Aircraft Operations Manual AUTOFLIGHT, CAT I Description NAV S NAV S AP control panel Altitude preselect/ alert panel FD/AP mode select panel Nav data EFIS 1 & 2 AP disconnect button Vert sync button Vert VNI (if installed) NO 1 Radio altim data FD/AP...
Page 148 Aircraft Operations Manual AUTOFLIGHT, CAT I Description CONTROLS AND INDICATORS A NAV SOURCE SELECTORS NAV S NAV S NAV SOURCE SELECTOR Pushbuttons (green). The NAV S Left respective Right pushbuttons are used to couple left or right navigation source to the FD/AP.
Page 149 Aircraft Operations Manual AUTOFLIGHT, CAT I Description Mode select panel. Mode select buttons are integrally lighted, mo- mentary push−on buttons. Indicators in mode buttons illuminate to annunciate mode selected. Active as well as preselected/armed modes are annunciated on EADI. In addition to modes selected on MSP, GA push buttons in the power levers provide GA mode.
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Page 151 Aircraft Operations Manual AUTOFLIGHT, CAT I Description DISTANCE display and annunciators. Indicates distance from aircraft to path capture when TO TRK annunciates NM and to aimpoint when TO ALT annunciates NM. VERTICAL NAVIGATION INDICATOR (VNI) (IF INSTALLED) Vertical Speed Required (VSR) display. SETUP display and annunciators.
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Page 153 Aircraft Operations Manual AUTOFLIGHT, CAT I Description LATERAL MODES: VERTICAL MODES: VVVV VS (Vert speed up − VVVV is rate in ft/min.) VOR 1 (Arm./Cap.) VVVV VS (Vert speed down − VVVV is rate in ft/min.) VOR 2 (Arm./Cap.) SSS I CLB (CLIMB −...
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Page 155 Aircraft Operations Manual AUTOFLIGHT, CAT I Description EFIS TEST PANEL DISPLAY CONTROL PANEL (DCP) MODE SELECT PANEL (MSP) AP CONTROL PANEL A/P DISC BUTTON SECTOR SELECT TURN ENGAGED TEST 2 PROP OVSP APPR BANK L GEN R ROSE CLIMB V NAV ENG OVSP AIR DATA EMER PWR AHRS...
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Page 157 Aircraft Operations Manual AUTOFLIGHT, CAT I Description ELECTRICAL POWER SUPPLY Flight director ......L AVIONIC BUS ..G−13 Autopilot .
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Page 159 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation LIMITATIONS Unit Normal OPERATING LIMITS − All AP/YD operation ..... . 1) 2) 1) 2) 1) 2) Before autopilot engagement the aircraft...
Page 160 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation NORMAL OPERATION FD/AP MODE LOGIC A. Vertical Modes SELECT- SELECT- VERTICAL LATERAL PITCH ROLL REMARK ABLE ABLE VER- COM- COM- KNOB KNOB LATERAL TICAL MANDS ON MANDS ON CAUSES CAUSES MODES MODES EADI EADI TO ZERO SEE SE-...
Page 161 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation A. Vertical Modes (Cont’d) PITCH ROLL REMARK SELECT- SELECT- VERTICAL LATERAL ABLE ABLE VER- COM- COM- KNOB KNOB MANDS ON CAUSES CAUSES LATERAL TICAL MANDS ON MODES MODES EADI EADI GS ”CAP” TO ZERO TO ZERO −−−...
Page 162 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation B. Lateral Modes (Cont’d) PITCH ROLL REMARK SELECT- SELECT- VERTICAL LATERAL ABLE ABLE VER- COM- COM- KNOB KNOB MANDS ON CAUSES CAUSES LATERAL TICAL MANDS ON MODES MODES EADI EADI APPR SEE SE- TO ZERO SEE SE- HDG BUG...
Page 163 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation NORMAL OPERATION (Cont’d) CONDITIONS NORMAL PROCEDURES AUTOPILOT The autopilot and its various modes shall normally be used to the greatest pos- GENERAL sible extent. As a general rule, the pilot flying the aircraft (1/P) shall operate the autopilot. The AP modes shall be monitored by use of the EADI.
Page 164 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES MODES Modes are normally selected by pressing the respective buttons on MSP. The GENERAL indicator in button illuminates. ALTS mode is always armed by the APA as indicates on the EADI by a white ALTS under the active vertical mode.
Page 165 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES VS MODE VS button ........PRESS (Basic mode) −...
Page 166 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES (Cont’d) − Monitor the system when approaching the selected altitude. Verify altitude alert and that the annunciation changes from armed (ALTS in white) to cap- ture (ALTS in green) when approaching the altitude. −...
Page 167 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES (Cont’d) VS Bug desired climb/descend rate ....− Rotate PUSH TEST knob as required for initial VS and check VS ARM −...
Page 168 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES (Cont’d) − Rotate SET/PUSH SEL knob until SETUP display indicates desired offset and offset annunciator shows correct location before or after the DME sta- tion. NOTE To change OFFSET from AFTER (A) to BEFORE (=), rotate SET/PUSH SEL knob clockwise, then counter−clockwise until annunciator shows BEFORE (=).
Page 169 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES (Cont’d) − Rotate SET/PUSH SEL knob until setup display indicates desired offset and offset annunciator shows correct location before or after the DME station. NOTE To change OFFSET from AFTER (A) to BEFORE (=), rotate SET/PUSH SEL knob clockwise, then counter−clockwise until annunciator shows BEFORE (=).
Page 170 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES (Cont’d) NAV SOURCE SELECTOR push button ... PRESS LEFT/ RIGHT MSP NAV button ....... PRESS −...
Page 171 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES (Cont’d) CRS selector ........SET ILS INBOUND COURSE NAV SOURCE SELECTOR push buttons...
Page 172 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES (Cont’d) WARNING If the course pointer is set to a wrong inbound course prior established or if the pointer is moved away from a correct inbound course after established on the localizer, the aircraft can or will deviate from the localizer.
Page 173 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS NORMAL PROCEDURES 2.16 GA MODE GA button on power levers ..... . . PRESS −...
Page 174 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation ABNORMAL OPERATION For Abnormal Operation, also see section 23, ABNORMAL PROCE- DURES and 24, EMERGENCY PROCEDURES. CONDITIONS ABNORMAL PROCEDURES FD WARNING INDICATIONS − FD warning (RED) in one or both EADI’s. − FD command bars disappear (from affected side/sides). −...
Page 175 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS ABNORMAL PROCEDURES Cont’d CAUTION Check mode annunciation before re−engagement. AP engage lever ....... . ENGAGED −...
Page 176 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS ABNORMAL PROCEDURES INDICATION WHEN ACTION PROCEDURES OR FAILURE FAILURES Engine failure Above 600 feet Approach may be continued to CAT I DURING ARTE minima. APPROACH Below 600 feet Perform immediate go−around unless ARTE visual contact has been established.
Page 177 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS ABNORMAL PROCEDURES ALTITUDE If it is evident that the system is not responding correctly to capture the selected PRESELECTOR altitude, disconnect the autopilot and manually fly the aircraft onto the altitude disregarding Flight Director command. Select ALT mode, verify mode annunci- ALERTER ation on EADI and re−engage autopilot.
Page 178 Aircraft Operations Manual AUTOFLIGHT, CAT I Operation CONDITIONS ABNORMAL PROCEDURES ELECTRICAL When flying in APPR and LOC and/or GS capture or in NAV mode and LOC POWER capture. Loss of electrical power to the NAV receiver will cause the following on INTERRUPTION the EADI: WHEN FLYING...
Page 179 Aircraft Operations Manual AUTOFLIGHT, CAT II Highlights MODIFICATION STANDARD The system in this chapter assumes a certain modi- fication standard of the aircraft. If a modification is not installed, the following applies as a complement to what is stated in this chapter. DESCRIPTION / OPERATION Flight Director comparator caution.
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Page 181 Aircraft Operations Manual AUTOFLIGHT, CAT II Description GENERAL Autopilot with yaw damper, AP/YD The AP function controls the aircraft in pitch and roll Flight Guidance & Autopilot System maneuvering axes on commands from the FD. The (FGAS) YD function is a part of the AP rudder steer channel and provides directional stability.
Page 182 Aircraft Operations Manual AUTOFLIGHT, CAT II Description − Lateral modes The AP/YD can be disengaged  HDG (basic mode) − by pushing the AP disconnect button on the con- trol wheel. A second push will reset the aural  NAV warning.
Page 183 Aircraft Operations Manual AUTOFLIGHT, CAT II Description on the control wheel. A new vertical speed refer- ence can be selected by the pitch knob on the − FCC holds the altitude existing at time of mode APP in steps of 50 ft. engagement or −...
Page 184 Aircraft Operations Manual AUTOFLIGHT, CAT II Description then automatically capture and track a VNAV d. if in GA mode, the FCC reference data changes to path as defined on the VNI. existing attitude. The vertical mode display on EADI simultaneously changes from GA to PTCH. −...
Page 185 Aircraft Operations Manual AUTOFLIGHT, CAT II Description intercept heading can be selected on the heading In GS ”CAP” a new vertical mode can only be bug. selected after a new lateral mode has been selected (other than APPR). − Mode is engaged at the capture point and NAV ”CAP”...
Page 186 Aircraft Operations Manual AUTOFLIGHT, CAT II Description − Report mode is the one of the three available are used to couple left or right navigation source as basic submodes that is to be notified. input to the FD/AP. − Available on ground only with AP and YD disen- Altitude Preselector Alerter (APA) gaged but before power shut−down.
Page 187 Aircraft Operations Manual AUTOFLIGHT, CAT II Description NAV S NAV S AP control panel Altitude preselect/ alert panel FD/AP mode select panel Nav data EFIS 1 & 2 AP disconnect button Vert sync button Vert VNI (if installed) NO 1 Radio altim data FD/AP...
Page 188 Aircraft Operations Manual AUTOFLIGHT, CAT II Description CONTROLS AND INDICATORS AP XFR button. The AP XFR button is a push−on/push−off transfer switch. The button is normally not illuminated and the AP uses signals from the left pilot side. When pushed (AP XFR illuminted), transfer to right pilot side takes place.
Page 189 Aircraft Operations Manual AUTOFLIGHT, CAT II Description Half bank mode (Optional) B MODE SELECT PANEL (MSP) Mode indicator Lateral modes APPR BANK Vertical modes CLIMB V NAV Vertical navigation (Optional) Mode select panel. Mode select buttons are integrally lighted, momentary push−on buttons.
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Page 191 Aircraft Operations Manual AUTOFLIGHT, CAT II Description DISTANCE display and annunciators. Indicates distance from aircraft to path capture when TO TRK annunciates NM and to aimpoint when TO ALT annunciates NM. VERTICAL NAVIGATION INDICATOR (VNI) (IF INSTALLED) Vertical Speed Required (VSR) display. SETUP display and annunciators.
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Page 193 Aircraft Operations Manual AUTOFLIGHT, CAT II Description LATERAL MODES: VERTICAL MODES: VVVV VS (Vert speed up − VVVV is rate in ft/min.) VOR 1 (Arm./Cap.) VVVV VS (Vert speed down − VVVV is rate in ft/min.) VOR 2 (Arm./Cap.) SSS I CLB (CLIMB −...
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Page 195 Aircraft Operations Manual AUTOFLIGHT, CAT II Description EFIS TEST PANEL DISPLAY CONTROL PANEL (DCP) MODE SELECT PANEL (MSP) AP CONTROL PANEL SECTOR SELECT TURN TEST 2 ENGAGED PROP OVSP APPR BANK L GEN R ROSE CLIMB V NAV ENG OVSP AIR DATA EMER PWR AHRS DISENGAGED...
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Page 197 Aircraft Operations Manual AUTOFLIGHT, CAT II Description ELECTRICAL POWER SUPPLY Flight director ......L AVIONIC BUS ..G−13 Autopilot .
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Page 199 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation LIMITATIONS Unit Normal OPERATING LIMITS AP Update 2 (FCC−86) AP speed limits − All AP/YD operation ..... . 1) 2) 1) 2) 1) 2)
Page 200 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation NORMAL OPERATION FD/AP MODE LOGIC A. Vertical Modes SELECT- SELECT- VERTICAL LATERAL PITCH ROLL REMARK ABLE ABLE VER- COM- COM- KNOB KNOB LATERAL TICAL MANDS ON MANDS ON CAUSES CAUSES MODES MODES EADI EADI TO ZERO SEE SE-...
Page 201 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation A. Vertical Modes (Cont’d) PITCH ROLL REMARK SELECT- SELECT- VERTICAL LATERAL ABLE ABLE VER- COM- COM- KNOB KNOB MANDS ON CAUSES CAUSES LATERAL TICAL MANDS ON MODES MODES EADI EADI GS ”CAP” TO ZERO TO ZERO −−−...
Page 202 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation B. Lateral Modes SELECT- SELECT- VERTICAL LATERAL PITCH ROLL REMARK ABLE ABLE VER- COM- COM- KNOB KNOB LATERAL TICAL MANDS ON MANDS ON CAUSES CAUSES MODES MODES EADI EADI SEE SE- TO ZERO SEE SE- HDG BUG BASIC LATERAL...
Page 203 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation NORMAL OPERATION (Cont’d) CONDITIONS NORMAL PROCEDURES AUTOPILOT The autopilot and its various modes shall normally be used to the greatest pos- GENERAL sible extent. As a general rule, the pilot flying the aircraft (1/P) shall operate the autopilot. The AP modes shall be monitored by use of the EADI.
Page 204 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES AUTOPILOT Modes on MSP ....... . . SELECT AS ENGAGEMENT DESIRED...
Page 205 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES VS MODE VS button ........PRESS (Basic mode) −...
Page 206 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) − Monitor the system when approaching the selected altitude. Verify altitude alert and that the annunciation changes from armed (ALTS in white) to cap- ture (ALTS in green) when approaching the altitude. −...
Page 207 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) VS Bug desired climb/descend rate ....− Rotate PUSH TEST knob as required for initial VS and check VS ARM −...
Page 208 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) − Rotate SET/PUSH SEL knob until SETUP display indicates desired offset and offset annunciator shows correct location before or after the DME sta- tion. NOTE To change OFFSET from AFTER (A) to BEFORE (=), rotate SET/PUSH SEL knob clockwise, then counter−clockwise until annunciator shows BEFORE (=).
Page 209 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) − Rotate SET/PUSH SEL knob until setup display indicates desired offset and offset annunciator shows correct location before or after the DME station. NOTE To change OFFSET from AFTER (A) to BEFORE (=), rotate SET/PUSH SEL knob clockwise, then counter−clockwise until annunciator shows BEFORE (=).
Page 210 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) NAV SOURCE SELECTOR push button ... PRESS LEFT/RIGHT MSP NAV button ....... PRESS −...
Page 211 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) CRS selector ........SET ILS INBOUND COURSE NAV SOURCE SELECTOR push buttons...
Page 212 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) WARNING If the course pointer is set to a wrong inbound course prior established or if the pointer is moved away from a correct inbound course after established on the localizer, the aircraft can or will deviate from the localizer.
Page 213 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Altitude set knob (APA) ......SET GA ALT CAUTION −...
Page 214 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation ABNORMAL OPERATION For Abnormal Operation, also see section 23, ABNORMAL PROCE- DURES and 24, EMERGENCY PROCEDURES. CONDITIONS ABNORMAL PROCEDURES FD WARNING INDICATIONS − FD warning (RED) in one or both EADI’s. − FD command bars disappear (from affected side/sides). −...
Page 215 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS ABNORMAL PROCEDURES Cont’d CAUTION Check mode annunciation before re−engagement. AP engage lever ....... . ENGAGED −...
Page 216 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS ABNORMAL PROCEDURES PROCEDURES INDICATION WHEN ACTION OR FAILURE FAILURES Engine failure Above 600 ft Approach may be continued to CAT I DURING ARTE minima. APPROACH Below 600 ft Perform immediate go−around unless ARTE visual contact has been established.
Page 217 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS ABNORMAL PROCEDURES ALTITUDE If it is evident that the system is not responding correctly to capture the selected PRESELECTOR altitude, disconnect the autopilot and manually fly the aircraft onto the altitude disregarding Flight Director command. Select ALT mode, verify mode annunci- ALERTER ation on EADI and re−engage autopilot.
Page 218 Aircraft Operations Manual AUTOFLIGHT, CAT II Operation CONDITIONS ABNORMAL PROCEDURES ELECTRICAL When flying in APPR and LOC and/or GS capture or in NAV mode and LOC POWER capture. Loss of electrical power to the NAV receiver will cause the following on INTERRUPTION the EADI: WHEN FLYING...
Page 219 Aircraft Operations Manual COMMUNICATIONS CONTENTS Audio Integrating 4/1.0 Highlights − not applicable 4/1.1 Description 4/1.2 Operation HF COM (OPTION) 4/2.0 Highlights − not applicable 4/2.1 Description 4/2.2 Operation VHF COM 4/3.0 Highlights 4/3.1 Description 4/3.2 Operation PA/Interphone 4/4.0 Highlights − not applicable 4/4.1 Description 4/4.2...
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Page 221 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description GENERAL Audio Control Panel (ACP) The audio integrating system provides the pilots Two ACP’s are installed in the cockpit, one for each with intercom and audio control. pilot. The ACP’s are furnished with slide levers for volume control and a number of pushbuttons and The VHF COM, HF COM and UHF COM (if switches that allow various controls of the audio...
Page 222 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description and does not require unplugging of the headset mi- and cockpit. Intercom volume is controlled with INT crophone. slide lever on both ACP’s. The white ground crew light on the ground status panel will be on whenever With Mod.
Page 223 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description Logic Cockpit speakers Audio Flight data recorder Jack panel Cockpit voice recorder PHONE Observer Jack panel switch Audio Jack panel IDENT signal Logic IDENT signal Steering wheel switch REMOTE IDENT signal Marker Hand Mic. ELECTRONIC UNIT IDENT signal...
Page 224 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description CONTROLS AND INDICATORS XMIT SELECT pushbuttons. − Momentarily press associated button to select COM/HF for transmitting (HF if installed, COM 3 not used). − Selected button illuminates. MIC switch. HOT− Headset or mask microphone is continuously on in the intercom.
Page 225 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description GROUND STATUS PANEL DOORS STATUS CARGO R PROP FUELING DOOR BRAKE MAIN MAIN DOOR DOOR HANDLE CREW EXT PWR HATCH AVAIL Ground crew light. A white light comes on when ground crew headset is connected in the nose wheel well.
Page 226 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description COCKPIT LOUDSPEAKER OBSERVERS JACK PANEL Connections for headsets. PHONE BOOM Two types of connectors are accepted. COLD With Mod. No. 3144 installed: Connection for power to ANR headsets. ANR PWR MIC switch. PHONE (Audio) switch. HOT−...
Page 227 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description GROUND CREW JACK PANEL COCKPIT CALL BUT- (option) GROUND CREW HEADSET TALK SWITCH (schematic) Talk switch Headset Microphone plug Earphone plug A11579 Fig. 5 Ground crew station and schematic 4/1.1 PAGE Apr 01/15...
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Page 229 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description OXY MASK A11565 Fig. 6 Observers oxygen mask microphone jack 4/1.1 A/C 180 − up PAGE Apr 01/15...
Page 230 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description THIS PAGE INTENTIONALLY LEFT BLANK ! 4/1.1 A/C 180 − up PAGE Apr 01/15...
Page 231 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description OBSERVER OXY MASK Connection for observer hand microphone. Observer hand microphone. A29408 Fig. 7 Observers hand microphone jack 4/1.1 With Mod. No. 2600 installed PAGE Apr 01/15...
Page 232 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description XMIT SELECT COLD MIC OBSERVER SWITCH BOOM COM 2 COM MASK NORM EMER 1 NAV 2 ADF 2 SPKR VOICE IDENT Observer/Pilot Hand Microphone selector switch (guarded) This switch selects which hand microphone is active for transmission. OBSVR −...
Page 233 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description ELECTRICAL POWER SUPPLY Left pilot audio ......L BAT BUS E−10 AUDIO L...
Page 234 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Description THIS PAGE INTENTIONALLY LEFT BLANK ! 4/1.1 PAGE Apr 01/15...
Page 235 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Operation LIMITATIONS Not applicable. NORMAL OPERATION The operation is described individually under each system which is connected to the Audio Integrating sys- tem; VOR/ILS, DME, ADF, PA/INTERPHONE, VHF COM, HF COM and UHF COM. ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES...
Page 236 Aircraft Operations Manual COMMUNICATIONS, AUDIO INTEGRATING Operation CONDITIONS ABNORMAL PROCEDURES COCKPIT IN- ACTIONS TERCOM DEAD CBs E−10 (AUDIO L) and L−10 (AUDIO R) ..CHECK/RESET End of procedure. 4/1.2 PAGE Apr 01/15...
Page 237 Aircraft Operations Manual COMMUNICATIONS, HF COM Description GENERAL There are also mode and squelch controls. The clarifier permits the pitch of the received signal The HF 230 communication system provides a two- to be varied 100 Hz in all modes except AM. way voice link in the high frequency range 2.0 to 22.9999 MHz.
Page 238 Aircraft Operations Manual COMMUNICATIONS, HF COM Description CONTROL UNIT MODE / SQUELCH / FREQ CLARIFIER / TEST COCPIT VOICE RECORDER AUDIO INTEGRATING SYSTEM TRANSCEIVER TUNING FAULT TRANSMIT / TUNING FLIGHT DATA RECORDER RECEIVE POWER AMPLIFIER TRANSMIT / TUNING RECEIVE ANTENNA COUPLER ANTENNA A26866 Fig.
Page 239 Aircraft Operations Manual COMMUNICATIONS, HF COM Description CONTROLS AND INDICATORS Channel / Frequency select knobs. Knob functions when selecting a descrete frequency: Knob functions when selecting a user programmed channel: Left outer − Selects the MHz digits (1 through 29 in the Left outer −...
Page 240 Aircraft Operations Manual COMMUNICATIONS, HF COM Description THIS PAGE INTENTIONALLY LEFT BLANK ! 4/2.1 COLLINS HF − 230 PAGE 4 Apr 01/15...
Page 241 Aircraft Operations Manual COMMUNICATIONS, HF COM Description CONTROL WHEEL PTT BUTTON HAND MICROPHONE AUDIO CONTROL PANEL, ACP XMIT SELECT COLD BOOM 1 COM 2 COM 3 HF XMIT SELECT button. MASK NORM EMER HF Volume control lever. 1 NAV 2 SPKR 1 ADF 2 VOICE...
Page 242 Aircraft Operations Manual COMMUNICATIONS, HF COM Description ELECTRICAL POWER SUPPLY ........L AVIONICS BUS E−14 COM HF...
Page 243 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation HF−230 COM SYSTEM For more detailed information see Collins Pilot’s Guide for HF−230 LIMITATIONS Do not tune or transmit on HF during refueling. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP L AVION switch .
Page 244 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Select the desired user channel. Rotate the left outer channel select knob in either direction until user channel 1 or 40 appears at the right side of the CHAN display. Then use the right outer channel select knob to select the desired channel number (from 1 to 40) to program.
Page 245 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Select the desired user channel. Rotate the left outer channel select knob in either direction until user channel 1 or 40 appears at the right side of the CHAN display. Then use the right outer channel select knob to select the desired channel number (from 1 to 40) to program.
Page 246 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Ensure that the CHAN/FREQ selector is in the CHAN position. Select the desired user channel. Rotate the left outer channel select knob in either direction until user channel 1 or 40 appears at the right side of the CHAN display.
Page 247 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation CONDITIONS NORMAL PROCEDURES WARNING Do not tune or transmit on HF system during fueling since fire and/or injury to FREQUENCY/ personnel may result. CHANNEL TUN- XMIT SELECT HF pushbutton ....PRESS −...
Page 248 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) PULL MODE knob ......SELECT AS REQUIRED −...
Page 249 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Squelch control ......−...
Page 250 Aircraft Operations Manual COMMUNICATIONS, HF COM Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES LOSS OF COM- ACTIONS MUNICATION SQUELCH control ......CHECK CLAR (clarifier) control .
Page 251 Aircraft Operations Manual COMMUNICATIONS, VHF COM Highlights MODIFICATION STANDARD DESCRIPTION/OPERATION VHF COM frequency range Without mod. no. 2060 embodied: − The frequency range of the VHF COM is 118.000 to 135.975 MHz. 4/3.0 PAGE Apr 01/15...
Page 252 Aircraft Operations Manual COMMUNICATIONS, VHF COM Highlights THIS PAGE INTENTIONALLY LEFT BLANK ! 4/3.0 PAGE Apr 01/15...
Page 253 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description GENERAL The control unit is also provided with a gas dis- charge type of display for two frequencies, one ac- There are two identical VHF communication sys- tive and one standby. The display will indicate TX tems independent of each other.
Page 254 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description CONTROLS AND INDICATORS Frequency display Upper display − Active frequency (ACT). Lower display − Standby frequency. NOTE: With Mod. No. 2938 installed, three decimal digits will be shown. − Memory frequencies available − Indicates transmitting. XFR/MEM switch When switched momentarily to: −...
Page 255 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description GENERAL a frequency information which is transferred to the transceiver as a data code. There are two identical VHF communication sys- Two frequencies can be selected and displayed. By tems independent of each other. The frequency means of a transfer button the operator can select range is 118.000 to 136.975 MHz selectable in 25 one frequency to be active and the other one as...
Page 256 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description CONTROLS AND INDICATORS Frequency display. UPPER − Displays active frequency. When transmitting, a T is displayed at the right of the active frequency display. Lower − Displays standby (SBY) frequency. NOTE: With Mod. No. 2938 installed, three decimal digits will be shown.
Page 257 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description GENERAL one frequency to be active and the other one as standby. The active one will be indicated by a ”T” There are two identical VHF communication sys- when the Press To Transmit (PTT) button is oper- tems independent of each other.
Page 258 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description CONTROLS AND INDICATORS Frequency display Upper: − Displays active frequency. When transmitting, a T is displayed at the right of the active frequency display. Lower − Displays standby (SBY) frequency. NOTE: With Mod. No. 2938 installed, three decimal digits will be shown.
Page 259 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description CONTROL WHEEL PTT BUTTON HAND MICROPHONE XMIT SELECT button. Momentarily press associated button to select COM for transmitting (COM 3 not used, ex- AUDIO CONTROL PANEL, ACP cept with Mod. No. 3142 installed ). XMIT SELECT NORM/EMER switch.
Page 260 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description PILOTS JACK PANEL BOOM MASK BOOM AUDIO CONTROL PANEL Oxygen mask use. XMIT SELECT The oxygen mask microphone plug is COLD normally connected to the OXY MASK re- COM 2 COM BOOM ceptacle (1) and with the BOOM/MASK switch (2) set to MASK when oxygen mask MASK NORM...
Page 261 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description ELECTRICAL POWER SUPPLY VHF 1 ........EMER AVIONIC BUS E−13 VHF COM 1...
Page 262 Aircraft Operations Manual COMMUNICATIONS, VHF COM Description THIS PAGE INTENTIONALLY LEFT BLANK ! 4/3.1 PAGE Apr 01/15...
Page 263 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP ESS, L and R AVION switches ....−...
Page 264 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation CONDITIONS NORMAL PROCEDURES COMMUNICA- Frequency set up TIONS Frequency selector ......SET FREQUENCY.
Page 265 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES LOSS OF COM- ACTIONS MUNICATION Headsets ........CHECK −...
Page 266 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation THIS PAGE INTENTIONALLY LEFT BLANK ! 4/3.2 COLLINS PRO LINE II PAGE Jun 01/18...
Page 267 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP ESS, L and R AVION switches ....−...
Page 268 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES LOSS OF COM- ACTIONS MUNICATION Headsets ........CHECK −...
Page 269 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP ESS, L and R AVION switches ....−...
Page 270 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation CONDITIONS NORMAL PROCEDURES COMMUNICA- Frequency set up TIONS Frequency selector ......SET FREQUENCY.
Page 271 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) PTT button ........PRESS −...
Page 272 Aircraft Operations Manual COMMUNICATIONS, VHF COM Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES LOSS OF COM- ACTIONS MUNICATION Headsets ........CHECK −...
Page 273 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description GENERAL Cockpit/cabin interphone The Passenger Address (PA) and Interphone are The similar type of interphones is used in cockpit two combined systems, utilizing the same amplifier and cabin. The handset is provided with noise can- unit (PA amplifier) located in the avionics rack.
Page 274 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description CABIN SIGN PANEL PILOTS L/R JACK PANEL CABIN INTERPHONE L/R RP BUTTON BOOM EMER MASK CABIN CALL AUDIO BOOM COCKPIT INTERPHONE CALL EMER Oxygen mask Headset Remote Audio/chime PA/Call/EMER reset electric unit Cockpit speakers CABIN INTERPHONE AUDIO Cockpit voice...
Page 275 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description CONTROLS AND INDICATORS EMER (emergency) light. Comes on flashing in red together with HI−LOW chime when cockpit is emergency called by cabin attendant. CABIN SIGN PANEL CALL light. CABIN SIGNS Comes on in amber together with HI−LOW SEAT chime when cockpit is called by cabin attendant.
Page 276 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description Call buttonlights. − Select to give passenger messages. CALL − Select to call cabin attendant. EMER − Select to give emergency call to cabin attendant. The selected CALL or EMER buttonlight comes on together with HI−LOW chime when cockpit crew;s called by cabin attendant.
Page 277 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description PILOT’S JACK PANEL PA calls with oxygen mask and use of the PA button. Calls to cabin: − When oxygen mask interphone button is press− ed, the mask microphone will automatically be switched to PA for passenger messages. No other function can be selected.
Page 278 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description CABIN CALL LIGHTS C/A PANEL PA (green). CALL (green). EMERGENCY (red and flashing). The selected CALL or EMER call light comes on together with HI−LOW chime when cabin attendant is called by cockpit crew. PA call light comes on without chime when cockpit crew CABIN INTERPHONE gives message to the passengers.
Page 279 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description ELECTRICAL POWER SUPPLY PA ........L BAT BUS E−12 PA L...
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Page 281 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description GENERAL Cockpit/cabin interphone The Passenger Address (PA) and Interphone are The similar type of interphones is used in cockpit two combined systems, utilizing the same amplifier and cabin. The handset is provided with noise can- unit (PA amplifier) located in the avionics rack.
Page 282 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description CABIN SIGN PANEL PILOTS L/R JACK PANEL BOOM EMER MASK CALL BOOM COCKPIT INTERPHONE Oxygen mask Digital Remote Audio/chime electric unit Cockpit speakers CABIN INTERPHONE AUDIO Cockpit voice CALL/EMER HI/LO chime recorder CABIN SIGN PANEL * PA amplifier Audio/chime SEAT...
Page 283 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description CONTROLS AND INDICATORS EMER (emergency) light. Comes on flashing in red together with HI--LOW chime when cockpit is emergency called by cabin attendant. CABIN SIGN PANEL CALL light. CABIN SIGNS Comes on in amber together with HI--LOW SEAT chime when cockpit is called by cabin attendant.
Page 284 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description Interphone calls with headset (with or without oxygen mask) in use Calls to cabin: -- Select a function button (PA, CALL, or EMER). -- Press the CAB interphone button and give message in headset/mask micro-- FLIGHT DECK INTERPHONE phone.
Page 285 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description PILOT’S JACK PANEL PA calls with oxygen mask and use of the PA button. Calls to cabin: -- When oxygen mask interphone button is press-- ed, the mask microphone will automatically be switched to PA for passenger messages. No other function can be selected.
Page 286 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description CABIN INTERPHONE Call buttons EMG -- Emergency call to flight deck -- Passenger calls FLT -- Flight deck call The phone is protected against inadvertent use, the handset must be released before use. EMG calls are identified by triple HI- -LOW chimes.
Page 287 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description C/A PANEL CABIN CALL LIGHTS PA (green). CALL (green). EMERGENCY (red and flashing). The selected CALL or EMER call light comes on together with HI--LOW chime when cabin attendant is called by cockpit crew. PA call light comes on without chime when cockpit crew gives message to the passengers.
Page 288 Aircraft Operations Manual COMMUNICATIONS, PA/INTERPHONE Description ELECTRICAL POWER SUPPLY PA ........L BAT BUS E--12 PA L...
Page 289 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP L BAT switch ........−...
Page 290 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation CONDITIONS NORMAL PROCEDURES (Cont’d) After message: CABIN interphone button ....RELEASE − When released, the interphone will reset which is indicated by selected button light going out.
Page 291 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Via oxygen mask microphone Oxygen mask PA button ......PRESS AND HOLD −...
Page 292 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation CONDITIONS NORMAL PROCEDURES CALLS FROM Cockpit announcement to the passengers are indicated by the PA buttonlight COCKPIT comes on. Handset (cabin interphone) ..... . LIFT CABIN ATTENDANT Handset talk button...
Page 293 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP L BAT switch ........−...
Page 294 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation CONDITIONS NORMAL PROCEDURES (Cont’d) After message: CAB button ....... . RELEASE −...
Page 295 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Handset talk button ......PRESS AND HOLD −...
Page 296 Aircraft Operations Manual COMMUNICATIONS, PA/CABIN INTERPHONE Operation ABNORMAL OPERATION It is recommended that the individual operator develop alternative procedures for normal operation in case of interphone system failure. CONDITIONS ABNORMAL PROCEDURES INTERPHONE ACTION SYSTEM DEAD CB E−12 (PA L) ....... . CHECK/RESET CABIN ATTENDANT End of procedure.
Page 297 Aircraft Operations Manual COMMUNICATIONS, ACARS Description GENERAL Control display panel ACARS is an abbreviation for ARINC communica- The Control display panel provides the aircrew in- tion and reporting system. The system is designed terface with ACARS. The touch sensitive display to reduce the requirement of voice communications screen provides Keypads, Alphabetic and Numeric by reporting automatically the arrival and departure...
Page 298 Aircraft Operations Manual COMMUNICATIONS, ACARS Description ACARS ground facilities The ARINC Electronics Switching Systems (ESS) network provides VHF radio coverage to enroute The ACARS ground stations consist of an ARINC aircraft and terminal coverage at more than 150 central computer, a switching network system and airports in North America.
Page 299 Aircraft Operations Manual COMMUNICATIONS, ACARS Description VHF COM CONTROL MANAGEMENT DISPLAY UNIT ARINC AIRLINE COMPUTER VHF RADIO SITE AIRLINE COMPUTER AIRLINE COMPUTER ARINC VHF RADIO SITE GROUN NET- WORK STATION WIRE LINE ARINC GROUN CENTRAL COMPUT- A9870 STATION Fig. 2 ACARS ground network 4/5.1 PAGE Apr 01/15...
Page 300 Aircraft Operations Manual COMMUNICATIONS, ACARS Description CONTROLS AND INDICATORS ACARS CONTROL DISPLAY PANEL Collins Ambient Light sensor. Touch sensitive display. A9866 Fig. 3 ACARS control display panel − controls 4/5.1 PAGE Apr 01/15...
Page 301 Aircraft Operations Manual COMMUNICATIONS, ACARS Description Menu page keypads Collins Label Function Performed Displays subsystem display page. Displays brightness control page. DIAG Displays MIDU location page which shows pgm pin status. Select / User Function page keypads 1/2 Label Function Performed Collins MENU Displays MIDU MENU page.
Page 302 Aircraft Operations Manual COMMUNICATIONS, ACARS Description Alphabetic keyboard Label Function Performed Collins MENU Displays MIDU MENU page. Displays subsystem page. Clears last operation/Clears last character. CLR LINE Clears scratch pad of last message/text entry. Displays numeric keyboard page. TEMPERATURE KEYS NAVIGATIONAL KEYS NUMERIC KEYS Collins...
Page 303 Aircraft Operations Manual COMMUNICATIONS, ACARS Description SELF TEST button. Starts the self test and will print a test pattern as long as the button is depressed. PPR ADV paper advance button. Depress for paper advance. The paper will advance as long as the button is depressed. PWR ON light (green).
Page 304 Aircraft Operations Manual COMMUNICATIONS, ACARS Description ELECTRICAL POWER SUPPLY Normal power VHF COM 3 ....R MAIN BUS L−14 VHF COM3 ACARS .
Page 305: Operation
Aircraft Operations Manual COMMUNICATIONS, ACARS Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP INVERTER Switch ......1 or 2 −...
Page 306 Aircraft Operations Manual COMMUNICATIONS, ACARS Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES ACARS FAIL- INDICATIONS URE (POWER ACARS display control panel is black and PWR ON light on the printer is extin- SUPPLY) guished. ACTIONS CB N−18 (ACARS PWR) ......CHECK/RESET CB N−19 (ACARS BACK UP) .
Page 307: Description
Aircraft Operations Manual COMMUNICATIONS, UHF COM Description GENERAL Antenna The Bendix/King KTR 909B UHF communication The transmitting and receiving is through a com- system is a two−way voice communication system. bined VHF/UHF antenna mounted on the bottom of It is amplitude modulated in the 225.000 to 399.975 the aircraft.
Page 308 Aircraft Operations Manual COMMUNICATIONS, UHF COM Description CONTROLS AND INDICATORS Transmit annunciation. Receive Mode annunciation. MN − Displayed when the MAIN or the BOTH mode is selected UHF COM CONTROL UNIT as receive mode. GD − Displayed when the BOTH BENDIX/KING mode is selected as receive mode.
Page 309 Aircraft Operations Manual COMMUNICATIONS, UHF COM Description CONTROL WHEEL PTT BUTTON HAND MICROPHONE AUDIO CONTROL PANEL, ACP XMIT SELECT COLD BOOM 1 COM 2 COM 3 UHF XMIT SELECT button. MASK NORM EMER UHF Volume control lever. 1 NAV 2 SPKR 1 ADF 2 VOICE...
Page 310 Aircraft Operations Manual COMMUNICATIONS, UHF COM Description ELECTRICAL POWER SUPPLY UHF ........RH AVIONIC BUS L−14 4/6.1...
Page 311: Operation
Aircraft Operations Manual COMMUNICATIONS, UHF COM Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP R AVION switches ......−...
Page 312 Aircraft Operations Manual COMMUNICATIONS, UHF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) NOTE When the receiver is in the BOTH mode, the Guard (GD) and Main (MN) annun- ciators come on. If the guard channel is selected in preset mode or the guard frequency is se- lected in manual mode, it is not possible to select the BOTH mode.
Page 313 Aircraft Operations Manual COMMUNICATIONS, UHF COM Operation CONDITIONS NORMAL PROCEDURES (Cont’d) CHAN button ........PRESS −...
Page 314 Aircraft Operations Manual COMMUNICATIONS, UHF COM Operation CONDITIONS NORMAL PROCEDURES MANUAL The CHAN button is used to toggle the radio between manual and preset FREQUENCY channel selection. When a frequency is selected manually, semi−duplex op- SELECTION eration is not available. To enter a frequency manually: CHAN button (COM control unit) .
Page 315 Aircraft Operations Manual COMMUNICATIONS, UHF COM Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES LOSS OF COM- ACTIONS MUNICATION SQUELCH ........CHECK.
Page 316 Aircraft Operations Manual COMMUNICATIONS, UHF COM Operation CONDITIONS ABNORMAL PROCEDURES (Cont’d) Display ........CHECK.
Page 317 Aircraft Operations Manual ELECTRICAL CONTENTS Electrical Highlight − not applicable Description Operation −CONTENTS PAGE Apr 01/15...
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Page 319 Aircraft Operations Manual ELECTRICAL Description GENERAL buses through the use of a load transfer relay. Each engine air intake anti−icing is supplied from respec- The electrical power system is divided into four sep- tive AC generator. arate parts, namely: Control and monitoring of the electrical system is −...
Page 320 Aircraft Operations Manual ELECTRICAL Description In case of fire handle is pulled, the corresponding perature of 71C, thereby disconnecting the battery generator is de−energized by its GCU and discon- from its GEN BUS and the START BUS, indicated nected from the GEN BUS. by a BAT HOT light on the overhead panel.
Page 321 Aircraft Operations Manual ELECTRICAL Description − External power available. The batteries will be charged from respective GEN BUS when at least one generator is on line. − External power overvoltage relay not energized. The EXT PWR switch is provided with an electro- L/R Start Relay magnetic hold function which will hold the switch When the start relay is closed, the starter/generator...
Page 322 Aircraft Operations Manual ELECTRICAL Description position or in AUTO position with both generators RCCB will close and supply power to the UTILITY on line. BUS provided both generators are on line or exter- nal power is switched on. L/R MAIN START BUS relay The respective BAT BUS supplies the L/R MAIN When a MAIN START BUS relay is closed, it con- START BUS via its main start bus relay and L/R...
Page 323 Aircraft Operations Manual ELECTRICAL Description MAIN INV light on the overhead panel comes on. In variable between 460 to 600 Hz due to variations in this case, the standby inverter can be selected by propeller rpm. There is one AC generator installed placing the 26V inverter switch to STBY INV.
Page 324 Aircraft Operations Manual ELECTRICAL Description A31859 Fig. 1 Electrical power DC system − schematic PAGE Jun 01/19...
Page 325 Aircraft Operations Manual ELECTRICAL Description A31860 Fig. 2 Electrical power DC system − schematic PAGE Jun 01/19...
Page 326 Aircraft Operations Manual ELECTRICAL Description A31861 Fig. 3 Electrical power DC system − schematic PAGE Jun 01/19...
Page 327 Aircraft Operations Manual ELECTRICAL Description A31862 Fig. 4 Electrical power DC system − schematic PAGE Jun 01/19...
Page 328 Aircraft Operations Manual ELECTRICAL Description A31863 Fig. 5 Electrical power DC system − schematic PAGE Jun 01/19...
Page 329 Aircraft Operations Manual ELECTRICAL Description A31864 Fig. 6 Electrical power DC system − schematic PAGE Jun 01/19...
Page 330 Aircraft Operations Manual ELECTRICAL Description A31865 Fig. 7 Electrical power DC system − schematic PAGE Jun 01/19...
Page 331 Aircraft Operations Manual ELECTRICAL Description A31866 Fig. 8 Electrical power DC system − schematic PAGE Jun 01/19...
Page 332 Aircraft Operations Manual ELECTRICAL Description L INV BUS R INV BUS L INV BUS R INV BUS 115 VAC 115 VAC 26 VAC 26 VAC MAIN STBY MAIN INV Inverter 115V Inverter L MAIN R MAIN MAIN AND STANDBY INVETER SYSTEM L INV BUS R INV BUS L INV BUS...
Page 333 Aircraft Operations Manual ELECTRICAL Description A12678 Fig. 10 Wild frequency AC system − schematic PAGE Jun 01/19...
Page 334 Aircraft Operations Manual ELECTRICAL Description 2.10 ELECTRICAL POWER DISTRIBUTION LIST DC POWER L HOT BAT BUS R HOT BAT BUS − L engine fire extinguisher. − R engine fire extinguisher. − Cargo fire extinguisher. − R fire handle: HP, Bleed and Gen shut off. −...
Page 335 Aircraft Operations Manual ELECTRICAL Description L BAT BUS R BAT BUS − Emergency battery charging (JET PACK). − Fuel used indication (if installed). − Cabin pressurization control. − Outflow valve auto dump on ground. − Cabin pressure emergency dumping. − R pilot audio. −...
Page 336 Aircraft Operations Manual ELECTRICAL Description L BAT BUS (Cont’d) R BAT BUS (Cont’d) − L engine intake anti−ice control. − R prop, oil temp and press. indication. − L prop oil temp and press indication. − Propeller brake. − L propeller de−ice control. −...
Page 337 Aircraft Operations Manual ELECTRICAL Description L ESS BUS (Cont’d) R ESS BUS (Cont’d) − Propeller overspeed test. − R propeller speed (Np). − Warning annunciator system, channel 1 (with- − R BETA indication. out mod 2328). − R autocoarsen system. −...
Page 338 Aircraft Operations Manual ELECTRICAL Description L MAIN START BUS R MAIN START BUS − Instrument lighting left, center and center − Instrument lighting right. pedestal. − Logo lights (if installed). − Emergency light cabin (a/c 359−up). L AVIONIC BUS R AVIONIC BUS −...
Page 339 Aircraft Operations Manual ELECTRICAL Description ESS AVIONIC BUS UTILITY BUS − VOR/ILS/Marker 1 and VOR/ILS indicator. − Passenger reading lights. − ATC Transponder 1 − Lavatory water heater (if installed). (depending on national regulations). − R Galley fan light and liquid heater. −...
Page 340 Aircraft Operations Manual ELECTRICAL Description AC POWER L INV BUS 26 V AC R INV BUS 26 V AC − AHRS 1 compass reference. − AHRS 2 compass reference. − NAV 1 compass reference. − NAV 2 compass reference. − Boarding music (if installed and AC powered). L INV BUS 115 V AC R INV BUS 115 V AC −...
Page 341 Aircraft Operations Manual ELECTRICAL Description CONTROLS AND INDICATORS L/R BAT switch. Controls the battery relay connecting the battery to the START BUS and the respective GEN BUS/ OVRD − Battery thermal switch overridden and battery connected after a battery over− heat and subsequent relay opening, independent of EXT PWR switch posi−...
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Page 343 Aircraft Operations Manual ELECTRICAL Description ESS AVION switch. Connects: − The ESS AVIONIC BUS to the L ESS BUS. − The EMER AVIONIC BUS to the EMER BUS. L/R AVION switch. Connects: − The L/R AVIONIC BUS to the respective MAIN BUS.
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Page 345 Aircraft Operations Manual ELECTRICAL Description AC/DC PANEL AC ELEC DC ELEC DC AMP/VOLT indicator. Indicates the voltage for respective selected 26V MAIN/STBY switch. bus or source. If L or R GEN selected the indicator also shows current load in amperes. MAIN INV −...
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Page 347 Aircraft Operations Manual ELECTRICAL Description AC/DC PANEL AC ELEC DC ELEC DC AMP/VOLT indicator. INVERTER Indicates the voltage for respective selected inverter lIGHT (AMBER). bus or source. If L or R GEN selected the indicator also shows current load in amperes. Comes on if the selected inverter fails or the INVERTER INVERTER switch is in OFF position.
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Page 349 Aircraft Operations Manual ELECTRICAL Description TEST 2 PANEL TEST 2 PROP OVSP PWR L ENG OVSP AIR DATA EMER AHRS EFIS RUD LIM CAB PRESS L/R GEN OVV switches (for maintenance only). Test switches for the generator overvoltage circuit. NOTE: With Mod.
Page 350 Aircraft Operations Manual ELECTRICAL Description ELEC light (amber). The ELEC light will come on flashing whenever a caution light associated with the electrical system comes on. CENTRAL WARNING PANEL AUTO PITCH RUDDER COARSEN TRIM LIMIT L FIRE R FIRE FUEL ELEC DET FAIL DET FAIL...
Page 351 Aircraft Operations Manual ELECTRICAL Description L PL MIN T/O STANDARD (HIGHEST MODIFICATION STANDARD SHOWN) A11394 Fig. 16 Left side pilot circuit breaker panels − standard PAGE 31 Jun 01/19...
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Page 353 Aircraft Operations Manual ELECTRICAL Description RELAYS R PL MIN T/O STANDARD (HIGHEST MODIFICATION STANDARD SHOWN) A11182 Fig. 17 Right side pilot circuit breaker panels − standard PAGE 33 Jun 01/19...
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Page 355 Aircraft Operations Manual ELECTRICAL Description DATA AQUIS DATA AQUIS TAWS TAWS EXT 1 DATA TAWS AQUIS Applies to Mod. No. 3523. L PL MIN T/O / TOILET DATA MAX OPTION (HIGHEST MODIFICATION STANDARD SHOWN) A24784 Fig. 18 Left side pilot circuit breaker panels − max option PAGE 35 Jun 01/19...
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Page 357 Aircraft Operations Manual ELECTRICAL Description AUDIO BOARD TAWS MUSIC TERR NOISE CTL RECORD EXT 2 DISP RELAYS R PL MIN T/O SW ICE MAX OPTION (HIGHEST MODIFICATION STANDARD SHOWN) A30942 Fig. 19 Right side pilot circuit breaker panels − max option PAGE 37 Jun 01/19...
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Page 359 Aircraft Operations Manual ELECTRICAL Description ELECTRICAL POWER SUPPLY DC buses L essential/Left main ....K−9 L ESS L MAIN R essential/Right main ....S−7 R ESS R MAIN L avionic .
Page 360 Aircraft Operations Manual ELECTRICAL Description L essential bus ......K−12 L ESS R essential bus ..... . . S−9 R ESS L avionic bus .
Page 361 Aircraft Operations Manual ELECTRICAL Operation LIMITATIONS Unit Normal OPERATING LIMITS DC generators − Voltage ........V DC 27.5 −...
Page 362 Aircraft Operations Manual ELECTRICAL Operation NORMAL OPERATION CONDITIONS NORMAL PROCEDURES ELECTRICAL Battery power SYSTEM Circuit breakers ....... . CHECK POWER UP BATTERY...
Page 363 Aircraft Operations Manual ELECTRICAL Operation CONDITIONS NORMAL PROCEDURES ELECTRICAL External power SYSTEM POWER UP EXTERNAL- NOTE POWER 2.1 Battery power must be connected before applying External power. EXT PWR AVAIL light ......CHECK ON External power available is indicated by EXT PWR AVAIL light ON EXT PWR voltage...
Page 364 Aircraft Operations Manual ELECTRICAL Operation ABNORMAL OPERATION For Abnormal Operation, see section 23, ABNORMAL PROCEDURES and 24, EMERGENCY PROCEDURES. PAGE Apr 01/15...
Page 365 Aircraft Operations Manual EMERGENCY EQUIPMENT CONTENTS Location Spare bulbs and fuses 6/1.0 Highlights − not applicable 6/9.0 Highlights − not applicable 6/1.1 Description 6/9.1 Description 6/1.2 Operations − not applicable 6/9.2 Operations − not applicable Oxygen. Exits 6/2.0 Highlights − not applicable 6/2.1 Description 6/10.0...
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Page 367 Aircraft Operations Manual EMERGENCY EQUIPMENT Location LOCATIONS Cockpit escape hatch Life vests (2) Fire extinguisher (1) Escape strap Flash light (1) Oxygen mask (1) Smoke goggles (1) Life vest (1) Flash light (1) ( P. B. E. (1), when required) Oxygen mask (1) Ë...
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Page 369 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen GENERAL manually operated shut−off valve to a pressure reg- ulator which reduces pressure to 70 psi before it is The aircraft is equipped with one fixed oxygen sys- distributed to outlets. tem, plus portable oxygen bottles. Each outlet gives approx.
Page 370 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen The shut−off valve incorporated in the regulator assembly is controlled from the cockpit by a push− pull handle, located on the forward right side pan- el, adjacent to the oxygen pressure gauge. The handle has a green mark at the base, indicating open position.
Page 371 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen CONTROLS AND INDICATORS OXYGEN PRESSURE GAUGE Oxygen pressure gauge. Shows bottle pressure in psi. CENTRAL WARNING PANEL Oxygen (CWP) light. Comes on if oxygen pressure drops to 800 35 L FIRE R FIRE FUEL ELEC psi.
Page 372 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen Pilot oxygen outlet Oxygen on/off OXYGEN valve handle Observers oxygen Press outlet switch Press indicator LP relief Regulator Pressure OXYGEN BOTTLE and supply indicator valve Passen- Charging connect oxygen HP relief outlets Pilot oxygen outlet Supply line Passen- oxygen...
Page 373 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen There are three plug−in type oxygen outlets in The quick−donning masks are diluter/demand type the cockpit: one for each pilot, located behind and with mask mounted regulator and microphone. outboard of each pilot’s seat on the side panel; and Each mask is supplied with a red flow indicator one for the observer, located on the left side wall which disappears when oxygen is flowing.
Page 374 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen Flight Attendant Oxygen The flight attendant can be supplied with oxygen either by the large walk−around bottle (310 l) or by plugging the oxygen mask (full face smoke mask) into one of the fixed passenger outlets, or into the observer’s outlet if not occupied.
Page 375 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen PORTABLE OXYGEN The aircraft is provided with portable oxygen bottles. There are two sizes: large (310 L) and small (120 L). Number and locations vary with national regulations. Description The large (310 L) bottle is intended for crew walk− around and is the F/A primary choice of oxygen supply.
Page 376 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen Full−face mask Portable oxygen operation The mask has an on−demand regulator and an General instructions emergency selector; it also has a built−in−micro- − NO SMOKING sign ON phone which can be connected to the observers −...
Page 377 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen FIXED OXYGEN SYSTEM DISPATCH Oxygen temperature PRESSURE OXYGEN SUPPLY DURATION charts are pres- ented for −20 C (−4 F), 0 C (32 F), +20 C (+70 Oxygen dispatch pressure varies with the number F) and +40 C (+105 F) oxygen temperature and of oxygen masks (passenger and crew), number of the MINIMUM DISPATCH PRESSURE tables are fixed bottles, oxygen temperature, descent profile...
Page 378 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen FAR 121 DESCENT PROFILE ALTITUDE 1000 FEET 1 bottle / 4 outlets 30 MIN. OXYGEN SUPPLY TO 4 PASSENGERS. AOM0006 FLIGHT TIME − MINUTES Fig. 9 FAR 135 DESCENT PROFILE ALTITUDE 1000 FEET 3 bottles / 30 outlets 30 MIN.
Page 379 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen OXYGEN SUPPLY DURATION Basic 1 bottle system − 2 crew masks in OXYGEN LOW PRESSURE WARNING SUPPLY PRESSURE OXYGEN BOTTLES TEMPERATURE −PSI 1000 1100 1200 1300 −20_C (−4_F) 1400 +0_C (32_F) 1500 +20_C (70_F) 1600 +40_C (105_F) 1700...
Page 380 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen OXYGEN SUPPLY DURATION Optional 3 bottle system − 2 crew masks in use OXYGEN LOW PRESSURE WARNING SUPPLY PRESSURE −PSI OXYGEN BOTTLES TEMPERATURE 1000 1100 1200 1300 −20_C (−4_F) 1400 +0_C (32_F) 1500 +20_C (70_F) 1600 +40_C (105_F) 1700...
Page 381 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen NOTE All OXYGEN SUPPLY DURATION charts are based on oxygen selector in NORM position. MINIMUM DISPATCH PRESSURE tables use and 34 passenger oxygen masks. The dis- patch pressure covers both the FAR 121 and 135 These tables are presented for 3 system configura- descent profiles (Fig.
Page 382 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen MINIMUM DISPATCH PRESSURE (Cont’d) Optional 3 bottle system − 30 passengers masks installation 2 COCKPIT CREW Minimum Dispatch Pressure − PSI Outside Air Temperature _C No. of Pax −50 −40 −30 −20 −10 10 or Less 11−15 1030 1060...
Page 383 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen MINIMUM DISPATCH PRESSURE (Cont’d) Optional 3 bottle system − 34 passengers masks installation 2 COCKPIT CREW Minimum Dispatch Pressure − PSI Outside Air Temperature _C No. of Pax −50 −40 −30 −20 −10 10 or Less 11−15 1030 1060...
Page 384 Aircraft Operations Manual EMERGENCY EQUIPMENT Oxygen OXYGEN CONSUMPTION figures As an extra information to operators who want to compile their own dispatch pressure table or for op- erators with a different system layout, oxygen con- sumption figures per crew and passenger masks are given.
Page 385 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Lighting GENERAL F/A−button is not pushed to ON or cockpit switch is not in ON position. The emergency lighting system provides necessary − Manually, by selecting the cockpit switch to OFF interior and exterior lighting for a minimum of ten position, provided any Battery switch is in ON minutes.
Page 386 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Lighting FLASH LIGHTS Three flash lights are provided with the aircraft as Indicator lamp standard. Two are located in the cockpit, outboard of each pilot’s seat, and one in the cabin entrance area close to the F/A seat. The F/A flashlight has a small red light, which keeps blinking when the batteries are properly charged.
Page 387 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Lighting CONTROLS AND INDICATORS F/A SERVICE PANEL EMERGENCY CONTROL PANEL EMERG LIGHT switch. The emergency lights come on. EMERGENCY LIGHTS button (F/A button) ARMEDThe emergency lighting system is Emergency lights may be selected on and off by armed.
Page 388 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Lighting CENTRAL WARNING PANEL EMER LTS UNARMED light (amber) The light will come on when the EMER LIGHT switch is in OFF position. A9920 Fig. 3 Emergency lights unarmed indication 6/3.1 PAGE Apr 01/15...
Page 389 Aircraft Operations Manual EMERGENCY EQUIPMENT Fire fighting equipment GENERAL Halon fire extinguisher Fire−fighting equipment comprises hand fire extin- The Halon fire extinguishers contain Halon 1211 guishers and a fire axe. which can be used against all types of fires. Halon 1211 is a liquid chemical which, when ex- NOTE pelled from the nozzle, contains approx.
Page 390 Aircraft Operations Manual EMERGENCY EQUIPMENT Fire fighting equipment 0 fire extinguisher Avionic rack inlet Water is used against fires in textiles, paper etc. It The avionics rack is provided with a red rubber inlet must not be used against burning liquids and when for fire−fighting, located on the wall behind the left electricity is involved.
Page 391 Aircraft Operations Manual EMERGENCY EQUIPMENT PBE / Smoke Goggles PBE (Protective Breathing Equipment) Requirements are subject to national regulations. Where required, there will be one PBE close to each hand fire extinguisher installed. Type and operational procedures vary. For full de- scription contact your Flight Operations department.
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Page 393 Aircraft Operations Manual EMERGENCY EQUIPMENT Flotation equipment GENERAL − All flotation equipment must be readily available to all persons on board. − Number, type and locations vary with national regulations. − The crew should have their own life vests, lo- cated adjacent to each crew station.
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Page 395 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter GENERAL Deactivation The Emergency Locator Transmitter (ELT) facili- Should the ELT be inadvertently activated, gain ac- tates search and rescue in case of a crash landing. cess to the transmitter, set its front panel ON−OFF− It activates automatically on impact, transmitting on ARM switch to OFF, depress the RESET pushbut- civil as well as military aeronautical distress fre-...
Page 396 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter EMERGENCY PANEL ELT switch. Manual activation of ELT. ARMED Automatic activation of ELT by impact switch. A11112 Fig. 1 ELT − controls 6/7.1 A/C 160 −170 PAGE Apr 01/15...
Page 397 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter ELT external antenna Access panel to the ELT, in the cargo compartment EMERGENCY LOCATOR TRANSMITTER RESET button. When pressed the ELT selector in OFF position, the ELT is deactivated. ELT switch. Automatic use: Normal position. Automat- Blade antenna for portable operation.
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Page 399 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter GENERAL two−position (ON−ARMED) switch on the cockpit overhead EMERGENCY panel. The Emergency Locator Transmitter (ELT) facili- tates search and rescue in case of a crash landing. OPERATION It activates automatically on impact, transmitting on Automatic activation civil as well as military aeronautical distress fre- quencies (121.5 and 243 MHz).
Page 400 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter EMERGENCY PANEL ELT switch. Manual activation of ELT. ARMED Automatic activation of ELT by impact switch. A11112 Fig. 1 ELT − controls 6/7.1 A/C 171−299 PAGE Apr 01/15...
Page 401 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter ELT external antenna Access panel to the ELT, in the cargo compartment EMERGENCY LOCATOR TRANSMITTER ELT switch. AUTO Normal position. Automatic ac- tivation by impact switch or ac- tivation by remote switch. ELT is off.
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Page 403 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter GENERAL Manual activation The Emergency Locator Transmitter (ELT) facili- The ELT can be purposely activated by setting the tates search and rescue in case of a crash landing. ELT switch in cockpit to ON. It activates automatically on impact, transmitting on Deactivation civil as well as military aeronautical distress fre-...
Page 404 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter Activation indicator. ELT activation indicated by red flashing light. Transmission occurs after 30 se- conds. EMERGENCY PANEL RESET ELT switch. Manual activation of ELT. Transmission starts after 30 seconds. ARMED Automatic activation of ELT by impact switch.
Page 405 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter The ELT will flash in upside ELT external antenna position in water. Activation indicator. ELT activation indicated by red flashing light. Transmis- sion occurs after 30 se- Access panel to the ELT, in the cargo compartment conds.
Page 406 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter THIS PAGE INTENTIONALLY LEFT BLANK ! 6/7.1 A/C 300 − UP or with Mod. No. 2204 installed. PAGE Apr 01/15...
Page 407 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter GENERAL Manual activation The Emergency Locator Transmitter (ELT) facili- The ELT can be purposely activated by setting the tates search and rescue in case of a crash landing. ELT switch in cockpit to ON. It activates automatically on impact, transmitting on Deactivation civil as well as military aeronautical distress fre-...
Page 408 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter Activation indicator. ELT activation indicated by red flashing light. Transmission occurs after 2 seconds. EMERGENCY PANEL RESET ELT switch. Manual activation of ELT. Transmission starts after 2 seconds. ARMED Automatic activation of ELT by impact switch.
Page 409 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter ELT EXTERNAL ANTENNA Flexible Antenna. For portable use. ACCESS PANEL TO THE ELT, IN CARGO COMPARTMENT EMERGENCY LOCATOR TRANSMITTER Activation indicator. ELT activation indicated by red flashing light. Transmission occurs after 2 seconds. AUTO RESET ELT switch.
Page 410 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter THIS PAGE INTENTIONALLY LEFT BLANK ! 6/7.1 With Mod No 3112 installed (Air Precision ELT) PAGE Apr 01/15...
Page 411 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter EMERGENCY LOCATOR TRANSMITTER Automatic activation The Emergency Locator Transmitter (ELT) is acti- For normal operation, the switch in the cockpit shall vated automatically on impact, transmitting on be in the ARMED position, and the switch on the 121.5, 243 and 406.25 MHz.
Page 412 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter Activation indicator ELT activation indicated by red flashing light. Transmission on 121.5 and 243 MHz starts upon activation and after 47 seconds on 406.25 MHz. EMERGENCY PANEL RESET ELT switch − Manual activation of ELT. Transmission on 121.5 and 243 MHz starts upon activation and after 47 seconds on 406.25 MHz.
Page 413 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter ELT external antenna Access panel to the ELT, in the cargo compartment Activation indicator. ELT activation indicated by red flashing light. Transmission on 121.5 and 243 MHz starts upon activation and after 47 seconds on 406.25 MHz.
Page 414 Aircraft Operations Manual EMERGENCY EQUIPMENT Emergency Locator Transmitter THIS PAGE INTENTIONALLY LEFT BLANK ! 6/7.1 Applicable for A/C with mod. 3504 (Artex ELT C406−1) PAGE Apr 01/15...
Page 415 Aircraft Operations Manual EMERGENCY EQUIPMENT First Aid Kit FIRST AID KIT First Aid Kit(s) is provided with the aircraft as stan- dard. It is located in the galley/entrance area and contains the following: Qty: 1 ”x3” plastic adhesive bandage (16 per unit) PVP iodine swabs (10 per unit) Ammonia inhalants...
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Page 417 Aircraft Operations Manual EMERGENCY EQUIPMENT Spare bulbs and fuses SPARE BULBS AND FUSES Two boxes, located in the cockpit L and R lower side panels respectively, contain spare bulbs and fuses as well as padlocks for external door locking. A11154 Fig.
Page 418 Aircraft Operations Manual EMERGENCY EQUIPMENT Spare bulbs and fuses THIS PAGE INTENTIONALLY LEFT BLANK ! 6/9.1 PAGE Apr 01/15...
Page 419 Aircraft Operations Manual EMERGENCY EQUIPMENT Exits GENERAL MAIN DOOR WARNING NOTE All crew members should receive adequate train- If the main door handle has been inadvertently ing in the handling of emergency exits and evac- moved to the closed position with the door open, a uation procedures.
Page 420 Aircraft Operations Manual EMERGENCY EQUIPMENT Exits CAUTION The main door will swing open if the door is un- locked and the cabin happens to be pressurized. Overcentering index window (closed position shown) Internal Door Handle Check centered prior flight Plastic Roller Latch Shoot bolt index window Shoot bolt...
Page 421 Aircraft Operations Manual EMERGENCY EQUIPMENT Exits FORWARD RIGHT and OVERWING EXITS Operation General NOTE Forward right and Overwing exits have identical Forward right exit outside handle is located on handles and are operated the same way from in- the bottom of the hatch. side.
Page 422 Aircraft Operations Manual EMERGENCY EQUIPMENT Exits COCKPIT ESCAPE HATCH Closed Ventilation General Open A removable hatch is installed in the cockpit ceiling to facilitate flight crew evacuation, should the door between cockpit and cabin be obstructed or should there be no suitable forward exit. This hatch can also be used for ventilation on ground, or for smoke evacuation in flight.
Page 423 Aircraft Operations Manual EMERGENCY EQUIPMENT Exits CARGO DOOR For inside operation there is a handle stowed in the cargo compartment. NOTE From a/c 260 and up there is no handle for door The cargo door is not to be considered as an emer- inside operation.
Page 424 Aircraft Operations Manual EMERGENCY EQUIPMENT Exits STAIR − push stair into parked position Release pedal.. The aircraft is equipped with a built−in folding stair Release to fold the stairs. at the main door. When not in use, the stair is folded and slid along a rail to its stowed position forward of the main door.
Page 425 Aircraft Operations Manual FIRE PROTECTION CONTENTS Fire Protection Highlights − not applicable Description Operation −CONTENTS PAGE Apr 01/15...
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Page 427 Aircraft Operations Manual FIRE PROTECTION Description GENERAL steady. The CWP light remains on as long as the caution condition exists. The fire protection system provides: The engine fire warning and detector failure system − Fire detection of the engines plus an extinguisher can be tested with two switches on the TEST 1 system.
Page 428 Aircraft Operations Manual FIRE PROTECTION Description single detector is enough to initiate an overheat TEST 1 panel. When activated, smoke conditions in warning. all compartments are simulated and all warnings activated. Applicable to a/c with mod. 3400/3401 Cargo compartment fire extinguisher There is one pneumatic detector for each engine system tailpipe.
Page 429 Aircraft Operations Manual FIRE PROTECTION Description Optional cargo compartment fire extin- guisher system An optional extinguisher system, identical to the standard system, may be installed on the left side of the cargo compartment. Like the standard system, the extinguisher is dis- charged in two stages, the first with rapid flooding and the second with a slower regulated flow.
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Page 431 Aircraft Operations Manual FIRE PROTECTION Description Triple chimes A11992 Fig. 1 Engine fire protection and exhaust duct overtemperature system Applicable to aircraft without Mod. No. 3400/3401 installed. PAGE Jun 01/20...
Page 432 Aircraft Operations Manual FIRE PROTECTION Description THIS PAGE INTENTIONALLY LEFT BLANK ! Applicable to aircraft without Mod. No. 3400/3401 installed. PAGE Apr 01/15...
Page 433 Aircraft Operations Manual FIRE PROTECTION Description TRIPLE CHIMES MASTER FLASHING WARNING L TAIL P FLASHING TAIL PIPE OVERTEMP SENSOR LOOP OVERTEMP TEST SIGNAL FIRE LOOP FIRE TEST FIRE FIRE SHORT CONTROL DETECTOR UNIT FAILURE TEST TEST 1 PANEL FIRE WARNING DETECTOR FAILURE FIRE BELL SINGLE CHIMES...
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Page 435 Aircraft Operations Manual FIRE PROTECTION Description Pressure gauge A11993 Fig. 2 Engine fire extinguishing system PAGE Apr 01/15...
Page 436 Aircraft Operations Manual FIRE PROTECTION Description Repetitive chimes Flashing MASTER WARNING AVIONIC SMOKE flashing SMOKE CARGO SMOKE Smoke signal Avionic smoke sensor TEST 1 PANEL SMOKE Test signals Lavatory smoke sensor NOTE Cargo smoke With Mod. No. 1819 sensor installed there are two smoke sensors in the cargo comparatment.
Page 437 Aircraft Operations Manual FIRE PROTECTION Description CONTROLS AND INDICATORS FIRE EXTG discharge switch (2) When an extinguishing discharge switch is moved from OFF after the engine fire handle has been pulled for the same side, the main extinguishant bottle is discharged to that engine.
Page 438 Aircraft Operations Manual FIRE PROTECTION Description L/R ENG FIRE light (red) Comes on flashing for an engine fire condition.The light will remain on as long as the fire exists. CENTRAL WARNING PANEL AVIONIC/LAV/CARGO SMOKE light (red) A light comes on to indicate a smoke condi- L ENG AVIONIC R ENG...
Page 439 Aircraft Operations Manual FIRE PROTECTION Description Smoke test switch. When activated, smoke conditions in the avionics compartment, lavatory and cargo comparments are simulated. The smoke test warnings are: − MASTER WARNING lights. − AVIONIC, LAV and CARGO SMOKE lights. − Repetitive chime. FIRE test switch.
Page 440 Aircraft Operations Manual FIRE PROTECTION Description A11994 Fig. 7 Fire protection − controls and indicators PAGE Apr 01/15...
Page 441 Aircraft Operations Manual FIRE PROTECTION Description ELECTRICAL POWER SUPPLY Detection. Left engine ....... . EMER BUS E−1 L ENG FIRE...
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Page 443 Aircraft Operations Manual FIRE PROTECTION Operation LIMITATIONS Not applicable NORMAL OPERATION CONDITIONS NORMAL PROCEDURES SYSTEM TEST Fire handles & extinguishers ..... CHKD −...
Page 444 Aircraft Operations Manual FIRE PROTECTION Operation ABNORMAL OPERATION For Abnormal Operation, see section 23, ABNORMAL PROCEDURES and 24, EMERGENCY PROCEDURES. PAGE Apr 01/15...
Page 445 Aircraft Operations Manual FLIGHT CONTROLS CONTENTS Flight Controls Highlights − not applicable Description Operation −CONTENTS PAGE Apr 01/15...
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Page 447 Aircraft Operations Manual FLIGHT CONTROLS Description GENERAL Geared tabs are used with the elevator and aileron systems while a spring tab is used with the rudder The flight controls are divided into two groups: system. − Primary flight controls consisting of elevators, The geared tabs deflect proportionally to control ailerons and rudder.
Page 448 Aircraft Operations Manual FLIGHT CONTROLS Description MAIN COMPONENTS AND SUBSYSTEMS from each other. If the handle is not pulled the dis- connect function is automatically reset when the Ailerons excessive control force no longer is applied. Each aileron is hinged to the wing trailing edge at After the handle has been pulled, disconnection is two points.
Page 449 Aircraft Operations Manual FLIGHT CONTROLS Description The autopilot rudder servo drive is mechanically To prevent flap damage due to excessive air loads, linked to the rudder control system. a blow−back protection is incorporated in the hy- draulic system. Rudder Limiter System There are four handle ”detents”, designated, 7, 15, The rudder control system includes a rudder limiter 20 and 35, respectively.
Page 450 Aircraft Operations Manual FLIGHT CONTROLS Description The gust lock handle also controls the following Standby pitch trim also deactivates the synchro- electrical functions. nization. In this case it can be reset with the PITCH RESET switch on the trim switch panel. With the gust lock engaged the following is pos- sible: With the pitch trim synchronization deactivated both...
Page 451 Aircraft Operations Manual FLIGHT CONTROLS Description CONTROLS AND INDICATORS FLAP POSITION INDICATOR Flap position indicator. FLAPS Dual pointers (L and R) indicate position of left and right flaps. FLAP HANDLE GUSTLOCK RELEASE FRICTION Flap handle. Used to select flap positions as indicated on the handle placard.
Page 452 Aircraft Operations Manual FLIGHT CONTROLS Description Gust lock handle. Moving the gust lock handle fully aft locks the elevators and the ailerons mechanically and the rudder electrically. When engaged, the movement of the power levers is limited Gust lock release knob. by a stop on the gust lock handle.
Page 453 Aircraft Operations Manual FLIGHT CONTROLS Description LCD Trim indicator. Displays trim tab deflection for pitch, roll and yaw. The indicator shows trim tab deflection for both main and LCD TRIM INDICATOR standby systems in units. (Mod No. 2949) Green band indicates takeoff range. MAIN STBY At power up, the built in test will illuminate all segments...
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Page 455 Aircraft Operations Manual FLIGHT CONTROLS Description CENTRAL WARNING PANEL PITCH TRIM light (amber). CONFIG light (red). The PITCH TRIM lights comes on when The CONFIG light comes on when apply- pitch trim synchronization is deactivated. L ENG AVIONIC R ENG ing take−off power on ground for: FIRE SMOKE...
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Page 457 Aircraft Operations Manual FLIGHT CONTROLS Description RUDDER LIMIT OVERRIDE SWITCH ALTERNATE LOCATION CENTER PEDESTAL RIGHT SIDE PANEL RUD LIM OVRD OVRD NORM NORM Rudder limiter override switch. With the switch in OVRD position, the rudder limit mechanism is retracted thus enabling full range of movement for the rudder.
Page 458 Aircraft Operations Manual FLIGHT CONTROLS Description ELECTRICAL POWER SUPPLY Flap indicator ......R BAT BUS N−8 FLAP IND Flap control .
Page 459 Aircraft Operations Manual FLIGHT CONTROLS Operation LIMITATIONS OPERATING LIMITS − Max speed for flap extension ......See section 27.
Page 460 Aircraft Operations Manual FLIGHT CONTROLS Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Actuate both STBY ROLL trim switches on pedestal to L and R positions and check STBY ROLL trim indicator to move towards corresponding posi- tions. Reset to 0. − Check that STBY ROLL trim can not be operated by just one switch. Actuate both YAW trim switches on pedestal to L and R positions and check YAW trim indicator to move towards corresponding positions.
Page 461 Aircraft Operations Manual FLIGHT CONTROLS Operation CONDITIONS NORMAL PROCEDURES RUDDER The following test is required by AMM section 27−22−25−2 Rudder Trim SUBTAB TRIM Tab / Procedure 1 − Adjust Rudder Sub Tab. CURVES TEST Flight conditions and aircraft configuration: Altitude: According to Table 201 in referenced AMM section.
Page 462 Aircraft Operations Manual FLIGHT CONTROLS Operation ABNORMAL OPERATION For Abnormal Operation, also see section 23, ABNORMAL PROCE- DURES and 24, EMERGENCY PROCEDURES CONDITIONS ABNORMAL PROCEDURES FLIGHT It is of utmost importance that a thorough and professional trouble shooting is per- CONTROL formed whenever an irregular or abnormal function the flight controls has oc- MALFUNC-...
Page 463 Aircraft Operations Manual FUEL CONTENTS Fuel 9/1.0 Highlights 9/1.1 Description 9/1.2 Operation Fueling instruction 9/2.0 Highlights 9/2.1 Description 9/2.2 Operation −CONTENTS PAGE Apr 01/15...
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Page 465 Aircraft Operations Manual FUEL Highlights MODIFICATION STANDARD The system described in this chapter assumes a certain modification standard of the aircraft. If a modification is not installed, the following apply as a complement to what is stated in this chapter. DESCRIPTION/OPERATION FUEL test switch Without Mod No 2091 embodied, the fuel quantity...
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Page 467 Aircraft Operations Manual FUEL Description GENERAL pump in each tank. The standby pump starts auto- matically by a pressure switch in case of a main Fuel is stored in two tanks, referred to as the left pump failure. The standby pumps are also used for and the right tank.
Page 468 Aircraft Operations Manual FUEL Description MAIN COMPONENTS AND SUBSYSTEMS cated inside the inboard tank cells. The outboard cells are replenished by overflow through the vent line from the inboard cells. Fuel storage Optical sensors are used to determine mid−level Each fuel tank consists of two cells, integral with and full level.
Page 469 Aircraft Operations Manual FUEL Description the overhead fuel panel indicates the condition. will activate the master caution, L/R LOW LEVEL Pressure relief valves in the shutoff valve and the light on the overhead panel and FUEL (CWP) light. suction check valves protect the feed line from ex- Mechanical quantity indication cessive pressure due to thermal expansion when There is a magnetic dipstick in each inboard tank...
Page 470 Aircraft Operations Manual FUEL Description CONTROLS AND INDICATORS Quantity placard (option). Located adjacent to the magnetic dipstick. Magnetic dipstick. Fuel tank drain valve. Graduation in inches. Use a coin or a screwdriv- To open: er to release the dipstick. Pull the dipstick down Use a fuel drain tool, turn fuel drain valve coun- and then push it up until it engages magnetically terclockwise to unlock the valve.
Page 471 Aircraft Operations Manual FUEL Description STANDBY PUMP DIFFERENTIAL PRESSURE SWITCH MAIN PUMP DIFFERENTIAL PRESSURE SWITCH A11644 Fig. 4 Fuel system − schematic 9/1.1 PAGE Apr 01/15...
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Page 473 Aircraft Operations Manual FUEL Description XFEED L VALVE R VALVE CLOSED CLOSED L FUEL R FUEL FILTER FILTER Â Â Â Â Â Â L MAIN R MAIN PUMP PUMP L STBY R STBY PRESS PRESS L LOW R LOW LEVEL LEVEL Engine feed...
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Page 475 Aircraft Operations Manual FUEL Description FUEL QUANTITY INDICATORS Fuel flow and fuel quantity indication either in lb or kg (option). BAT FUEL TEMP PANEL Temperature display. Indicates FUEL TEMP as selected by the switch. At UPR lamp test, the digital display will show +88.
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Page 477 Aircraft Operations Manual FUEL Description XFEED ON light (amber). Comes on when the crossfeed is open. L/R VALVE CLOSED light (amber). Comes on when the fire shutoff valve is closed. FUEL CONTROL PANEL L/R FUEL FILTER light (amber). Comes on if the fuel filter becomes clogged and L/R MAIN PUMP light (amber).
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Page 479 Aircraft Operations Manual FUEL Description FUEL test switch. L − Left fuel quantity indicators shows ; without mod. 2091: 950 " 50 lb (432 " 23 kg) with mod. 2091: 1000 " 50 lb (455 " 23 kg) Left fuel flow indicator shows 760 " 35 lb/h or TEST 1 PANEL 345 "...
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Page 481 Aircraft Operations Manual FUEL Description ELECTRICAL POWER SUPPLY Standby pumps and control Left standby pump power ....L BAT BUS J−16 L STBY PUMP PWR Left standby pump control .
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Page 483 Aircraft Operations Manual FUEL Operation LIMITATIONS Unit Normal OPERATING LIMITS − Minimum fuel for takeoff, each tank ....− − − − − Maximum unbalance between tanks ....−...
Page 484 Aircraft Operations Manual FUEL Operation NORMAL OPERATION CONDITIONS NORMAL PROCEDURES CROSS FEED Crossfeed valve test VALVE AND IN- XFEED switch ........TERCONNECT VALVE TEST −...
Page 485 Aircraft Operations Manual FUEL Operation CONDITIONS NORMAL PROCEDURES (Cont’d) XFEED switch ........−...
Page 486 Aircraft Operations Manual FUEL Operation ABNORMAL OPERATION For Abnormal Operation, see section 23, ABNORMAL PROCEDURES. 9/1.2 PAGE Apr 01/15...
Page 487 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Highlights MODIFICATION STANDARD The system described in this chapter assumes a certain modification standard of the aircraft. If a modification is not installed, the following apply as a complement to what is stated in this chapter. DESCRIPTION/OPERATION IND TEST button Without Mod No 2091 embodied, the fuel quantity...
Page 488 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Highlights THIS PAGE INTENTIONALLY LEFT BLANK ! 9/2.0 PAGE Apr 01/15...
Page 489 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Description GENERAL For system description see FUEL 9/1.1 Fuel quantity indicators. Shows fuel quantities in pounds or kilograms. MAIN COMPONENTS AND SUBSYSTEMS Not applicable. OVERFULL light (red). Light on indicates that the level in the corresponding Pressure fueling receptacle.
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Page 491 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Description Fuel additive blender Handle Trigger Hold additive upright during blending Blender tube with nozzle attachment Fuel nozzle A12401 Fig. 2 Fuel additive blender 9/2.1 PAGE Apr 01/15...
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Page 493 General Electric’s Specification No. D50TF2 are approved for use in all General Electric CT7 engines and in the Saab 340 aircraft. Approved fuel types and additives are listed in General Electric Ser- vice Bulletin 73−0048 R00 Engine−Fuel System (73−00−00) − Fuel and Additive Requirements. The GE SB also includes special conditions for use of other fuel types such as CIS and Ukraine TS−1.
Page 494 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation (Cont’d) Kerosene fuels − JET−A freezing point − 40F or −40C. − JET−A1, JP5 freezing point − 53F or −47C. − JP8, freezing point − 58F or −50C. Specification: IATA Guidance Material for Aviation Turbine Fuels, Addendum 76−1. Equivalent specifications: Canada CAN 2−3.23 (3−GP−24) France AIR 3405...
Page 495 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation NORMAL OPERATION CONDITIONS NORMAL PROCEDURES GENERAL For general fueling safety regulations, refer to the appropriate national regula- tions. Smoking, use of open fire or any activity that can cause sparks are not per- mitted in the fueling area.
Page 496 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) In cockpit Overhead fuel panel ......CHECK −...
Page 497 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Order fueling to start. Monitor the fueling. − If an OVERFULL light comes on, set the fueling control switches to OFF and stop the fueling. Investigate. When correct fuel quantity is reached Fueling control switches .
Page 498 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Fueling access door ......OPEN −...
Page 499 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) Clearance aircraft/ground equipment ....CHECK − The change in fuel load may change the landing gear shock strut exten- sion.
Page 500 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) DE−FUEL switch ......CLOSE In cockpit L/R STBY PUMP switch...
Page 501 Aircraft Operations Manual FUEL, FUELING INSTRUCTION Operation CONDITIONS NORMAL PROCEDURES BLENDING This procedure can only be used in conjunction with procedure 2.3, GRAVITY WITH ANTI− FUELING, when anti−icing additive is required and pre−blended fuel is not ICING available. ADDITIVE The procedure is applicable to Hi−Flo Prist blender model PHF.204, using Hi− Flo Prist additive manufactured by PPF Industries Inc., Pittsburg PA, USA.
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Page 503 Aircraft Operations Manual HYDRAULICS CONTENTS Hydraulics 10.0 Highlights − not applicable 10.1 Description 10.2 Operation −CONTENTS PAGE Apr 01/15...
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Page 505 Aircraft Operations Manual HYDRAULICS Description GENERAL cubic inches (2.5 liters) and is filled through a gravi- ty fill port. Overflow from the main reservoir relief Hydraulic power is used to operate the following valve and bleed valve is also directed into this res- aircraft systems: ervoir.
Page 506 Aircraft Operations Manual HYDRAULICS Description Hand pump selector As the hand pump does not have the capacity to simultaneously operate all systems, a selector valve is installed. The valve allows pressure to be di- rected to the following accumulators, one at a time: −...
Page 507 Aircraft Operations Manual HYDRAULICS Description Gear emergency uplock actuator actuator Return A11221 Fig. 1 Hydraulic system − schematic 10.1 PAGE 3 Apr 01/15...
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Page 509 Aircraft Operations Manual HYDRAULICS Description CONTROLS AND INDICATORS HYD QTY indicator. Indicates fluid quantity in the main reservoir. HYDRAULIC PANEL HYDR PUMP switch − OVRD (override) The pump runs continuously. − AUTO The pump will operate during the following con- ditions: _ If main hydraulic pressure falls below 2100 psi and until pressure reaches 2900 psi.
Page 510 Aircraft Operations Manual HYDRAULICS Description HYDR caution light (amber) Comes on to indicate low hydraulic pressure in any of the hydraulic accumulators or high tem- perature of the fluid in the main reservoir. CENTRAL WARNING PANEL L FIRE R FIRE FUEL ELEC DET FAIL...
Page 511 Aircraft Operations Manual HYDRAULICS Description ELECTRICAL POWER SUPPLY Hydraulic pump power ....L GEN BUS No CB, protected by a 200 amp fuse in the L PDU.
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Page 513 Aircraft Operations Manual HYDRAULICS Operation LIMITATIONS Unit Normal OPERATING LIMITS Pressure − Electrical pump AUTO ....2050 2100−2900 2950 − Electrical pump OVRD ....−...
Page 514 Aircraft Operations Manual HYDRAULICS Operation NORMAL OPERATION CONDITIONS NORMAL PROCEDURES OPERATION OF Before engine start HYDRAULIC HYDR PUMP switch ......AUTO SYSTEM −...
Page 515 Aircraft Operations Manual HYDRAULICS Operation ABNORMAL OPERATION For Abnormal Operation, also see section 23, ABNORMAL PROCED- URES. CONDITIONS ABNORMAL PROCEDURES HYDRAULIC INDICATIONS PRESSURE − Hydraulic pressure above 3 000 psi on all four hydraulic pressure indica- HIGH tors. NOTE The hydraulic system pressure relief valve will open at 3 750 psi (in main sys- tem).
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Page 517 Aircraft Operations Manual ICE & RAIN PROTECTION CONTENTS Ice & Rain Protection 11.0 Highlights − not applicable 11.1 Description 11.2 Operation −CONTENTS PAGE Apr 01/15...
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Page 519 Aircraft Operations Manual ICE AND RAIN PROTECTION Description GENERAL for ice and rain protection. Bleed air is used for the wing and stabilizer inflatable boots, the engine split The aircraft is fully equipped for all−weather opera- lip and inlet guide vanes. Electrical power is used tion.
Page 520 Aircraft Operations Manual ICE AND RAIN PROTECTION Description MAIN COMPONENTS AND SUBSYSTEMS NOTE On a/c s/n 240−up (post Mod 2083) the regu- Wing and stabilizer (boot) de−ice lated pressure is directed to a distribution duct Wing and stabilizer de−icing is provided by conven- supplying all boots through five ejector flow con- tional inflatable boots located on the wing and lead- trol valves.
Page 521 Aircraft Operations Manual ICE AND RAIN PROTECTION Description − Pressure remains on in Left and Right inboard valve ported to the Splitter Lip, the inlet guide vanes wing or Left and Right outboard wing boot zones and the Inlet Particle Separator Ejector Duct. When after more than 8 seconds.
Page 522 Aircraft Operations Manual ICE AND RAIN PROTECTION Description 2.2.3 Upper and Lower Duct (Applicable to A/C with COX intakes  one back−up sensor (with mod no. 2095 installed)  one primary and one back−up sensor The upper duct and the lower duct, including the particle separator and exhaust nozzle, are each in one duct section (upper or lower) provided with four thin film resistor type temperature...
Page 523 Aircraft Operations Manual ICE AND RAIN PROTECTION Description − The L/R PROP DE−ICE lights (blue) on the flight Windshield heating (Fig. 4) status panel which will come on when the system The front windshields and the forward part of the is working and will go out in case of system fail- side windshields are electrically heated from the ure.
Page 524 Aircraft Operations Manual ICE AND RAIN PROTECTION Description NORM power will be applied whenever the aircraft Ice detector is on ground (WOW, weight on wheels switches (Optional Mod No. 1933) sensing ground mode). The ice detector consists of an ultrasonic axially A/C 300−UP vibrating tube as sensing element.
Page 525 (This modification is mandatory for Canadian registrated aircraft). For description see Supplement 37/3. 2.10 Improved Stall Warning System for icing conditions (Mod. no. 3529 for 340B / 3530 for 340WT) For description see Section 19 WARNING AND CAUTIONS, STALL WARNING.
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Page 527 Aircraft Operations Manual ICE AND RAIN PROTECTION Description CONTROLS AND INDICATORS 28VDC POWER Left side distribution valve 28VDC POWER Left side overheat sensor Inboard boots Inboard boots Left side shut off 28VDC valve POWER 28VDC CONTROL Outboard boots Outboard boots POWER TIMER Distribution duct...
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Page 529 Aircraft Operations Manual ICE AND RAIN PROTECTION Description Heating failure L 115 VAC GEN BUS PROPELLER signal L PROP R PROP To RAC GEN Switch L PROP R PROP É É É É NORM É É Control power Power to heating boots É...
Page 530 Aircraft Operations Manual ICE AND RAIN PROTECTION Description THIS PAGE INTENTIONALLY LEFT BLANK ! 11.1 This page is applicable to aircraft with LUCAS intake. PAGE Without Mod No 2095 and without Mod. No. 3529 or 3530 Jun 01/17...
Page 531 Aircraft Operations Manual ICE AND RAIN PROTECTION Description PROPELLER Heating failure signal L PROP R PROP L 115 VAC GEN BUS L PROP R PROP To RAC GEN Switch É É NORM É É Control power É É É É 28 VDC Norm Power to heating boots...
Page 532 Aircraft Operations Manual ICE AND RAIN PROTECTION Description THIS PAGE INTENTIONALLY LEFT BLANK ! 11.1 This page is applicable to aircraft with LUCAS intake. PAGE Without Mod No 2095 and with Mod. No. 3529 or 3530 Jun 01/17...
Page 533 Aircraft Operations Manual ICE AND RAIN PROTECTION Description Heating failure L 115 VAC GEN BUS PROPELLER signal L PROP R PROP To RAC GEN Switch L PROP R PROP É É É É NORM É É Control power Power to heating boots É...
Page 534 Aircraft Operations Manual ICE AND RAIN PROTECTION Description THIS PAGE INTENTIONALLY LEFT BLANK ! 11.1 This page is applicable to aircraft with COX intake. PAGE With Mod no 2095 and without Mod. No. 3529 or 3530. Jun 01/17...
Page 535 Aircraft Operations Manual ICE AND RAIN PROTECTION Description Heating failure L 115 VAC GEN BUS PROPELLER signal L PROP R PROP To RAC GEN Switch L PROP R PROP É É É É NORM É É Control power Power to heating boots (A) FI STOP É...
Page 536 Aircraft Operations Manual ICE AND RAIN PROTECTION Description THIS PAGE INTENTIONALLY LEFT BLANK ! 11.1 This page is applicable to aircraft with COX intake. PAGE With Mod no 2095 and with Mod. No. 3529 or 3530. Jun 01/17...
Page 537 Aircraft Operations Manual ICE AND RAIN PROTECTION Description L Bat Bus R Bat Bus L Bat Bus R Bat Bus Gen Bus Gen Bus Gen Bus Gen Bus A9913 Fig. 4 Window heat − schematic 11.1 A/C 160−299 PAGE Jun 01/17...
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Page 539 Aircraft Operations Manual ICE AND RAIN PROTECTION Description L Bat Bus R Bat Bus L Bat Bus R Bat Bus Gen Bus Gen Bus Gen Bus Gen Bus A11029 Fig. 4 Window heat − schematic 11.1 A/C 300 − up PAGE Jun01/17...
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Page 541 Aircraft Operations Manual ICE AND RAIN PROTECTION Description 28 VDC 28 VDC Ice detector optional (Mod No 1933) Right angle Left angle of attack of attack Right pitot Windshield wipers Standby pitot Left pitot Temperature probe RW o W Switch R 115VAC L 115VAC GEN BUS...
Page 542 Aircraft Operations Manual ICE AND RAIN PROTECTION Description Timer light (amber). Will come on if: − no pressure is sensed downstream the valve sequenced for opening within 4 seconds. − the activated timer gives no inflation signal. − the boots are not cycling. −...
Page 543 Aircraft Operations Manual ICE AND RAIN PROTECTION Description L/R INTAKE light (amber). Will come on for a failure in the engine duct electrical anti−icing systems. L/R AIR light (amber). Will come on under the following conditions: − If the Electronic Solenoid Valve does not open when respective ENGINE anti−ice switch is turned ON.
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Page 545 Aircraft Operations Manual ICE AND RAIN PROTECTION Description L/R SIDE/FRONT light (amber). Will come on when an overheat or controller fault occurs. PROPELLER AND WINDSHIELD DE−ICE PANEL L/R FRONT windshield heating switch. Regulated power is applied to front windshield when set to ON. L/R PROP light (ambers).
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Page 547 Aircraft Operations Manual ICE AND RAIN PROTECTION Description L/R SIDE/FRONT light (amber). Will come on when an overheat or controller fault occurs. PROPELLER AND WINDSHIELD DE−ICE PANEL L/R FRONT windshield heating switch. Regulated power is applied to front windshield when set to ON. L/R PROP light (ambers).
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Page 549 Aircraft Operations Manual ICE AND RAIN PROTECTION Description WINDSHIELD WIPER PANEL EFIS WIPER PARK DRIVE XFR XSIDE DATA ADI REV HSI REV Wiper rotary switch PARK Wiper is returned to stowed position. Wiper stops in present positon. Wiper operates at low speed. HIGH Wiper operates at high speed.
Page 550 Aircraft Operations Manual ICE AND RAIN PROTECTION Description CENTRAL WARNING PANEL ICE PROT light (amber) The ICE PROT light will come on flashing whenever a caution light associated with the ice protectin system comes on. A9920 Fig. 10 Ice and rain protection master caution −controls and indicators 11.1 PAGE Jun01/17...
Page 551 Aircraft Operations Manual ICE AND RAIN PROTECTION Description A SIDE PANEL ICE DETECTOR switch Optional Mod No 1933 TEST− Self test of the ice detector mi- cro−processor. Flashing of the L and R ENG ANTI−ICE blue sta- tus light within 5 seconds while the switch is hold in TEST posi- tion is a confirmation of a suc- cessful selftest.
Page 552 Aircraft Operations Manual ICE AND RAIN PROTECTION Description B CENTER INSTRUMENT PANEL SIDE PANEL ICE COND indication light (white) Optional Mod No 3168 The ice detection indication light comes on if the ice detector senses ice. ICE DETECTOR switch Optional Mod No 3168 TEST−...
Page 553 Aircraft Operations Manual ICE AND RAIN PROTECTION Description CENTER INSTRUMENT PANEL L BETA L PROP DE−ICE L ENG ANTI−ICE ICE SPD L APR ON/OFF pushbutton L IGN ICE SPD A14690 Fig. 13 ICE SPD button (Option Mod No 2650) 11.1 PAGE Jun01/17...
Page 554 Aircraft Operations Manual ICE AND RAIN PROTECTION Description ELECTRICAL POWER SUPPLY Wing and stabilizer de−ice Timer control ... . . L BAT BUS K−21 STAB & WING AUTO CTL Shutoff valves ... . . R BAT BUS S−21 STAB &...
Page 555 Aircraft Operations Manual ICE AND RAIN PROTECTION Description Windshield heat L front PWR Ø A ....L 115 VAC GEN BUS J−23 PWR Ø A PWR Ø...
Page 556 Aircraft Operations Manual ICE AND RAIN PROTECTION Description (Cont’d) Ice detector with Mod No 1933 and 2546 ..R 115 VAC GEN BUS Ice detector with Mod No 3168 ... . . R 115 VAC GEN BUS Not in cockpit Improved S/W system...
Page 557 Aircraft Operations Manual ICE AND RAIN PROTECTION Description Windshield heat L front PWR Ø A ....L 115 VAC GEN BUS J−23 PWR Ø A PWR Ø...
Page 558 Aircraft Operations Manual ICE AND RAIN PROTECTION Description (Cont’d) Ice detector with Mod No 3168 ... . . R 115 VAC GEN BUS Not in cockpit Improved S/W system Mod No 3529 or 3530 ..R BAT BUS S−28 ICE SPD IND...
Page 559 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation LIMITATIONS Unit Normal SYSTEM LIMITS − Windshield heating  Switching side windows direct from OFF to HIGH is not authorized  Time in NORM before switching to HIGH − Pitot tubes  Time from switching STBY PITOT ON until full ice−protection is obtained −...
Page 560 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation CONDITIONS NORMAL PROCEDURES DEFINITIONS DEFINITIONS AND FOD Definition of icing conditions for engine anti−icing operation PREVENTION For engine anti−ice system operation, icing conditions exist whenever the out- side air temperature (OAT) or static air temperature (SAT) is + 5 degrees C (Plus 5 °...
Page 561 FAA AD 96−01−04 R1 and 2008−06−11) and below (operation may be restricted by national rules). For a/c with Mod.no 3529 for 340B / 3530 for 340WT Departure when icing conditions on ground and expected icing after lift− − When engine anti−ice is selected, before take−off, L/R ENG ANTI−ICE lights on the Flight Status Panel will come on.
Page 562 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) If icing conditions have been encountered during flight − If operationally feasible, avoid use of reverse thrust below 50 KIAS. WING AND The Boot De−icing must be used As defined for operation of wing and stabilizer STABILIZER de−icing boots ( see page 2), or upon annunciation from an ice detector system (if DE−ICE...
Page 563 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) AUTO CYCLING switch ......CONT Use CONT mode or operate the system as needed.
Page 564 − Check L/R ENG ANTI−ICE light to come on. For a/c with Mod.no. 3529 340B / 3530 340WT the Improved Stall Warning System for Icing condition will be ”armed” or ”activated” depending on flight phase and elapsed time from lift−...
Page 565 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation CONDITIONS NORMAL PROCEDURES PROPELLER Propeller de−icing shall be used DE−ICING − As defined in icing conditions as defined for propeller de−ice operation OPERATION (see page 2)  In NORM mode when the temperature is between −5 C and −12C SAT. ...
Page 566 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) L/R PROP switches ......NORMAL/MAX −...
Page 567 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation CONDITIONS NORMAL PROCEDURES WINDSHIELD − Do not operate windshield wipers on dry windshields. WIPER − Max IAS in LOW position is 130 kts and 160 kts in HIGH position. OPERATION Windshield wipers .
Page 568 With Mod. No. 3529 for However, activation is inhibited until approximately 6 minutes after lift−off. 340B / 3530 for 340WT The activation is indicated by illumination of a blue ICE SPEED p/b on the cen- (Improved stall warn- ter instrument panel.
Page 569 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation CONDITIONS NORMAL PROCEDURES (Cont’d) − Deactivation of the system in flight is done by; first switching both Engine Anti−ice switches to OFF and then pressing the illuminated ICE SPEED p/b. The light in the button will then go out. −...
Page 570 Aircraft Operations Manual ICE AND RAIN PROTECTION Operation ABNORMAL OPERATION For Abnormal Operation, see also section 23, ABNORMAL PROCEDURES. CONDITIONS ABNORMAL PROCEDURES GENERAL General notes applicable to the ice protection systems NOTE In case of unserviceable engine intake anti−icing system, ice may have accumu- lated in the birdcatcher.
Page 571 Aircraft Operations Manual INSTRUMENTS AND RECORDERS CONTENTS Air Data System 12/1.0 Highlights − not applicable 12/1.1 Description 12/1.2 Operation Clocks 12/2.0 Highlights − not applicable 12/2.1 Description 12/2.2 Operation − not applicable Flight Recorder System 12/3.0 Highlights − not applicable 12/3.1 Description 12.3.2...
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Page 573 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description GENERAL Air Data Computer (ADC) The air data system uses three Pitot/Static tubes The ADC senses the air temperature, it also con- which senses the pitot and the static pressures and verts the pitot and static pressures into electrical feeds that information to the pneumatic instruments signals from which the ADC calculates the various...
Page 574 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description C0714 Fig. 1 Pitot/static systems − schematic 12/1.1 PAGE Apr 01/15...
Page 575 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description EFIS MFD if installed A25727 Fig. 2 ADC inputs/outputs 12/1.1 PAGE Apr 01/15...
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Page 577 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description Airspeed indicators SAT/TAS indication The electromechanical airspeed indicator is sup- Static Air Temperature and True Air Speed are de- plied with information from the ADC regarding indi- termined by the ADC and displayed on the EHSI’s. cated airspeed (IAS) and Maximum operating Altitude Preselector Alerter speed (V...
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Page 579 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description CONTROLS AND INDICATORS Altitude indication. Shows aircraft altitude with a smallest STANDBY ALTIMETER scale increment of 20 ft by a digital and an analogue scale. Baroset indication. Displays set barometric pressure in millibars (MB), or as an option in inches of mercury (INHG).
Page 580 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description LEFT IAS INDICATOR Warning flag (red). Flag is indicated if: − The test button is pressed. − The IAS indicator fails. − Loss of airspeed data from the ADC. pointer. IAS pointer.
Page 581 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description CONTROLS AND INDICATORS Altitude indication. STANDBY ALTIMETER Shows aircraft altitude with a smallest scale increment of 20 ft by a digital and an analogue scale. Baroset indication. Displays set barometric pressure in millibars (MB), or as an option in inches of mercury (INHG).
Page 582 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description LEFT IAS INDICATOR Warning flag (red) Flag is indicated if: − The test button is pressed. − The IAS indicator fails. − Loss of airspeed data from the ADC. pointer IAS pointer IAS bug knob When IAS mode (FD/AP) is selected...
Page 583 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description RIGHT IAS INDICATOR pointer IAS pointer Airspeed reference bug C0720 Fig. 5 Right Indicated Airspeed (IAS) indicator 12/1.1 PAGE Apr 01/15...
Page 584 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description LEFT ALTIMETER Altitude indication Shows aircraft altitude by a digital and an analogue scale with a smallest scale increment of 20 ft. Baroset indication Displays set barometric pressure in inch- es mercury (IN HG) or millibars (MB).
Page 585 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description RIGHT ALTIMETER VIB flag (red) Indicates inoperative vibrator. Altitude indication. Shows aircraft altitude by a digital and an analogue scale with a smallest scale increment of 20 ft. Baroset indication. Displays set barometric pressure in milli−...
Page 586 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description Ñ LEFT VERTICAL SPEED INDICATOR 1000 FPM Vertical speed pointer Vertical speed scale. Scaled in fpm x 1000. Warning flag (red) Flag is indicated if: − The test button is pressed. −...
Page 587 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description Ñ Push TEST knob. Slews the VS bug when rotated and initiates VNI self test when pushed and released. Warning flag (red). Test Flag is indicated if. − VS pointer goes to 6000 FPM up. −...
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Page 589 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description RIGHT VERTICAL SPEED INDICATOR Vertical speed pointer. Vertical speed scale. Scaled in fpm x 1000. A26670 Fig. 10 Right Vertical Speed, VS, indicator 12/1.1 PAGE Apr 01/15...
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Page 591 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description EADI Fast−Slow speed indication. LOC1 VNAV GS Green diamond shaped pointer indi- cates the difference between the speed selected with the IAS bug on the IAS indicator and the actual IAS. 1 dot = 5 knots.
Page 592 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/1.1 PAGE Apr 01/15...
Page 593 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description TAS indication. True airspeed in knots. If ADC speed information fails, readout turns to red dashes, flashes for 10 s then steady. SAT indication. Static air temperature in degrees centigrade. If ADC temperature information fails, read- out turns to red dashes, flashes for 10 s EHSI...
Page 594 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description TEST 2 PANEL TEST 2 PROP OVSP AIR DATA Computer test switch L GEN R (for maintenance only) When pressed and held on ground: − The left IAS, ALT and VS or VNAV ENG OVSP AIR DATA EMER PWR AHRS...
Page 595 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description ALTITUDE PRESELECTOR ALERTER Selected altitude display. − The two left digits displays thousands of feet. ALTITUDE SET PUSH TO − The digit right of the comma displays hundereds of feet. ALERT −...
Page 596 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description Deviation altitude 1000ft Preselected altitude 1000ft No alert light Altitude alert light illuminates steady Altitude alert light flashing Aural alert (c−chord tone) Deviation altitude 300 ft deviation altitude alert with Collins PRE 80D P/N − 015. 200 ft deviation altitude alert with Collins PRE 80D P/N −...
Page 597 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description ELECTRICAL POWER SUPPLY ADC/IAS indicator ..... L AVIONIC START BUS F−15 ADC L ASI ADC/altimeter .
Page 598 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/1.1 PAGE Apr 01/15...
Page 599 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Operation LIMITATIONS ALTIMETER OPERATIONAL TOLERANCES Deviation from true altitude at ground check and difference between two indicators according to national regulations. AIRSPEED INDICATOR OPERATIONAL TOLERANCES Difference between two indicators according to national regulations. AIRSPEED INDICATOR AND ALTIMETER POSITION ERROR CORRECTION Fig.
Page 600 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Operation 12/1.2 PAGE Jun30/15...
Page 601 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Operation NORMAL OPERATION CONDITIONS NORMAL PROCEDURES L and R AVION switches ......POWER UP - The Air Data system is switched ON/OFF by L and R AVION switches.
Page 602 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Operation ABNORMAL OPERATION. CONDITIONS ABNORMAL PROCEDURES ALTITUDE INDICATIONS PRE- SELEC- Altitude Preselector Alerter warning flag comes on. TOR ALERTER FLAG WARNING ACTIONS CB F- 13 L VSI/VNI PRESEL ..... CHECK/RESET End of procedure.
Page 603 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Operation CONDITIONS ABNORMAL PROCEDURES RIGHT ALTIME- INDICATIONS TER VIB FLAG VIB flag in view. WARNING ACTIONS CB M- 9 ALTIM VIBR OVSP ..... CHECK/RESET - If flag out of view - end of procedure.
Page 604 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, AIR DATA SYSTEM Operation CONDITIONS ABNORMAL PROCEDURES DIFFERENTIAL INDICATIONS INDICATION If differential indication appears between any of the airspeed and/or altimeter BETWEEN ANY indicators: OF THE - L and R side; INDICATIONS - L and standby; - R and standby.
Page 605 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, CLOCKS Description GENERAL HOT BAT BUS also supplies the optional second chronometer if installed. The aircraft is provided with one mechanical chro- The chronometer displays: nometer, located on left instrument panel. As an option, an additional chronometer is provided on the −...
Page 606 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, CLOCKS Description CONTROLS AND INDICATORS (if installed) Chronometer button. CHRONOMETER Momentarily press button to: − Start − Stop − Reset Minute hand. Elapsed time minutes. Elapsed time seconds. Hour hand. Spring wind−up knob (only mechanical). Pull knob and rotate to correct time.
Page 607 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, CLOCKS Description ELECTRICAL POWER SUPPLY Chronometer ......R HOT BAT BUS M−17 CLOCK...
Page 608 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, CLOCKS Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/2.1 PAGE Apr 01/15...
Page 609 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description GENERAL Digital Flight Data Recorder (DFDR) The Flight Recorder system consists of four units: This is a recorder with a crashproof tape magazine installed in the rear compartment. The recorder −...
Page 610 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description CONTROLS AND INDICATORS FLIGHT RECORDER PANEL EVENT button. Press to mark events on the tape. DFDR light (amber). − Light goes out after first engine is started and one generator on line, indicating Flight Recorder is valid.
Page 611 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description GENERAL Digital Flight Data Recorder (DFDR) The Flight Recorder system consists of four units: This is a recorder with a crashproof tape magazine installed in the rear compartment. The recorder −...
Page 612 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description CONTROLS AND INDICATORS Thumb wheel switches. Used to set operator flight/trip number data. EVENT button. Press to mark events on the tape. FLIGHT DATA ENTRY PANEL DFDR light (amber). − Light goes out after first engine is started and one generator on line, indicating Flight Recorder FDAU light (amber).
Page 613 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description GENERAL Digital Flight Data Recorder (DFDR) The Flight Recorder system consists of four units: This is a recorder with a crashproof tape magazine installed in the rear compartment. The recorder −...
Page 614 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description CONTROLS AND INDICATORS Thumb wheel switches. Used to select flight data to be inserted. FLIGHT DATA ENTRY PANEL INSERT button. Press to insert selected flight data. EVENT button. Press to mark events on the tape. DFDR light (amber).
Page 615 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description GENERAL vided with an underwater locator beacon, automati- cally started when submerged in water. It is battery The Flight Recorder system consists of four units: powered and transmits an acoustic signal for 30 −...
Page 616 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description CONTROLS AND INDICATORS Thumb wheel switches. Used to set operator flight/trip number data. EVENT button. FLIGHT DATA ENTRY PANEL Press to mark events on the tape and to enter event data in ETM. MEM light (white) (maintenance).
Page 617 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description ELECTRICAL POWER SUPPLY Applicable for A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: Flight recorder ..... L INV BUS 115 VAC F−19 RECORD FLIGHT FDAU .
Page 618 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/3.1 PAGE Apr 01/15...
Page 619 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP Applicable for A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: R AVION and MAIN INV switches ....−...
Page 620 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES DFDR LIGHT ACTION Applicable for A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: CB F−19, RECORD FLIGHT ..... CHECK/RESET End of procedure.
Page 621 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP Applicable to A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: R AVION and MAIN INV switches ....−...
Page 622 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Operation CONDITIONS NORMAL PROCEDURES EVENT EVENT button ........PRESS −...
Page 623 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES DFDR LIGHT ACTION Applicable to A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: CB F−19, RECORD FLIGHT ..... CHECK/RESET End of procedure.
Page 624 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, FLIGHT RECORDER SYSTEM Operation THIS PAGE INTENTIONALLY LEFT BLANK ! 12/3.2 PAGE Apr 01/15...
Page 625 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description GENERAL The whole tape can be erased in a few seconds provided aircraft is on ground and gust lock set. The Cockpit Voice Recorder (CVR) records the last The recorder is provided with an underwater locator 30 minutes of cockpit communications and sounds beacon which is automatically started when sub- using a four channel endless magnetic tape.
Page 626 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description CONTROLS AND INDICATORS Cockpit area microphone. CABIN SIGN PANEL CABIN SIGNS SEAT EMER BELT SMOKING CALL TEST button. CVR CONTROL PANEL When pressed, an internal test starts pro- ducing: −A 600 Hz audio tone to headset output. −A green band indication on the monitor TEST ERASE...
Page 627 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description ELECTRICAL POWER SUPPLY Applicable for A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: Voice recorder ..... L BAT BUS F−18 RECORD VOICE Applicable for A/C 160−249 with Mod.
Page 628 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/4.1 A/C 160−399 PAGE Jun 01/19...
Page 629 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description GENERAL The whole tape can be erased in a few seconds provided aircraft is on ground and gust lock set. The Cockpit Voice Recorder (CVR) records the last The recorder is provided with an underwater locator 2 hours of cockpit communications and sounds us- beacon which is automatically started when sub- ing a four channel endless magnetic tape.
Page 630 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description CONTROLS AND INDICATORS Cockpit area microphone. CABIN SIGN PANEL CABIN SIGNS SEAT EMER BELT SMOKING CALL TEST button and TEST light. When TEST button pressed, an internal CVR CONTROL PANEL test starts producing: −The green TEST light comes on (extin- COCKPIT VOICE...
Page 631 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description ELECTRICAL POWER SUPPLY Voice recorder ..... L BAT BUS E−15 RECORD VOICE 12/4.1 A/C 400−up...
Page 632 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/4.1 A/C 400−up PAGE Jun 01/19...
Page 633 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description GENERAL ment area. The CVR continuously records each of the four audio inputs in the solid state flash memory The Solid State Cockpit Voice Recorder (SSCVR) for a maximum period of 30 minutes, before new records the last 30 minutes of cockpit communica- data is recorded.
Page 634 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description CONTROLS AND INDICATORS CABIN SIGN PANEL Cockpit area microphone. CABIN SIGNS SEAT EMER BELT SMOKING TEST button. CALL When pressed, an internal test starts pro- ducing: −A 800 Hz audio tone to headset output. −A green band indication on the monitor meter.
Page 635 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description ELECTRICAL POWER SUPPLY Applicable for A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: Voice recorder ..... L BAT BUS F−18 RECORD VOICE Applicable for A/C 160−249 with Mod.
Page 636 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/4.1 Applicable to A/C with Solid State with 30 minutes recording time PAGE Jun 01/19...
Page 637 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description GENERAL With a Solid State Cockpit Voice Recorder with 2 hours recording time is installed, both pilots and the The Solid State Cockpit Voice Recorder (SSCVR) PA communications are combined in a fifth audio records the last 2 hours of cockpit communications channel and in the sixth audio channel the audio in and sounds using digital solid state memory cir-...
Page 638 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description CONTROLS AND INDICATORS CABIN SIGN PANEL Cockpit area microphone. CABIN SIGNS SEAT EMER BELT SMOKING TEST button. CALL When pressed, an internal test starts pro- ducing: −A 800 Hz audio tone to headset output. −A green band indication on the monitor meter.
Page 639 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description ELECTRICAL POWER SUPPLY Applicable to A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: Voice recorder ..... L BAT BUS F−18 RECORD VOICE Applicable to A/C 160−249 with Mod.
Page 640 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Description THIS PAGE INTENTIONALLY LEFT BLANK ! 12/4.1 Applicable to A/C with Solid State with 2 hours recording time PAGE Jun 01/19...
Page 641 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP ESS AVION switch ......The Cockpit Voice Recorder is switched ON/OFF by ESS AVION switch.
Page 642 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES FAILURE AT ACTION TEST Applicable to A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: CB F−18, RECORD VOICE ..... . CHECK/RESET End of procedure.
Page 643 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP ESS AVION switch ......The Cockpit Voice Recorder is switched ON/OFF by ESS AVION switch.
Page 644 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES FAILURE AT ACTION TEST CB E−15, RECORD VOICE ..... . CHECK/RESET End of procedure.
Page 645 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP ESS AVION switch ......The Cockpit Voice Recorder is switched ON/OFF by ESS AVION switch.
Page 646 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES FAILURE AT ACTION TEST Applicable to A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: CB F−18, RECORD VOICE ..... . CHECK/RESET End of procedure.
Page 647 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation LIMITATIONS Not applicable. NORMAL OPERATION CONDITIONS NORMAL PROCEDURES POWER UP ESS AVION switch ......The Cockpit Voice Recorder is switched ON/OFF by ESS AVION switch.
Page 648 Aircraft Operations Manual INSTRUMENTS AND RECORDERS, COCKPIT VOICE RECORDER Operation ABNORMAL OPERATION CONDITIONS ABNORMAL PROCEDURES FAILURE AT ACTION TEST Applicable to A/C 160−249 without Mod. No. 2245 and/or without Mod. No. 2948: CB F−18, RECORD VOICE ..... . CHECK/RESET End of procedure.
Page 649 Aircraft Operations Manual LANDING GEAR CONTENTS Landing Gear 13.0 Highlights − not applicable 13.1 Description 13.2 Operation −CONTENTS PAGE Apr 01/15...
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Page 651 Aircraft Operations Manual LANDING GEAR Description GENERAL Normal extension/retraction With gear UP selected, an electrically operated con- The aircraft is equipped with a conventional retract- trol valve ports hydraulic pressure to release the able landing gear. downlocks and pressurize the hydraulic actuators. The main gears are located in the engine nacelles A mechanical lock on the landing gear control han- and the nose gear in the forward fuselage.
Page 652 Aircraft Operations Manual LANDING GEAR Description connected from the gear, leaving the doors in fully own accumulator. Hydraulic pressure is normally open position. The disconnection is made by an supplied by the electrical hydraulic pump but the explosive separation bolt that is electrically acti- hand pump may be used as an alternative.
Page 653 Aircraft Operations Manual LANDING GEAR Description brake pressure is reduced for both inboard brakes A PARK BRK ON (CWP) light comes on when ap- since they are connected to the same circuit. Simi- plying the parking brake and the trapped pressure larly, a skid on an outboard wheel will reduce brake exceeds 1700 psi.
Page 654 Aircraft Operations Manual LANDING GEAR Description used to control various air/ground functions in differ- − RIGHT INBOARD SWITCH: ent systems. Some of the systems receive signals  Anti−Skid (left and right inboard wheels). from the WOW and up− and downlock switches via ...
Page 655 Aircraft Operations Manual LANDING GEAR Description − RIGHT MLG UPLOCK SWITCH. tarded below minimum takeoff power (62 Power Lever Angle). The horn may be silenced by pushing  Landing gear indication. the master warning light.  Flight Recorder. If, subsequently, flaps 20 or more is selected, the ...
Page 656 Aircraft Operations Manual LANDING GEAR Description Left pilot Right pilot Brake pedals Inboard accumulator Outboard accumulator L Inboard R Inboard L outboard R outboard power power power power Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï Ï valve valve valve...
Page 657 Aircraft Operations Manual LANDING GEAR Description To explosive Emergency separation extension bolts handle Landing gear handle DOWN Solenoid Ground Flight mode mode Up−signal 28 VDC Down signal 28 VDC Main accumulator Hydraulic hand pump Emergency Hydraulic Gear gear pump selector selector DOWN pressure UP pressure...
Page 658 Aircraft Operations Manual LANDING GEAR Description Steering wheel Actuator Solenoid steering brake Return Control Î Î valve Main accumulator Hydraulic handpump Shutoff valve Solenoid L WoW Hydraulic pump R WoW 28 VDC Ground handling NLG down Lockout switch and locked Deflection >20...
Page 659 Aircraft Operations Manual LANDING GEAR Description CONTROLS AND INDICATORS LANDING GEAR CONTROL PANEL Landing gear down and locked lights (green) NOSE When the NOSE, LEFT or RIGHT light is on, the LEFT RIGHT respective gear is down and locked. TEST button. When pressed: With the gear locked in down position the amber DOWN...
Page 660 Aircraft Operations Manual LANDING GEAR Description Hand pump Provides hydraulic pressure to operate flaps, brakes and landing gear. Operated by a detach- able handle, stowed on the right rear cockpit wall. HAND PUMP AND EMER- Hand pump selector GENCY Directs hand pump pressure to the systems EXTENSION CONTROLS served by the hand pump.
Page 661 Aircraft Operations Manual LANDING GEAR Description ANTI−SKID switch. ON − Anti−skid system active when:  Landing Gear handle is down.  Both PL below FI or at least one in−board and one outboard WOW switch activated. OFF − Anti−skid system is off and A− SKID INOP caution light on cen- tral warning panel illuminated.
Page 662 Aircraft Operations Manual LANDING GEAR Description CENTRAL WARNING PANEL PARK BRK ON light (amber). AUTO Comes on when parking brake handle is pulled COARSEN and brake pressure exceeds 1700 psi and goes L FIRE R FIRE off when parking brake handle is pushed down FUEL ELEC DET FAIL...
Page 663 Aircraft Operations Manual LANDING GEAR Description CONFIG light (red). Will come on together with the intermittent CENTRAL WARNING PANEL horn when the aircraft is not in landing configuration. (Gear not down below 500 ft L ENG AVIONIC R ENG radio height and at least one power lever FIRE SMOKE SMOKE...
Page 664 Aircraft Operations Manual LANDING GEAR Description ELECTRICAL POWER SUPPLY Landing gear control ..... . L BAT BUS F−7 LDG CONTROL Landing gear control .
Page 665 Aircraft Operations Manual LANDING GEAR Operation LIMITATIONS Unit Normal OPERATING LIMITS Regarding speed limits for landing gear operation, for gear extended, and for max tire speed, ref. sec- tion 27, SPEEDS. Gear extension time ......−...
Page 666 Aircraft Operations Manual LANDING GEAR Operation NORMAL OPERATION CONDITIONS NORMAL PROCEDURES RETRACTION Preflight check AND EXTEN- Landing gear handle ......SION −...
Page 667 Aircraft Operations Manual LANDING GEAR Operation CONDITIONS NORMAL PROCEDURES OPERATION OF Preflight check NOSEWHEEL STEERING Do not use nosewheel steering when aircraft is standing still. Taxi Nosewheel steering ......CHECK −...
Page 668 Aircraft Operations Manual LANDING GEAR Operation CONDITIONS NORMAL PROCEDURES OPERATION OF Preflight check BRAKE SYSTEM Hydraulic pressure ......CHECK −...
Page 669 Aircraft Operations Manual LANDING GEAR Operation CONDITIONS NORMAL PROCEDURES (Cont’d) During landing rollout Depress brake pedals as required. − For NORMAL braking, set brake pedals to obtain desired deceleration, tak- ing runway length and surface conditions into consideration. Do not pump brake pedals.
Page 670 Aircraft Operations Manual LANDING GEAR Operation ABNORMAL OPERATION For Abnormal Operation, see section 23 ABNORMAL PROCEDURES. 13.2 PAGE Apr 01/15...

Saab 340B Operation Manual

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Summary of Contents for Saab 340B

Page 137: Table Of Contents

Page 139: Highlights

Page 141: Description

Page 305: Operation

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Page 311: Operation