Page 1 FlightSafety international COURSEWARE SUPPORT—HURST 8900 Trinity Blvd. Hurst, Texas 76053 (817) 276-7500 Fax (817) 276-7501 CL 601-3A/R PILOT TRAINING MANUAL VOLUME 2 Record of Revision No. .01 This is a revision of the CL 601-3A/R Volume 2 Pilot Training Manual. The portion of the text or figure affected by the current revision is indicated by a solid vertical line in the margin.
Page 2 FlightSafety Canada L t ee L t d . Canadair CHALLENGER CL-601-3A/R MODEL CL-600-2B16 PILOT TRAINING MANUAL VOLUME 2 AIRCRAFT SYSTEMS FlightSafety Canada L t e e L t d . 9555 Ryan Avenue Dorval, Quebec, Canada H9P 1A2 (800) 573-4025 www.
Page 3 Courses for the Canadair Challenger Model CL-600-2B16 and other Canadair aircraft are taught at: FlightSafety Canada Ltd. Montreal Learning Center 9555 Ryan Avenue Dorval, Quebec Canada H9P 1A2 (800) 573-4025 • Fax (514) 631-2263 FlightSafety Texas Houston Learning Center 7525 Fauna Street Houston, TX 77061 (800) 927-1521 •...
Page 4 F O R T R A I N I N G P U R P O S E S O N LY NOTICE The material contained in this training manual is based on information obtained from the aircraft manufacturer ’s Pilot Manuals and Maintenance Manuals.
Page 5 CONTENTS SYLLABUS Chapter 1 AIRCRAFT GENERAL Chapter 2 ELECTRICAL POWER SYSTEMS Chapter 3 LIGHTING Chapter 4 MASTER WARNING SYSTEM Chapter 5 FUEL SYSTEM Chapter 6 AUXILIARY POWER UNIT Chapter 7 POWERPLANT Chapter 8 FIRE PROTECTION Chapter 9 PNEUMATICS Chapter 10 ICE AND RAIN PROTECTION Chapter 11 AIR CONDITIONING...
Page 6 MODIFYING YOUR PTM VOLUME 2 Please note that the Challenger Model CL-600-2B16 Pilot Training Manual Volume 2 includes a compilation of both the CL 601-3A and CL 601-3R. Where information is standard for both models, the footer shall denote CL 601-3A/R. If information is specific to one model the footer shall read CL 601-3A or CL 601-3R as appropriate.
Page 7: Table Of Contents
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL SYLLABUS CONTENTS Page COURSE INFORMATION ....................SYL-1 Learning Center Information..................SYL-1 Description of Training Facility ................. SYL-1 Type of Aircraft ......................SYL-7 Category of Training ....................SYL-7 Duty Position......................
Page 8 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FLIGHT TRAINING CURRICULUM SEGMENT ............SYL-21 Training Hours ......................SYL-21 Flight Training Module Outlines ................SYL-21 Completion Standards ....................SYL-25 FOR TRAINING PURPOSES ONLY SYL-ii CL 601-3A/R...
Page 9 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page SYL-1 Montreal Facility Floor Plan................SYL-2 SYL-2 Houston Facility Floor Plan ................SYL-3 SYL-3 Tucson Facility Floor Plan.................. SYL-5 FOR TRAINING PURPOSES ONLY CL 601-3A/R SYL-iii...
Page 10: Course Information
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL SYLLABUS COURSE INFORMATION LEARNING CENTER INFORMATION FlightSafety International is an aviation training company that provides type-specific training programs for over 50 different models of aircraft, using a fleet of over 150 simulators. FlightSafety operates 38 Learning Centers, including Centers in Europe and Canada.
Page 11 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL EXIT CLASSROOM CLASSROOM Ltee ´ FlightSafety Canada Ltd. Canadair Challenger Learning Center WOMEN CLASSROOM LOUNGE DIRECTOR PARKING AREA CUSTOMER SUPPORT OFFICE MANAGER ✚ LEGEND EMERGENCY OXYGEN EQUIPMENT MARKETING ✚...
Page 12 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FlightSafety T E X A S 7525 FAUNA HOUSTON, TEXAS ATR-42 CLASSROOM COMPUTER ROOM LOUNGE BRIEFING BRIEFING ROOM ROOM PROGRAM MANAGERS STORAGE ROOM 143 ROOM 142 ROOM 141 ROOM 140 CUSTOMER SUPPORT...
Page 13 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FlightSafety T E X A S 7526 WYNLEA (Back) HOUSTON, TEXAS DIRECTOR STANDARDS HAWKER OFFICE FALCON EMB-120 OFFICE WOMEN ATR 42/72 BRIEFING POWER ROOM ROOM CLOSET STORAGE CUSTOMER COMPUTER ROOM...
Page 14 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FlightSafety international Learjet Learning Center Tucson, Arizona BALCONY BRIEF BRIEF BRIEF LEAR 25 LEAR 55 LEAR 35 (200) COMPUTER ROOM LEAR 60 BRIEF BRIEF MAINTENANCE SIMULATOR ROOM LEAR 45 SIMULATOR ROOM MAINT.
Page 15 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FlightSafety international Learjet Learning Center Tucson, Arizona STORAGE CLASSROOM CLASSROOM CLASSROOM CLASSROOM CLASSROOM STORAGE CLASSROOM CLASSROOM CLASSROOM CLASSROOM CLASSROOM CLASSROOM WOMEN CLASSROOM CLASSROOM LIBRARY SELF LEARNING TELE TELE VEND...
Page 16: Type Of Aircraft
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL TYPE OF AIRCRAFT The Canadair Challenger CL-600 series, which includes the Challenger 600, 601-1A, 601-3A, and 601-3R. CATEGORY OF TRAINING Initial Equipment and Transition training for a CL-600 type rating added to an existing pilot certificate or the issuance of an Airline Transport Pilot Certificate with a CL-600 type rating.
Page 17 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Specialty Training Curriculum Prerequisites §61.55 A pilot may enroll in the SIC course and complete all of the training that is authorized to be ac- complished in the Level A through D flight simulator, then complete the items required in flight in a CL-600 Series aircraft, if the pilot: 1.
Page 18 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 4. Has at least 500 hours of actual flight time in CL-600 Series airplanes; or 5. Has at least 1,000 hours of flight time in at least two different airplanes requiring a type rating.
Page 19: Course Objectives
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Completion Standards Completion is based on proficiency. Syllabus times are estimates. Pilots must demonstrate sat- isfactory performance through formal and informal examinations in the classroom and flight simulator, and in flight to ensure they meet the knowledge and skill requirements necessary to meet the course objectives.
Page 20 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Day 4 Classroom ..........................6.0 Review Hydraulics Systems Landing Gear and Brakes Day 5 Classroom ..........................6.0 Review Flight Controls Fuel System Day 6 Classroom ........................... 6.0 Review Powerplant Thrust Reversers...
Page 21 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Simulator Training (Based on Training as a Crew) Hours Day 12 Simulator Pre/Post Briefings....................1.5 Flight Simulator—Period One ..................... 4.0 Day 13 Simulator Pre/Post Briefings....................1.5 Flight Simulator—Period Two.....................
Page 22: Simulator And Flight Training
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL SIMULATOR AND FLIGHT TRAINING Pilot performance during simulator and flight training shall be graded as: Proficient (1), Normal Progress (2), Additional Training Required (3), Unsatisfactory (4), or Discussed (D). The criteria for grading shall be as follows: •...
Page 23: Aircraft Ground Training Curriculum Segment
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AIRCRAFT GROUND TRAINING CURRICULUM SEGMENT CURRICULUM SEGMENT OUTLINE Objective: To provide pilots with the necessary knowledge for understanding the basic func- tions of aircraft systems, the use of the individual system controls, and the integration of air- craft systems with operational procedures to sufficiently prepare them to enter the flight training curriculum segment.
Page 24: Training Module Outlines
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Q. Avionics R. Oxygen S. Systems Review and Examination Completion Standards A. Systems—The pilot must demonstrate adequate knowledge of the aircraft systems, per- formance, and flight planning by successfully completing a written examination with a min- imum score of 70%, that is corrected to 100%.
Page 25 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 3. Limitations Section 4. Maneuvers and Procedures Section 5. General Performance Section 6. Systems Description 7. Appendices and Bulletins E. Windshear (optional) 1. Windshear Weather 2. High Altitude Meteorology 3.
Page 26 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Aircraft Systems Modules A. Aircraft General Module 1. General Elements System Description Controls and Components Annunciators d. Miscellaneous 2. Operational Elements 3. Limitations Elements 4. Emergency/Abnormal Procedure Elements B.
Page 27 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL E. Fuel Module 1. General Elements 2. Operational Elements 3. Limitation Elements 4. Emergency/Abnormal Procedure Elements F. Auxiliary Power Unit (APU) Module 1. General Elements 2. Operational Elements 3.
Page 28 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL K. Ice and Rain Protection Module 1. General Elements System Description Controls and Components Annunciators 2. Operational Elements 3. Limitations Elements 4. Emergency/Abnormal Procedure Elements L. Air Conditioning Module 1.
Page 29 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 2. Operational Elements 3. Limitation Elements 4. Emergency/Abnormal Procedure Elements P. Flight Controls Module 1. General Elements System Description Controls and Components Indicators/Indications d. Annunciators 2. Operational Elements 3.
Page 30: Flight Training Curriculum Segment
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL NOTE An individual who has experience as a SIC in the aircraft and has previously completed an equivalent training curriculum without obtaining a type rating may complete Systems Integration Training during the prebriefing sessions prior to each Simulator Module.
Page 31 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 2. Surface Operation Starting Taxi Pretakeoff Checks 3. Takeoff and Departure Normal Area Departure Rejected d. Instrument Crosswind Powerplant Failure V g. Takeoff with Lower than Standard Minimum 4.
Page 32 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL d. Precision Approach ILS with One Engine Inoperative Missed Missed Approach—with a Powerplant Failure Nonprecision Approach One Engine Out Missed Missed Approach—with a Powerplant Failure Coupled Approach g.
Page 33 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 10. System Procedures (Normal, Abnormal, and Emergency) Air Conditioning Aircraft Fires Anti-icing and Deicing d. APU Autopilot Cabin Fire/Smoke g. Communication Equipment h. Electrical Fire Protection Flap Systems k.
Page 34: Completion Standards
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL COMPLETION STANDARDS The pilot must perform all procedures and maneuvers to the tolerances listed in the Airline Transport Pilot/Type Rating Practical Test Standards. It is expected, during the earlier simula- tor flights, that the tolerance for completion of a maneuver or procedure be greater than during the later simulator flights.
Page 35 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Bearing Pointer ........±5° Deviation MDA .
Page 36 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 1 AIRCRAFT GENERAL CONTENTS Page INTRODUCTION ........................1-1 GENERAL..........................1-1 STRUCTURES ........................1-6 Fuselage ........................... 1-6 Doors..........................1-9 Wing..........................1-13 Airplane Parking and Mooring ..................1-14 AIRPLANE SYSTEMS ......................
Page 37 FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL Flight Controls ....................... 1-18 Avionics ......................... 1-19 Oxygen System ......................1-19 FOR TRAINING PURPOSES ONLY 1-ii CL 601-3A/R...
Page 38 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Canadair Challenger ....................1-2 Dimensions and Ground Clearances ................ 1-2 Turning Radii......................1-4 Danger Areas......................1-5 Flight Compartment ....................1-6 Structural Subassemblies..................1-7 Nose Landing Gear Assembly..................
Page 39: Introduction
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 1 AIRCRAFT GENERAL INTRODUCTION This training manual provides a description of the major airframe and engine systems installed in the Canadair Challenger CL-600-2B16, model CL-601-3A/R. This chapter covers the structural makeup of the airplane and provides a general overview of the systems.
Page 40 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 1-1 shows a completed Challenger, and Figure 1-2 displays the dimensions and ground clearances of the airplane. Figure 1-1. Canadair Challenger 3 FT 1 IN. 20 FT 8 IN.
Page 41 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 19 FT 2 IN. 12 FT 2 IN. 9 FT 4 IN. 7 FT 6 IN. 10 FT 5 IN. 64 FT 4 IN. STATIC GROUND LINE 27 FT 8 IN.
Page 42 FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL Figure 1-3 shows the turning radii applicable quired for a 180-degree turn at the maximum to the maximum nosewheel steering angle of steering angle, and the turning radii for the 55 degrees, the minimum taxi strip width re- maximum towing angle of 90 degrees.
Page 43 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL While engines are running, there are dan- gines. Figure 1-4 shows the temperature ger areas to the front and rear of the en- and distance criteria. IDLE MAXIMUM THRUST THRUST...
Page 44: Structures
FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL STRUCTURES Nose Section The nose section is effectively divided by the FUSELAGE flight compartment floor into upper and lower halves. The upper half comprises the flight The fuselage is an all-metal, semimonocoque compartment and forward avionics bay.
Page 45: Flight Compartment
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL EMERGENCY EXIT BAGGAGE PRESSURIZED PASSENGER DOOR COMPARTMENT ELEVATORS (FUSELAGE CENTER SECTION) VERTICAL STABILIZER HORIZONTAL RUDDER STABILIZER FLIGHT MAIN ENTRANCE COMPARTMENT DOOR TAIL CONE FORWARD VERTICAL STABILIZER/REAR AVIONICS BAY FUSELAGE FRAME (UNPRESSURIZED) AFT AUXILIARY TANK...
Page 46 FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL The lower half of the nose section comprises Center Section compartments for the brake accumulators and brake valve control mechanism, the air-driven The center section is divided by a single-level generator, the flight control forward mechanisms, floor into the pressurized passenger com- and the nose wheel well and mounting structure.
Page 47: Doors
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL rear equipment bay houses the auxiliary power The baggage compartment and emergency exit unit (APU), two air-conditioning units (ACU), doors are of the plug type which open inward; the reservoirs and other components of hy- all other doors open outward.
Page 48 FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL stowed in the riser of the stair. Four red visual DOOR,” is located just forward of the en- alignment marks located on the center latch trance door. Holding the switch to the RAISE cams (2) and the upper latch cams (2) should position activates the system, which raises be checked to ascertain door security.
Page 49: Baggage Compartment Door
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Emergency Exit Baggage Compartment Door An overwing emergency exit is provided on The baggage compartment door is located the right side of the cabin over the wing (Fig- on the left side of the airplane immediately ure 1-12).
Page 50: Rear Equipment Bay Door
FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL The baggage compartment door can be opened be turned to release the locking plungers and or closed from both inside and outside. The ex- open the door (Figure 1-13). ternal handle incorporates two locking mech- anisms, one to hold the handle flush with the Rear Equipment Bay Door...
Page 51: Wing
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Fuel for the airplane is stored in three tank areas. The deep section of the airfoil on each side is used as a main tank, and the center sec- tion is used as an auxiliary tank.
Page 52: Airplane Parking And Mooring
FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL AIRPLANE PARKING AIRPLANE SYSTEMS AND MOORING ELECTRICAL SYSTEM When the airplane is stationary on the ground, precautions must be taken to ensure safety of The Challenger was the first executive jet to personnel and equipment.
Page 53: Lighting
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 3. External system lighting includes four landing lights and two taxi/recognition lights; two rotating red bea- 4. Emergency system cons; standard red, green , and white navigation lights;...
Page 54 FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL large increase in thrust over that available AUXILIARY POWER UNIT from a comparable turbojet, while consuming The auxiliary power unit (APU) installed in the the same amount of fuel. This significantly in- Challenger is a self-contained gas turbine en- creases the range capability of the airplane.
Page 55 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL The air-conditioning system includes the pres- ICE AND RAIN PROTECTION sure regulating and shutoff valves, refrigerated Ice and rain protection is divided into two cat- and conditioned air ventilations system, and egories, depending on whether they use bleed separate cabin and flight compartment tem- air or electrical power as a source of energy.
Page 56 FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL Override controls are incorporated into the with the switches, lights, and gauges for sys- outflow valves, which will provide for: tem management. • Overpressure limiting, which limits the LANDING GEAR AND BRAKES maximum cabin differential pressure to 9.1 ±0.1 psi, regardless of the selector The Challenger employs three retractable land-...
Page 57 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL a stick shaker, autopilot disconnect, aural and AVIONICS visual warning, and a stick pusher actuation. The following equipment is fitted to the Chal- Roll, pitch, and yaw changes are generated lenger before the completion center modifi- from the control wheels, control columns, and cations are added:...
Page 58 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 2 ELECTRICAL POWER SYSTEMS CONTENTS Page INTRODUCTION ........................2-1 GENERAL..........................2-1 AC SYSTEM ........................... 2-2 Primary AC System......................2-2 Auxiliary AC System ....................... 2-4 External AC System ......................2-6 Emergency AC System ....................
Page 59 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page AC System Components Locations................2-2 Integrated-Drive Generator..................2-3 Main AC Power (Power Off)..................2-4 Main AC Power APU Feed ..................2-5 Main AC Power Normal GEN Feed................. 2-5 Main AC Power GEN 1 Feed (GEN 2 INOP)............
Page 60 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 2-24 Both ESS TRUs Failed (W off W) ................. 2-18 2-25 DC Electrical Controls ................... 2-19 2-26 BATTERY MASTER Switch................. 2-19 2-27 Total Electrical System................... 2-20 2-28 CBP-A Main AC and DC Bus 1................
Page 61 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 2 ELECTRICAL POWER SYSTEMS INTRODUCTION The Canadair Challenger CL-600-2B16, model CL601-3A/R has an electrical system that is comparable to that of a modern airliner. It was the first business jet to have a primary electrical system based on AC power.
Page 62 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL AC SYSTEM Integrated-Drive Generators (IDG) The AC electrical system is divided into Each IDG (Figure 2-2) is made up of a con- four subsystems: primary, auxiliary, exter- stant speed drive (CSD) and an AC generator nal, and emergency.
Page 63: Generator Trip Levels
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The CSD oil also acts as a cooling agent for Generator Control Unit (GCU) the CSD and the generator. The oil is cooled in a heat exchanger located on the engine Each generator has its own generator control pylon service assembly.
Page 64 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Provided no airplane generators are on line, cooled by APU fuel through a heat exchanger. the GTC is capable of accepting power from The auxiliary power system GCU provides a suitable external AC source (Figure 2-3).
Page 65 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AP/EP CONT LEGEND UNPOWERED POWERED BUS APU GENERATOR POWER MAIN AC BUS 1 MAIN AC BUS 2 Figure 2-4. Main AC Power APU Feed AP/EP CONT LEGEND UNPOWERED POWERED BUS...
Page 66 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL AP/EP MONITOR MONITOR CONT LEGEND UNPOWERED POWERED BUS IDG 1 POWER MAIN AC BUS 1 MAIN AC BUS 2 Figure 2-6. Main AC Power GEN 1 Feed (GEN 2 INOP) EXTERNAL AC SYSTEM AC external power is supplied through a stan- dard six-pin AC power receptacle located on...
Page 67 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-7. AC External Power Connector AP/EP MONITOR MONITOR CONT LEGEND UNPOWERED POWERED BUS EXTERNAL AC POWER MAIN AC BUS 1 MAIN AC BUS 2 Figure 2-8. External AC Power Feed (All GENs INOP) FOR TRAINING PURPOSES ONLY CL 601-3A/R 2-7...
Page 68 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL AP/EP MONITOR MONITOR CONT LEGEND UNPOWERED POWERED BUS ADG POWER ADG BUS EMERG MAIN AC BUS 1 ESS AC BUS MAIN AC BUS 2 Figure 2-9. Emergency AC Power Feed (All GENs INOP) EMERGENCY AC SYSTEM The emergency AC power system provides 115-/200-volt, 3-phase, 400-Hz AC power au-...
Page 69 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AC POWER DISTRIBUTION Refer to Figure 2-12 while reading this sec- tion. There are a total of eight AC buses. 1. AC bus 1 2. AC bus 2 3.
Page 70 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AP/EP MONITOR CONT A 23 B 23 ADG BUS EMERG AC TC MAIN AC BUS 2 MAIN AC BUS 1 ESS AC BUS ESS 26 VAC 26 VAC 2 LEGEND UNPOWERED...
Page 71 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 26-VAC Bus 2 and 26-VAC Essential Bus There are two transformers which convert AC bus 2 and AC essential bus 115 VAC to 26 VAC and power the airplane flight instru- ments.
Page 72 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Figure 2-15. Electrical Control Panel Indication of a Good Test Generator OFF Light Ground Mode: 1 sec blank then green light on Illumination of a GEN OFF light indicates for 2 secs then out.
Page 73 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MAIN BUS OFF Light Voltage and Frequency Metering The MAIN BUS OFF light illuminates when both sides of a generator line contactor are A rotary selector allows for the monitoring of deenergized.
Page 74 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL start the APU and to supply backup DC power TRUs 1 and 2 normally supply their own as- when a primary DC power source has failed sociated buses.
Page 75 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MAIN AC BUS 1 ESS AC BUS MAIN AC BUS 2 TRU 1 TRU 2 DC UTILITY BUS 1 DC UTILITY BUS 2 DC TIE CONT LEGEND DC TIE ESS DC BUS...
Page 76: Battery Master Switch
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MAIN AC BUS 2 TRU 1 TRU 2 BATT CHGR ESS DC BUS EMER DC 2 TC W OFF W BATTERY MASTER MAIN BATT LEGEND EMER SENSOR DC 1 TC UNPOWERED...
Page 77 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL emergency DC2 transfer contactor (W off W only) to close. This will allow the BATTERY DIRECT BUS to provide backup power to both the BATTERY BUS and the DC ES- SENTIAL BUS.
Page 78: Both Ess Trus Failed (W Off W)
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MAIN AC BUS 2 TRU 1 TRU 2 BATT CHGR ESS DC BUS EMER DC 2 TC W OFF W BATTERY MASTER MAIN BATT EMER DC 1 TC SENSOR RELAY LEGEND...
Page 79: Dc Electrical Controls
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CONTROL AND MONITORING A rotary selector on the DC metering portion of the electrical control panel (Figure 2-25) al- lows for the monitoring of voltage and load conditions.
Page 80: Total Electrical System
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AP/EP MONITOR CONT LEGEND APU POWER ADG POWER IDG 1 POWER IDG 2 POWER EXTERNAL AC POWER TRU 1 POWER TRU 2 POWER ADG BUS EMERG ESSENTIAL TRU 1 POWER ESSENTIAL TRU 2 POWER MAIN AC BUS 1...
Page 81: Circuit-Breaker Panels
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CIRCUIT-BREAKER PANEL LOCATIONS Table 2-2 lists circuit-breaker panels by name and describes their locations. Table 2-2. CIRCUIT-BREAKER PANELS BUS NAME LOCATION Battery Direct Bus Aft fuselage, close to battery •...
Page 82 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-28. CBP-A Main AC and DC Bus 1 FOR TRAINING PURPOSES ONLY 2-22 CL 601-3A...
Page 83: Cbp-A Battery Bus
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-29. CBP-A Battery Bus FOR TRAINING PURPOSES ONLY CL 601-3A 2-23...
Page 84 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-30. CBP-B Main AC and DC Bus 2 FOR TRAINING PURPOSES ONLY 2-24 CL 601-3A...
Page 85: Cbp-B Battery Bus
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-31. CBP-B Battery Bus FOR TRAINING PURPOSES ONLY CL 601-3A 2-25...
Page 86: Cbp-C Ac Essential Bus
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-32. CBP-C AC Essential Bus FOR TRAINING PURPOSES ONLY 2-26 CL 601-3A...
Page 87: Cbp-D Dc Essential Bus
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL NOTE: RED IDENTIFICATION COLLAR INSTALLED (POST SB 601–0379) Figure 2-33. CBP-D DC Essential Bus FOR TRAINING PURPOSES ONLY CL 601-3A 2-27...
Page 88: Cbp-E Battery Direct Bus
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-34. CBP-E Battery Direct Bus FOR TRAINING PURPOSES ONLY 2-28 CL 601-3A...
Page 89 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The primary Challenger electrical sys- A source of emergency in-flight AC power tem is: A. 115-volt AC A. IDG B. 30-volt DC B. CSD C. 24-volt DC C.
Page 90 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CIRCUIT-BREAKER PANEL LOCATIONS Table 2-2 lists circuit-breaker panels by name and describes their locations. Table 2-2. CIRCUIT-BREAKER PANELS BUS NAME LOCATION Battery Direct Bus Aft fuselage, close to battery •...
Page 91 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-28. CBP-A Main AC and DC Bus 1 FOR TRAINING PURPOSES ONLY 2-22 CL 601-3R...
Page 92 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-29. CBP-A Battery Bus FOR TRAINING PURPOSES ONLY CL 601-3R 2-23...
Page 93 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-30. CBP-B Main AC and DC Bus 2 FOR TRAINING PURPOSES ONLY 2-24 CL 601-3R...
Page 94 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-31. CBP-B Battery Bus FOR TRAINING PURPOSES ONLY CL 601-3R 2-25...
Page 95 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 2-32. CBP-C AC Essential Bus FOR TRAINING PURPOSES ONLY 2-26 CL 601-3R...
Page 96 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL NOTE: RED IDENTIFICATION COLLAR INSTALLED (POST SB 601–0379) Figure 2-33. CBP-D DC Essential Bus FOR TRAINING PURPOSES ONLY CL 601-3R 2-27...
Page 97 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL S5KJ S3KJ S4KJ TEST TEST RESET DS3KJ DS2KJ OIL FILTER DS5KJ DS4KJ CHIP DETECT IGN B BATT SHUNT FUSES OIL CONT BYPASS BACKUP POWER START EXT AC CONT CONT FUEL...
Page 98 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The primary Challenger electrical sys- A source of emergency in-flight AC power tem is: A. 115-volt AC A. IDG B. 30-volt DC B. CSD C. 24-volt DC C.
Page 99 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 3 LIGHTING CONTENTS Page INTRODUCTION ........................3-1 GENERAL..........................3-1 INTERIOR LIGHTS ......................3-2 Cockpit Lights........................3-2 Passenger Compartment Lights ..................3-4 Service Lights ........................3-4 EXTERIOR LIGHTS ......................
Page 100 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Interior Lighting Controls ..................3-2 Boarding Lights Control................... 3-4 Ordinance Lights Controls ..................3-4 Exterior Lighting Locations ..................3-5 Landing and Taxi-Recognition Lights Controls ............3-5 External Lighting Control Panel................
Page 101: Introduction
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 3 LIGHTING INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3A/R lighting system provides exterior and interior illumination. Interior lighting groups include cockpit lights, pas- senger compartment lights, and service lights. Exterior lighting includes the standard required package of airplane lights.
Page 102: Interior Lights
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL emergency evacuation. This self-contained, INTERIOR LIGHTS battery-powered system is automatically ac- tivated by loss of airplane power. COCKPIT LIGHTS Wiring, logic, and power are provided to allow The cockpit lights consist of incandescent installation of ordinance signs.
Page 103 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Incandescent Lighting The integral lighting in the cockpit is con- trolled in two individual areas: Incandescent lighting consists of floor lights and map reading lights. Floor lights are sup- •...
Page 104: Passenger Compartment Lights
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL PASSENGER COMPARTMENT LIGHTS Passenger compartment lights consist of dome lights, boarding lights, and ordinance lights. Dome and boarding lights are contained in a single assembly above the main entrance door. The dome light is powered by the battery bus and is controlled with a switch on the overhead lighting panel.
Page 105: Landing And Taxi-Recognition Lights
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ROTATING NAVIGATION EMERGENCY BEACON (OPTIONAL) AND STROBE LIGHTS LIGHT NAVIGATION LIGHT LANDING LIGHTS WING INSPECTION LIGHT TAXI-RECOGNITION ROTATING AND LANDING BEACON (OPTIONAL) LIGHTS Figure 3-4. Exterior Lighting Locations LANDING AND TAXI- RECOGNITION LIGHTS L a n d i n g a n d t a x i - r e c o g n i t i o n l i g h t s a r e...
Page 106: Wing Ice Inspection Lights
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL WING ICE INSPECTION LIGHTS EMERGENCY LIGHTS Wing ice inspection lights are mounted in both Four emergency lights are provided to illu- sides of the fuselage just above the wing. They minate escape routes during emergency evac- are controlled with the WING switch located uation.
Page 107: Questions
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The control switches for the floor lights The nosewheel bay service light control are located on the: is located: A. Pilot’s fascia A. On the overhead panel B.
Page 108 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 4 MASTER WARNING SYSTEM CONTENTS Page INTRODUCTION ........................4-1 GENERAL..........................4-1 MASTER CAUTION SYSTEM....................4-2 General ..........................4-2 Components ........................4-4 Lamp Test Switches ......................4-4 Illumination Causes......................4-5 AURAL WARNING SYSTEM .....................
Page 109: Table Title Page
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Master Caution System .................... 4-3 Lamp Test Switches....................4-4 System Warning Annunciators................4-10 System Status Annunciators................... 4-12 Landing Gear MUTE HORN Button ..............4-13 Aural Warning System ...................
Page 110: Introduction
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 4 MASTER WARNING SYSTEM TEST INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3A/R master warning system pro- vides the crew with information on malfunctions of airplane equipment, unsafe operat- ing conditions which require immediate attention, or the operation of a particular system that is not normally used.
Page 111: Master Caution System
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL of the two amber switchlights labeled “MAS- • Anti-icing TER CAUTION PRESS TO RESET.” The lights in the annunciator panels are also extinguished • Auxiliary Power Unit when the MASTER CAUTION switchlights are reset.
Page 112 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL A flashing MASTER CAUTION light directs any annunciators associated with a system cur- the pilots’ attention to the 10 and 8 channel an- rently malfunctioning illuminate on the 10 and nunciator panels to determine which system 8 channel annunciator panels.
Page 113: Components
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL COMPONENTS Dimming Modules The master caution system (see Figure 4-1) The dimming modules provide interface be- contains the two annunciator panels, an elec- tween the airplane systems and the annunci- tronic circuit-breaker unit, two MASTER ator panels.
Page 114: Illumination Causes
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUMINATION CAUSES Table 4-1 lists the 10 and 8 channel annun- ciators and the individual system caution an- nunciators, shows their color, and gives the cause for their illumination. The 10 and 8 channel annunciator panel locations are shown in the Annunciator Section.
Page 115 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Table 4-1. CAUTION ANNUNCIATORS (Cont) ASSOCIATED ANNUNCIATOR CAUSE FOR ILLUMINATION ANNUNCIATOR CABIN ENV CONT Cabin pressurization has failed. PRESS LOW AUTO The pressurization controller has failed. FAULT Indicated air-conditioning unit has been shut down automatically.
Page 116 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Table 4-1. CAUTION ANNUNCIATORS (Cont) ASSOCIATED ANNUNCIATOR CAUSE FOR ILLUMINATION ANNUNCIATOR PASS DR NOT RDY DOORS The main entrance door's inner T-handle is not stowed. PASS DR READY PASS DR UNLKD The main entrance door is not locked.
Page 117 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Table 4-1. CAUTION ANNUNCIATORS (Cont) ASSOCIATED ANNUNCIATOR CAUSE FOR ILLUMINATION ANNUNCIATOR CHAN 1 INOP FLT CONT Indicated pitch trim channel has failed. CHAN 2 INOP OVSP Pitch trim has overspeed failure; and the channel 1 brake has been applied.
Page 118 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Table 4-1. CAUTION ANNUNCIATORS (Cont) ASSOCIATED ANNUNCIATOR CAUSE FOR ILLUMINATION ANNUNCIATOR FIRE FAULT Indicated Firex bottle has low pressure. PRESS FIRE WARN Indicated fire warning system has failed. FAIL HIGH O/P FAIL...
Page 119 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Table 4-2 lists annunciators that do not acti- Table 4-3 lists the red warning annunciators, vate MASTER CAUTION annunciators. causes for their illumination, and their power sources. Figure 4-3 illustrates the warning annuncia- tors in schematic form.
Page 120 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Table 4-3. WARNING ANNUNCIATORS MASTER ASSOCIATED POWER WARNING CAUSE FOR ILLUMINATION ANNUNCIATOR SOURCE ANNUNCIATOR BLEED DUCT CLOSED A leak is detected in the L/R 10th- or Dimming modules DUCT 14th-stage bleed-air manifold.
Page 121 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Figure 4-4 illustrates the status annunciators Table 4-4 lists the nondimmable annunciators in schematic form. and their associated systems. 1 OF 40 POWER OUTPUTS B-161 BATT BUS DIMMING D-41 ELECTRONIC...
Page 122: Aural Warning System
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL AURAL WARNING each event in turn on the rotary selector and pressing the mute switch to ensure that only SYSTEM the two sounds indicated above can be muted. GENERAL Tone Muting The aural warning system provides an aural...
Page 123 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Table 4-5. AURAL WARNINGS WARNING SOUND DURATION CAUSE INPUT Engine fire Bell As long as hazard Fire detected in: • APU fire detection APU fire exists but may be •...
Page 124 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL RH ENGINE FIRE DETECTION UNIT AURAL WARNING SELCAL FIRE VOLUME CONTROL OVSPD LDG GR TONE APU FIRE MUTED STALL DETECTION UNIT ALT ADV FLAP PRESS TO MUTE OVSPD TONE TEST LH ENGINE FIRE DETECTION UNIT...
Page 125: Questions
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS If an illuminated system malfunction light The color light that indicates a situation suddenly extinguishes, it indicates: requiring attention, but not immediate action is: A. Five minutes have passed. A.
Page 126 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 5 FUEL SYSTEM CONTENTS Page INTRODUCTION ........................5-1 GENERAL..........................5-1 FUEL STORAGE ........................5-2 FUEL DISTRIBUTION ......................5-3 Gravity Flow ........................5-3 Scavenge Ejectors ......................5-3 Main Ejectors ........................5-3 Transfer Ejectors ......................
Page 127 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL DEFUELING......................... 5-16 TAIL TANK........................... 5-17 General........................... 5-17 Normal Transfer......................5-17 Fuel Jettison ........................5-18 Refueling and Defueling....................5-18 QUESTIONS ......................... 5-20 FOR TRAINING PURPOSES ONLY 5-ii CL 601-3A...
Page 128 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Fuel System—General Layout ................. 5-2 Fuel Distribution—Normal Operation (without Powered Crossfeed)...... 5-5 Fuel Distribution—Normal Operation (with Powered Crossfeed Service Bulletin 601-0225) ..................5-5 Fuel Distribution—Abnormal Operation, Main Electrical (without Powered Crossfeed) ...................
Page 129: Fuel System
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 5 FUEL SYSTEM MAIN FUEL LBS X 100 INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3A fuel system provides fuel for the two turbofan engines, as well as the auxiliary power unit (APU). Fuel is also used to cool the APU generator adapter oil and the main engine oil.
Page 130: Fuel Storage
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL The airplane may be refueled over the wings access panels in the lower surface of each wing. by gravity. However, the normal method is The gravity filler port for each main tank is lo- through an adapter located in the right wing cated on the upper outboard wing surface.
Page 131: Fuel Distribution
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL valves. Flow to the opposite engine is not pos- FUEL DISTRIBUTION sible because of one-way check valves in the feed lines. Failure of a main ejector will cause GRAVITY FLOW illumination of an amber caution light in the cockpit, and will activate both standby elec-...
Page 132: Engine-Driven Pumps
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL ENGINE-DRIVEN PUMPS POWERED CROSSFEED VALVE Each two-stage engine-driven fuel pump is a When depressing the LEFT TO RIGHT or single unit containing two pumps mounted in RIGHT TO LEFT switchlight , the associated piggyback fashion.
Page 133 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL MAIN CROSSFLOW MAIN OVERFLOW LINE OVERFLOW LINE EJECTOR EJECTOR VALVE COLLECTOR COLLECTOR FLAPPER TANK TANK VALVE GRAVITY FLOW LINES GRAVITY FLOW LINES FLOAT FLOAT VALVE VALVE FLAPPER FLAPPER VALVES VALVES TRANSFER...
Page 134 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL MAIN CROSSFLOW MAIN OVERFLOW LINE OVERFLOW LINE EJECTOR VALVE EJECTOR COLLECTOR COLLECTOR FLAPPER TANK TANK VALVE GRAVITY FLOW LINES GRAVITY FLOW LINES FLOAT FLOAT VALVE VALVE FLAPPER FLAPPER VALVES VALVES TRANSFER...
Page 135 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL MAIN CROSSFLOW MAIN OVERFLOW LINE OVERFLOW LINE EJECTOR VALVE EJECTOR COLLECTOR COLLECTOR TANK TANK FLAPPER VALVE GRAVITY FLOW LINES GRAVITY FLOW LINES FLOAT FLOAT VALVE VALVE FLAPPER FLAPPER VALVES VALVES TRANSFER...
Page 136: Apu Fuel System
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL The APU fuel feed line is fitted with two APU APU FUEL SYSTEM fuel shutoff valves that are synchronized and controlled by the APU electronic control unit. The APU is normally supplied with fuel from To ensure uninterrupted operation of the APU the right main tank by an electric fuel pump.
Page 137: Fuel Controls And Indicators
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL RIGHT MAIN TANK STANDBY PUMPS FROM LEFT MAIN EJECTOR FUEL PUMP CENTER TANK TO PNEUMATIC PRESSURE SYSTEM SWITCH TO LEFT LOAD ENGINE APU FUEL FEED APU NEGATIVE-G CONTROL RESTRICTOR SHUTOFF VALVE SHUTOFF VALVE...
Page 138 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL FUEL CONTROL LEFT RIGHT PUSH ON OFF RIGHT LEFT PUMP X-FLOW PUMP SCAV SCAV OPEN MAIN INOP INOP MAIN VALVE VALVE FUEL CLOSED CLOSED FILTER FILTER °C PRESS PRESS L.
Page 139: Fuel Quantity
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL the valve is fully opened. The light extin- • A fuel temperature indicator in the cen- guishes when the valve is fully closed. Since ter of the fuel control panel indicates the valve is motor operated, expect a delay of the temperature of the fuel as it leaves approximately 2 seconds from the time the...
Page 140: Vent System
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL a slight positive tank pressure during flight due VENT SYSTEM to ram-air effect. Each tank is vented at two different points There are no valves or screens in the vent through a series of vent lines which allow air lines, so dirt or ice accumulation does not nor- to enter or escape the tanks, depending upon...
Page 141: Refueling
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL REFUELING PRESSURE REFUELING The pressure-refueling system (Figure 5-12) GENERAL consists of a single-point adapter, a pressure manifold containing a two-way check valve, All tanks are normally fueled by means of the three shutoff valves (SOV) associated with single-point pressure adapter located in the three float-operated, full level-control valves,...
Page 142 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL AUXILIARY TANK GRAVITY PRESSURE REFUEL- DEFUEL REFUELING PORT CONTROL PANEL MAIN TANK PRESSURE REFUELING GRAVITY REFUELING PORT ADAPTER Figure 5-13. Exterior Fueling Components FOR TRAINING PURPOSES ONLY 5-14 CL 601-3A...
Page 143 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL • Connect fueling nozzle from the truck • After 30–40 seconds, the SOV CLosed to the single-point adapter. light will illuminate and the OPen light will extinguish, indicating that the au- •...
Page 144: Defueling
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL • Check that the SOV OPen lights are il- The tanks may be selectively defueled using luminated. Add fuel to the desired level. the refuel-defuel control panel in the DEFUEL mode as follows: •...
Page 145: Tail Tank
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL TAIL TANK NORMAL TRANSFER With the ARMED—OFF switch on the tail tank GENERAL fuel transfer panel (Figure 5-17) set to ARMED, the fuel transfers automatically to the auxiliary An additional fuel tank, which will increase tank at the rate of approximately 25 pounds the fuel load by some 187.7 U.S.
Page 146: Fuel Jettison
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL The fuel transfer line has a nitrogen-pres- surized shroud in the rotor boost zone. A WARNING perforation in this shroud signals all open shutoff valves to close and shuts down the Do not jettison fuel in known light- boost pump.
Page 147 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL FUELING ADAPTER AUX TANK FUEL LEVEL NO. 1 AUX TANK AND MANIFOLD SWITCH LEVEL SWITCH PRIMARY LEFT RIGHT MAIN MAIN TANK TANK TANK NO. 2 AUX TANK REAR FUELING LEVEL SWITCH LINE...
Page 148: Questions
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The engine-driven fuel pumps are nor- Flapper valves in the main tanks prevent: mally supplied with fuel by the: A. Reverse flow of fuel from the main A.
Page 149 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL When an amber MAIN light illuminates 13. The maximum negative pressure allowed on the fuel control panel: for single-point defueling is: A. The firewall shutoff valves close au- A.
Page 150 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 5 FUEL SYSTEM CONTENTS Page INTRODUCTION ........................5-1 GENERAL..........................5-1 FUEL STORAGE ........................5-2 FUEL DISTRIBUTION ......................5-3 Gravity Flow ........................5-3 Scavenge Ejectors ......................5-3 Main Ejectors ........................5-4 Transfer Ejectors ......................
Page 151 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL DEFUELING......................... 5-14 TAIL TANK........................... 5-15 General........................... 5-15 Normal Transfer......................5-15 Tail Tank Amber Warning Lights Versus Master Caution ..........5-16 Fuel Jettison ........................5-16 Refueling and Defueling....................5-16 QUESTIONS .........................
Page 152 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Fuel System—General Layout ................. 5-2 Fuel Distribution—Normal Operation ..............5-3 Fuel Distribution—Engine Start................5-4 Fuel Distribution—Abnormal Operation, Main Ejector Fail ........5-5 APU Fuel System—Normal Operation..............5-7 APU Fuel System—Negative G Condition ..............
Page 153: Introduction
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 5 FUEL SYSTEM MAIN FUEL LBS X 100 INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3R fuel system provides fuel for the two turbofan engines, as well as the auxiliary power unit (APU). Fuel is also used to cool the APU generator adapter oil and the main engine oil.
Page 154: Fuel Storage
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL The airplane may be refueled over the wings nance access panels in the lower surface of by gravity. However, the normal method is each wing. The gravity filler port for each through an adapter located in the right wing main tank is located on the upper outboard root using a single-point pressure system.
Page 155: Fuel Distribution
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL FUEL DISTRIBUTION SCAVENGE EJECTORS Gravity flow to the collector tanks is sup- GRAVITY FLOW plemented by scavenge ejectors located at the rear of the inboard section of each main Fuel flows by gravity within the main tanks tank.
Page 156: Main Ejectors
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL small-volume, high-pressure motive flow at cause illumination of an amber caution light the throat of the ejector into large-volume, in the cockpit, and will activate both standby low-pressure output at the ejector nozzle. electric pumps as long as the standby pump on the same side as the main ejector failure is se- lected on.
Page 157: Standby Electric Pumps
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL A one-way check valve in each transfer ejec- Once armed by cockpit switches, the standby tor prevents fuel migration from the main pumps operate automatically when the output tanks to the auxiliary tank.
Page 158: Engine-Driven Pumps
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL ENGINE-DRIVEN PUMPS APU FUEL SYSTEM Each two-stage engine-driven fuel pump is a The APU is normally supplied with fuel from single unit containing two pumps mounted in the right main tank by an electric fuel pump. piggyback fashion.
Page 159 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL RIGHT MAIN TANK STANDBY PUMPS FROM LEFT MAIN EJECTOR FUEL PUMP CENTER TANK TO PNEUMATIC PRESSURE SYSTEM SWITCH TO LEFT LOAD ENGINE APU FUEL FEED APU NEGATIVE-G CONTROL RESTRICTOR SHUTOFF VALVE SHUTOFF VALVE...
Page 160: Fuel Controls And Indicators
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL reminder. An interlock prevents simultane- FUEL CONTROLS ous operation of both switchlights. AND INDICATORS The remaining five lights for each engine pro- vide information as follows: GENERAL • The amber SCAV light illuminates to in- The fuel controls and indicators are grouped dicate an inoperative scavenge ejector.
Page 161 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL FUEL CONTROL LEFT RIGHT PUSH ON OFF RIGHT LEFT PUMP X-FLOW PUMP SCAV SCAV OPEN MAIN INOP INOP MAIN FUEL VALVE VALVE CLOSED CLOSED FILTER FILTER °C PRESS PRESS TAIL TANK DUMP...
Page 162: Fuel Quantity
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL The fuel quantity indicators are powered via FUEL QUANTITY the SDC as follows: The fuel quantity in each main tank as well as • RH, LH, the auxiliary tank is measured by a system of the capacitance-type transmitters located in AUX, TAIL ..
Page 163: Refueling
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL terminate under the trailing edge on each side PRESSURE REFUELING in a flush-mounted NACA scoop. The scoop, which has ice rejection capability, maintains The pressure-refueling system (Figure 5-10) a slight positive tank pressure during flight due consists of a single-point adapter, a pressure to ram-air effect.
Page 164 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL AUXILIARY TANK GRAVITY PRESSURE REFUEL- DEFUEL REFUELING PORT CONTROL PANEL MAIN TANK PRESSURE REFUELING GRAVITY REFUELING PORT ADAPTER Figure 5-9. Exterior Fueling Components FOR TRAINING PURPOSES ONLY 5-12 CL 601-3R...
Page 165 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL LEGEND VENT LINES REFUELING PRESSURE FUEL SINGLE-POINT TANK SOV MANIFOLD ADAPTER TWO-WAY CHECK VALVE LEVEL CONTROL VALVE VENT VENT VENT (RELIEF) TEST TEST VALVES* *NOTE VALVE * VALVE * ENERGIZED CLOSED DURING FUELING ONLY Figure 5-10.
Page 166: Defueling
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL • After 30–40 seconds, the SOV CLosed quantity panel. For this, AC electrical power light will illuminate and the OPen light must be provided, usually from the APU or will extinguish , indicating that the au- external AC unit.
Page 167: Tail Tank
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL • When the tank quantity decreases to the L. MAIN R. MAIN desired level, move the tank switch to OFF. This will cause the shutoff valve to close and the green CLOSED light TAIL will illuminate.
Page 168: Tail Tank Amber Warning Lights Versus Master Caution
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL Figure 5-13 shows the location of the con- SELECT/DUMP OPEN guarded switchlight. trols and lights. Figure 5-14 has the schematic Once armed, pressing the green DUMP OPEN of the tail tank system. switchlight causes it to illuminate and opens the jettison valve.
Page 169 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL FUELING ADAPTER AUX TANK FUEL LEVEL NO. 1 AUX TANK AND MANIFOLD SWITCH LEVEL SWITCH PRIMARY LEFT RIGHT MAIN MAIN TANK TANK TANK NO. 2 AUX TANK REAR FUELING LEVEL SWITCH LINE...
Page 170: Questions
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The engine-driven fuel pumps are nor- Flapper valves in the main tanks prevent: mally supplied with fuel by the: A. Reverse flow of fuel from the main A.
Page 171 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL When an amber MAIN light illuminates 13. The maximum negative pressure allowed on the fuel control panel: for single-point defueling is: A. The firewall shutoff valves close au- A.
Page 172 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 6 AUXILIARY POWER UNIT CONTENTS Page INTRODUCTION ........................6-1 GENERAL..........................6-1 AUXILIARY POWER UNIT (APU)..................6-2 General ..........................6-2 Major Sections ......................... 6-2 APU SYSTEMS ........................6-4 Lubricating System ......................
Page 173 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page APU Installation ....................... 6-2 APU Engine Cutaway....................6-3 APU Air Intake......................6-3 APU Exhaust Outlet ....................6-4 APU Control Panel ....................6-5 APU Remote Indicating Panel ................. 6-7 Auxiliary Battery Panel ....................
Page 174: Auxiliary Power Unit
FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 6 AUXILIARY POWER UNIT INTRODUCTION This chapter deals with the auxiliary power unit (APU) installed as standard equipment on the Canadair Challenger CL-600-2B16, model CL-601-3A/R. The APU renders the airplane completely independent of such ground servicing requirements as electrical power, pneumatic power for engine starting, and an air supply for the environmental systems.
Page 175: Auxiliary Power Unit (Apu)
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AUXILIARY POWER 4. Turbine UNIT (APU) 5. Exhaust 6. Accessory Gear GENERAL Air Intake The APU (Figure 6-1) is mounted on a skid support assembly enclosed in a fireproof metal The main air inlet to the compressor is located container in the aft equipment bay.
Page 176 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL LOAD CONTROL VALVE COMPRESSOR GEARBOX DC STARTER MOTOR AIR INTAKE EXHAUST DRIVE PADS FUEL CONTROL COMBUSTOR IGNITER TURBINE Figure 6-2. APU Engine Cutaway Figure 6-3. APU Air Intake FOR TRAINING PURPOSES ONLY CL 601-3A/R 6-3...
Page 177: Apu Systems
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Combustor Accessory Gear The combustor consists of a single combustion The accessory gear forms an integral part of chamber. The chamber is designed to provide the APU. It converts high turbine rpm to the for the proper mixing of air and fuel and con- speeds required for the APU accessories tainment of the combustion gases.
Page 178: Ignition System
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Fuel metering is controlled by a torque motor, INSTRUMENTATION operating in response to input signals from the electronic control unit. Fuel is metered to APU instrumentation consists of rpm and EGT the combustor so that the power developed by indicators (Figure 6-5) located on the APU the APU is equal to the power required, thereby...
Page 179: Bleed-Air Control System
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL BLEED-AIR CONTROL SYSTEM • The left engine 10th stage bleed-air switchlight is pushed in. General • The right engine 10th stage bleed-air The bleed-air control system consists of an switchlight and the bleed-air ISOL electropneumatic surge valve and an elec- switchlight are both pushed in.
Page 180 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL APU FAULT OVER- OVER SPEED CURRENT HIGH PRESS LOW TEMP HIGH GEN ADAPTER OIL PRESS LOW TEMP HIGH IND RESET APU STOP Figure 6-6. APU Remote Indicating Panel Remote Fault Panel In addition to the malfunction flags, the remote indicating panel has two push button switches,...
Page 181: Apu Starting System
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL APU STARTING SYSTEM luminate the APU GENerator OFF light (Figure 6-7). Four seconds later, the green APU ReaDY light will illuminate. The rpm and EGT will stabilize at the steady-state, no-load values.
Page 182: Apu Normal Shutdown
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL On aircraft with SB 601-0418 and serial num- bers 5135 and subsequent, a backup battery is provided to power the APU ECU during cold weather starts. While the APU ECU is pow- ered from the battery bus, it also receives power from the avionics IRS No.
Page 183: Questions
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS With the BATTERY MASTER switch APU ignition is activated when the: on, pushing in the PWR– FUEL switch- A. APU rpm reaches 10% during starting. light will: B.
Page 184: Powerplants
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 7 POWERPLANT CONTENTS Page INTRODUCTION ........................7-1 GENERAL..........................7-1 ENGINES ..........................7-2 General ..........................7-2 Major Sections ......................... 7-2 Operation.......................... 7-4 ENGINE SYSTEMS ....................... 7-5 Engine Oil System ......................7-5 Engine Fuel System ......................
Page 185 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page CF34 Major Sections and Gas Flow................. 7-2 CF34 Engine Modules....................7-3 Oil-Replenishing Control Panel ................7-5 Junction Box 4 (JB4)....................7-6 Oil Pressure and Temperature Indicators ..............7-7 Oil System Schematic ....................
Page 186: Introduction
FlightSafety Canada Lt ée Lt d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 7 POWERPLANT INTRODUCTION This chapter describes the powerplant of the Canadair Challenger CL-600-2B16, model CL-601-3A. In addition to the basic powerplant information, the chapter also includes information on all powerplant-related systems, such as engine oil, engine fuel, ignition, engine power control, instrumentation, engine starting, engine speed control and APR sys- tems, engine vibration monitoring, and thrust reversing.
Page 187: Engines
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ENGINES 1. Air inlet section 2. Fan section GENERAL 3. Compressor The engines (Figure 7-1) on the Canadair 4. Combustor Challenger are GE Series CF34. This engine has a high bypass ratio (6.2 to 1). The CF34 5.
Page 188 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL HIGH-PRESSURE COMBUSTION TURBINE SECTION SECTION COMPRESSOR SECTION FRONT FRAME FAN SECTION POWER TAKEOFF ASSEMBLY DRIVE SHAFT FAN DRIVE SHAFT LOW-PRESSURE TURBINE SECTION RADIAL ACCESSORY DRIVE GEARBOX SHAFT Figure 7-2. CF34 Engine Modules air to the compressor of the core engine and the The variable-geometry system is controlled by second path directs air into the fan bypass duct.
Page 189: Operation
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Combustor Accessory Gearbox The combustor includes a straight-flow an- The accessory gearbox is attached to the lower nular combustion chamber, a liner, and the side of the front frame. The gearbox is driven first-stage turbine inlet nozzle.
Page 190: Engine Systems
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ENGINE SYSTEMS Control An oil-replenishing control panel, powered The engine systems and engine-related systems from the battery direct bus (Figure 7-3) con- of the Canadair Challenger CL-601-3A are: tains a power switch, a green power ON light, and two green oil full switchlights labeled “LH •...
Page 191 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL A separate two-element scavenge pump provides across the filter element exceeds a preset for positive scavenging of the fan bearing sump limit, it causes the impending bypass indica- during all flight attitudes (climb or descent).
Page 192: Engine Fuel System
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ENGINE FUEL SYSTEM General The engine fuel system is an integrated hy- dromechanical-electronic system. The fuel sys- TEMP PRESS tem meters fuel to the combustor to provide for starting, acceleration, deceleration, and full power requirements under all operating conditions.
Page 193 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL FOR TRAINING PURPOSES ONLY 7-8 CL 601-3A...
Page 194 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Fuel Filter revert to a fixed temperature reference. If high thrust is set at the time of failure, a minor de- A bypass fuel filter removes solids from the crease in thrust may result.
Page 195: Ignition System
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Fuel Flow Distributor inputs representing N rpm and compressor discharge pressure, directs fuel pressure to The fuel flow distributor is a pressure-oper- the variable-geometry actuators to position ated unit that senses compressor discharge the inlet guide vanes and stator to produce a pressure and fuel pressure at opposite ends of safe surge margin across the compressor.
Page 196 LEFT COLLECTOR TANK INLET JET PUMP STATOR BOOST PUMP GUIDE COMBUSTOR VANES VANES INOP TO RIGHT COLLECTOR TANK INJECTORS FUEL FLOW 4000 3500 3000 18 FUEL HOSES FIREWALL VARIABLE 2000 SOV’S GEOMETRY FUEL FLOW ACTUATORS 1000 DISTRIBUTOR FEEDBACK TO APU FUEL LINE LINK DRAIN VALVE ECOLOGY TANK...
Page 197 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Ground Start Ignition will continue until the start cycle is termi- nated. Ignition and start termination will be in- The ground start ignition is integrated with the dicated when the ignition ON light and the engine start system from initiation of start to START light extinguish.
Page 198: Engine Power Control
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Control Thrust Levers The automatic ignition system is controlled by The individual engine thrust levers (Figure 7- the stall protection computer using inputs 9) operate in quadrant slots from a full aft po- from the angle-of-attack vanes.
Page 199 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL LEFT ENGINE LEGEND IGNITION CONTROL AC ESSENTIAL BUS RELAY BATTERY BUS A IGNITER POWER B IGNITER POWER FROM STALL PROTECTION FROM STALL PROTECTION STATIC INVERTER SYSTEM STATIC INVERTER C-28 B-169 AC ESSENTIAL BUS...
Page 200: Engine Instrumentation
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL the thrust levers. Clockwise rotation will in- for example, the left analog scale and the right crease friction, and counterclockwise rota- digital scale have the same power source. A tion will decrease friction.
Page 201 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL the corresponding SDC power supply by il- luminating all analog and digital displays in- cluding the fuel panel. Indications BLEED ADPTR PWR FUEL START/ ON/OFF STOP The amber light above the instrument test FAILED STARTER PRESS...
Page 202: Engine Starting
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL The analog scales are calibrated in pounds of 7-14) should show approximately 50 psi. Push fuel per hour from 0 to 4,000. The digital dis- IGN A or IGN B switchlight (Figure 7-8) to plays are in pounds per hours times 10.
Page 203 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL NOTE CAUTION Two conditions must be met before If idle speed stabilizes at approxi- moving the thrust lever to IDLE for mately 57% N , the engine must be all engine starting: shut down immediately and the con- dition reported to maintenance.
Page 204 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Figure 7-15. External Air Supply Adapter LEFT ENGINE RIGHT ENGINE RIGHT START LEFT START VALVE VALVE LEFT ISOLATION RIGHT BLEED-AIR VALVE BLEED-AIR 10TH STAGE 10TH STAGE BLEED-AIR BLEED-AIR LEGEND EXTERNAL AIR APU BLEED AIR...
Page 205 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Failure to Start tures below 15° C (59° F) the start sequence may exceed 60 seconds (Figure 7-18). Light-off as indicated by rising ITT will nor- mally occur within 10 seconds after moving Before attempting another start, dry motor the thrust lever to IDLE.
Page 206: Engine Speed Control And Apr Systems
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Airstarts Prior to initiating a windmilling airstart, all checklist items affecting the start must be Airstarts are divided into starter-assisted and completed. Then push the appropriate IN windmilling airstarts. FLighT START switchlight.
Page 207 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Control and Indication • Either or both N input signals are out of limits. A three-position switch (Figure 7-20) with p o s i t i o n s l a b e l e d “A R M ,” “ O F F,” a n d •...
Page 208 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL d. APR is still on N speed control (above 79% N ) and illuminates the green L. ON legend when it has e. Test (will remain on as long as TEST increased the required amount (approximately is held) 2% N...
Page 209 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL METERED FUEL TO COMBUSTOR FEEDBACK FEEDBACK DESIRED DESIRED POWER POWER FUEL CONTROL FUEL CONTROL LEGEND AMPLIFIER AMPLIFIER FUEL FLOW (ECU) (ECU) BATTERY POWER INPUT INPUT APR TRIGGER MV—METERING VALVE TM—TORQUE MOTOR INPUT POWER...
Page 210: Engine Vibration-Monitoring System
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ENGINE VIBRATION- Testing MONITORING SYSTEM The vibration indicating system can be tested by pressing and holding the HIGH VIBration General switchlight. The needles will show a vibration level of 4.0 mils DA and after 3 seconds, the An engine vibration-monitoring system con- amber HIGH VIB light will illuminate accom- tinuously monitors the vibration level of each...
Page 211: Thrust Reversers
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL side being tested will move to 4.0 MILLS DA. Forward movement of the translating sleeve When the switchlight is held pressed for more positions the blocker doors to lie flat and form than 3 seconds, the respective amber CORE part of the fan airflow exit nozzle.
Page 212 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL BYPASS AIRFLOW CORE AIRFLOW NORMAL OPERATION BYPASS AIRFLOW CORE AIRFLOW REVERSER DEPLOYED Figure 7-24. Thrust Reversers FOR TRAINING PURPOSES ONLY CL 601-3A 7-27...
Page 213: Indication
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL INDICATION Electrical control is provided by a dual-leg- end switchlight (Figure 7-25) for each thrust reverser. The switchlights are located on the reverse thrust control panel on the center pedestal.
Page 214: Operation
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Emergency Stow When thrust reversers are no longer required, move the thrust reverser levers to the full If the REVERSER UNLOCKED light remains stow position. The REVERSE THRUST light illuminated or cycles on and off during flight, and the REVERSER UNLOCKED light on the pushing the switchlight will back up the au-...
Page 215: Questions
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The CF 34 engine may be defined as a: Electrical power for engine ignition is supplied by the: A. Single-spool, medium-bypass turbofan A. Battery bus and essential AC bus B.
Page 216 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 7 POWERPLANT CONTENTS Page INTRODUCTION ........................7-1 GENERAL..........................7-1 ENGINES ..........................7-2 General ..........................7-2 Major Sections ......................... 7-2 Operation.......................... 7-4 ENGINE SYSTEMS ....................... 7-5 Engine Oil System ......................7-5 Engine Fuel System ......................
Page 217 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page CF34 Major Sections and Gas Flow................. 7-2 CF34 Engine Modules....................7-3 Oil-replenishing Control Panel................. 7-5 Junction Box 4 (JB4)....................7-6 Oil Pressure and Temperature Indicators ..............7-7 Oil System Schematic ....................
Page 218: Introduction
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 7 POWERPLANT INTRODUCTION This chapter describes the powerplant of the Canadair Challenger CL-600-2B16, model CL-601-3R. In addition to the basic powerplant information, the chapter also includes information on all powerplant-related systems, such as engine oil, engine fuel, ignition, engine power control, instrumentation, engine starting, engine speed control and APR sys- tems, engine vibration monitoring, and thrust reversing.
Page 219: Engines
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL 1. Air inlet section ENGINES 2. Fan section GENERAL 3. Compressor The engines (Figure 7-1) on the Canadair Chal- 4. Combustor lenger are GE Series CF 34. This engine has a high bypass ratio (6.2 to 1).
Page 220 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL HIGH-PRESSURE COMBUSTION TURBINE SECTION SECTION COMPRESSOR SECTION FRONT FRAME FAN SECTION POWER TAKEOFF ASSEMBLY DRIVE SHAFT FAN DRIVE SHAFT LOW-PRESSURE TURBINE SECTION RADIAL ACCESSORY DRIVE GEARBOX SHAFT Figure 7-2. CF34 Engine Modules air to the compressor of the core engine and the The variable-geometry system is controlled by second path directs air into the fan bypass duct.
Page 221: Operation
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL Combustor Accessory Gearbox The combustor includes a straight-flow an- The accessory gearbox is attached to the lower nular combustion chamber, a liner, and the side of the front frame. The gearbox is driven first-stage turbine inlet nozzle.
Page 222: Engine Systems
FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL ENGINE SYSTEMS Control An oil-replenishing control panel, powered The engine systems and engine-related systems from the battery direct bus (Figure 7-3) con- of the Canadair Challenger CL-601-3R are: tains a power switch, a green power ON light, and two green oil full switchlights labeled “LH •...
Page 223 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL A separate two-element scavenge pump provides the filter element exceeds a preset limit, it for positive scavenging of the fan bearing sump causes the impending bypass indicator on during all flight attitudes (climb or descent).
Page 224: Engine Fuel System
FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL ENGINE FUEL SYSTEM General The engine fuel system is an integrated hy- dromechanical-electronic system. The fuel sys- tem meters fuel to the combustor to provide for TEMP PRESS starting, acceleration, deceleration, and full power requirements under all operating conditions.
Page 225 SUMP VENT REGULATOR LEGEND A SUMP B SUMP C SUMP SUPPLY OIL PRESSURE SCAVENGE OIL FUEL COMPRESSOR COMPRESSOR TURBINE VENT LINES BEARINGS BEARINGS BEARINGS BEARINGS ELECTRICAL CHIP DETECTOR CHIP DETECTOR RESTRICTOR BYPASS VALVE PRESSURE TRANSDUCER AND ∆ LOW-PRESSURE CHIP WARNING SWITCH DETECTORS FILTER COOLER...
Page 226 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL is set at the time of failure, a minor decrease in Fuel Filter thrust may result. If failure occurs at idle thrust, A bypass fuel filter removes solids from the possible compressor damage can result if an at- fuel.
Page 227 LEFT COLLECTOR TANK INLET JET PUMP STATOR GUIDE COMBUSTOR BOOST PUMP VANES VANES INOP TO RIGHT COLLECTOR TANK INJECTORS FUEL FLOW 4000 3500 3000 FIREWALL 2000 VARIABLE SOV’S GEOMETRY 1000 ACTUATORS FEEDBACK TO APU FUEL LINE LINK P 3 T 2 C VALVE CLOSED FILTER...
Page 228: Ignition System
FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL The ignition system for each engine consists Operation of an ignitor plug A and an ignitor plug B in Figure 7-7 illustrates operation of the fuel the combustor with each ignitor powered system in its simplest form.
Page 229 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL Continuous Ignition and Indication Continuous ignition is primarily used as an IGNITION anti-flameout ignition. When selected, it pow- ers one ignition exciter continuously on both IGN A IGN B CONT engines.
Page 230 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL LEFT ENGINE LEGEND IGNITION CONTROL AC ESSENTIAL BUS RELAY BATTERY BUS A IGNITER POWER B IGNITER POWER FROM STALL PROTECTION FROM STALL PROTECTION STATIC INVERTER SYSTEM STATIC INVERTER C-28 B-169 AC ESSENTIAL BUS BATTERY BUS...
Page 231: Engine Power Control
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL The switchlights on the ignition and start con- thrust lever can be moved to or from the SHUT trol panel provide for ignition arming and se- OFF position. lection of the ground start ignition mode, the continuous ignition mode, and the in-flight A go-around button is mounted in each thrust...
Page 232 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL Automatic Dimming A photoelectric cell (Figure 7-12) is provided on the engine instrument control panel to pro- vide for automatic engine instrument dim- ming as ambient light conditions change. A FUEL rheostat on the same panel allows the crew to °C...
Page 233: Engine Starting
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL (Fan) RPM ENGINE STARTING (fan) rpm (Figure 7-11) is sensed by a General monopole transmitter located on the engine front frame. Electrical signals are sent via the Engine starting is divided into ground starts, SDC to the appropriate analog and digital starter-assisted airstarts, and windmilling airstarts.
Page 234 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL FLOOR STOP is provided to prevent from decreasing below 56.9%. CAUTION BLEED ADPTR PWR FUEL START/ ON/OFF STOP FAILED STARTER PRESS CLOSED PRESS If idle speed stabilizes at approxi- PUMP OPEN TEMP...
Page 235 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL Figure 7-15. External Air Supply Adapter LEFT ENGINE RIGHT ENGINE RIGHT START LEFT START VALVE VALVE LEFT ISOLATION RIGHT BLEED-AIR VALVE BLEED-AIR 10TH STAGE 10TH STAGE BLEED-AIR BLEED-AIR LEGEND EXTERNAL AIR APU BLEED AIR...
Page 236 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL above 15°C (59°F) the start should be aborted Ground Start (Cross Bleed Air) by pushing the STOP switchlight anytime up The procedures for a ground start using a cross to 55% N rpm.
Page 237 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL TIME FROM THROTTLE OPENING TO LIGHT-OFF TOTAL TIME TO STABILIZED IDLE –20 –40 Figure 7-18. Maximum Allowable Start Time and Time to Stabilized Idle—Seconds WARNING AIRSTART ALTITUDE LIMIT WINDMILL START Airstarts, windmilling or starter- 10,000–21,000 FT...
Page 238: Engine Speed Control And Apr Systems
FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL START switchlight again. The green light and the IGN A and B ON lights will extinguish, then complete the After Start checklist. ENGINE SPEED CONTROL AND APR SYSTEMS General The automatic performance reserve (APR) is a solid-state system which constantly moni- tors the thrust of both engines during takeoff.
Page 239 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL NOTE Dynamic Test The APR system is used only for The dynamic test is done just prior to flight. takeoff and is then disarmed. The It is automatically performed for both engines APR fail light is inhibited in flight by the APR controller and verifies that the through WOW logic and for landing...
Page 240 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL METERED FUEL TO COMBUSTOR FEEDBACK FEEDBACK DESIRED DESIRED POWER POWER FUEL CONTROL FUEL CONTROL LEGEND AMPLIFIER AMPLIFIER FUEL FLOW (ECU) (ECU) BATTERY POWER INPUT INPUT APR TRIGGER MV—METERING VALVE TM—TORQUE MOTOR INPUT POWER...
Page 241: Engine Vibration-Monitoring System
FlightSafety Canada L té e L td. CL-600-2B16 PILOT TRAINING MANUAL ENGINE VIBRATION- indicator panel; in turn, the pointer on the side being tested will move to 4.0 mils DA. MONITORING SYSTEM When the switchlight is held pressed for more than 3 seconds, the respective amber CORE General and FAN lights will illuminate accompanied...
Page 242: Control
FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL gaged to prevent more than 20° of lever travel CONTROL while the air motor operates the ballscrew The thrust reversers are controlled by levers jacks to drive the translating sleeve aft, ex- (Figure 7-10) piggyback-mounted on the thrust posing the cascade vanes and closing the 10 levers.
Page 243: Indication
FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL INDICATION Electrical control is provided by a dual-leg- end switchlight (Figure 7-24) for each thrust reverser. The switchlights are located on the reverse thrust control panel on the center pedestal.
Page 244 FlightSafety Canada Lt é e Lt d. CL-600-2B16 PILOT TRAINING MANUAL When thrust reversers are no longer required, Emergency Stow move the thrust reverser levers to the full If the REVERSER UNLOCKED light remains stow position. The REVERSE THRUST light illuminated or cycles on and off during flight, and the REVERSER UNLOCKED light on the pushing the switchlight will back up the au-...
Page 245 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The CF 34 engine may be defined as a: Electrical power for engine ignition is supplied by the: A. Single-spool, medium-bypass turbo- A. Battery bus and essential AC bus B.
Page 246 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 8 FIRE PROTECTION CONTENTS Page INTRODUCTION ........................8-1 GENERAL..........................8-2 FIRE DETECTION ......................... 8-2 General ..........................8-2 Components ........................8-2 Operation.......................... 8-4 System Test ........................8-4 FIRE EXTINGUISHING ......................8-4 General ..........................
Page 247 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Engine Fire Detection Components ................. 8-3 Fire-Sensing Loop ....................8-3 Engine Fire Detection System.................. 8-5 Engine Firex Bottle ....................8-6 Engine Fire-Extinguishing System................8-7 APU Firex Bottle Installation...................
Page 248: Fire Protection
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 8 FIRE PROTECTION FIRE WARN FIRE PULL INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3A/R fire protection system pro- vides the means for detecting and extinguishing fires in the engines and auxiliary power unit.
Page 249: General
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL GENERAL In addition, the systems detect failures in the loops and will usually advise the flight crew if a loop resistance falls to zero instantaneously, Fire and overheat detection is provided for such as might happen for a short circuit.
Page 250 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ENGINE ENGINE COMBUSTION-ZONE COMBUSTION-ZONE SENSING ELEMENT SENSING ELEMENT FIRE PUSH BOTTLE ARMED PUSH TO DISCH SENSING ELEMENT Figure 8-1. Engine and APU Fire Detection Components OUTER CONDUCTOR (GROUNDED) INSULATOR INNER CONDUCTOR...
Page 251: Operation
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ENG FIRE and APU FIRE Lights If a fire and overheat detection control unit detects a false warning signal caused by a short These lights are located in the center of the in a sensing cable, it powers the appropriate glareshield.
Page 252 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ENGINE ENGINE COMBUSTION-ZONE COMBUSTION-ZONE SENSING ELEMENT SENSING ELEMENT TO FIRE BELL TO MASTER CAUTION (FIRE FAULT) Figure 8-3. Engine Fire Detection System Engine Firex Bottles valve prevents one bottle from discharging its contents into the other bottle (if it is empty).
Page 253 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL BOTTLE ARMED Lights These switchlights, located in the center of the glareshield, illuminate when either ENG FIRE light is depressed. If either bottle has pressure below 275 psi, its associated light will not illuminate.
Page 254: Apu Fire Extinguishing
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ENG FIREX ENG FIREX BOTTLE BOTTLE Figure 8-5. Engine Fire-Extinguishing System APU FIRE EXTINGUISHING The electrically operated port is connected by tub- ing to the APU compartment and contains a squib The APU fire-extinguishing system operates (with dual-firing cartridges for redundancy).
Page 255 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL APU FIREX BOTTLE Figure 8-6. APU Firex Bottle Installation FOR TRAINING PURPOSES ONLY 8-8 CL 601-3A/R...
Page 256 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL APU FIREX BOTTLE Figure 8-7. APU Fire-Extinguishing System APU FIRE Light BOTTLE ARMED Light The unguarded APU FIRE switchlight is lo- This switchlight, located adjacent to the FIRE cated in the center of the glareshield (Figure light, illuminates whenever the FIRE light is 8-7).
Page 257: Operation
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Firex Monitor Panel • The bottle 1 pressure drops, causing the green BOTTLE 1 ARMED light to ex- This panel contains the split legend green tinguish and the amber BOTTLE 1 LOW SQUIB and amber LO PRESS test switchlight.
Page 258: Portable Extinguisher
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL PORTABLE EXTINGUISHER A portable fire extinguisher is located in the flight compartment on the bulkhead behind the copilot's seat (Figure 8-8). The extinguisher is charged with Halon 1211 extinguishing agent and is suitable for use on Classes A, B, DISCHARGE and C fires.
Page 259: Main Landing Gear Bay Overheat Detection
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MAIN LANDING GEAR One detection loop is attached to the top of each main wheel well bin. The OVHT and BAY OVERHEAT OVHT WARN FAIL switchlights are located below the landing gear control panel.
Page 260: Test
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL loops have cooled sufficiently, the OVHT test). When the red OVHT light illuminates, switchlight extinguishes. The gear may be re- it indicates that: tracted in accordance with AFM procedure. •...
Page 261: Engine Jet Pipe/Pylon Overheat Detection
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ENGINE JET PIPE/PYLON The engine jet pipe/pylon panel is located on the top right corner of the center instrument OVERHEAT DETECTION panel. It incorporates four press-to-test switch- lights, two labeled “OVHT”...
Page 262: Operation
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL OPERATION Should a loop become shorted, the overheat de- tection unit illuminates the amber OVHT The sensing loops are connected in series and WARN FAIL light. This also brings up the will give a cockpit indication if they detect a flashing master caution lights and the engine temperature in excess of 375°F in the pylon and...
Page 263: Questions
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The area other than the engine and APU The number of Firex bottles that can be compartments that is provided with fire discharged into a single engine com- detection is the: partment is: A.
Page 264 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 9 PNEUMATICS CONTENTS Page INTRODUCTION ........................9-1 GENERAL..........................9-1 PNEUMATIC SUBSYSTEMS....................9-2 SUPPLY AND DISTRIBUTION .................... 9-2 BLEED-AIR VALVES (10TH STAGE) .................. 9-2 Control and Indication ..................... 9-2 Operation (10th Stage) .....................
Page 265 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Bleed-Air Panel ......................9-3 Engine Start and Ignition Control Panel ..............9-3 Bleed-Air Supply—Right Engine Operating ............9-4 Bleed-Air Supply—Normal Operation ..............9-5 Bleed-Air Supply—APU Operating.................
Page 266: Introduction
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 9 PNEUMATICS BLEED AIR INTRODUCTION This chapter describes the pneumatic system of the Canadair Challenger (CL-600-2B16, model CL-601-3A). The subsystems supplied from the pneumatic sources, as well as con- trol indications and pneumatic leak detection, are also discussed.
Page 267: Pneumatic Subsystems
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The bleed-air manifolds (10th and 14th stages) electropneumatic valves. These valves re- and their associated shutoff valves (SOV) are quire electrical power and pneumatic pressure located in the rear fuselage compartment. The to operate.
Page 268 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Automatic Control (10th Stage) Automatic opening of both engine bleed-air shutoff valves and the isolation valve will take place if electrical power and a pneumatic source are available, and either engine START switchlight (Figure 9-2) on the engine start and ignition control panel is pushed.
Page 269: Operation (10Th Stage)
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Pressure Indication The right side of the bleed-air manifold is pressurized, and pressure indication is avail- (10th Stage) able on the right scale of the bleed-air pres- sure indicator.
Page 270 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 9-4 illustrates the normal airborne con- to start the first engine. The second engine can figuration of the engine bleed-air system. Note be started using the same source or a cross that the bleed-air supply from the left engine bleed source from the operating (first) engine.
Page 271 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 9-5 illustrates the APU bleed-air sup- even though the line is fitted with a check ply. Unless prevented by the interlock de- valve. The isolation valve alone may be open scribed above, when the APU is operating and to permit the APU bleed air to pressurize the the APU RDY light is illuminated, pushing the...
Page 272 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL An approved external air supply can be con- nected to an adapter (Figure 9-6) located in a covered access on the left side of the rear fuse- lage.
Page 273: Bleed-Air Valves (14Th Stage)
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL BLEED-AIR VALVES The valves are shut automatically whenever the appropriate ENG FIRE PUSH switchlight (14TH STAGE) is activated, and the BLEED CLOSED light will illuminate. Air from the single port at the 14th stage is used for wing and cowl anti-icing and thrust re- OPERATION (14TH STAGE) verser operation.
Page 274: General
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FOOTWARMER AND DEMIST SYSTEM GENERAL The footwarmer and demist system uses hot engine bleed air. Some temperature reduction conditioning is achieved by a heat exchanger that is cooled by ram airflow. The heat ex- changer also has an electric fan to provide cooling air on the ground.
Page 275 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL To prevent possible overheat damage to a heat exchanger where either ram air (in flight windshield, an overheat switch will deenergize operation) or fan air (ground operation) pro- both left and right footwarmer-demist shutoff vides the cooling medium.
Page 276: General
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL BLEED-AIR LEAK DETECTION GENERAL The bleed-air system can operate at extremely high temperatures and pressures. Therefore, structural damage and fatigue could result in catastrophic consequences if leakage occurs. 14 STAGE The insulation surrounding the bleed-air ducts RIGHT...
Page 277 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL DEMIST CONTROL KNOB EMER FOOTWARMER PRESS SOV CONTROL KNOB DUCT SENSOR PRESSURE HEAT PRESSURE RELIEF EXCHANGER PRESSURE RELIEF PRESSURE VALVE SWITCH VALVE SWITCH THRUST THRUST REVERSER REVERSER RAM AIR PRESSURIZATION...
Page 278: Questions
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS If the 10th-stage bleed-air shutoff valve A. Isolation valve to fail open is open, it will automatically close if: B. Bleed-air valves to remain in the po- sition selected.
Page 279 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 9 PNEUMATICS CONTENTS Page INTRODUCTION ........................9-1 GENERAL..........................9-1 PNEUMATIC SUBSYSTEMS....................9-2 SUPPLY AND DISTRIBUTION .................... 9-2 BLEED-AIR VALVES (10TH STAGE) .................. 9-2 Control and Indication ..................... 9-2 Operation (10th Stage) .....................
Page 280 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Bleed-Air Panel ......................9-3 Engine Start and Ignition Control Panel ..............9-3 Bleed-Air Supply—Right Engine Operating ............9-4 Bleed-Air Supply—Normal Operation ..............9-5 Bleed-Air Supply—APU Operating.................
Page 281: Introduction
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 9 PNEUMATICS BLEED AIR INTRODUCTION This chapter describes the pneumatic system of the Canadair Challenger (CL-600-2B16, model CL-601-3R). The subsystems supplied from the pneumatic sources, as well as con- trol indications and pneumatic leak detection, are also discussed.
Page 282: Pneumatic Subsystems
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The bleed-air manifolds (10th and 14th stages) BLEED-AIR VALVES and their associated shutoff valves (SOV) are (10TH STAGE) located in the rear fuselage compartment. The 10th stage provides air to the air conditioners, pressurization jet pump, and air turbine The 10th-stage bleed-air manifold supply is starters.
Page 283 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL shutoff valves and the isolation valve will au- 14TH STAGE 10TH tomatically close at the termination of start, PUSH BLEED BLEED CLOSED CLOSED the BLEED CLOSED lights will illuminate, DUCT DUCT BLEED...
Page 284: Operation (10Th Stage)
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL OPERATION (10TH STAGE) The pressurization jet pump is supplied from up- stream of the right engine bleed-air shutoff valve. Figure 9-3 illustrates that the right engine is operating and the right bleed-air shutoff valve Both sides of the manifolds can be pressurized is open.
Page 285 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The engines incorporate air turbine starters Prior to selecting an engine start using APU (ATS), therefore, a bleed-air source is required bleed air, both engine bleed-air switches must to start the first engine.
Page 286 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 9-5 illustrates the APU bleed-air sup- Initiating an engine start (either engine) while ply. Unless prevented by the interlock de- the APU is supplying the manifold will auto- scribed above, when the APU is operating and matically open both engine bleed-air shutoff the APU RDY light is illuminated, pushing the...
Page 287 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 9-7 illustrates that the pneumatic sys- tem is being supplied from an external air- source. Basically, the external supply directs airflow to the left side of the 10th pneumatic manifold.
Page 288: Bleed-Air Valves (14Th Stage)
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL BLEED-AIR VALVES activated, and the BLEED CLOSED light will illuminate. (14TH STAGE) OPERATION (14TH STAGE) Air from the single port at the 14th stage is used for wing and cowl anti-icing and thrust Before starting the engine, the switchlights are reverser operation.
Page 289: Footwarmer And Demist System
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FOOTWARMER The system is turned ON and OFF by selec- tion of a two position switch mounted on the AND DEMIST SYSTEM temperature control panel on the right side console (Figure 9-10).
Page 290: Bleed-Air Leak Detection
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL footwarmer and windshield demist manifolds both have airflow. With the knob pulled all the way, only the windshield demist manifold re- ceives airflow. The fan and the heater are powered by 115 volts AC.
Page 291 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL INDICATION A red DUCT FAIL light (Annunciator Panel section) is located on the center instrument panel. This light will flash as a master warn- ing to alert the crew to a bleed-air leak. At the same time, a steady red DUCT FAIL light in one of the engine bleed-air switchlights (Figure 9-1) or a single red DUCT FAIL light...
Page 292 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL PRESSURE PRESSURE RELIEF RELIEF VALVE VALVE PRESSURE PRESSURE LH COWL SWITCH SWITCH RH COWL ANTI-ICE THRUST THRUST ANTI-ICE VALVE REVERSER REVERSER VALVE PRESSURIZATION RH ATS LH ATS JET PUMP VALVE VALVE...
Page 293 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS If the 10th-stage bleed-air shutoff valve The APU bleed-air supply is connected is open, it will automatically close if: to the pressure manifold: A. E i t h e r e n g i n e S TA RT s w i t c h i s A.
Page 294 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 10 ICE AND RAIN PROTECTION CONTENTS Page INTRODUCTION ......................... 10-1 GENERAL ..........................10-1 ICE DETECTION SYSTEM ....................10-3 General.......................... 10-3 Operation ........................10-3 Failure Detection......................10-4 Test Function........................
Page 295 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 10-1 Anti-iced Areas ...................... 10-2 10-2 Ice Detectors......................10-3 10-3 ICE DETECTOR Panel..................10-3 10-4 Cowl Anti-icing...................... 10-5 10-5 Engine Anti-icing Controls and Indicators ............10-5 10-6 Wing Anti-icing......................
Page 296: Ice And Rain Protection
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 10 ICE AND RAIN PROTECTION INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3A/R is equipped with both ice detection and anti-icing systems. The ice detection system warns the pilots of potential ice accumulation before it becomes visible on any airplane components.
Page 297 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL TOTAL AIR TEMPERATURE PROBE COWL PITOT-STATIC (RIGHT SIDE ONLY) HEADS ALT STATIC ICE DETECTORS PORTS ANGLE-OF-ATTACK VANES WING LEADING EDGES WINDSHIELDS SIDE WINDOWS COWL Figure 10-1. Anti-iced Areas FOR TRAINING PURPOSES ONLY 10-2 CL 601-3A/R...
Page 298: General
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL Figure 10-1 depicts the areas which are anti- the slipstream. The strut and probe contain iced on the Challenger. heating elements which deice the detectors after ice is detected. ICE DETECTION OPERATION SYSTEM...
Page 299: General
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL When ice is detected, the crew must activate ANTI-ICING SYSTEMS the wing and cowl anti-icing systems. This causes the white ICE lights on the right side PNEUMATICALLY OPERATED of the panel to illuminate and the red (Canadian amber) ICE lights to extinguish.
Page 300 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL PRESSURE PRESSURE RELIEF SWTCH VALVE COWL ANTI-ICE VALVE 14TH STAGE BLEED-AIR SOV WING ANTI-ICE VALVE Figure 10-4. Cowl Anti-icing Controls and Indicators The cowl anti-icing system is controlled by a pair of split-legend switchlights on the anti-ice panel located on the right side of the overhead panel (see Figure 10-5 and Annunciator Panel...
Page 301 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL builds to above the trip point of the pressure The 14th-stage bleed-air shutoff valves must be switch. If the system is not selected on, illu- open to provide air for the wing anti-icing system. mination of a FAIL light indicates valve fail- ure in the open position.
Page 302 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL The temperature sensor will detect sufficient heat (85°F) and will turn on the white HEAT lights. If the overheat sensor detects an over- heat condition (265°F), it will illuminate the OVHT light.
Page 303: Electrically Operated Systems
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL for low pressure only. The red light labeled ELECTRICALLY OPERATED “OVHT” will illuminate if the overheat switch SYSTEMS senses a leading-edge temperature above nor- mal limits. The light could be an indication that General the automatic controller is malfunctioning and may be accompanied by the amber SEN-...
Page 304 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL This prevents fogging of the panels. The for- Temperature in the left and right panels is ward windshields operate at higher tempera- controlled by two independent anti-icing con- tures to provide anti-icing.
Page 305 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Controls and Indicators A PRESS TO TEST pushbutton, located on the anti-icing control panel, tests both the left and Windshield anti-ice and side window defog- right systems. When the button is pressed, a ging are controlled by a pair of three-posi- signal is sent to override the temperature sen- tion WSHLD switches on the right side of the...
Page 306 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL A % HTR CURRENT meter is located to the Failure of the heater in either left or right right of the PWR & METER SELECT switch. pitot-static probe causes illumination of the ap- Placing the rotary switch in any of the seven ON propriate amber PITOT HEAT light located on positions allows the crew to monitor the cur-...
Page 307 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Failure of any of the other five heaters is in- dicated by illumination of the HTR FAIL light on the ADS heater control panel. Illumination of either PITOT HEAT light or the HTR FAIL light is accompanied by illu- mination of the ANTI-ICE annunciator and the flashing MASTER CAUTION lights.
Page 308 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS Illumination of the flashing red ICE lights The wing anti-ice HEAT lights illumi- indicates that: nate to indicate that: A. The anti-icing system has been acti- A. A minimum acceptable temperature vated automatically.
Page 309 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 10. Pulling the DC essential bus ADS HTR CONT circuit breaker: A. Deactivates all the ADS heaters B. Activates all the ADS heaters C. Deactivates the pitot-static heaters in case of a feeder fault D.
Page 310 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 11 AIR CONDITIONING CONTENTS Page INTRODUCTION ......................11-1A GENERAL.......................... 11-1A ENVIRONMENTAL REQUIREMENTS ................11-2A AIR CONDITIONING ....................... 11-2A General ........................11-2A Humidity Control ......................11-2A TEMPERATURE CONTROL .................... 11-2A General ........................
Page 311 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL RAM-AIR VENTILATION....................11-8A General ........................11-8A Control......................... 11-8A QUESTIONS ........................11-9A FOR TRAINING PURPOSES ONLY 11-ii CL 601-3A...
Page 312 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 11-1 Temperature Control Panel.................. 11-3A 11-2 Bleed-Air Panel ....................11-4A 11-3 Air-Conditioning Distribution ................11-5A 11-4 APU Control Panel ....................11-5A 11-5 Air-Conditioning Airflow Schematic ..............11-7A 11-6 Ram-Air Inlet.......................
Page 313: Air Conditioning
FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 11 AIR CONDITIONING INTRODUCTION This chapter deals with the air-conditioning system of the Canadair Challenger CL-600- 2B16, model CL-601-3A. The description also includes such auxiliary systems as the temperature control system, the instrument panel cooling system, ventilation of the avionics bay, and ram-air ventilation.
Page 314: Environmental Requirements
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL primary airflow to the cockpit is from the left HUMIDITY CONTROL ACU. The right ACU supplies the cabin area. Each ACU has a mechanical water separator The ACU delivery ducts are interconnected by that removes water droplets by swirl action, balance ducts to provide a more even distri-...
Page 315: Temperature Control
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL from the circuit and the temperature selector output signals are directed to the affected tem- perature control valve. TEMPERATURE CONTROL The temperature range in this mode extends from a low of 2°...
Page 316: Acu Valves
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ACU VALVES AIR switchlight and the OPEN light for the ISOL switchlight will extinguish. Each ACU has a dual-pressure regulating and shutoff valve controlled through separate ACU If a problem is caused by overtemperature in switch-lights labeled “L”...
Page 317 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL LEGEND COLD AIR LEFT ACU SUPPLIES: CABIN CONDITIONED AIR COLD AIR FOR CABIN COCKPIT CONDITIONED AIR CONDITIONED AIR FOR CABIN AIR EXHAUST— CABIN AND COCKPIT VENTED UNDERFLOOR ACU'S AND RAM AIR RIGHT ACU SUPPLIES: COLD AIR FOR CABIN...
Page 318: Ground Operation
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL NOTE directed to the cabin conditioned air outlets. The crossover, or balance, ducts also allow this The left and right engine bleed-air air to enter the cockpit conditioned air ducts. switches must remain off.
Page 319 LEGEND RAM AIR ACU VALVE BLEED AIR HOT BLEED AIR MANIFOLD EJECTOR EJECTOR PRECOOLED HOT BLEED AIR VALVE COOLED BLEED AIR ACU COMPRESSOR AIR COOLED ACU COMPRESSOR AIR COLD AIR SERVO PRESSURE REGULATOR CONDITIONED AIR ACU THERMAL WATER TURBINE COMPRESSOR PRECOOLER COLD AIR SAFETY SWITCH...
Page 320 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL RAM-AIR VENTILATION CONTROL The ram-air ventilation system is controlled GENERAL by a guarded switchlight (labeled “RAM AIR VENT”) on the pressurization control panel The ram-air ventilation system may be used (Figure 11-7).
Page 321 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS Air conditioning of the Challenger is If the engines are not operating, the APU achieved by: has started, the APU READY light is on, and the APU fails to deliver air to the A.
Page 322 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 11 AIR CONDITIONING CONTENTS Page INTRODUCTION ......................11-1R GENERAL.......................... 11-1R ENVIRONMENTAL REQUIREMENTS ................11-2R AIR CONDITIONING ....................... 11-2R General ........................11-2R Humidity Control ......................11-2R TEMPERATURE CONTROL .................... 11-2R General ........................
Page 323 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL RAM-AIR VENTILATION....................11-8R General ........................11-8R Control......................... 11-8R QUESTIONS ........................11-9R FOR TRAINING PURPOSES ONLY 11-ii CL 601-3R...
Page 324 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 11-1 Temperature Control Panel.................. 11-3R 11-2 Bleed-Air Panel ....................11-4R 11-3 Air-Conditioning Distribution ................11-5R 11-4 APU Control Panel ....................11-5R 11-5 Air-Conditioning Airflow Schematic ..............11-7R 11-6 Ram-Air Inlet.......................
Page 325 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 11 AIR CONDITIONING INTRODUCTION This chapter deals with the air-conditioning system of the Canadair Challenger CL-600- 2B16, model CL-601-3R. The description also includes such auxiliary systems as the temperature control system, the instrument panel cooling system, ventilation of the avionics bay, and ram-air ventilation.
Page 326: Environmental Requirements
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL primary airflow to the cockpit is from the left HUMIDITY CONTROL ACU. The right ACU supplies the cabin area. Each ACU has a mechanical water separator The ACU delivery ducts are interconnected by that removes water droplets by swirl action, balance ducts to provide a more even distri-...
Page 327: Temperature Control
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL output signals are directed to the affected tem- perature control valve. The temperature range in this mode extends TEMPERATURE CONTROL from a low of 2°C (35°F) to a high of 99°C COCKPIT HEAT (210°F).
Page 328: Acu Valves
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AIR switchlight and the OPEN light for the ISOL switchlight will extinguish. L-14TH STAGE-R 10TH PUSH BLEED BLEED CLOSED CLOSED BLEED If a problem is caused by overtemperature in DUCT DUCT FAIL...
Page 329: General
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL LEGEND COLD AIR LEFT ACU SUPPLIES: CABIN CONDITIONED AIR COLD AIR FOR CABIN COCKPIT CONDITIONED AIR CONDITIONED AIR FOR CABIN AIR EXHAUST— CABIN AND COCKPIT VENTED UNDERFLOOR ACU'S AND RAM AIR RIGHT ACU SUPPLIES: COLD AIR FOR CABIN...
Page 330: Ground Operation
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL bleed-air panel. Pressure will be approxi- and temperature increase occurs. Outflow mately 50 psi. APU bleed air can be supplied from the ACU compressor is directed through to the right side of the bleed-air manifold by the secondary heat exchanger where temper- pushing the ISOL switchlight.
Page 331 LEGEND BLEED AIR SWIRL FILTER RAM AIR ACU VALVE BLEED AIR HOT BLEED AIR MANIFOLD EJECTOR EJECTOR PRECOOLED HOT BLEED AIR VALVE COOLED BLEED AIR ACU COMPRESSOR AIR COOLED ACU COMPRESSOR AIR SERVO COLD AIR PRESSURE REGULATOR CONDITIONED AIR ACU THERMAL WATER TURBINE COMPRESSOR...
Page 332 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL RAM-AIR VENTILATION CONTROL The ram-air ventilation system is controlled GENERAL by a guarded switchlight (labeled “RAM AIR VENT”) on the pressurization control panel The ram-air ventilation system may be used (Figure 11-7).
Page 333 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS Air conditioning of the Challenger is If the engines are not operating, the APU achieved by: has started, the APU READY light is on, and the APU fails to deliver air to the A.
Page 334 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 12 PRESSURIZATION CONTENTS Page INTRODUCTION ......................12-1A GENERAL.......................... 12-1A PRESSURIZATION ......................12-2A General........................12-2A Air Sources........................12-2A MAJOR COMPONENTS....................12-2A Automatic Selector..................... 12-2A Manual Regulator......................12-3A Outflow Valves......................12-3A Jet Pump........................
Page 335 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Automatic Mode ......................12-6A Manual Mode ......................12-6A EMERGENCY PRESSURIZATION ................. 12-8A General........................12-8A Air Source ........................12-8A Control ........................12-8A Operation........................12-8A Cabin Altitude Control....................12-8A EMERGENCY DEPRESSURIZATION................
Page 336 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 12-1 Pressurization Control Panel ................12-2A 12-2 Cabin Altimeter—Differential—Rate Indicator..........12-4A 12-3 Outflow Valve (Typical) ..................12-7A 12-4 Pressurization Profile ..................12-7A 12-5 Emergency Pressurization Schematic ..............12-9A 12-6 Footwarmer and Demist Controls ...............
Page 337: Pressurization
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 12 PRESSURIZATION INTRODUCTION This chapter deals with the pressurization system of the Canadair Challenger CL-600- 2B16, model CL-601-3A. Chapter 11 described the controlled inflow of air to the oc- cupied areas of the airplane and the conditioning of that air supply to achieve and maintain the desired temperatures.
Page 338: General
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL throughout the operating envelope. Dual safety Chapter 9, “Pneumatics,” and Chapter 11, “Air systems limit maximum cabin pressure dif- Conditioning,” for bleed-air operation.) ferential if the normal controls fail. Additional The emergency source of air pressurization is dual safety override controls limit cabin alti- the left engine’s compressor.
Page 339: Manual Regulator
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL In the lower right corner, the knob marked OUTFLOW VALVES “B” is used for setting barometric pressure. The knob moves an arrowhead pointer across Two outflow valves are located on the rear a barometric pressure scale at the bottom of pressure bulkhead to meter air from the oc- the automatic selector.
Page 340: Protection Systems
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL INDICATIONS PROTECTION SYSTEMS When electrical power is initially provided, or The protection systems incorporated in the the mode selector switch is moved to auto pressurization system are: from manual, the computerized controller per- forms a self-test which, if successful, illumi- •...
Page 341: Negative Pressure Relief
FlightSafety Canada Lt ée Lt d. CL-600-2B16 PILOT TRAINING MANUAL NEGATIVE PRESSURE RELIEF mode and the automatic selector controls the left outflow valve, causing both valves to go A negative pressure-relief feature is part of to the full open position. This condition will each outflow valve to prevent atmospheric prevail until the thrust levers are advanced pressure from exceeding cabin pressure.
Page 342: Flight Mode
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL FLIGHT MODE MANUAL MODE The manual mode of operation is required if AUTOMATIC MODE the automatic mode malfunctions or if elec- trical power is lost. Constant monitoring of the After takeoff the control logic switches into cabin differential pressure will be necessary flight mode.
Page 343 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL TRUE STATIC PRESSURE CABIN PRESSURE TO PNEUMATIC OUTFLOW VALVE OVERPRESSURE LIMITER FILTER ALTITUDE LIMITER CABIN PRESSURE VACUUM LINE (TO AIR JET PUMP) CLOSING SPRING DIAPHRAGM CHAMBER CABIN ATMOSPHERE VALVE POPPET OUTER AMBIENT...
Page 344: Emergency Pressurization
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL EMERGENCY OPERATION PRESSURIZATION Figure 12-5 illustrates operation of the emer- gency pressurization system. Notice that all normal bleed-air valves are closed. An air GENERAL supply directly from the left engine is routed through the left footwarmer-demist valve to the An emergency pressurization system must be heat exchanger.
Page 345 FlightSafety Canada Lt ée Lt d. CL-600-2B16 PILOT TRAINING MANUAL DEMIST CONTROL KNOB EMER FOOTWARMER PRESS SOV CONTROL KNOB DUCT SENSOR HEAT EXCHANGER RAM AIR PRESSURIZATION JET PUMP RH FOOT-WARMER LH FOOT-WARMER VALVE (NORM) VALVE (STBY) ATS VALVE LH 10TH STAGE RH 10TH STAGE BLEED-AIR BLEED-AIR...
Page 346: Emergency Depressurization
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL EMERGENCY DEPRESSURIZATION GENERAL An emergency depressurization system is avail- able to provide rapid decompression of the air- p l a n e w h e n a n e m e rg e n cy s u c h a s a i r contamination, cabin fire, or failure of the max- imum differential control occurs (other situations may also require emergency depressurization).
Page 347 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The electrical power supply for automatic When the EMERgency DEPRESSuriza- pressurization control is supplied from: tion switchlight is pushed, it will: A. DC bus 2 A. Open the ram-air valve and close the engine bleed-air valves.
Page 348 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 12 PRESSURIZATION CONTENTS Page INTRODUCTION ......................12-1R GENERAL.......................... 12-1R PRESSURIZATION ......................12-2R General........................12-2R Air Sources........................12-2R MAJOR COMPONENTS....................12-2R Automatic Selector..................... 12-2R Manual Regulator......................12-3R Outflow Valves......................12-3R Jet Pump........................
Page 349 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Automatic Mode ......................12-6R Manual Mode ......................12-8R EMERGENCY DEPRESSURIZATION................12-8R General........................12-8R Control ........................12-8R Cabin Altitude Control....................12-8R QUESTIONS ........................12-9R FOR TRAINING PURPOSES ONLY 12-ii CL 601-3R...
Page 350 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 12-1 Pressurization Control Panel ................12-2R 12-2 Cabin Altimeter—Differential—Rate Indicator..........12-4R 12-3 Outflow Valve (Typical) ..................12-7R 12-4 Pressurization Profile ..................12-7R FOR TRAINING PURPOSES ONLY CL 601-3R 12-iii...
Page 351 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 12 PRESSURIZATION INTRODUCTION This chapter deals with the pressurization system of the Canadair Challenger CL-600- 2B16, model CL-601-3R. Chapter 11 described the controlled inflow of air to the oc- cupied areas of the airplane and the conditioning of that air supply to achieve and maintain the desired temperatures.
Page 352: Major Components
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL systems limit maximum cabin pressure dif- MAJOR COMPONENTS ferential if the normal controls fail. Additional dual safety override controls limit cabin alti- The major components of the pressurization tude as well as negative cabin differential pres- system are: sure in both the automatic and manual modes.
Page 353: Manual Regulator
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The third knob, labeled “A,” located in the OUTFLOW VALVES lower left corner allows the pilot to set field elevation or altitude. The range is from –1,000 Two outflow valves are located on the rear to +10,000 feet.
Page 354 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL INDICATIONS needle is labeled “ALT,” and the cabin differ- ential pressure needle is labeled “PSI.” Both indicate on the same scale. The cabin rate-of- When electrical power is initially provided, or change needle indicates on the left scale and the mode selector switch is moved to auto the needle is not labeled.
Page 355: Protection Systems
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL PROTECTION SYSTEMS NEGATIVE PRESSURE RELIEF A negative pressure-relief feature is part of The protection systems incorporated in the each outflow valve to prevent atmospheric pressurization system are: pressure from exceeding cabin pressure.
Page 356: Flight Mode
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ASSOCIATED SYSTEM FLIGHT MODE (GROUND MODE) AUTOMATIC MODE A ground pressurization control mode is in- After takeoff the control logic switches into corporated and is identified as an associated flight mode.
Page 357 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL TRUE STATIC PRESSURE CABIN PRESSURE TO PNEUMATIC OUTFLOW VALVE OVERPRESSURE LIMITER FILTER ALTITUDE LIMITER CABIN VACUUM LINE PRESSURE (TO AIR JET PUMP) CLOSING SPRING DIAPHRAGM CHAMBER CABIN ATMOSPHERE VALVE POPPET...
Page 358 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MANUAL MODE EMERGENCY DEPRESSURIZATION The manual mode of operation is required if the automatic mode malfunctions or if elec- trical power is lost. Constant monitoring of the GENERAL cabin differential pressure will be necessary throughout the entire operation and especially...
Page 359 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The electrical power supply for automatic When the EMERgency DEPRESSuriza- pressurization control is supplied from: tion switchlight is pushed, it will: A. DC bus 2 A.
Page 360 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 13 HYDRAULIC POWER SYSTEMS CONTENTS Page INTRODUCTION ......................... 13-1 GENERAL ..........................13-1 Control and Indication ....................13-2 HYDRAULIC SYSTEM NO. 1 .................... 13-3 HYDRAULIC SYSTEM NO. 2 .................... 13-4 HYDRAULIC SYSTEM NO.
Page 361 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 13-1 Hydraulic Systems Controls and Indicators............13-2 13-2 No. 1 Hydraulic System Schematic ............... 13-3 13-3 No. 1 Hydraulic System ..................13-4 13-4 No. 2 Hydraulic System Schematic ............... 13-5 13-5 No.
Page 362: Hydraulic Power Systems
FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 13 HYDRAULIC POWER SYSTEMS INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3A/R has three independent hydraulic systems, designated systems “No. 1,” “No. 2,” and “No. 3.” Employing both engine-driven and electrically driven pumps, the systems provide pressure for actuation of primary flight controls, flight and ground spoilers, landing gear, nosewheel steering, and brakes.
Page 363 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Each system has its own reservoir, pressur- lights for the primary pumps (engine ized by a boot strap system to provide positive and 3A) are always active. Lights for feed to the pumps.
Page 364 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL When pushed, the ENG FIRE PUSH switch- Pressurized fluid is filtered by a nonbypass- lights will activate a motor-driven firewall type filter incorporating an indicator that ex- shutoff valve that isolates fluid from the en- tends if the element is becoming blocked.
Page 365 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 13-3. No. 1 Hydraulic System Pump case drain (bypass) fluid is routed System components, located on the right side of through heat exchangers to maintain fluid tem- the aft equipment bay, are shown in Figure 13-5.
Page 366 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL RESERVOIR TEMP PRESSURE RELIEF/ BLEED VALVE HEAT EXCHANGER/ OVERFLOW BOTTLE AC BUS 1 CASE RH ENG CASE DRAIN FIRE DRAIN FILTER PUSH FILTER ELECTRIC RETURN FIREWALL FILTER PUMP SHUTOFF VALVE...
Page 367 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL RESERVOIR TEMP PRESSURE RELIEF/ BLEED VALVE OVERFLOW BOTTLE AC BUS 2 AC BUS 1 CASE CASE DRAIN DRAIN FILTER FILTER ELECTRIC ELECTRIC RETURN PUMP PUMP FILTER SWITCH SWITCH PUMP...
Page 368 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL OPERATING No. 2 hydraulic system will be unusable. This electrical load shedding continues as long as CONDITIONS the generator is not operating and the airplane is in flight. NORMAL CONDITIONS The No.
Page 369 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL HYDRAULIC SUBSYSTEMS Landing gear, flight and ground spoilers, pri- mary flight controls, nosewheel steering, and brakes are hydraulically powered. System de- s c r i p t i o n s a r e p r e s e n t e d i n C h a p t e r 1 4 , “Landing Gear and Brakes,”...
Page 370 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL LEGEND HYDRAULIC SYSTEM NO. 1 HYDRAULIC SYSTEM NO. 2 HYDRAULIC SYSTEM NO. 3 Figure 13-8. Hydraulic Pressure Generation and Distribution FOR TRAINING PURPOSES ONLY CL 601-3A/R 13-9...
Page 371 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS Hydraulic systems No. 1 and No. 2 each If the left generator fails in flight, B have: pump(s): A. One engine-driven pump and one elec- A.
Page 372 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 14 LANDING GEAR AND BRAKES CONTENTS Page INTRODUCTION ......................... 14-1 GENERAL ..........................14-1 LANDING GEAR ......................... 14-2 General........................... 14-2 Weight on Wheels (WOW) System ................14-3 Main Landing Gear......................14-4 Nose Landing Gear ......................
Page 373 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 14-1 Downlock Safety Pins .................... 14-2 14-2 Proximity Switch....................14-3 14-3 WOW Output/Input Fail Lights ................14-3 14-4 Main Landing Gear ....................14-4 14-5 Main Landing Gear Door ..................
Page 374: Landing Gear And Brakes
FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 14 LANDING GEAR AND BRAKES INTRODUCTION The Canadair Challenger CL-600-2B16, model CL-601-3A/R landing gear is electrically controlled, hydraulically actuated, and is partially enclosed by mechanically or hy- draulically actuated doors.
Page 375 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The indication that the landing gear is safely LANDING GEAR down is provided by three green lights above the landing gear control panel. In addition, a GENERAL warning horn sounds if all landing gear are not down and locked when flap position is greater...
Page 376 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL • Air conditioning WEIGHT ON WHEELS (WOW) SYSTEM • Cabin pressurization The WOW system circuitry processes inputs • Autopilot from six proximity (WOW) switches (four on the main gear and two on the nose gear) and •...
Page 377 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MAIN LANDING GEAR The main landing gear consists of a main beam that is connected to the wing structure, a trail- ing link with an axle and main wheels, a shock strut connecting the main beam to the trailing link, and a hydraulic actuator (Figure 14-4).
Page 378 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL NOSE LANDING GEAR Nose Landing Gear Doors The nose landing gear assembly includes a When retracted, the nose gear is enclosed by two hydraulic actuator, scissors, a conventional forward doors and a rear door (Figure 14-7).
Page 379 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CONTROLS AND INDICATORS The MUTE HORN button, when pressed, mutes the landing gear unsafe warning horn unless the flaps are extended beyond the 30° position. Controls Landing gear operation is controlled with the Indicators landing gear handle (Figure 14-8).
Page 380 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL A red NOSE DOOR OPEN light located below • The red landing gear handle lights flash. the LDG GEAR control panel illuminates if the nose gear forward doors are not locked closed. •...
Page 381 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL • The forward nose landing gear doors downlocking is assured by downlock assist hydraulically open, and the red NOSE springs (see Figure 14-6). When the landing DOOR OPEN light illuminates.
Page 382 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL L.G. PULL NOSE DOOR NOSE RELEASE MECHANISM UPLOCK LEGEND NO. 2 SYSTEM PRESSURE LEFT MAIN RIGHT MAIN RETURN UPLOCK UPLOCK FROM GEAR ACTUATORS AND NOSE DOOR DUMP VALVE ACTUATOR DOWNLOCK ASSIST SELECTOR VALVE...
Page 383 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL NOTE Do not exert force on the steering con- trol wheel. Do not position the N/W STEER switch to the ARMED position until reengagement has been made. STEER ARMED BRAKES...
Page 384 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL A wear indicator pin on each brake assembly • Touchdown protection provides visual indication of brake wear. When the end of the pin is flush with the spring hous- •...
Page 385 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL PARKING BRAKES The parking brakes can be set with the PARK- ING BRAKE handle (Figure 14-16). Fully depress either set of pedals, pull the handle, and rotate it 90° counter clockwise. This ANTI-SKID TEST mechanically latches the brake metering...
Page 386 PILOT’S COPILOT’S BRAKE BRAKE ACCUMULATOR ACCUMULATOR PEDALS PEDALS METERING METERING METERING METERING VALVE VALVE VALVE VALVE ANTI-SKID ANTI-SKID ANTI-SKID ANTI-SKID PARKING VALVE VALVE VALVE VALVE SHUTOFF VALVE LEGEND FUSE FUSE FUSE FUSE HYDRAULIC SYSTEM NO. 3 PRESSURE HYDRAULIC SYSTEM NO. 2 PRESSURE RETURN NITROGEN PRESSURE LEFT...
Page 387 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL PARKING STEER BRAKE FAIL Figure 14-16. Parking Brake System FOR TRAINING PURPOSES ONLY 14-14 CL 601-3A/R...
Page 388 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS Normally, landing gear downlocks are If the nosewheels are driven past 55°, the engaged: disengaged rack and pinion should be: A. Hydraulically A. Reengaged hydraulically B. Mechanically B.
Page 389 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 15 FLIGHT CONTROLS CONTENTS Page INTRODUCTION ......................... 15-1 GENERAL ..........................15-2 PRIMARY FLIGHT CONTROLS..................15-3 General........................... 15-3 Roll Control System ...................... 15-3 Yaw Control System ...................... 15-7 Pitch Control System .....................
Page 390 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 15-1 Flight Control Surfaces ..................15-2 15-2 Roll Disconnect...................... 15-3 15-3 Aileron Trim and Artificial Feel Mechanism............15-4 15-4 Rudder and Aileron Trim Controls and Indicators ..........15-5 15-5 Flight Control Surface Position Indicators ............
Page 391 FlightSafety Canada Lt é e Lt d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 15 FLIGHT CONTROLS INTRODUCTION This chapter deals with the flight controls of the Canadair Challenger CL-600-2B16, model CL-601-3A/R. The hydraulically powered primary flight control surfaces are operated by pilot inputs from the control columns, control wheels, and rudder pedals.
Page 392 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL GENERAL A proportional flight spoiler on the upper sur- face of each wing, forward of the outboard flaps, provides lift modulation. Hydraulic ac- Primary flight control surfaces are positioned tuation of the spoilers is initiated by inputs by hydraulic power control units (PCU’s).
Page 393 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL PRIMARY FLIGHT With no hydraulic pressure available, restricted flow within the actuator provides slow, con- CONTROLS trolled movement of the surface. GENERAL ROLL CONTROL SYSTEM Each aileron and each elevator is actuated by General two PCU’s, each powered by a separate hy- draulic system.
Page 394 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The aileron system has dual control linkages. Aileron load feel is provided by an artificial Movement of either control wheel actuates feel unit (Figure 15-3) that forms part of the both sets of linkages to position control valves aft quadrant.
Page 395 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL STAB PITCH TRIM AIL TRIM RUD TRIM PUSH CHAN 1 OVSP INOP CHAN 2 CHANGE TRIM CHAN INOP Figure 15-4. Rudder and Aileron Trim Controls and Indicators Aileron trim is provided by small displace- stopping and holding the ailerons in the ments of the ailerons by the PCU’s.
Page 396 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FLT SPLR SERVO MONITOR AILERON ROLL PITCH ELEVATOR SAFE RUDDER Figure 15-6. Servo Monitor Panel Figure 15-5. Flight Control Surface Position Indicators CROSS-COUPLING RUDDER PEDAL ADJUSTMENT JAM BREAKOUT MECHANISM SEE FIGURE 15-8...
Page 397 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL YAW CONTROL SYSTEM The rudder control system consists of dual con- trol linkages. Movement of either set of rudder pedals actuates both sets of linkages to position General control valves on all three rudder PCU’s.
Page 398 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Operation PITCH CONTROL SYSTEM General Movement of either set of rudder pedals me- chanically positions the control valves on all Two independent, hydraulically powered el- three rudder PCUs. Pressure from hydraulic evators, mechanically controlled by control systems No.
Page 399 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL Operation device that prevents actuator overspeed and overtravel. A control unit determines rate and Fore or aft movement of either control column motor drive direction. mechanically positions the control valves of all four elevator PCU’s.
Page 400 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL If the trim motor overspeeds, the amber OVSP shafts. Airflow is directed over the flaps by switchlight illuminates and system operation fixed- and variable-position vanes. ceases. Transfer to Channel 2 can be made by pressing the OVSP–CHNG CHAN switchlight.
Page 401 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL position indicator. The amber LH FLT SPLR are hydraulically released for spoiler exten- and the RH FLT SPLR lights extinguish when sion. Spoiler operation is controlled by a the spoilers are fully retracted and locked.
Page 402 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FLAPS When armed, the ground spoilers will deploy au- tomatically if the following conditions are met: General • Wheel spinup has occurred, or both channels of the WOW system indicate The flap system consists of two inboard and two outboard flaps.
Page 403 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL Figure 15-12. Wing Flaps OVHT FLAPS MOT 1 FAIL OVHT MOT 2 10 10 FLAPS FLAPS DEG. Figure 15-13. Flaps Controls and Indicators FOR TRAINING PURPOSES ONLY CL 601-3A/R 15-13...
Page 404 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FLAPS FLAPS FAIL FLAP DC BUS 1 CONTROL DC BUS 2 UNIT MOTOR MOTOR AC BUS 1 AC BUS 2 RELAYS RELAYS MOTOR 1 MOTOR 2 OVHT OVHT MOT 1...
Page 405 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL STALL PROTECTION establishes actuation points for stick shaking, continuous ignition, aural warning, and stick SYSTEM pushing. The WOW inputs prevent system op- eration on the ground, except during testing. GENERAL Two transducers, receiving static pressure, supply altitude information to the computer for...
Page 406 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL OPERATION TESTING As angle of attack (AOA) begins to increase, To test the stall protection system, perform the pointers of the SPS TEST indicators the following: (Figure 15-15) move counterclockwise to indicate decreasing stall margin.
Page 407 FlightSafety Canada L t ée L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS Aileron and elevator flutter is prevented by: Travel of the primary flight controls is limited by: A. Hydraulic dampers A. PCU travel only B. The associated PCU’s B.
Page 408 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 16 AVIONICS CONTENTS Page INTRODUCTION ......................... 16-1 GENERAL ..........................16-1 COMMUNICATIONS ......................16-3 VHF Communications ....................16-4 HF Communications ...................... 16-5 SELCAL ........................16-6 Audio Integrating System ....................16-7 ATC Transponder......................
Page 409 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Flight Management System ..................16-58 Flight Guidance System....................16-61 Weather Radar System....................16-76 Radio Altimeter System....................16-80 Avionics Cooling ......................16-80 16-ii CL 601-3A/R FOR TRAINING PURPOSES ONLY...
Page 410 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 16-1 Communication Antennas..................16-2 16-2 Communication Control Unit Locations..............16-3 16-3 VHF Control Unit ....................16-4 16-4 HF Control Unit ..................... 16-5 16-5 SELCAL Panel.......................
Page 411 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 16-24 Pitot-Static System....................16-26 16-25 Pitot-Static Heads, Static Ports, and Static Selector Valves......... 16-28 16-26 Standby Selectors and TAT Probe................ 16-29 16-27 Air Data System Flow..................16-30 16-28 Advisory Display and MASI ................
Page 412 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 16-50 MFD Cockpit Locator..................16-53 16-51 MFD Controller ....................16-54 16-52 MFD Map Mode ....................16-55 16-53 MFD Plan Mode ....................16-56 16-54 MFD Checklist Displays..................16-57 16-55 FMS Components ....................
Page 413 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 16 AVIONICS INTRODUCTION The standard factory-installed Canadair Challenger CL-600-2B16, model CL-601-3A/R avionics package includes communications systems, electronic flight instrument sys- tems, a digital automatic flight control system (DAFCS), and navigation systems. The avionics package may also include other systems not discussed in this chapter due to the large number of customer options available.
Page 414 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL • Dual yaw damping (YD) There are two types of airborne navigation systems: dependent position-determining sys- • Dual MACH trim (MTRIM) tems (DPDS), which require ground trans- m i t t e r s f o r o p e r a t i o n , a n d i n d e p e n d e n t •...
Page 415: Communications
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL COMMUNICATIONS • Audio integrating system • Dual ATC transponder The communication system integrates the fol- lowing systems: • Cockpit voice recorder • Dual VHF communications Figure 16-1 displays the antennas associated with the communication system.
Page 416: Vhf Communications
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL VHF COMMUNICATIONS channels allow backup capabilities for VHF transmission and reception. Located in the The primary voice communication system nose compartment, the transceiver receives with air traffic controllers or other aircraft signal input from the antenna and provides consists of two VHF radios (VHF 1 and 2).
Page 417: Hf Communications
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL HF COMMUNICATIONS separately to the antenna-coupler units. Each receiver-transmitter receives inputs from the The HF communication system provides the antenna-coupler and provides outputs to the primary voice communication system during audio integrating system.
Page 418: Selcal
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL SELCAL The SELCAL system consists of a decoder unit, a code selection box, and a SELCAL The SELCAL feature allows an ATC ground control panel (Figure16-5). When the decoder station to call the flight crew over the HF radio receives a signal from a ground station, the de- when out of VHF communication range.
Page 419 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AUDIO INTEGRATING SYSTEM • Automatic direction finder (ADF 1 and An audio integrating system provides volume, interphone, and navaid monitoring controls. • Distance measuring equipment (DME The audio integrating system consists of an in- 1 and 2) terphone, loudspeakers, microphone jacks,...
Page 420 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The interphone system provides communica- disconnected in flight via the weight-on- tion between the pilot, copilot, and up to three wheels (WOW) system. ground crew stations. Placing the MIC selec- tor to the INPH position allows interphone An emergency mode of operation automati- communication between any two stations.
Page 421: Atc Transponder
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ATC TRANSPONDERS and a control unit (Figure 16-8). The anten- nas are mounted on the underside of the The ATC transponder system is part of the air forward fuselage.
Page 422 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL COCKPIT VOICE RECORDER microphone records flight deck conversations and sounds. The microphone filters 400 HZ The cockpit voice recorder (CVR) system con- electrical noise from adjacent equipment and tinuously records the previous 30 minutes of wiring.
Page 423: Navigation
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL NAVIGATION Figure 16-10 displays the antenna locations for the navigation control units. Figure 16-11 shows the location of the cockpit controls. The aircraft systems that receive radio tuned navaids for short-range navigation consist of Associated controls and displays for the nav- the following:...
Page 424: Vhf Navigation
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL VHF NAVIGATION NAV system provides VOR, LOC, and GS de- viation; VOR, LOC, and MKR audio; VOR The VHF NAV systems No. 1 and No. 2 receive bearing, VOR TO/FROM data, and MKR and process the following ground-based VHF- annunciation.
Page 425 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The VHF NAV system provides options to se- CAUTION lect VHF NAV and DME frequencies. Located on both instrument panels, a NAV TUNE switch- light allows either FMS or manual VHF navaid For manual (control head selected) frequency tuning.
Page 426 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL COURSE PRESELECT NO. 1 BEARING SOURCE ANNUNCIATOR POINTER INDICATES THE SOURCE INDICATES THE BEARING DISTANCE DISPLAY OF THE COURSE PRE- TO THE SOURCE SELECTED DISPLAYS THE DME SELECTED INFORMATION.
Page 427 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL DISTANCE MEASURING The VHF control unit automatically selects a DME channel if the navaid contains a paired EQUIPMENT DME frequency. The VHF control unit pro- vides manual frequency selection, and the The distance measuring equipment consists of FMS provides automatic frequency selection.
Page 428 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AUTOMATIC DIRECTION permits voice reception or continuous wave (CW) transmission. FINDING The EHSI displays the relative bearing indi- The dual, low-frequency ADF system pro- cation on the EHSI. The ADF supplies the vides reception of selected ground station sig- audio identification signals to the audiointe- nals in the 190 to 1799.5 kHz frequency range.
Page 429: Digital Clocks
FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Each ADF system consists of a receiver, con- DIGITAL CLOCKS trol unit (Figure16-15), and a shared ADF antenna. The display controllers provide se- A 6 VDC battery-powered digital clock on lection options of either ADF 1 or 2 bearing each instrument panel displays local, flight, information for EHSI display.
Page 430 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL NORMAL EFIS DISPLAYS The EHSI displays the primary navigation se- lections chosen from the display controller. Figure 16-17 shows the normal operational EFIS display using the navigation radios. EADI ASEL KIAS...
Page 431 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL EFIS FAILURE DISPLAYS Figure 16-18 shows the most common EFIS failure displays. Consult the applicable flight m a n u a l f o r e a c h o f t h e s p e c i fi c f a i l u r e messages.
Page 432 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL DIGITAL AUTOMATIC The DAFCS system provides fail-operational execution of flight director guidance, autopi- FLIGHT CONTROL lot, yaw damper, and trim functions. The flight guidance computers (FGC) generate auto- SYSTEM matic flight path commands and use attitude and direction from the IRS and FMS, air data...
Page 433 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL INERTIAL REFERENCE • Two inertial reference units (IRUs) SYSTEM • Two backup battery/chargers The dual IRS (3rd is optional) calculates highly • Two mode select units (MSU) accurate aircraft attitude, position, velocity, and heading information.
Page 434 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Inertial Reference Unit opposite side IRU for EFIS attitude and head- ing source information. Selection of the The main component for each IRS consists of opposite IRU provides a backup if the onside an IRU.
Page 435 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL R E M OT E AU X I L I A RY BAT T E RY / A P U CDUs. The primary method of initialization BATT/CHARGER FAIL annunciator panel consists of using the FMS CDU.
Page 436 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ATT Mode NOTE To select ATT, the mode select knob If the NAV mode fails, the ATT mode pro- must be pulled away from the MSU vides a reversionary mode option that recov- front panel and then rotated clock- ers attitude and heading information.
Page 437 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Inertial System Display Unit Navigation Display Unit The ISDU allows the entry of present position The NDU, or LASERTRAK, provides limited directly to any of the installed ITUs, and it pro- IRS navigation capability by allowing a direct vides display of several IRS parameters.
Page 438 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 16-26 CL 601-3A/R FOR TRAINING PURPOSES ONLY...
Page 439 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL DIGITAL AIR DATA SYSTEM The pitot-static pressures for both the standby pneumatic airspeed indicator and altimeter The DADS consists of systems that detect and flow through two guarded standby instruments measure raw flight environmental data for use pitot-static selector valves on the copilot’s within the flight data computers.
Page 440 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL to S3 static ports. The S3 static ports always STALL PROTECT Selector Valves provide the static pressure for the cabin dif- In normal operation, the STALL PROTECT se- ferential pressure indicator.
Page 441 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Standby Instruments Pitot and Static resistance changes value to provide tempera- ture signals to the respective DADC 1 and Selectors DADC 2. Static air temperature (SAT) and In normal operation, the STANDBY INSTR TAT readouts displayed on the advisory dis- pitot and static selector valves are in the PITOT...
Page 442 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The ADS consists of two complete systems The ADS consists of the following: with two digital air data computers (DADC 1 and DADC 2). The DADCs accept both digi- •...
Page 443 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL TAS/SAT/TAT Indications An three position VMO/OFF/Black warning shows black during normal operations. Failures The advisory display on the center instrument detected in the Vmo loop display the black panel displays true airspeed (TAS), static air VMO on an orange background.
Page 444 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL preselected altitude. An OFF flag displays failure warning (OFF) flag. The failure warn- during loss of 26 VAC ESSENTIAL BUS. ing flag appears during loss of 26 VAC ES- SENTIAL BUS.
Page 445 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL • Standby horizon indicator The airspeed pointer operates through a me- chanical linkage connected to a differential • Standby magnetic compass pressure capsule that responds to changes in pitot pressure.
Page 446 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL counter is graduated in increments of 1,000 Standby Horizon Indicator feet to 50,000 feet. The altimeter pointer and The self-contained standby horizon indicator counter operate through mechanical linkages provides visual pitch and roll aircraft attitude connected to barometric capsules that expand information (Figure 16-31).
Page 447 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL changeover relay connects the standby hori- integral lighting is supplied from the standby zon indicator through the STBY HORIZ circuit compass circuit breaker on BATT BUS, CBP- breaker to the BATT BUS, CBP-B.
Page 448 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL DC-815 DISPLAY CONTROLLER FULL GSPD FMS 1 FMS 2 ADF 1 ADF 2 TEST VOR 1 VOR 2 PUSH PUSH PUSH SYNC IAS/MACH RI-815 INSTRUMENT RECEIVER SG-815 REMOTE SYMBOL...
Page 449 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL systems that compare relative data prior to The EADIs, EHSIs, and the MFD are inter- output display. Figure 16-34 displays the EFIS changeable and identical, with the exception cockpit locator.
Page 450 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL formats for the EFIS displays. Data presented • Reversion functions for display on the same physical side of the cockpit is considered on-side information. • Comparison monitoring Data originating from the opposite side SG is considered cross-side information.
Page 451 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL • IRS reversion—Selects the cross-side computer (FGC) to provide backup for IRS for backup. the onside flight director. • IAS reversion—The IAS REV selects • NAV source reversion—The V/L and the cross-side ADC to display IAS in- FMS buttons on the display controller formation.
Page 452 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL EFIS SYMBOL GENERATOR ATT COMPARISON IRS 1 PITCH AND ROLL COMPARATOR IRS 2 PITCH AND ROLL >3° MISCOMPARE IN PITCH OR ROLL LOC COMPARISON PILOT'S COMPARATOR COPILOT'S TWO-THIRDS OF A DOT MISCOMPARE ON LOC AND RA LESS THAN 1,200 FT...
Page 453 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL flight crew of the condition. Pressing the as- • Indicated airspeed (IAS) comparison— sociated comparator warning switchlight re- 5-knot miscompare for more than two sets all comparator warnings. The SGs detect seconds exists with valid on-side and miscompares for the following limits: cross-side IAS and IAS greater than 90...
Page 454 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Warning and Failure Displays annunciation and a red boxed RA flag indicates the failure of the radio alti- The following displays (Figure 16-39) occur tude function. during associated failure of equipment: •...
Page 455 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL EHSI Compass Modes The EHSI operates within a variety of modes The electronic horizontal situation indicator to display specific information. The EHSI (EHSI) displays the primary course, magnetic may display a full compass, an arc, or a weather heading, and bearing information in full- radar and map mode.
Page 456 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Arc Mode Weather Radar and Map Mode In the arc mode, the EHSI only displays 45 Selecting the WX function from the display degrees left and right of the aircraft present controller automatically places the EHSI into magnetic heading.
Page 457 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL WX RADAR TARGET ALERT ANNUNCIATOR RANGE RING WX RETURN DISPLAY RANGE MODE ANNUNCIATOR GSPD ANNUNCIATOR *YELLOW IF CROSS SIDE NAV SOURCE SALON VOR BEARING WAYPOINT* TO WAYPOINT TO WAYPOINT IDENTIFIER SALON...
Page 458 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Reversion • Rising runway pointer The reversionary feature allows selection of • Vertical deviation pointer cross side SG or IRS if either on-side system fails. The V/L and FMS buttons on the display •...
Page 459 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Comparison Monitoring The EHSI compares on-side heading with cross-side heading informating. A miscom- pare exists if headings differs by 3° or more with valid data and the same type of heading (MAG/TRU).
Page 460 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Failure Warning Annunciations boxed IRS flag indicates the heading failure. The EHSI displays red boxed annunciations that indicate failures of the heading, naviga- • Navigation source failure—Removal of tion source, glideslope, and symbol generator the DTK pointer, deviation, FMS read- (Figure 16-45).
Page 461 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL • Symbol generator—A red boxed SG in- 46). Combinations of flight phase, NAV radio dicates a symbol generator internal tuning, selected flight director mode, absolute failure. altitude, and other selections determine the dis- plays represented on the composite display.
Page 462 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Instrument Remote Controller Display Controller Each instrument remote controller on the The primary control for the EADI and EHSI glareshield allows selection of a desired course consists of the display controller (Figure 16- and heading bug settings (Figure 16-47).
Page 463 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL WX PUSHBUTTON GS/TTG PUSHBUTTON SELECTS WEATHER RADAR RETURNS FOR SELECTS BETWEEN GROUNDSPEED (GS) DISPLAY ON THE HSI. IF THE FULL COMPASS AND TIME-TO-GO (TTG) FOR DISPLAY ON IS DISPLAYED PRIOR TO WX SELECTION, THE HSI.
Page 464 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL EFIS Self-Test (EADI and EHSI) seconds, all comparators are removed, and all red flags are displayed with their corre- The TEST pushbutton on the display con- sponding logic.
Page 465 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MULTIFUNCTION DISPLAY eration of the failed display. The EFIS con- troller on that side will continue to operate the SYSTEM EFIS display formats. The multifunction display (MFD) system con- The MFD also functions as a backup EHSI if sists of the following components (Figure 16-50): a display tube fails.
Page 466 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL MFD Symbol Generator MFD Controller The multifunction SG controls the inputs and The MFD controller (Figure 16-51) controls outputs to the MFD. The MFD SG also pro- both the MFD operational mode and the dis- vides backup capability to the EFIS symbol play mode presented on the display tube.
Page 467 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Display Modes Selecting the MAP/PLAN pushbutton on the The MFD provides four display modes: MFD controller changes the display to either map or plan displays. The MAP mode pro- •...
Page 468 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Plan controller and WX radar controller operate the functions for the two modes. The PLAN mode provides a North up display of the FMS mapping. The aircraft symbol is Checklist oriented to the navigational route of flight.
Page 469 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The NORM pushbutton on the MFD controller plays the first page of the emergency check- provides normal procedures checklist entry. list index. An EMERGENCY PROCEDURE The normal checklists are arranged in order of COMPLETE text display occurs at the com- standard flight operations.
Page 470 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FLIGHT MANAGEMENT d i r e c t a c c e s s t o s p e c i fi c d i s p l a y p a g e s . Annunciators on the top of the unit continu- SYSTEM ously advise the pilot of the system status.
Page 471 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Navigation Computer high-altitude airway intersections. The re- gionalized data base includes the above in- The FMC provides accurate, long-range lat- formation plus airway routes and SIDs/STARs eral and vertical navigation outputs to the procedures.
Page 472 Figure 16-57. AFCS Data Flow...
Page 473 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FLIGHT GUIDANCE SYSTEM controllability and stability in all flight regimes. The aircraft flight guidance system consists of a fail-operational automatic flight control sys- • Servo torques are also programmed as tem (AFCS) (Figure 16-67) that provides au- a function of flight condition to result topilot functions throughout most phases of...
Page 474 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL BANK CAT 2 PUSH PUSH PUSH PUSH PUSH SYNC SYNC STBY M TRIM IAS/MACH ALT SEL VNAV PILOT INSTRUMENT COPILOT INSTRUMENT REMOTE REMOTE FLIGHT GUIDANCE CONTROLLER CONTROLLER CONTROLLER MANUAL PITCH...
Page 475 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL 2 controls the autopilot and FD functions if Lateral Modes manually selected or if the selected pilot FGC The lateral modes (Figure 16-69) for the flight 1 fails.
Page 476 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Heading Select approach mode lateral control using a valid tuned VHF localizer frequency. The approach Pressing the HDG button on the flight guid- mode has an arm and capture phase that allows ance controller activates the heading select setup of a path intercept with automatic tran- mode.
Page 477 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Altitude Preselect Vertical Speed The ALT provides automatic level-off at an al- The VS button directs flight director com- titude preselected through the air data com- mands to the EADI to maintain the present ver- puter and the copilot ALT button on the tical speed indicated on the VSI.
Page 478 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Basic Functions • Standby (STBY) The basic functions for the flight guidance • Autopilot (AP) controller consists of the following: • Yaw damper (YD) • BANK •...
Page 479 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Bank autopilot disconnect or if an autopilot fault requiring autopilot disengagement occurs. The bank button allows manual selection of the bank angle limit in the HDG select, VOR, or Yaw Damper LNAV modes.
Page 480 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Turn and Pitch Controller Turn Knob Rotation of the turn knob out of seated detent The turn and pitch controller (Figure 16-62) with the autopilot engaged results in a roll consists of a pitch wheel and turn knob.
Page 481 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Advisory Display guidance computer and transmitted to the ad- visory display over the ASCB. The advisory The advisory display (Figure 16-63) provides display unit generates both operational and warning, caution, status, failure, and invalid warning/caution messages.
Page 482 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The warning/caution messages consist of the • Flight fault monitoring and real-time following: bite • Disengage messages • Flight fault summary • Primary caution messages Power-Up Test •...
Page 483 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL until test 98 L FLIGHT FAULT SUMMARY? • NAV receivers tuned to LOC and valid appears (B). To obtain the fault data, push the RESET button, and data for the first flight •...
Page 484 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL If AP is engaged at the moment of failure de- message on the advisory display. The autopi- tection, the active channel disengages fol- lot then automatically selects the remaining- lowing a fault detection, and the standby s i d e s e n s o r d a t a f o r f l i g h t g u i d a n c e channel automatically takes over the correct...
Page 485 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL • Pressing either control wheel AP/SP Manual FD Sensor Data Selection DISC switch All flight director sensor data sources are se- lected via the CPL pushbutton on the flight •...
Page 486 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL data) cancel and will not reengage until the in- Flight Director Command Bars valid condition clears. During normal operation, the flight director function of the FGC uses sensor data from the Annunciation coupled side.
Page 487 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL system to revert to the cross-side FGC with- n a v i g a t i o n - r e l a t e d s e n s o r s , s u c h a s out disengagement during a FGC-detected VOR/LOC/FMS/DME, and radio altitude.
Page 488 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL WEATHER RADAR SYSTEM identify coastlines, hilly or mountainous re- gions, cities, or large structures. The weather radar system is an X-band radar designed for weather detection and analysis. The radar system consists of the following The radar displays storm intensity levels in Figure 16-67):...
Page 489 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Receiver/transmitter/antenna • SBY—Placing the radar in standby keeps the radar in a ready state with the antenna Unit stopped, the transmitter inhibited, and the display memory erased. If selection of The antenna tilt range is ±15°.
Page 490 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL HEADING LUBBER TUNED SELECTED DIAL LINE VOR/DME NAV SOURCE DISTANCE AND COURSE TO DESIGNATOR DESIRED TRACK LINE WEATHER WAYPOINT RADAR 95.0/040° FMS 1 MODE VOR/DME SYMBOL TARGET KXYZ VOR/DME...
Page 491 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Visual indications are provided by the TRB Function test pattern for display of color, display Pressing the TRB button activates the turbu- sensitivity, and transmitter and receiver lence mode with the rotary RADAR mode integrity faults.
Page 492 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Forced Standby Mode operation. Radio altitude is displayed on the pilot’s and copilot’s EADIs. The weather radar system is automatically forced from the selected operating mode into The radio altimeter system consists of a trans- the standby mode when the aircraft lands, to mitter/receiver, transmitter antenna, and re-...
Page 493 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL The cabin overhead ducting supplies cold air • Left fan—Pilot’s EHSI and EADI through flexible tubes and nozzles to augment cooling for the following components in the •...
Page 494 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS On the VHF COMM control head the The IRS MSU BATT FAIL light illumi- upper digital readout displays: nates when: A. The preset (inactive) frequency and di- A.
Page 495 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL Once the aircraft has landed, the radar is 12. When the autopilot is engaged, the bank forced into standby mode by the action of limit is set at 24° (27° heading select or 30° the WOW logic regardless of mode se- LNAV).
Page 496 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 17 MISCELLANEOUS SYSTEMS CONTENTS Page INTRODUCTION ......................... 17-1 OXYGEN SYSTEM......................17-1 Crew Oxygen System Description and Operation ............17-2 LIMITATIONS ........................17-5 QUESTIONS ......................... 17-6 FOR TRAINING PURPOSES ONLY CL 601-3A/R 17-i...
Page 497 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 17-1 Oxygen System ...................... 17-2 17-2 Oxygen Ground Service Panel ................17-3 17-3 Oxygen Cylinder Assembly ................... 17-3 17-4 Crew Oxygen Pressure Indicator................17-3 17-5 Oxygen Mask Stowage Box...................
Page 498 FlightSafety Canada L té e L td . CL-600-2B16 PILOT TRAINING MANUAL CHAPTER 17 MISCELLANEOUS SYSTEMS ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; ;;;;;;;;;;;;;;;;;;;;;;; ;;;;;;;;;;;; RESET ANTI-ICE TEST BLOWER NO 1 FUEL ENG 1 XMSN TRANS...
Page 499 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Oxygen regulators and controls are installed CREW OXYGEN SYSTEM on the EROS quick-donning oxygen masks. DESCRIPTION AND The masks and hoses are permanently con- OPERATION nected in the system, eliminating the need for conventional outlets and hose connectors.
Page 500 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Oxygen Cylinder Assembly the low-pressure system. The high-pressure system relief valve ruptures if an overpres- The oxygen filler valve (Figure 17-2) is lo- sure occurs, venting the oxygen overboard. cated in the ground service panel.
Page 501 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL Figure 17-5. Oxygen Mask Stowage Box Figure 17-6. Oxygen Mask and Regulator oxygen is available. Closing the doors does not tions marked "N" (normal) and "100% PUSH," turn the shutoff valve off; the switch must be and an EMERGENCY ON-OFF rotary control repositioned to RESET-TEST.
Page 502 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL Overboard Discharge Indicator The green overboard discharge indicator (Figure 17-7) is located on the right side of the exterior nose section. When missing, it pro- vides a visual indication that an overpressure condition existed in the oxygen cylinder and that the pressure has been vented overboard.
Page 503 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL QUESTIONS The fully serviced crew oxygen system The diluter-demand quick-donning mask pressure is: delivers oxygen: A. 1,850 psi A. At all times B. 700 psi B. Upon inhalation C.
Page 504 FlightSafety Canada Lté e Ltd. CL-600-2B16 PILOT TRAINING MANUAL WALKAROUND The following section is a pictorial walkaround. It shows each item called out in the exterior power-off preflight inspection. The fold-out pages at the beginning and end of the walkaround section should be unfolded before starting to read. The general location photographs do not specify every checklist item.
Page 505 FlightSafety Canada L tée FlightSafety Canada L tée L td. L td . CL-600-2B16 PILOT TRAINING MANUAL CL-600-2B16 PILOT TRAINING MANUAL WALKAROUND LEFT FORWARD FUSELAGE 1. EMERGENCY LIGHT—CHECKED 4. PITOT TUBE—COVER REMOVED AND CHECKED 2. STATIC PORT—COVER REMOVED AND CHECKED 5.
Page 506 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 8. RADOME—CONDITION CHECKED, LATCHES 7. FORWARD AVIONICS BAY LATCHES—SECURE SECURE NOSE LANDING GEAR BAY 9. TIRES—CHECK INFLATION, TREAD WEAR, CUTS 12. REAR DOORS AND STEERING ACTUATOR— AND SLIPPAGE MARKS CHECK FOR LEAKS 10.
Page 507 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL 17. ADG SAFETY PIN—REMOVED (IF NO 14. WEIGHT-ON-WHEELS SWITCHES AND RESISTANCE FELT) HARNESSES—INTACT 15. PROXIMITY SWITCHES—INTACT 18. NOSE DOOR CANNON PLUG—CONNECTED (IF NO. 3 HYD SYSTEM IS DEPRESSURIZED) 16.
Page 508 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL RIGHT FORWARD FUSELAGE 24. PITOT TUBE—COVER REMOVED AND 20. AC EXTERNAL POWER SERVICE DOOR— SECURE CHECKED 21. OXYGEN PANEL—OPENED, PRESSURE 25. ICE DETECTOR PROBE—CHECKED CHECKED, SECURE 22. FORWARD AVIONICS BAY LATCHES—SECURE 26.
Page 509 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL 29. STATIC PORT—COVER REMOVED AND 27. TAT PROBE—CHECKED CHECKED 28. ANGLE-OF-ATTACK VANE—COVER REMOVED, CHECKED FOR MOVEMENT RIGHT WING 30. PRESSURE FUELING PANEL—VALVES CLOSED, 31. FUEL ADAPTER SERVICE DOOR—SECURE SWITCH OFF, SECURE 32.
Page 510 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 36. EMERGENCY LIGHTS (3)—CHECKED 33. TAXI AND LANDING LIGHTS—CHECKED 34. AUXILIARY FUEL TANK FILLER CAP—SECURE 37. RIGHT MAIN FUEL DRAIN—CHECK FOR LEAKS 38. RIGHT MAIN FUEL TANK FILLER CAP—SECURE 35.
Page 511 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL 45. WINGLET—CHECK CONDITION 39. WING LEADING EDGE—CONDITION AND ANTI- ICE EXHAUST CHECKED 46. AILERON—CHECK FOR LEAKAGE AND CONDITION, NO MOVEMENT 40. FUEL VENT VALVE EXHAUST—CHECKED 47. SPOILERS (2)—CHECK FOR LEAKAGE AND CONDITION 41.
Page 512 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 49. FUEL NACA VENT—COVER REMOVED, CHECK CONDITION MAIN LANDING GEAR BAYS 50. NO. 3 HYDRAULIC SYSTEM ACCUMULATOR— 52. RIGHT AND LEFT MLG SENSING LOOPS— CHECK 1500 PSI CHECK CONDITION AND CONNECTIONS 51.
Page 513 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL 59. LEFT MAIN UPLOCK AND PROX SWITCH— 54. DOWNLOCK PIN—REMOVED, SLIDE DUST CHECKED PROTECTION RING IN PLACE 55. LEFT MAIN BRAKES—CHECK WEAR INDEX 60. RIGHT MAIN HYDRAULIC ACTUATOR—CHECK PINS AND LINES FOR LEAKS, DAMAGE, AND CONDITION, LEAKS, INTEGRITY, PROXIMITY SECURITY...
Page 514 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 62. RIGHT MAIN BRAKES—CHECK WEAR INDEX 65. RIGHT MAIN LANDING GEAR DOOR—INSPECT PIN AND LINES FOR LEAKS, DAMAGE, AND FOR SECURITY SECURITY 63. RIGHT MAIN OLEO EXTENSION—CHECKED 64.
Page 515 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL 72. RIGHT ACU EXHAUST—REMOVE COVER AND 69. FUEL VENT SHROUD DRAINS—INSPECT FOR CHECK LEAKAGE 70. DC EXTERNAL POWER SERVICE DOOR— 73. APU AIR INTAKE—REMOVE COVER AND SECURE CHECK 71.
Page 516 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL RIGHT ENGINE AREA 75. COWL ANTI-ICE PRESSURE RELIEF VALVE AND 77. ENGINE DRAIN LINES—CHECK FOR LEAKS EXHAUST LOUVERS—CHECKED FLUSH AND AND CONDITION CLEAR 76. UPPER AND LOWER COWLING—CHECKED, LATCHES SECURE 78.
Page 517 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL EMPENNAGE 81. RUDDER—CHECK FOR LEAKS AND CONDITION 86. HYDRAULIC HEAT EXCHANGE EXHAUST— 82. HORIZONTAL STABILIZER—CHECK POSITION CHECK CLEAR AND CONDITION 83. ELEVATORS—CHECK FOR LEAKS AND CONDITION 84. NAVIGATION LIGHTS—CHECK FUNCTION 85.
Page 518 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 93. PNEUMATIC DUCTING—CHECK CONDITION 89. APU ENCLOSURE—CHECK FOR LEAKS AND CONDITION 90. APU SERVICE DOOR—SECURE 91. PRESSURIZATION OUTFLOW VALVES (2)— 94. BATTERY—CHECK CONDITION AND CHECK CLEAR CONNECTIONS 92.
Page 519 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL 96. RIGHT ACU—CHECK 99. ENGINE OIL REPLENISHMENT RESERVOIR— CHECK CONDITION 97. NO. 2 HYDRAULIC SYSTEM—CHECK FILTERS, 100. NO. 1 HYDRAULIC SYSTEM—CHECK FILTERS, LEAKS, AND ACCUMULATOR PRESSURE 1500 LEAKS, AND ACCUMULATOR PRESSURE 1500 98.
Page 520 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 104. SERVICE LIGHT—SELECT OFF 102. APU FIREX BOTTLE—CHECK PRESSURE 600 PSI AND SQUIB CONNECTION 103. OIL REPLENISHING SYSTEM—CHECKED 105. EQUIPMENT BAY DOOR—CLOSE AND LOCK FOR TRAINING PURPOSES ONLY CL 601-3A/R W-17...
Page 521 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL LEFT ENGINE AREA 109. ENGINE DRAIN LINES—CHECK FOR LEAKS AND CONDITION 106. ENGINE EXHAUST COVER—REMOVED 107. REAR TURBINE BLADES—CHECKED 110. UPPER AND LOWER COWLING—CHECKED, LATCHES SECURE 108. ENGINE PYLON—CHECKED 111.
Page 522 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 112. ENGINE INTAKE PLUG—REMOVED LEFT REAR FUSELAGE AREA 113. LEFT ACU EXHAUST—REMOVE COVER AND CHECK 115. APU FAULT PANEL—CHECK INDICATORS AND RESET 114. CROSSOVER HEAT EXCHANGER EXHAUST— 116.
Page 523 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL 118. APU WITNESS DRAINS—INSPECT FOR 119. BAGGAGE COMPARTMENT DOOR—SECURED EXCESSIVE LEAKS LEFT WING 120. FUEL NACA VENT—COVER REMOVED, CHECK 122. SPOILERS (2)—CHECK FOR LEAKAGE AND CONDITION CONDITION, NO MOVEMENT 121.
Page 524 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL 124. STATIC DISCHARGERS—CHECK FOR DAMAGE 129. LEFT MAIN FUEL TANK FILLER CAP—SECURE 125. NAVIGATION LIGHT—CHECK FUNCTION 126. WINGTIP—CHECK CONDITION 127. UNDERSIDE—CHECK FOR FUEL LEAKS 130. WING LEADING EDGE—CONDITION AND ANTI- ICE EXHAUST CHECKED 128.
Page 525 FlightSafety Canada L t ée L t d. CL-600-2B16 PILOT TRAINING MANUAL INTENTIONALLY LEFT BLANK FOR TRAINING PURPOSES ONLY W-22 CL 601-3A/R...
Page 526 FlightSafety Canada Lté e FlightSafety Canada L tée Ltd. L td . CL-600-2B16 PILOT TRAINING MANUAL CL-600-2B16 PILOT TRAINING MANUAL 132. AUXILIARY TANK FUEL VENT VALVE 135. MAIN ENTRANCE DOOR AREA—CHECKED EXHAUST—CHECKED 50 51 52 53 54 55 56 57 59 60 61 62 63 64 65 66 133.
Page 527 FlightSafety Canada L tée L td. CL-600-2B16 PILOT TRAINING MANUAL PREFLIGHT WALKAROUND SEQUENCE PRE-WALKAROUND CHECKS-COCKPIT EMPENNAGE LEFT FWD FUSELAGE AFT FUSELAGE UNDERSIDE NLG BAY AFT EQUIPMENT BAY RIGHT FWD/FUSELAGE LEFT ENGINE RIGHT MID FUSELAGE/WING LEFT AFT FUSELAGE RIGHT MAIN LANDING GEAR BAY LEFT MAIN LANDING GEAR BAY RIGHT AFT FUSELAGE LEFT MID FUSELAGE/WING...
Page 528 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CL-601-3A/R APPENDIX FOR TRAINING PURPOSES ONLY CL 601-3A APP-1...
Page 529 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ELECTRICAL Air-Driven Generator AP/EPC Aux Power/External Power Contactor Constant Speed Drive Electronic Circuit Breaker Generator Control Unit Generator Line Contactor Generator Transfer Contactor “GPWR” Ground Power Integrated Drive Generator “OVLD”...
Page 530 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL ANTI-ICE Air Data System Static Air Temperature (Ambient or True Temperature) Total Air Temperature (Ambient Compressibility) AVIONICS Attitude Director Indicator AFCS Automatic Flight Control System (Autopilot Stability Augmentation) Altitude AP, A/P Autopilot...
Page 531 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL AVIONICS VANG Vertical Angle Vertical Gyro Maximum Operating Speed AVIONICS VNAV Vertical Navigation Vertical Speed Weather Yaw Damper FOR TRAINING PURPOSES ONLY APP-4 CL 601-3A/R...
Page 532 FlightSafety Canada L t é e L t d. CL-600-2B16 PILOT TRAINING MANUAL CL-601-3A ANNUNCIATOR PANEL FOR TRAINING PURPOSES ONLY CL 601-3A ANN-1...
Page 533 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FOR TRAINING PURPOSES ONLY ANN-2 CL 601-3A...
Page 534 FlightSafety Canada Ltée FlightSafety Canada L té e Ltd. L td . CL-600-2B16 PILOT TRAINING MANUAL CL-600-2B16 PILOT TRAINING MANUAL ENGINE °C PUSH VIBRATION RESET 1000 HIGH AP DISC MACH TRIM YD OFF MILLS PRESS D.A. TEST COMP PRESS AC POWER AC METERING DC METERING GEN 1...
Page 535 FlightSafety Canada Lté e FlightSafety Canada L té e Ltd. L td . CL-600-2B16 PILOT TRAINING MANUAL CL-600-2B16 PILOT TRAINING MANUAL ICE DETECTOR T/TANK FUEL TRANS PUSH NOSE PUSH TO TEST RESET DUMP SYS 1 FAIL SYS 1 ARMED LEFT RIGHT AP DISC MACH...
Page 536 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL CL-601-3R ANNUNCIATOR PANEL FOR TRAINING PURPOSES ONLY CL 601-3R ANN-1...
Page 537 FlightSafety Canada L t é e L t d . CL-600-2B16 PILOT TRAINING MANUAL FOR TRAINING PURPOSES ONLY ANN-2 CL 601-3R...
Page 538 FlightSafety Canada Ltée FlightSafety Canada L té e Ltd. L td . CL-600-2B16 PILOT TRAINING MANUAL CL-600-2B16 PILOT TRAINING MANUAL °C PUSH L/H ENG R/H ENG HI VIB FAN VIB HI VIB RESET 1000 AP DISC MACH TRIM CORE CORE YD OFF PRESS PRESS...
Page 539 FlightSafety Canada Lté e FlightSafety Canada L té e Ltd. L td . CL-600-2B16 PILOT TRAINING MANUAL CL-600-2B16 PILOT TRAINING MANUAL PUSH NOSE ICE DETECTOR RESET PUSH TO TEST LEFT RIGHT AP DISC MACH TRIM FAIL SYS 1 SYS 1 YD OFF LDG GEAR SYS 2...

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BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual

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