FlightSafety LEARJET 45 Pilot Training Manual

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LEARJET 45

PILOT

TRAINING

MANUAL

VOLUME 2

FlightSafety International

1071 E. Aero Park Blvd.

Tucson, AZ 85706

(800) 203-5627

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Summary of Contents for FlightSafety LEARJET 45

Page 1 FlightSafety international LEARJET 45 PILOT TRAINING MANUAL VOLUME 2 FlightSafety International 1071 E. Aero Park Blvd. Tucson, AZ 85706 (800) 203-5627...
Page 2 Courses for the Learjet 45 and other Learjet aircraft are taught at the following FlightSafety Learning Centers: FlightSafety International Tucson Learning Center 1071 East Aero Park Blvd. Tucson, AZ 85706 (800) 203-5627 • Fax (520) 918-7111 FlightSafety International Atlanta Learning Center...
Page 3 FAA, that of the manufacturer or the FAA shall take precedence. We at FlightSafety want you to have the best training possible. We welcome any suggestions you might have for improving this manual or any other aspect of our training program.
Page 4 CONTENTS 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 Chapter 12...
Page 5: Table Of Contents
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 1 AIRCRAFT GENERAL CONTENTS Page INTRODUCTION ........................1-1 GENERAL..........................1-2 STRUCTURES ........................
Page 6 Windshield and Window Locations ............... 1-14 1-16 Tailcone Access Doors................... 1-15 1-17 Wing Configuration ....................1-16 1-18 Learjet 45 Wing ..................... 1-17 1-19 Learjet 45 Empennage ................... 1-17 1-20 Airplane Static Discharge Wicks ................1-18 1-21 Airplane Antennas ....................1-19...
Page 7: Introduction
INTRODUCTION This training manual provides a description of the major airframe and engine systems installed in the Learjet 45 Model. This chapter covers the structural makeup of the air- plane and gives a general description of the systems. The material presented has been prepared for the basic design data, and all subsequent changes in airplane appearance or system operation will be covered during academic train- ing and in subsequent revisions to this manual.
Page 8: General
GENERAL intakes and aft of the engine exhaust cone. The Learjet 45 is certified under FAR Part 25 FUSELAGE and Part 36 as a transport category airplane. The aircraft is also certified under EC JAR 25 General (European Community–Joint Airworthiness...
Page 9 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 5.4' 9.9' 2.3' 3.7' 17.2' 3.7' 9.3' 45.8' 47.8' 14.3' 58.4'...
Page 10: Turning Radius
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FS 141.85 FS 454.87 FBL 180.72 NOTE: TURNING RADIUS EXPRESSED ABOVE IS BASED UPON 60 NOSEWHEEL DEFLECTION.
Page 11: Danger Areas
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L NOTE: THE ANTENNA SCAN AREA WEATHER RADAR MUST BE FREE OF METALLIC 9 FEET (2.7 M)
Page 12: Fuselage Sections
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FORWARD AFT PRESSURE FORWARD EDGE OF DOOR BULKHEAD PRESSURE BULKHEAD...
Page 13 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Pressurized Section The pressurized area is between the forward pressure bulkhead and the aft pressure bulk- head.
Page 14: Cockpit Layout (Typical)
1. PEDESTAL AND THROTTLE QUADRANT 8. SUNVISOR 2. AIR OUTLETS (ANKLE) 9. DOME LIGHT 3. PILOT'S CIRCUIT BREAKER PANEL 10. PILOT'S CONTROL COLUMN AND WHEEL 4. COPILOT'S CIRCUIT BREAKER PANEL 11. COPILOT'S CONTROL COLUMN AND WHEEL 5. PUBLICATION STORAGE AREAS 12.
Page 15 DISPLAY FLIGHT GUIDANCE DISPLAY CONTROLLER CONTROLLER CONTROLLER PILOT'S CO-PILOT'S PRIMARY MULTI- PRIMARY EICAS FUNCTION FLIGHT FLIGHT DISPLAY DISPLAY DISPLAY RMU-1 RMU-2 AUDIO AUDIO DU-1 DU-2 DU-3 DU-4 SYS TEST/CDH 1 - L/R DISPLAY UNIT REV PANEL 10 - ELECTRICAL CONTROL PANEL 2 - L/R AOA INDICATOR (OPTIONAL) 11 - REVERSION CONTROL PANEL 3 - L/R DIGITAL CHRONOMETER...
Page 16: Airplane Doors
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L TAILCONE ACCESS DOOR (RIGHT SIDE) EMERGENCY DOOR (RIGHT SIDE) VENT DOOR...
Page 17: Passenger/Crew Entry Door (Closed/Open)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L VENT DOOR KEYLOCK OUTSIDE HANDLE PULL-UP CABLE LOWER HANDLE Figure 1-11. Passenger/Crew Entry Door (Closed/Open) There are a total of 12 locking pins on the two Also, the “ENTRY DOOR”...
Page 18: Airplane Door Messages And Warnings
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ENTRY DOOR ENTRY EMERGENCY EXIT DOOR EXTERNAL DOORS ENTRY DOOR PIN...
Page 19: Door Latch Inspection Ports And Inside Locking Handle
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 1-13. Door Latch Inspection Ports and Inside Locking Handle The lower passenger/crew door has a cable Figure 1-14.
Page 20: Windshield And Window Locations
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 1-15. Windshield and Window Locations Windows Fuel Section The fuel section is located aft of the rear pres- Windshield sure bulkhead.
Page 21: Wing
This compartment houses major components of the The Learjet 45 wing, as shown in Figures 1- electrical, environmental and engine fire ex- 17 and 1-18, is a swept (13°) high aspect ratio tinguishing systems.
Page 22: Wing Configuration
AILERON FLAP SPOILERON SAWTOOTH (3) SAWTOOTH (TOP VIEW) VORTILONS (4) WING ROOT TRIANGLES (8) STALL STRIP (1) NOTE: ILLUSTRATION NOT TO SCALE Figure 1-17. Wing Configuration...
Page 23: Empennage
L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 1-18. Learjet 45 Wing • Four vortilons are added to the underside •...
Page 24: Static Discharge Wicks
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Wicks on each Winglet (4) Wicks on each Elevator (3)
Page 25: Airplane Antennas
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 1-21. Airplane Antennas The master MEL reads as follows: “Four (static discharge wicks) may be miss-...
Page 26: Review Questions
L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS A white “ENTRY DOOR PIN” and a red The Learjet 45 wing has the following “ENTRY DOOR” CAS message illumi- specific features: nated at the same time could indicate: A.
Page 27 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 2 ELECTRICAL POWER SYSTEMS CONTENTS Page INTRODUCTION ........................2-1 GENERAL..........................
Page 28 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Generator Busses ......................2-24 Main Busses........................2-24 Main Avionic Busses ..................... 2-24 Essential Busses......................
Page 29 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page Component Locations....................2-2 Electrical Control Panel ................... 2-2 Main Batteries Location...................
Page 30 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS (CONT.) Figure Title Page 2-24 System with Double Generator Failure (In Flight) ..........2-37 2-25 Emergency Power Supply System .................
Page 31: Introduction
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 2 ELECTRICAL POWER SYSTEMS L ESS VOLT EMER BUS VOLTS R ESS VOLT 28.2...
Page 32: General
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L APU (OPTIONAL) ALTERNATOR GENERATOR EMERGENCY BATTERY MAIN LEFT RIGHT BATTERIES &...
Page 33: Dc Power Sources
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L close when the battery switch is selected on. DC POWER SOURCES...
Page 34: Emergency Battery
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Battery starts may be made at temperatures cations under normal operation. The emer- above 0°C.
Page 35: Ground Power Unit (Gpu)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The EMER BATT is normally selected on be- fore engine start and remains on throughout t h e f l i g h t .
Page 36: Auxiliary Power Unit (Apu)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L AUXILIARY POWER UNIT (APU) The optional APU generator can provide the...
Page 37: Generators
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L GENERATORS DEEC Two engine-driven starter/generators, one on each engine accessory section (Figure 2-7), provide the normal source of 28 VDC power.
Page 38: Generator Control Units
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L starter. This is a back-up to the normal cutoff GENERATOR CONTROL...
Page 39: Electrical Control Panel
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ELECTRICAL CONTROL PANEL GENERAL The electrical switches and indicators include...
Page 40 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L closed when operating on battery power only. ELECTRICAL SWITCH The CAS also provides a BUS TIE CLSD and INDICATORS (S/I’...
Page 41 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If a generator trips off-line, the switch displays The top half of the EMER BATT switch dis- “OFF”...
Page 42: Electrical System Indicators
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell FMS1 BATT OVHT KDVT L R GEN FAIL 75.0...
Page 43 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell 75.0 75.0 50.0 50.0 75.0 75.0 OIL °C...
Page 44: Electrical Limits
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L if emergency bus voltage is less than 22 volts Table 2-1. ELECTRICAL LIMITS or more than 29.5 volts.
Page 45 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L BATT EMER R BATT GEN FAIL OVHT BATT OVHT...
Page 46 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L ESS VOLT EMER BUS VOLTS R ESS VOLT 28.0 28.0...
Page 47: Cas Message Database And Logic Summary
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 2-2. CAS MESSAGE DATABASE AND LOGIC SUMMARY Type Logic Summary...
Page 48: Distribution System Components
CIRCUIT BREAKER PANELS for a short period of time. Extreme or pro- longed overloading will cause a fuse to blow, On the Learjet 45 airplanes, the circuit break- isolating a particular circuit and precluding ers are grouped by systems rather than by progressive failure of other electrical compo- busses (see Figures 2-15 and 2-16).
Page 49: Normal Contactor Operation
Table 2-3. NORMAL CONTACTOR OPERATION L START R START ELECTRICAL CONTROL EMER L AV R AV L AV R AV EXT PWR BUS-TIE L GEN R GEN L BATT R BATT BATT MSTR MSTR MSTR MSTR L MAIN R MAIN NON-ESS NON-ESS PANEL...
Page 50 F O RWA R D AVIONICS INSTRUMENTS/INDICATIONS GEAR/HYDRAULICS FLIGHT ELECTRICAL DISPLAY NOSE STEER L AV BUS COMMUNICATIONS STALL AUDIO 1/ L WARN ELEV L WHL DU 1 WARN SELCAL HF 1 ATC 1 COMM 1 CLR DLY PANEL L CTRL DU 2 SG 1 MOTOR...
Page 51 F O RWA R D FLIGHT INSRUMENTS/INDICATIONS AVIONICS ELECTRICAL GEAR /HYD DISPLAY COMMUNICATIONS R AV BUS R WHL R WARN STALL MAIN R GEN WARN MSTR FORCE SQUAT SG 2 DU 3 DU 4 R CTRL PANEL AUDIO 2 COMM 2 ATC 2 HF 2 COMM 3 R ESS BUS TRIM...
Page 52 R ESS BUS L ESS AV BUS L ESS BUS EMER BATT BUS R ESS AV BUS 100A 100A L AV R AV MSTR MSTR R ISOLATION L ISOLATION CONTACTOR CONTACTOR EMER BATT START/STOP EMER EMER START BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 53: Distribution
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • Left & right audio control unit (L & R...
Page 54: Split Bus System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L SPLIT BUS SYSTEM MAIN BUSSES The split bus electrical system (Figure 2-17)
Page 55: Isolation Contactors
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L fed by the left and right generator busses re- Since the right isolation contactor is normally...
Page 56: Emergency Battery Bus
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L EMERGENCY BATTERY BUS DISTRIBUTION SUMMARY The emergency battery bus (Figure 2-17) is...
Page 57: Ac Power
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 2-21 illustrates the status of the con- tactors and busses after engine start with one engine-driven generator on-line.
Page 58 R ESS BUS L ESS AV BUS L ESS BUS EMER BATT BUS R ESS AV BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 59 R ESS BUS L ESS AV BUS L ESS BUS EMER BATT BUS R ESS AV BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 60 L ESS AV BUS L ESS BUS EMER BATT BUS R ESS BUS R ESS AV BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 61 EMER BATT BUS R ESS BUS L ESS AV BUS L ESS BUS R ESS AV BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN BUS R MAIN BUS R MAIN AV BUS L MAIN AV BUS...
Page 62 EMER BATT BUS R ESS BUS R ESS AV BUS L ESS AV BUS L ESS BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 63: Abnormal Modes Of Operation
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ABNORMAL MODES OF OPERATION BATTERY OVERHEAT If either nickel-cadmium main battery exceeds the temperature value shown in Table 2-1, the crew will be alerted in several different ways.
Page 64: Single Generator Failure
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L SINGLE GENERATOR FAILURE In the event of a single generator failure in...
Page 65 R ESS BUS L ESS AV BUS L ESS BUS EMER BATT BUS R ESS AV BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 66: Dual Generator Failure
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 2-4 shows what components and sub-sys- DUAL GENERATOR FAILURE...
Page 67: System With Double Generator Failure (In Flight)
R ESS BUS L ESS AV BUS L ESS BUS EMER BATT BUS R ESS AV BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 68: Emergency Power Supply System
L ESS AV BUS L ESS BUS EMER BATT BUS R ESS BUS R ESS AV BUS R ISOLATION L ISOLATION CONTACTOR CONTACTOR 100A 100A EMERGENCY R ESS AVIONIC L ESS AVIONIC CONTACTOR CONTACTOR CONTACTOR EMER BATT L MAIN AV BUS L MAIN BUS R MAIN BUS R MAIN AV BUS...
Page 69: Dc Power Distribution With Double Generator Failure
Table 2-4. DC POWER DISTRIBUTION WITH DOUBLE GENERATOR FAILURE L ESS BUS L ESS AV EMER BATT BUS R ESS AV R ESS BUS COMM 1, AUDIO 1, CABIN PA, ADF 1 DU 1 EMER BUS/VOLTS DU 3 AUDIO 2 RAD ALT 1 DME 1, NAV 1, FMS 1, ATC 1 DAU1 CH A...
Page 70: Abnormal Contactor Operation
Table 2-5. ABNORMAL CONTACTOR OPERATION L START R START ELECTRICAL EMER L AV R AV L AV R AV CONTROL EXT PWR BUS-TIE L GEN R GEN L BATT R BATT BATT MSTR MSTR MSTR MSTR L MAIN R MAIN NON-ESS NON-ESS PANEL...
Page 71: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS The battery contactor for a main battery Which of the following items is not on one...
Page 72 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L When operating inflight with a dual gen- 13. How long will the emergency battery erator failure, __________ .
Page 73 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 17. Which of the following statements is true regarding use of the APU for electrical power? A.
Page 74 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 3 LIGHTING CONTENTS Page INTRODUCTION ........................3-1 GENERAL..........................3-1 INTERIOR LIGHTING......................
Page 75 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page Interior Lighting Locations ..................3-2 Cockpit Lighting....................... 3-3 Pilot L CREW LIGHTS Control Panel ..............
Page 76: Introduction
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 3 LIGHTING EXIT INTRODUCTION Lighting is used to illuminate the cockpit area and all flight instruments. The majority of the instruments are internally lighted.
Page 77: Interior Lighting
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Cabin lighting consists of entry, overhead, sources to lighting groups. See Figure 3-2 and table and reading lights (spot lights), and lava- the descriptions within this chapter.
Page 78 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L DISPLAY FLIGHT GUIDANCE DISPLAY CONTROLLER CONTROLLER CONTROLLER PILOT'S CO-PILOT'S PRIMARY...
Page 79 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 3-3. Pilot L CREW LIGHTS Figure 3-4. Copilot R CREW LIGHTS...
Page 80: Cabin Lighting
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L in the CABIN group of circuit breakers on A S/I bulb test may be initiated by selecting the copilot side.
Page 81 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L is located on the left-hand storage cabinet, for- ward of the cabin door. Additional lighting...
Page 82 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CABIN LIGHT SPOT LIGHT COCKPIT DISABLE ENTRY CABIN CABIN LIGHT...
Page 83: Baggage/Tailcone Lighting
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L seats on each side of the cabin. Some seats have...
Page 84: Emergency Lighting System
OFF position the The emergency lighting system is standard on emergency lights are inhibited. When the the Learjet 45 and consists of cabin overhead, cockpit switch is in the ON position, the emer- floor proximity lights (seat-base mounted), Figure 3-9.
Page 85: Abnormal Interior Lighting Conditions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L gency lighting group illuminates. Activation ABNORMAL INTERIOR periods are limited by a timing circuit to a min-...
Page 86 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L STANDBY COMPASS CREW WARNING PANEL AUDIO AUDIO CONTROL CONTROL PANEL...
Page 87: Exterior Lighting
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L control power from the respective left and EXTERIOR LIGHTING r i g h t m a i n bu s s e s t h r o u g h t h e L a n d R TAXI/LDG CTRL circuit breaker.
Page 88 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L POSITION/NAV LIGHT TAIL – UPPER (WHITE) ANTICOLLISION/STROBE BEACON – UPPER...
Page 89: Anticollision Lights (Beacon/Strobe)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 3-18. Upper Anticollision Light Figure 3-16. Wing-Tip Navigation Light ANTICOLLISION LIGHTS airborne.
Page 90: Wing Inspection Light
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Selection of the baggage area light is by an ad-...
Page 91 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS The instrument panel floodlight control Which of the following lights can be op-...
Page 92 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 4 MASTER WARNING SYSTEM CONTENTS Page INTRODUCTION ........................4-1 GENERAL..........................
Page 93: Table Title Page
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page Master Warning System ................... 4-3 System Test Switch ....................4-4 CAS Message Display on EICAS ................
Page 94: Introduction
Crew alerting is through visual and aural means. GENERAL The Learjet 45 master (crew) warning system annunciators and/or voice and tone messages. consists of the crew warning panel (CWP),...
Page 95: Master Warning/Caution Lights
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L tion of the EICAS (Engine Instrument/Crew announce the condition; and in some cases,...
Page 96 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L ENG NORMAL R ENG L REV EMER R BATT...
Page 97: Warning System Lights
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • Activating the airplane system light • All switch/indicators (S/Is) will illu- (LTS) test on the system test switch.
Page 98: Bulb Change
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L to provide power, the other essential bus pro- an amber “LR WARN PWR FAIL” and amber vides a redundant power source.
Page 99: Collector Messages
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L COLLECTOR MESSAGES When an engine stops running, as the engine...
Page 100: Cas Message Inhibit Mode Of Operation
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • Both squat switches are in the ground CAS MESSAGE INHIBIT MODE mode.
Page 101: Aural Warnings
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L in ground mode and either thrust lever in TAKEOFF idle and airspeed below 40 knots).
Page 102 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-1. AURAL WARNING AND VOICE SUMMARY WARNING AURALS SOUND/VOICE FREQUENCY REF.
Page 103: Abnormal Condition Indications
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • Parking brake is ON (white CAS message ABNORMAL CONDITION “EMER/PARK BRK”...
Page 104 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.1. CWP/CAS MESSAGE SUMMARY FOR TRAINING PURPOSES ONLY 4-11...
Page 105 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.2. CWP/CAS MESSAGE SUMMARY (CONT) FOR TRAINING PURPOSES ONLY...
Page 106 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.3. CWP/CAS MESSAGE SUMMARY (CONT) FOR TRAINING PURPOSES ONLY...
Page 107 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.4. CWP/CAS MESSAGE SUMMARY (CONT) Land Chpt CAS Message...
Page 108 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.5. CWP/CAS MESSAGE SUMMARY (CONT) Land Chpt CAS Message...
Page 109 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.6. CWP/CAS MESSAGE SUMMARY (CONT) Land Chpt CAS Message...
Page 110 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.7. CWP/CAS MESSAGE SUMMARY (CONT) Land Chpt CAS Message...
Page 111 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 4-2.8. CWP/CAS MESSAGE SUMMARY (CONT) Land Chpt CAS Message...
Page 112 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS How are the master WARN/CAUT lights To eliminate nuisance warning/caution...
Page 113 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 5 FUEL SYSTEM CONTENTS Page INTRODUCTION ........................5-1 GENERAL..........................5-1 WING TANKS ........................
Page 114 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Expansion Lines......................5-16 FUEL SYSTEM DRAIN VALVES..................5-19 FUELING/DEFUELING ...................... 5-19 General...........................
Page 115 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page Fuel System ......................5-3 Fuselage Fuel Gravity Fill Port ................5-4 Fuel Quantity Indicating System................
Page 116: Introduction
ENG SYNC EDS RECORD INTRODUCTION The Learjet 45 fuel system consists of the fuel storage, quantity indicating, transfer, vent system and single-point pressure refueling system. The fuel system is covered in this chapter from the storage areas to the high-pressure engine fuel pumps, at which point fuel system operation becomes a function of the powerplant.
Page 117: Wing Tanks
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L of these jet pumps is to pull fuel through the WING TANKS transfer lines from the fuselage tank.
Page 118 STANDBY COLLECTOR PUMP (2) TANK (2) SCAVENGE TRANSFER JET PUMP (8) JET PUMP (2) LEFT RIGHT CROSSFLOW WING WING VALVE TANK TANK (1678#) (1676#) FLOAT SWITCH (2) FUEL FILTERS MAIN JET PUMP (2) LEGEND NACA RAM AIR INLET PRESSURE WING/FUSELAGE TANKS GRAVITY SWITCH (2) FILL...
Page 119: Fuselage Tank
The total fuel capacity of the Learjet 45 is ap- proximately 904 gallons (3,422 liters) or ap- proximately 6,062 pounds (2,748 kg.) when a fuel density of 6.7 pounds per gallon factor is applied.
Page 120: Fuel Quantity Indicating System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FUEL DENSITY COMPENSATOR PROBES FUSELAGE TANK RIGHT WING LEFT WING...
Page 121: Fuel Quantity Display
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Following aircraft system power-up, the fuel FUEL QUANTITY DISPLAY quantity computer BITE sequence is initiated.
Page 122 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell FMS1 MAG2 L R FUEL PRESS LOW L R FUEL HEATER KDVT 75.0...
Page 123 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell 75.0 75.0 50.0 50.0 75.0 75.0 OIL °C...
Page 124: Crew Alerting System (Cas)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 5-1. FUEL SYSTEM CAS MESSAGES TYPE CAS MESSAGE LOGIC SUMMARY Low pressure to engine fuel pump inlet (<...
Page 125 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 4300 LBS ON BOARD R WING L WING 1650 1650...
Page 126: Fuel Transfer System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L tects less than 350 pounds of fuel in the re- CROSSFLOW VALVE spective wing tank.
Page 127: Standby Pumps
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L the crew with the Master Caution light and an breaker located in the FUEL group of circuit amber “FUEL XFLO”...
Page 128 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L FUEL PRESS FUEL R STBY FIRE L STBY XFLOW...
Page 129: Motive-Flow Fuel And Jet Pumps
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L fuel to the engine after start. The engine-driven Another jet pump is located in each fuselage-...
Page 130: Fuel Low-Pressure Switches
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 10-20 psi 150-420 psi LEGEND HIGH PRESSURE LOW PRESSURE STORAGE Figure 5-9.
Page 131: Ram-Air Vent System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The most probable cause of a FUEL PRESS LOW light is failure of the affected wing jet pump.
Page 132 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L RIGHT WING FUEL TANK LEFT WING FUEL TANK VENT/EXPANSION LINE...
Page 133 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CROSSFLOW R ENGINE FEED L ENGINE FEED R TRANSFER LINE...
Page 134: Fuel System Drain Valves
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FUELING/DEFUELING GENERAL The aircraft fuel system and engines are qualified for use with the fuel types spec- ified in the Aircraft Flight Manual FUEL S E RV I C I N G A d d e n d u m .
Page 135: Single-Point Pressure Refueling (Sppr)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L light (Figure 5-15). The READY position of the defuel switch has an amber annunciator as- sociated with it and the OFF position has a green annunciator associated with it.
Page 136 REFUEL/DEFUEL NOTE: On some aircraft equipped with the optional pylon lights, the FUEL SYS switch has three positions: Up is labeled TOTAL FUEL QTY ON/FLD LT (flood light); middle – ON; and down – OFF. READY PWR ON PILOT VALVE PILOT LINE VENT/EXPANSION LINE REFUEL SHUTOFF VALVE...
Page 137: Gravity Refueling
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • Precheck Valve GRAVITY REFUELING Refueling the aircraft can also be accom-...
Page 138 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FUEL XFLO OPEN DEFUEL VALVE DEFUEL OPEN REFUEL/DEFUEL TOTAL FUEL QTY...
Page 139: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS The approximate maximum usable fuel A FUEL IMBALANCE caution message...
Page 140 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The wing fuel tanks are pressurized/ven- 13. The allow pressure to equal- tilated inflight by: ize between all three fuel tanks.
Page 141 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 6 AUXILIARY POWER UNIT CONTENTS Page INTRODUCTION ........................6-1 GENERAL..........................
Page 142 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page Auxiliary Power Unit (APU)..................6-2 APU Major Sections....................6-3 APU Air Intake......................
Page 143: Introduction
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 6 AUXILIARY POWER UNIT INTRODUCTION The optional Auxiliary Power Unit (APU) provides an electrical power supply and a pneu- matic source for operation of the aircraft environmental system during ground opera- tions.
Page 144: Auxiliary Power Unit (Apu)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ate all load requirements. The APU is said to APU operation is self-governing with auto-...
Page 145 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L COMPRESSOR SECTION INTAKE EXHAUST COMBUSTION & ACCESSORY TURBINE GEARBOX SECTION Figure 6-2.
Page 146: Apu Cooling Fans
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 6-4. APU Exhaust Outlet Figure 6-5. Left Side APU Cooling Fan...
Page 147: Apu Systems
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 80 psi, depending upon oil temperature. A re- lief valve is set at 200 psi to prevent over- pressure.
Page 148 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L When system faults are detected, the ECU au- Fuel System...
Page 149: Apu Operation
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • On-speed governing APU OPERATION • Normal shutdown General • Fault detection and fault logging...
Page 150 PACK EMER PRESS HI FLOW FROM RH CHECK ENGINE VALVE L BLEED R BLEED APU BLEED ENVIRONMENTAL CONTROL UNIT PACK PRESSURIZATION CONTROL PANEL (SEE CHAPTER 11) FROM LH BI-LEVEL ENGINE PRSOV MASTER GEN AMPS I 0 0 FIRE MONOPOLE START/STOP FUEL NOZZLES START...
Page 151 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The ECU activates the firewall fuel solenoid Additionally, to allow APU bleed air into the and the right standby boost pump, a white “R...
Page 152 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If the APU is running with ground power Automatic Shutdown and...
Page 153: Maintenance Panel
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Addendum indicates that action is re- MAINTENANCE PANEL quired. At the time the LOW annun-...
Page 154: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS The APU is approved for use during The AFM limitation (field pressure alti- ground and flight operations.
Page 155 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 7 POWERPLANT CONTENTS Page INTRODUCTION ........................7-1 GENERAL..........................7-1 MAJOR SECTIONS........................
Page 156 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Backup Engine Indicators....................7-14 ENGINE CONTROL SYSTEM.................... 7-15 General........................... 7-15 Engine/Fuel Control Panel.....................
Page 157 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ENGINE OIL SYSTEM......................7-29 General........................... 7-29 Oil Supply ........................7-29 Oil System Operation.....................
Page 158 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page TFE731-20 Major Sections ..................7-3 Airflow Diagram ...................... 7-4 Accessory Drive Components ..................
Page 159 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 7-24 Thrust Reverser (Dee Howard TR 5045) ............... 7-33 7-25 Thrust Reverser Doors and Latches ...............
Page 160: Introduction
CHAPTER 7 POWERPLANT INTRODUCTION This chapter describes the components and operation of the Learjet 45 powerplant. In addition to the powerplant, engine-related sub-systems such as the oil, fuel, ignition, engine controls and instrumentation, synchronization, and the thrust reverser system are described.
Page 161: Major Sections
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L MAJOR SECTIONS FAN SECTION The fan section consists of a single-stage fan...
Page 162 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L COMBUSTOR COMPRESSOR AIR INLET TURBINE LP HP HP LP EXHAUST DUCT...
Page 163: Combustion Section
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CENTRIFUGAL FOUR-STAGE AXIAL SINGLE-STAGE COMPRESSOR COMPRESSOR TURBINE BYPASS AIR TOTAL AIR...
Page 164: Exhaust Section
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L High-Pressure (HP) Turbine DEEC The HP turbine is a single-stage, axial-flow...
Page 165: Engine Instruments
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell 75.0 75.0 89.6 89.6 Honeywell 75.0 75.0 89.6 89.6 50.0...
Page 166: Fan Speed (N 1 )
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Normal circuit for engine EICAS indications to (DU 2) (DU 3)
Page 167 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L LEFT N1 RIGHT N1 RIGHT DEEC N1 INDICATOR INDICATOR REFERENCE...
Page 168: Turbine Temperature (Itt)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 7-1. ENGINE SPEED Turbine Temperature (ITT) Turbine temperature is sensed by ten parallel-...
Page 169: Turbine Speed (N 2 )
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 7-2. ITT DISPLAY OPERATING WHITE AMBER ° C ° C °...
Page 170: Fuel Flow
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 1014 1014 CONDITION 2 CONDITION 1 • Engine start or •...
Page 171: Eicas Engine Indications
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • Thrust lever position (MCR, MCT, T/O) EICAS Engine Indications (EIs) Listed below are the indications that can ap- •...
Page 172 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 7-3. EICAS ENGINE INDICATIONS Type EICAS Eng Ind (EI)
Page 173: Crew Warning Panel (Cwp)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L REV R REV UNSAFE UNSAFE L OIL L FUEL...
Page 174: General
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell 75.0 75.0 OIL C FF PPH 1002 75.0 75.0...
Page 175: Engine/Fuel Control Panel
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ON position where they provide electrical ENGINE/FUEL CONTROL power to the DEECs for computer-on opera- PANEL tion.
Page 176 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • MCR (maximum cruise thrust) torque motor in the fuel controller to sched- ule fuel to achieve the computed N1.
Page 177: Digital Electronic Engine Control (Deec)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L DIGITAL ELECTRONIC ENGINE CONTROL (DEEC) GENERAL A digital electronic engine control (DEEC),...
Page 178 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PT 2 TT 2 SURGE VALVE IDLE CUTOFF IGNITION RELAY...
Page 179: Engine Fuel System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The engine remains in computer-on control and switch, the ultimate overspeed protection will engine operation is not affected.
Page 180: Engine Fuel Pumps
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FUEL HEATER/OIL COOLER FUEL PUMP FUEL CONTROL UNIT (FCU) FILTER...
Page 181: Fuel Control Unit (Fcu)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L provides a signal to generate a “L/R FUEL • A manual shutoff valve, operated me- FILTER”...
Page 182 LR ENGCMPTR FAULT ENGINE/FUEL CONTROL PANEL (MINOR FAULT) LR ENGCMPTR FAULT R ENGINE L ENGINE FUEL EXTINGUISHER FIRE L STBY XFLOW R STBY FIRE EXTINGUISHER (MAJOR FAULT) CLOSED CLOSED ARMED ARMED ARMED ARMED FIRE FIRE FUEL USED RESET PUSH PUSH ELECTRONIC CONTROL L START...
Page 183: Flow Divider
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The DEEC activates the ignition during three FLOW DIVIDER automatic modes of operation. (1) The first is...
Page 184: Starter
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 7-17. Engine Start and Ignition Switches STARTER to amber if the starter relay is still energized closed above 51% N2.
Page 185 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L DEEC begins the auto-start sequence by en- The engine can be started in the manual mode...
Page 186: Engine Synchronization
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 75.0 75.0 SYNC SYNC 50.0 50.0 OIL PSI Figure 7-19. ENG SYNC Switch OIL °C...
Page 187: Automatic Performance Reserve (Apr)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L vertently activated on the ground (i.e. if the AUTOMATIC PERFORMANCE...
Page 188: Engine Oil System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L mentarily depressing the EDS RECORD but- ton on the engine/fuel control panel (Figure 7-19).
Page 189 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L VENT TO AMBIENT TRANSFER NO. 4 AND NO. 5 NO. 4 AND NO. 5...
Page 190 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Type Logic Summary CAS Message Low oil pressure, < 50 psi.
Page 191: Engine Chip Detector
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 7-5. OIL PRESSURE DISPLAY Table 7-6. OIL TEMPERATURE DISPLAY...
Page 192: Thrust Reverser System
THRUST REVERSER SYSTEM GENERAL The thrust reverser system is installed as stan- dard equipment on the Learjet 45. The thrust reversers are electrically controlled and hy- draulically actuated target type thrust reversers (Figure 7-24) which operate independently of each other. When the thrust reverser doors are deployed, engine exhaust is deflected in a for- ward direction.
Page 193 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L UPPER DOOR ASSEMBLY LATCH LINK ASSEMBLY RODS DEPLOY SWITCH PRIMARY...
Page 194: Actuators
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L an ANN circuit breaker, also one on each side, Control Valve...
Page 195 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L LATCH HOOK LOCK/UNLOCK SWITCH (TRIPS THE "UNL" INDICATOR) LATCH ACTUATOR...
Page 196: System Operation
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L (Figure 7-25) will cause the UNL annunciator SYSTEM OPERATION to extinguish and a green DEP annunciator to General illuminate.
Page 197 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Type Logic Summary CAS Message L R REV AUTOSTOW Autostow activated due to uncommanded unlock.
Page 198 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L MAIN HYDRAULIC SYSTEM PRESSURE ISOLATION VALVES (IN TAILCONE) PRESSURE SWITCHES...
Page 199: Stow (Normal & Automatic)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L AIRSPEED — KIAS Figure 7-29. Reverser Thrust Limit Schedule than one hook is in the unlocked position. An Stow (Normal &...
Page 200: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS The TFE731-20 engines each provide If both channels of DAU 1 fail, how will...
Page 201 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 10. Automatic ignition is provided to the en- 16. When operating with a dual generator...
Page 202 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 20. The performance reserve system provides 25. A/an DEP displayed on the...
Page 203 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 8 FIRE PROTECTION CONTENTS Page INTRODUCTION ........................8-1 ENGINE FIRE DETECTION ....................8-1 ENGINE FIRE INDICATION....................
Page 204 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page Engine Fire Detection System.................. 8-2 Engine Fire Detection System Indicators..............8-3 Engine/Fuel Control Panel ..................
Page 205: Introduction
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 8 FIRE PROTECTION FIRE PUSH ARMED ARMED INTRODUCTION The fire protection system consists of fire detector sensing elements for each engine and APU...
Page 206 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L R ENG FIRE FAIL ON GROUND L R ENG FIRE FAIL...
Page 207: Engine Fire Indication
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L WARN WARN AUDIO TONE: CHIME, CHIME, CHIME FIRE 75.0 AUDIO VOICE: AUDIO VOICE: "LEFT ENGINE FIRE,...
Page 208: Engine Fire Extinguishing
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L ENGINE FUEL R ENGINE EXTINGUISHER FIRE L STBY R STBY...
Page 209 L ENGINE R ENGINE EXTINGUISHER FIRE FIRE EXTINGUISHER CLOSED CLOSED ARMED ARMED ARMED ARMED FIRE FIRE PUSH PUSH L FWSOV CLSD R FWSOV CLSD BLEED AIR BLEED AIR PRESSURE SHUTOFF SHUTOFF VALVE VALVE PRESSURE GAGE GAGE TWO-WAY CONTAINER CONTAINER CHECK FUEL FUEL VALVES...
Page 210: Extinguisher Containers
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L EXTINGUISHER CONTAINERS The two fire extinguisher agent containers (Figure 8-5) are spherical in shape and are lo- cated on the right side in the tailcone equip- ment bay.
Page 211: Apu Fire Protection System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 8-7. APU Fire Detection Loop The APU fire extinguishing agent container is...
Page 212 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 8-8. APU Fire Extinguisher Container and Pressure Gage may use this panel to operate the APU fire- APU Maintenance Control Panel, open and bottle if a fire occurs.
Page 213 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L APU FIRE MASTER GEN AMPS I 0 0 FIRE START/STOP...
Page 214: System Operation
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L SYSTEM OPERATION FIRE DETECTION SYSTEM TEST APU Fire Detection System...
Page 215: Hand-Held Fire Extinguishers
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 8-12. Cabin Fire Extinguisher HAND-HELD FIRE EXTINGUISHERS FIRE EXTINGUISHERS Two, readily accessible, 2.5 pound fire extin-...
Page 216: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS Engine fire extinguisher containers are lo- When an overheat/fire condition is de-...
Page 217 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 9 PNEUMATICS CONTENTS Page INTRODUCTION ........................9-1 GENERAL..........................9-1 DESCRIPTION AND OPERATION ..................
Page 218 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page Pressurization/Oxygen Control Panel ..............9-3 Bleed-Air System ..................... 9-6 Bleed-Air System Control Schematic ..............
Page 219: Introduction
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 9 PNEUMATICS BLEED AIR INTRODUCTION The airplane pneumatic system consists of two independent engine bleed-air distribution sys- tems.
Page 220: Description And Operation
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The pneumatic system incorporates overheat, HIGH-PRESSURE (HP) BLEED- overpressurization and leak protection through AIR SYSTEM continuous monitoring and aircrew alerting.
Page 221: Bleed-Air System Components
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PAX OXYGEN PRESSURIZATION DEPLOY OXY/AUTO CABIN PRESSURE CONTROL 3 5 0 CAB RATE I .
Page 222: Ecs Pressure Regulator Shutoff Valves (Ecs Prsov)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L troller to operate the following: HP SHUTOFF VALVES (HP SOV) The left and right HP SOVs are independently •...
Page 223 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 9-1. BLEED-AIR VALVE CONFIGURATION SWITCH POSITION VALVE STATUS L/R BLEED...
Page 224 WING WING FLIGHT CABIN DECK GASPERS CHECK DISTRIBUTION VALVE FLOW CHECK VALVES (5) LIMITING PRSOV VENTURI PRSOV AFT BULKHEAD EMER PRESS SOV EMER PRESS SOV R ENGINE L ENGINE EMER PRESS FLOW NACELLE CHECK NACELLE ISOLATION LIMITING CHECK VALVES VALVE VENTURI HP BLEED HP BLEED...
Page 225 FLIGHT CABIN DECK GASPERS PRSOV PRSOV AFT BULKHEAD EMER PRESS SOV EMER PRESS SOV R ENGINE L ENGINE NACELLE NACELLE HP BLEED HP BLEED OUTLETS OUTLETS PACK CHECK BI-LEVEL VALVE CHECK PRSOV VALVE PRESS PRESS SWITCH SWITCH 130 PSI 130 PSI PRSOV PRSOV WING...
Page 226 WING WING FLIGHT CABIN DECK GASPERS CHECK DISTRIBUTION VALVE FLOW CHECK VALVES (5) LIMITING PRSOV VENTURI PRSOV AFT BULKHEAD EMER PRESS SOV EMER PRESS SOV R ENGINE L ENGINE EMER PRESS FLOW NACELLE CHECK NACELLE ISOLATION LIMITING CHECK VALVES VALVE VENTURI HP BLEED HP BLEED...
Page 227: Pylon Overhear Detection
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PYLON OVERHEAT DETECTION TAILCONE LEAK DETECTION T h e r e a r e f o u r 2 5 0 ° F ove r- t e m p e r a t u r e...
Page 228 WING WING FLIGHT CABIN DECK GASPERS CHECK DISTRIBUTION VALVE FLOW CHECK VALVES (5) LIMITING PRSOV VENTURI PRSOV AFT BULKHEAD EMER PRESS SOV EMER PRESS SOV R ENGINE L ENGINE EMER PRESS FLOW NACELLE CHECK NACELLE ISOLATION LIMITING CHECK VALVES VALVE VENTURI HP BLEED HP BLEED...
Page 229: Emergency Pressurization
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L EMERGENCY EMER PRESS Operation PRESSURIZATION The emergency pressurization valves (labeled...
Page 230: Servo Air System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L bleed-air is routed directly into the cabin area, SERVO AIR SYSTEM...
Page 231 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L ENG NORMAL L ENG R ENG R ENG L REV...
Page 232 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The HI FLOW switch/indicator, located be- neath the PACK S/I, signals the pack bi-level valve to go to a full open position.
Page 233 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS In order to provide engine bleed-air to the Illumination of a “L or R BLEED AIR...
Page 234 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If emergency pressurization activates in- 12. Which of the following is true regarding...
Page 235 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 236 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 237: Introduction
CHAPTER 10 ICE AND RAIN PROTECTION INTRODUCTION Anti-icing and rain protection equipment on the Learjet 45 is designed to detect and prevent the build-up of ice on: • The engine nacelle lip and engine inlet pressure and temperature probe • The windshield •...
Page 238: Ice Detection
FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Icing conditions also exist when the SAT on anti-ice equipment turned on, the “ICE DE-...
Page 239: Instrument Panel
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • “ICE DETECTED” (amber)–This mes- NOTE sage is displayed when the system de-...
Page 240: Engine Anti-Ice System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L perature sensor, stall warning vanes, total tem- ulated pressure duct by the nacelle anti-ice perature (TAT) probe, and the windshield.
Page 241 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Whenever a “NAC” annunciator is displayed Engine Anti-Ice Annunciations in amber for the above reasons, there is a cor- When the NAC switches are selected ON, responding amber “L or R NAC HT”...
Page 242: Windshield Anti-Ice And Defog System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell L R NAC HT L R NAC HT FAIL ON 75.0...
Page 243 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 10-1. ICE AND RAIN PROTECTION CAS MESSAGE DATABASE Type...
Page 244 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L NORMAL SENSOR OVHT SENSOR *PDP POWER DISTRIBUTION HEATING ELEMENT HEATING ELEMENT...
Page 245: Wing/Stab Anti-Ice System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The A/I PRSOVs are opened and closed (mod- WING/STAB ANTI-ICE SYSTEM...
Page 246 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L (SEE TABLE 10-1) WING/STAB L WING/ R WING/ STAB HT...
Page 247 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L ENG NORMAL R ENG L REV EMER R BATT...
Page 248 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L LEFT SIDE RIGHT SIDE Figure 10-8. Pitot-Static Probes, AOA Transducer Vanes, and Total Air Temperature Probe...
Page 249: Pitot-Static And Stall Warning Anti-Ice Systems
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 10-2. PROBES HEAT SUMMARY SWITCH COMPONENT CAS MESSAGE CIRCUIT BREAKER...
Page 250: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS An amber ICE DETECTED message on Which of the following is heated electri-...
Page 251 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L With the pitot heat system selected off (PROBE S/I’s), what CAS messages should be displayed? A.
Page 252 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 11 AIR CONDITIONING CONTENTS Page INTRODUCTION ......................... 11-1 GENERAL ..........................11-1 AIR CONDITIONING SYSTEM (TAILCONE COMPONENTS)........
Page 253 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page 11-1 PACK and HI FLOW Switches on Pressurization/Oxygen Control Panel .... 11-3 11-2 ACM Airscoop .......................
Page 254: Introduction
AIR CONDITIONING INTRODUCTION The Learjet 45 air-conditioning system consists of a bleed-air temperature control sys- tem and independent distribution systems to the cockpit and cabin for pressurization and ventilation. Prior to engine start, the system can also be operated during ground opera- tions using the auxiliary power unit (APU), if installed.
Page 255: Air Conditioning System (Tailcone Components)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L bleed-air is cooled in an air-to-air heat ex- allows bleed airflow to the ECU and air dis- changer and cooling turbine within the ECU.
Page 256: Air Cycle Machine (Acm)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PRESSURIZATION PAX OXYGEN DEPLOY OXY/AUTO CABIN PRESSURE CONTROL 3 5 0 CAB RATE I .
Page 257: Pack Overtemp Sensor
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PACK OVERTEMP SENSOR Located downstream from the ACM com- pressor stage, an overtemperature sensor (Item 4 in Figure 11-5) signals the cockpit, to an overtemperature condition.
Page 258: Component Description
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L trol valves will be lost. The temperature con- COMPONENT DESCRIPTION...
Page 259 Figure 11-4. Bleed-Air Distribution System...
Page 260 Figure 11-5. Environmental Control Unit (ECU)
Page 261: Controls And Operation
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 11-1. AIR CONDITIONING SYSTEM CAS MESSAGE DATABASE addition to providing a duct temp reference for...
Page 262 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 11-6. Temperature Controls and Indications in direct response to the position of the tem-...
Page 263 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 11-7. Cockpit/Cabin Air Distribution System As depicted in Figure 11-6 the analog supply...
Page 264: Distribution System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 11-8. Cockpit Overhead WEMACs Figure 11-9. Cabin Air Distribution...
Page 265: Emergency Pressurization System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L EMERGENCY PRESSURIZATION SYSTEM In the event of normal airplane system failure,...
Page 266: Electric Footwarmer Heat System (Cockpit)
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L panel. The circuit breaker is located on the ELECTRIC copilot’s circuit breaker panel.
Page 267 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS The Pack Bilevel PRSOV is commanded Which airplane environmental control...
Page 268 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Cabin temperature can be read: A. On the cabin temperature indicator located on the Environmental Control Panel.
Page 269 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L RIGHT ENGINE HP BLEED LP BLEED 1-10 RIGHT OVER-TEMPERATURE WING...
Page 270 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 12 PRESSURIZATION CONTENTS Page INTRODUCTION ......................... 12-1 GENERAL ..........................12-1 MAJOR COMPONENTS .....................
Page 271: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L High Altitude Airport Operation ................. 12-18 REVIEW QUESTIONS ...................... 12-21...
Page 272 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page 12-1 Pressurization Control Panel .................. 12-2 12-2 Cabin Pressure Control Displays ................
Page 273: Introduction
PRESSURIZATION INTRODUCTION The Learjet 45 pressurization system maintains a cabin altitude much lower than actual airplane altitude. This is accomplished by controlling the outflow of air that has been provided to the occupied areas of the airplane through pneumatic, air conditioning and ventilation distribution systems.
Page 274: Major Components
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L MAJOR COMPONENTS PACK SWITCH The PACK switch (Figure 12-1), located on...
Page 275: Manual Pressurization Switch
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L MANUAL PRESSURIZATION LANDING ALTITUDE SWITCH SELECTOR KNOB The airplane pressurization system may be...
Page 276: Manual Rate Selector Knob
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L must be rotated in the appropriate direction MANUAL RATE SELECTOR until the manual cabin rate reaches zero.
Page 277 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CABIN PRESSURE ADC1/ADC2 SECONDARY TORQUE LDG GEAR SW MOTOR (RIGHT)
Page 278: Pressurization Controller Power Source
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L operates between a maximum of 600 fpm PRESSURIZATION climb, to 375 fpm descent rate.
Page 279: Outflow Valves
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Cabin-to-atmospheric differential pressure OUTFLOW VALVES (Delta P) relief valves are located on each out-...
Page 280: Indications
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L and are displayed as CAS messages (Table INDICATIONS 12-1). PRIMARY AND SECONDARY...
Page 281 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CABIN RATE 1000 CAB TEMP 78° F DELTA P TEMP CONT...
Page 282 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 12-1. CPCS CAS MESSAGE LOGIC Type Logic Summary CAS Message CABIN ALTITUDE Cabin alt.
Page 283 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 12-2. PRESSURIZATION PROTECTION AND WARNING FEATURES (NORMAL) LDG ALT SET AT 8,000 FEET OR LESS...
Page 284 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 12-3. PRESSURIZATION PROTECTION AND WARNING FEATURES (HIGH ALTITUDE AIRPORT)
Page 285 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 12-4. PRESSURIZATION PROTECTION AND WARNING (DELTA P) DELTA P PROTECTION AND WARNING •...
Page 286 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CABIN SEALED AIRFLOW ON THROTTLES THROTTLES ADVANCED RETARDED FIELD LEVEL...
Page 287 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L pressurized cabin pressure. This schedule is tion if the airplane descends 1,000 feet within...
Page 288 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 1,000 FT DESCENT DETECTED AIRCRAFT ALTITUDE ≤ 6,000 FT ABOVE TAKE-OFF FIELD ELEV...
Page 289 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L MAXIMUM AIRCRAFT CRUISING ALTITUDE DESCENT DETECTED 1,000 FT BELOW CRUISING ALTITUDE AIRCRAFT ALTITUDE CHANGES <...
Page 290 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L system operates the same as the automatic The second situation, that takes off from an el-...
Page 291 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 12-10. Controller — Takeoff and Landing Above 8,000 feet...
Page 292 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L AIRCRAFT ALTITUDE DESCENDS 1,000 FT THROTTLES ADVANCED LIFT-OFF 10,000 FT...
Page 293 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS A white L CAB PRESS FAIL message If the cabin altitude is climbing due to a...
Page 294 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L With failure of electrical power to both 11. After experiencing a dual generator fail-...
Page 295 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 13 HYDRAULIC POWER SYSTEMS CONTENTS Page INTRODUCTION ......................... 13-1 GENERAL ..........................
Page 296 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page 13-1 Hydraulic System Schematic ................. 13-2 13-2 Gear/Hydraulic System Control Panel ..............
Page 297: Introduction
HYDRAULIC POWER SYSTEMS INTRODUCTION The Learjet 45 hydraulic power system includes the reservoir, pumps, manifolds, con- trol and shutoff valves, and a brake accumulator. Transducers, pressure switches, and fluid level switches provide inputs on the systems status to the IC-600’s for display on the engine instrument/crew alerting system (EICAS), the multifunctional display (MFD), the radio management units (RMUs) and on the ground service panel.
Page 298 ENGINE PRESS BLEED AIR MODULE OVERFULL (OVER) (GSP INDICATOR) RESERVOIR FULL (FULL) (GSP INDICATOR) PASS LANDING GEAR THROUGH ADD FLUID (ADD) SPOILERS/ CONTROL VALVE FLAP (CAS/GSP) TR'S MAIN SPOILERONS MODULE DRIVE AUX FLUID LOW SYSTEM CLOSED ACCUM (CAS) FIRE PUSH LDG GEAR HYD FLUID CONTROL...
Page 299: Pumps
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ing gear and flaps by selecting HYD XFLOW HYD QTY LO” caution message (with mas- on.
Page 300 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If the aux pump is on for 20 minutes, it auto- GEAR / HYD matically shifts to a reduced capacity mode.
Page 301 ENGINE PRESS OVERFULL (OVER) BLEED AIR MODULE (GSP INDICATOR) RESERVOIR FULL (FULL) (GSP INDICATOR) ADD FLUID (ADD) LANDING GEAR (CAS/GSP) CONTROL VALVE SPOILERS/ FLAP MAIN TR'S SPOILERONS MODULE DRIVE SYSTEM AUX FLUID LOW ACCUM CLOSED (CAS) FIRE PUSH LDG GEAR HYD FLUID CONTROL LEVEL...
Page 302: Filter Manifolds
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L is operating and the pump output pressure to FILTER MANIFOLDS the manifold is less than 1,900 psi.
Page 303 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L HYD/ECS ELECT VOLTS 28.5 28.0 SPLR MAIN 3000 EMER-V 28.0...
Page 304 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 13-1. HYDRAULIC SYSTEM CAS MESSAGE DATABASE Type Logic Summary...
Page 305: Main System
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 13-2. HYDRAULIC DIGITAL PRESSURE INDICATIONS (SUMRY and HYD System Schematic)
Page 306 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L RESERVOIR BRAKE ACCUM 3000 MAIN 3000 ENGINE PUMPS PUMP NORMAL HYDRAULIC SYSTEM SCHEMATIC PAGE...
Page 307: Abnormal Operations
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell 75.0 75.0 1400 FUEL 1450 3000 HYDM-B 1000 SPLFLP...
Page 308: Review Questions
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS The auxiliary hydraulic system, when ac- The main system digital indication on...
Page 309 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If a leak in a main supply line to an en-...
Page 310 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 311 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 312 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 14-24 Nose Steering Components..................
Page 313 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 314 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 315 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 316 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 14-1.
Page 317 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L switches are not on.
Page 318 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 14-2.
Page 319 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L retract side of the actuator (Figure 14-11, page 14-11).
Page 320 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L gear rests against, and are held up by the in- board gear doors.
Page 321 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 322 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 323 FLAP LANDING GEAR CONTROL DRIVE VALVE MODULE LEGEND LDG GEAR CONTROL VALVE MAIN HYD PRESS MAIN RETURN HYD EXTEND RETRACT FREE-FALL AUX HYD PRESS VALVE LANDING AUX RETURN HYD GEAR FREE-FALL ELECTRICAL LEVER DOOR CONTROL XFLOW MECHANICAL VALVE VALVE EXTEND RETRACT CENTER PEDESTAL...
Page 324 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 325 FLAP LANDING GEAR CONTROL DRIVE VALVE MODULE LEGEND LDG GEAR CONTROL VALVE MAIN HYD PRESS MAIN RETURN HYD EXTEND RETRACT FREE-FALL AUX HYD PRESS VALVE LANDING AUX RETURN HYD GEAR FREE-FALL ELECTRICAL LEVER DOOR CONTROL XFLOW MECHANICAL VALVE VALVE EXTEND RETRACT CENTER PEDESTAL...
Page 326 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L side each gear actuator.
Page 327 FLAP LANDING GEAR CONTROL DRIVE VALVE MODULE LEGEND LDG GEAR CONTROL VALVE MAIN HYD PRESS MAIN RETURN HYD EXTEND RETRACT FREE-FALL AUX HYD PRESS VALVE LANDING AUX RETURN HYD GEAR FREE-FALL ELECTRICAL LEVER DOOR CONTROL XFLOW MECHANICAL VALVE VALVE EXTEND RETRACT CENTER PEDESTAL...
Page 328 FLAP LANDING GEAR CONTROL DRIVE VALVE MODULE LEGEND LDG GEAR CONTROL VALVE MAIN HYD PRESS MAIN RETURN HYD EXTEND RETRACT FREE-FALL AUX HYD PRESS VALVE LANDING AUX RETURN HYD GEAR FREE-FALL ELECTRICAL LEVER DOOR CONTROL XFLOW MECHANICAL VALVE VALVE EXTEND RETRACT CENTER PEDESTAL...
Page 329 UP, a 200 psi braking command is applied for GENERAL a few seconds to stop wheel rotation. The Learjet 45 is provided with a brake-by- Should the main hydraulic system fail, the wire system that electronically controls the hy- auxiliary hydraulic system provides pressure...
Page 330 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 331 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L brakeline pressure transducer inputs.
Page 332 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L accumulator pressure is annunciated on page 1, to the right of the caption “HYDM-B.”...
Page 333 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 334 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 335 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 336 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L...
Page 337 FlightSafety FlightSafety international international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The steering authority decreases from a max- down and locked for landing, the “ON”...
Page 338 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS If the landing gear has been extended After a normal gear extension, and the...
Page 339 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Following a gear retraction sequence, and 10. Whenever an “AUX HYD QTY LO” cau-...
Page 340 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 13. When the anti-skid is operating prop- 16. The nosewheel steering system can be...
Page 341 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 15 FLIGHT CONTROLS CONTENTS Page INTRODUCTION ......................... 15-1 GENERAL ..........................15-1 PRIMARY FLIGHT CONTROLS ..................
Page 342 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page 15-1 Flight Control Surfaces ..................15-2 15-2 Elevator Control System ..................
Page 343 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L TABLES Table Title Page 15-1 Flight Control System CAS Message Database........... 15-15...
Page 344 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 15 FLIGHT CONTROLS AILERON FLAPS 4500 RUDDER PITCH 180 RA 29.92 IN...
Page 345 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L axis. The pitch trim system incorporates au- A controls lock is provided to prevent wind...
Page 346 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ELEVATOR DISCONNECT SENSOR SWITCH ELEVATOR DISCONNECT LINEAR ACTUATOR ELEVATORS ELEVATOR AFT...
Page 347 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L dual, redundant mechanical cable system, Elevator Up/Down Spring push/pull tubes, sectors, and bellcranks.
Page 348 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L SYS TEST/RESET PIT TRIM BIAS I 3 I . I 5...
Page 349 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The elevator forward disconnect is a me- AILERONS chanical clutch mechanism located on the...
Page 350 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L AUTOPILOT ROLL SERVO NO AILERON CABLES IN ROTOR BURST ZONE...
Page 351 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L TRIM-AIL circuit breaker if the malfunction ROLL is isolated to the roll trim system.
Page 352 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L RUDDER AFT SECTOR (COMMON TO BOTH RUDDER CONTROL AFT CABLE CIRCUITS)
Page 353 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 6" STRIP ADDED 8" STRIP ADDED TRIM TAB RUDDER Figure 15-11. Rudder Trim Tab...
Page 354 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L der and trim tab has been modified with the ad- landing can be made with only light control dition of an 8”...
Page 355 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L r u d d e r p e d a l f o r c e r e a c h e s 2 5 p o u n d s .
Page 356 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FOR TRAINING PURPOSES ONLY 15-13...
Page 357 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 15-14. Trim Control Panel allow the crew to select primary or secondary the #1 IC-600.
Page 358 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 15-1. FLIGHT CONTROL SYSTEMS CAS MESSAGE DATABASE Type Logic Summary CAS Message Pitch trim bias not at zero, take-off config.
Page 359 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L board horn of each control wheel. The CWTSs toring function by the IC-600 takes place dur-...
Page 360 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L caused by the movement of the spoilers or When the “MACH TRIM FAIL” message is flaps.
Page 361 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell FMS1 KDVT 75.0 75.0 12.5 NM GSPD 12 MIN...
Page 362 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PITCH SPLRS FLAPS AILERON RUDDER FLIGHT CONTROL SYSTEM PAGE – NORMAL DISPLAY...
Page 363 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The secondary trim actuator also monitors for Trim Indications uncommanded trim, trim in wrong direction and incorrect trim rate.
Page 364 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L must be within the takeoff bands for takeoff. bration, etc., is prevented by the irreversibil- When the airplane is on the ground, digital dis- ity of each actuator.
Page 365 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L L FLAP R FLAP FLAP INDICATIONS ON EICAS AND FLT MENUS...
Page 366 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Flap Indications The flap position indicating unit (Figure 15- 17) has two separate and independent channels...
Page 367 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L One malfunction that will cause a FLAPS FAIL message is flap asymmetry. If the flap SYS TEST/RESET control unit detects flaps split by more than 2°...
Page 368 “FLT” col- umn on the right side of the page. On the FLT In the Learjet 45, spoileron operation is full system schematic display, spoiler extension is time. Anytime either control wheel is turned presented as a digital display and as a verti- more than 5°, there is a differential displace-...
Page 369 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ELECT HYD/ECS PITCH AILERON SPLRS FLAPS VOLTS 28.5 28.0 SPLR...
Page 370 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L spoileron operation, the pointers will indicate the differential on the analog scale.
Page 371 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Spoilers shall not be extended at the same time for the roll commanded, the computer then flaps are extended while inflight except as extends the right spoiler as required.
Page 372 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L When the roll disconnect mode is activated spoiler shutoff valve is depowered closed and within the spoileron computer, it outputs a the spoilers should blow down to a “float”...
Page 373 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L LOW SPEED AWARENESS (LSA) INDICATION (RED) CAS CAUTION MESSAGE AURAL VOICE MESSAGE L R STALLWARN FAIL "STALL, STALL, STALL, .
Page 374 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L computer will activate the control col- STALL WARNING SYSTEM umn shaker motors.
Page 375 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L In addition, both PFD’s will indicate 40 knots and the Vspeed digits will be replaced by the Low Speed Awareness cues which appear on the airspeed tape during the test.
Page 376 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS Configuration trim automatically adjusts If the white “PRI TRIM FAULT” message...
Page 377 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 10. If flap position is not the same as the po- 14.
Page 378 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 18. The trim-in-motion clacker will sound: A. Anytime primary or secondary trim runs continuously for more than 1 second.
Page 379 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 16 AVIONICS CONTENTS Page INTRODUCTION ......................... 16-1 GENERAL ..........................16-2 DISPLAY GUIDANCE COMPUTER (IC-600 or IC/SG)............
Page 380 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L RMU Self-Test..................... 16-25 RMU Power Source..................... 16-25 FMS Radio Tuning Operation ..................16-25 Clearance Delivery Head (CDH).................
Page 381 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L MFD Bezel Controller ..................16-40 Display Controller ....................... 16-40 Display Controller Buttons .................. 16-40 Display Controller Knobs ..................
Page 382 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Autopilot/Yaw Damper Controls and Operation ............16-79 Flight Director Controls and Operation............... 16-85 FLIGHT MANAGEMENT SYSTEM (FMS)..............
Page 383 L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page 16-1 Learjet 45 Instrument Panel ................... 16-2 16-2 Primary Display Units.................... 16-4 16-3A Primus 1000 System Block Diagram ..............16-5 16-4 System Reversion Panel ..................
Page 384 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 16-23 Standby Instrument Group................... 16-32 16-24 Attitude Heading Reference System (AHRS) Schematic........16-34 16-25 Typical PFD and MFD Displays................
Page 385 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 16-49 Descent Profiles (FLC/FLCH) ................16-90 16-50 Flight Management System (FMS)..............16-91 16-51 WX-Radar Controller...................
Page 386 INTRODUCTION This chapter describes the Honeywell Primus 1000 avionics system installed in the Learjet 45. Dual independent flight directors are integrated with a fail passive autopi- lot and yaw damper. The flight instruments, engine instruments, systems status, navi- gation, TCAS, RADAR, and electronic checklist (when available) are all displayed on four display units.
Page 387 GENERAL tor). Each of the IC-600s contains circuitry that performs the symbol generation (SG) function The avionics system in the Learjet 45 incor- for the EFIS. porates many advanced features into a “glass cockpit” design. A glossary of acronyms and...
Page 388 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If display information is lost on one side due DISPLAY GUIDANCE...
Page 389 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell Honeywell Honeywell FMS1 CHK EICAS KDVT 75.0 75.0 12.5 NM...
Page 390 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L DU3 MFD DU1 PFD DU2 EICAS DU4 PFD WEATHER RADAR...
Page 391 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The system configuration provides for dual flight directors and single autopilot/yaw REVERSION damper operation.
Page 392 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Normal circuit for engine EICAS indications to (DU 2) (DU 3)
Page 393 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L trol panel located beneath the DU2 (Figure 16-4). The switch selections are labeled “A”...
Page 394 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-1. AVIONIC BUS LOADS L MAIN AV R MAIN AV...
Page 395 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PRIMARY PILOT'S SECONDARY BUS COPILOT'S SECONDARY BUS RADIO MANAGEMENT UNIT...
Page 396 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L TRANSMIT EMER VHF 1 VHF 2 HF 1 HF 2...
Page 397 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L One knob, labeled DME, controls the audio re- The INPH (interphone) volume control ad- ception for both DME1 and DME2.
Page 398 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The RMU has a color LCD (liquid crystal dis- play) and uses the concept of pushing a line...
Page 399 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L is selected to “1 ATC ON” using the right Cross Side Operation RMU, “1 ATC ON”...
Page 400 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L With the main tuning page displayed, the pilot A NB or WB will appear at the top of the COM...
Page 401 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell NARROW NAV 1 COM 1 BANDWIDTH 123.20 109.35...
Page 402 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Pressing the DME key a third time will cause tion in the listing. For example, to insert a...
Page 403 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ADF Tuning and Mode Control Transponder/TCAS ADF operation is the same as COM and NAV...
Page 404 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L tuning knobs. The tuning knobs will have no A selected transponder code may be stored effect if the transponder is in a standby mode.
Page 405 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L contains a combination vertical analog and TCAS Controls digital readout for N1 at the top of the display.
Page 406 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell 75.0 75.0 50.0 50.0 75.0 75.0 OIL °C...
Page 407 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell 109.90 429.5 116.00 172.5 350° 330° 010° 35.9...
Page 408 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ing information is invalid, the digital display course can be changed as desired by rotating the is replaced with amber dashes, the compass tuning knobs.
Page 409 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L RMU Self-Test FMS RADIO TUNING OPERATION The radio system has an extensive built-in-test.
Page 410 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L • Nav section of the integrated navigation CLEARANCE DELIVERY HEAD (CDH) unit #1.
Page 411 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L tifier legend are backlit with electrolumines- when the CDH has been placed in the cent lighting.
Page 412 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PITOT-STATIC SYSTEM The primary pitot-static system consists of two pitot probes (Figure 16-19), located one on each side of the airplane nose.
Page 413 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ADC 1 ADC 2 PILOT'S HEATED COPILOT'S PITOT-STATIC (LOWER) HEATED...
Page 414 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L dicated by failure flags and loss of air data on NORM position, an annunciator of the se- t h e c o r r e s p o n d i n g P F D ( F i g u r e 1 6 - 4 3 ) .
Page 415 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVERSION PANEL ADC NORM IC-600 #1 IC-600 #2 IC/SG IC/SG...
Page 416 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 16-23. Standby Instrument Group STANDBY INSTRUMENTS The standby attitude indicator and it's inter-...
Page 417 GENERAL weather radar antenna, and the fuel quantity computer. AHRS No.2 provides heading in- As illustrated in Figure 16-24, the Learjet 45 formation through DAU2 for the backup nav- is equipped with dual attitude heading refer- igation display on the RMU.
Page 418 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVERSION PANEL IC-600 #1 IC-600 #2 AHRS NORM IC/SG IC/SG...
Page 419 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L be displayed in amber. AHRS reversion is de- AHRS POWER SOURCE scribed later in this chapter.
Page 420 GENERAL DUs are the same and the bezel controllers for the inboard DUs are the same. The Learjet 45 electronic display system (EDS) provides the flightcrew with complete flight- The brightness of the display units is con- path, navigation, engine and systems infor- trolled through dimming knobs located on mation (Figure 16-25).
Page 421 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell FMS1 CHK EICAS MAG2 KDVT 12.5 NM GSPD...
Page 422 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell Honeywell 4500 4500 4000 4000 200 RA 4200 BARO 29.99 IN...
Page 423 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L SUMRY ELEC FUEL Honeywell Figure 16-27. EICAS Bezel Controller and Menu •...
Page 424 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PUSH TEST OUTBD INBD Honeywell Figure 16-29. Display Controller MFD Bezel Controller...
Page 425 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PFD ARC or MAP displays. The radar the HSI or ARC displays to a particular transmitter is turned on/off using the radar navigation source.
Page 426 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L DU 2 DU 3 NORM NORM WARN WARN CAUT CAUT...
Page 427 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Placing the reversion selector to the PFD po- display configuration will occur. Navigation...
Page 428 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L However, to extend battery life, the AFM pro- • Altitude (ALT) + 200 feet cedure also calls for turning DU2 off with the •...
Page 429 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L When a system parameter miscompare be- PRIMARY FLIGHT DISPLAY (PFD) tween Channel A and B of it’s on-side DAU,...
Page 430 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-2. AVIONICS CAS MESSAGES Type Logic Summary CAS Message...
Page 431 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L AUTOPILOT MESSAGE DISPLAY ARMED LATERAL ("AP TEST" - AMBER) FLIGHT DIRECTOR ("AP FAIL"...
Page 432 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The PFD format is divided into two main sec- PFD Displays tions.
Page 433 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L AIR DATA SOURCE REFERENCE OVERSPEED ANNUNCIATION SPEED BUG INDICATOR ARMED VERTICAL...
Page 434 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L the roll angle of the airplane. The display will • V speed bugs and readouts blank from the PFD for invalid attitude roll in- formation.
Page 435 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FLIGHT PATH ANGLE SYMBOL W/FPA ACCELERATION MACH COMMAND (GREEN - NORMAL)
Page 436 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L the "D" to the right edge of the altitude tape.
Page 437 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CAPTURED LATERAL CAPTURED VERTICAL ALTITUDE PRESELECT FLIGHT DIRECTOR FLIGHT DIRECTOR...
Page 438 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L aural tone sounds, and the preselect dig- tape if Mach is at or above .40M (Figure ital display and box change to amber.
Page 439 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CAT2 ADC TEST ANNUNCIATION ANNUNCIATION (GREEN/AMBER) ADC TEST CAT2 1500...
Page 440 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-3. FLAP POSITION OVERSPEED DISPLAY FLAP POSITION FLAP OVERSPEED VALUE 8°...
Page 441 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L will be removed from the display when always in display and will not overwrite the Mach decreases below .38M...
Page 442 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Additional HSI annotations are as follows: dependently selectable on the pilot and copilot sides using the two course set •...
Page 443 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-4. NAV DISPLAY COLOR LOGIC ON PFD Vertical NAV Information...
Page 444 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L tion to the operator that IC/SG reversion – Selected heading shown as "HDGSEL"...
Page 445 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L in nautical miles the airplane is off the de- sired track and the direction "L" for left and "R"...
Page 446 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 75.0 75.0 89.6 89.6 DISPLAY AREA CAS DIVIDER (15 LINES X...
Page 447 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ENGINE INSTRUMENT AND System Display Pages CREW ALERTING SYSTEM In the lower third of the EICAS format is an...
Page 448 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L source will be annunciated to the right of MULTI-FUNCTIONAL DISPLAY (MFD) the digital heading readout if AHRS or IC/SG reversion is selected.
Page 449 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L HEADING TEST ANNUNCIATION FMS1 HEADING BUG KDVT OUT-OF-VIEW ARROW 12.5 NM...
Page 450 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L TRUE AIRSPEED AHRS REVERSION (LABEL - CYAN) CHECK EICAS LRN SOURCE...
Page 451 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L – Wind speed and vector MFD Plan Mode The following (Figures 16-39 and 16-40) is –...
Page 452 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L PLAN AIRCRAFT HEADING TEST SYMBOL FLIGHT PLAN PLAN CIRCLE ANNUNCIATION...
Page 453 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L F M S 1 PBD01 L L 0 1 LL01 1 2 .
Page 454 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L – MAP/WX ranges are: 5, 10, 25, 50, • Waypoints are symbolized as four pointed...
Page 455 • Selection of a submenu Learjet 45 normal operational and abnor- mal/emergency procedure checklist pages may • Toggling selection of a menu item also be displayed within this area. The check- list pages are arranged procedurally and are •...
Page 456 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L main menu, or the menu that created the dis- System Menu play, to deselect or change a display option.
Page 457 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L only the first 10 waypoints of a flight Checklist Menu plan.
Page 458 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L EDS SELF-TEST EICAS Test Mode The EICAS test mode, illustrated in Figure 16-...
Page 459 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L INVALID VERTICAL FLIGHT DIRECTOR DEVIATION FAIL ANNUNCIATION (RED "X") INVALID ATTITUDE...
Page 460: Learjet 45
FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L LEARJET 45EICAS TST 1LEARJET 45ABCDEFG - - - . - - - - .
Page 461 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L INVALID HEADING INVALID DIGITAL DISPLAY TRUE AIRSPEED (AMBER DASHES) (AMBER DASHES)
Page 462 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell CRS 1 CRS 2 ASEL PUSH IAS/M PUSH SYNC...
Page 463 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L SERVO ACTUATORS AP/YD Annunciation At the top center of the PFDs is a field dedi-...
Page 464 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-5. AUTOMATIC FLIGHT CONTROL SYSTEM CAS MESSAGES Type Logic Summary...
Page 465 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L XFR (Transfer) AP/YD Engage The center section of the FGC (Figure 16-46)
Page 466 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L pressed and held. Applying aileron or eleva- Manual AP Control...
Page 467 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L AP Disengage YD Disengage Normally, the autopilot is disengaged by de-...
Page 468 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-6. FLIGHT DIRECTOR MODE ANNUNCIATIONS NAV SOURCE FD MODE SELECTED...
Page 469 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L FLIGHT DIRECTOR CONTROLS FD Cue AND OPERATION The flight director symbology is selectable on the display control panels.
Page 470 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Depressing the FD “HDG” select button en- Heading Set Knob gages the heading mode and displays a green Heading is selected via a rotary knob.
Page 471 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If the FD NAV button is depressed when es- with the lateral command gains optimized for tablished on an intercept heading to a selected operation within 10 miles of the VOR station.
Page 472 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L will also arm the FMS vertical mode if a VNV the vertical speed bug position.
Page 473 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L the high speed profile. The IAS/Mach refer- ence display and bug indicate the commanded speed reference.
Page 474 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 16-49. Descent Profiles (FLC/FLCH) a green ALT. The green bar next to the ALT The GA pitch attitude has no significance in mode switch will also illuminate.
Page 475 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L moved and the flight director resumes the pre- The FMS interfaces with the IC-600s for a vious vertical mode reference.
Page 476 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L gression of smart prompts similar to those Holding Patterns used on departure may be utilized to input a The holding pattern definition page provides STAR, the approach and landing runway.
Page 477 The Primus 660 is the standard radar installed OFF – This position removes electrical power in the Learjet 45. It is an X-band radar system from the system. designed for weather detection and analysis.
Page 478 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L C H K E I C A S M A G 2...
Page 479 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-7. WX RADAR STORM INTENSITY LEVELS DISPLAY RAINFALL RATE...
Page 480 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell FMS1 KDVT 12.5 NM GSPD 12 MIN PLAB1 PBD01...
Page 481 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-8. TARGET DEPTH AND RANGE CHARACTERISTICS TARGET SELECTED TARGET...
Page 482 TCAS resolution ad- visory (RA). TUNE With TCAS II installed, the Learjet 45 will also be equipped with a Mode S ATC Transponder. TCAS II is capable of generating a TA display of traffic from Mode A transponder equipped Figure 16-53.
Page 483 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Honeywell CHK EICAS FMS1 KDVT 12.5 NM GSPD 12 MIN...
Page 484 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L OFF SCALE INTRUDER MAP/PLAN DISPLAY AREA TCAS II MODE TCAS ZOOM...
Page 485 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L MAP/PLAN DISPLAY AREA RA NO BEARING DISPLAY (RED) ABOVE/BELOW DISPLAY MODE...
Page 486 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-9. TCAS DISPLAY SYMBOLS TREND OTHER TRAFFIC RESOLUTION RELATIVE...
Page 487 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L If the depicted traffic is reporting altitude and Altitude Band...
Page 488 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 16-10. TCAS RESOLUTION ADVISORIES AND VOICE ANNOUNCEMENTS CONDITION ADVISORY MESSAGE TRAFFIC ADVISORY "Traffic, Traffic"...
Page 489 A Sundstrand solid state cockpit voice recorder to draw air from the center pedestal area and is installed in the Learjet 45. The three chan- directs it to the area behind the instrument nel CVR provides 30 minutes of recording.
Page 490 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L M850 CHRONOMETER 03:48 SELECT CONTROL DAVTRON Figure 16-58. Multi-Function Chronometer...
Page 491 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS Simultaneous failure of both large display How is the backup navigation display se-...
Page 492 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The overspeed indicator on the airspeed 12. Which of the following statements is true...
Page 493 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 16. Which of the following statements is/are 20. The PFD navigation source is selected...
Page 494 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 25. The FMS reference speed bug is selected 29. Which of the following would discon-...
Page 495 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 17 MISCELLANEOUS SYSTEMS CONTENTS Page OXYGEN SYSTEM......................17-1 General........................... 17-1 Oxygen Storage Cylinder....................
Page 496 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ILLUSTRATIONS Figure Title Page 17-1 Oxygen System Diagram ..................17-2 17-2 Oxygen Supply Cylinder..................
Page 497 CHAPTER 17 MISCELLANEOUS SYSTEMS OXYGEN SYSTEM GENERAL The Learjet 45 oxygen system (Figure 17-1) quire oxygen. The system is not intended for consists of system storage, the crew distribu- extended periods of use during flight at alti- tion system and the passenger distribution tudes requiring oxygen, or as a substitute for system.
Page 498 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L OXYGEN OVERBOARD CYLINDER DISCHARGE SHUTOFF VALVE INDICATOR OXYGEN CYLINGER OXYGEN CYLINDER...
Page 499 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L provides the means of isolating the oxygen output to between 60 and 80 psig. It also in- supply from the distribution system.
Page 500 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L OVERBOARD DISCHARGE INDICATOR The overboard discharge indicator (green blowout disk) (Figure 17-4B) provides the...
Page 501 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L OXYGEN OFF OXYGEN QTY LOW OXY PRESS HI PAX OXY FAIL...
Page 502 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 17-1. OXYGEN SYSTEM CAS MESSAGE DATABASE TYPE CAS MESSAGE...
Page 503 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Puritan-Bennett Sweep-On 2000 Mask STOWAGE BOX INFLATABLE HARNESS OXYGEN MASK...
Page 504 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The Puritan-Bennett mask, incorporates a purge valve, which will automatically bias open when the mask is used in conjunction with smoke goggles.
Page 505 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Figure 17-9. Harness Inflation Tab Figure 17-10. Crew Oxygen Mask...
Page 506 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L The masks must not be set to EMER while fectively increases the oxygen duration. The...
Page 507 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L When armed, the passenger oxygen distribu- tion system is automatically controlled by the cabin pressure controller (CPCS).
Page 508 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table 17-3. AVERAGE TIME OF USEFUL CONSCIOUSNESS 45,000 feet............9 to 15 seconds 40,000 feet............15 to 20 seconds...
Page 509 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REVIEW QUESTIONS During preflight, the pilot can determine If the oxygen cylinder shutoff valve was...
Page 510 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L WALKAROUND The following section is a pictorial walkaround. It shows each item called out in the exterior power-off preflight inspection.
Page 511 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L WALK-AROUND 1a. Left Pitot-Static Probe – Cover removed and clear of obstructions, Stall Warning Vane –...
Page 512 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 3c. L and R BATT Switches – On. 3d. EMER BATT Switch – EMER.
Page 513 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 3j. SUMRY Page B-ACUM Pressure – 3i. EMERGENCY/PARKING BRAKE – Set.
Page 514 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 4a. Windshield – Condition. 4b. Gear and Wheel Well – Hydraulic leakage, condition, and cooling vents clear.
Page 515 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 6a. Windshield – Condition. 6b. Oxygen System Discharge Indicator and Service Door – Check and secure.
Page 516 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 7a. Emergency Exit – Secure. 7b. Upper Fuselage Antenna, and Dorsal Inlets – Condition.
Page 517 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 7f. Lower Fuselage Antennas, Landing Light Fairing and Lens – Condition.
Page 518 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 7i. Right Main Gear – (1) Wheel Well – Hydraulic/fuel leakage and condition.
Page 519 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 8a. Right Wing – (1) Leading Edge, Stall Strip, Triangles, Vortilons and Ice Detect Patch –...
Page 520 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 9a. Right Winglet Navigation Light/Lens and Static Wicks (4) – Condition.
Page 521 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 10b. Right Spoiler and Flap – Condition. 11a. Right Brakes and Brake Wear Indicators – Condition.
Page 522 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 12a. Single-point Fueling Access Door – Secure. 12b. Fuel Quantity Panel Access Door – Secure.
Page 523 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 14a. Tailcone Interior – Open access, Check for fluid leaks, main engine fire bottle pressures, APU fire bottle pressure, security and condition of installed equipment, remote circuit beakers set, condition of door seal, then close access.
Page 524 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 14b. Engine Fire Extinguisher Discharge 14c. Right VOR/LOC Antenna – Condition.
Page 525 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 15d. Tailstand – Removed. 16b. Left VOR/LOC Antenna 16a. APU Inlet (if installed) –...
Page 526 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 17a. Left Engine Turbine Exhaust Area – 17b. Left Thrust Reverser– Condition and Condition, clear of obstructions.
Page 527 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 19a. Left Spoiler and Flap – Condition. 19b. Left Aileron – Check free motion, balance and trim tab linkage and brush seal condition.
Page 528 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 20a. Left Winglet Navigation Light/Lens and Static Wicks (4) – Condition.
Page 529 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 21a. Left Wing – Check (1) Leading Edge, Stall Strip, Triangles, Vortilons and Ice Detect Patch –...
Page 530 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L 22b. Left Main Gear – (1) Wheel Well – 22b. Left Main Gear – (2) Taxi Light and Hydraulic/fuel leakage and condition.
Page 531 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L APPENDIX This appendix contains the following conversion tables: Table Title Page APP-1 Conversion Factors .....................
Page 532 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Table APP-1. CONVERSION FACTORS FOR TRAINING PURPOSES ONLY APP-1...
Page 533 Table APP-2. FAHRENHEIT AND CELSIUS TEMPERATURE CONVERSION...
Page 534 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L ANSWERS TO QUESTIONS CHAPTER 1 CHAPTER 7 CHAPTER 9 CHAPTER 4...
Page 535 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L CHAPTER 12 CHAPTER 15 CHAPTER 16 CHAPTER 13 CHAPTER 14...
Page 536 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L LEAR 45 GLOSSARY A/I PRSOV Anti-Icing Pressure Brake Shutoff Valve...
Page 537 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L E nv i r o n m e n t a l...
Page 538 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L Ignition (EI) Minimum Descent Altitude Insrument Landing System Minimum Equipment List...
Page 539 FlightSafety international L E A R J E T 4 5 P I L O T T R A I N I N G M A N U A L REACT TA/RA Traffic / Resolution Advisory REACT Rain Echo Attenuation...

FlightSafety LEARJET 45 Pilot Training Manual

Chapter 1 Aircraft General

Chapter 2 Electrical Power Systems

Flightsafety Chapter 3 Lighting

Flightsafety Chapter 4 Master Warning System

Flightsafety 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

Chapter 12 Pressurization

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