BOMBARDIER LEARJET 40 Pilot'S Manual Download Page 24 | Manualshive

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Pilot’s Manual

1-24

PM-132A

NOTE:

Engine exhaust danger areas are

shown for idle RPM. Values are
approximately double for takeoff RPM.

40 ft (12.19 m) from tailpipe 100° F (38° C)

ENGINE INTAKE
12 ft (3.66 m)

from intake

ENGINE INTAKE
12 ft (3.66 m)

from intake

WEATHER RADAR

15 ft (4.57 m)

ENGINE EXHAUST

750° F (399° C)
at tailpipe

DANGER AREAS

Figure 1-14

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Summary of Contents for LEARJET 40

Page 1: ...pening Cabin Door From Inside Figure 1 7 1 13 To Close Cabin Door From the Outside 1 14 Closing Cabin Door From the Outside Figure 1 8 1 14 Emergency Exits 1 15 Left Forward Emergency Exit 1 15 Left F...

Page 2: ...Fuel Gravity Fill Access Door 1 22 Single Point Pressure Refueling Access Door 1 22 Single Point Pressure Refueling Control Panel Access Door 1 22 Oil Servicing Doors 1 22 Turning Radius Figure 1 13 1...

Page 3: ...hrust is provided by two pod mounted TFE 731 20 turbofan engines manufactured by Honeywell Independent fuel systems supply fuel to the engines with fuel storage provided in wing and fuselage tanks En...

Page 4: ...1 2 PM 132A AIRPLANE THREE VIEW Figure 1 1 51 ft 11 in 15 83 m 56 ft 4 in 17 18 m 14 ft 1 in 4 29 m 17 ft 2 in 5 23 m 9 ft 4 in 2 84 m 47 ft 10 in 14 58 m NOTE All dimensions shown for aircraft in st...

Page 5: ...Leading Edge Triangles 9 Taxi Light 10 Vortilons 11 Wing Position Navigation Light 12 Fuel System Air Scoop 13 Baggage Compartment Door 14 Delta Fin 15 Rudder 16 Elevator 17 Tail Navigation Light 18...

Page 6: ...ock is installed on the outside of the upper door to secure the aircraft from the outside Rotating the key lock will prevent the outer upper door handle mechanism from moving into the open position Th...

Page 7: ...fuselage structure and two pins are driven from the upper door into overlapping halves in the lower door There are a total of eight pins installed in the upper door Two of the six upper door latching...

Page 8: ...r cabin entry forward emergency exit door is locked and electrical power is applied to the aircraft the red ENTRY DOOR light on the CWP will illuminate steady to prevent operations with the emergency...

Page 9: ...per door by hand until the gas struts automatically raise the door up and hold it fully open 4 While holding the lower door reach inside and rotate the lower door locking handle aft clockwise to the O...

Page 10: ...he cable and knob until the lower door is within reach Immediately grasp the flip down step before it falls inward and lower it by hand into the stowed position against the inside of the lower door 2...

Page 11: ...sition If preparing for flight check that the ENTRY DOOR warning annunciator light on the CWP is extinguished and the ENTRY DOOR and ENTRY DOOR PIN messages on the CAS are extinguished 6 Inspect the c...

Page 12: ...PIN SIGHT WINDOWS Figure 1 6 CABIN DOOR OPERATION CONT Cabin Door Closed and Latched Verification The cabin door is equipped with thirteen sight windows located in the cabin door panels nine in the u...

Page 13: ...r door locking handle aft clockwise to the OPEN position 4 Grasp the cable knob pull out any slack in the cable and while holding tension on the cable release the secondary latch located on the forwar...

Page 14: ...inside and rotate the lower door handle forward counterclockwise to the locked position 4 With the upper door handle in the OPEN position pull the upper door down and hold it tightly against the door...

Page 15: ...outside of the cabin door which operate a common shaft Because the upper door is equipped with a keylock it must be unlocked before flight to ensure optimum operation as an emergency exit However in t...

Page 16: ...Leave the lower cabin door in place and exit through the open upper cabin door LEFT FORWARD EMERGENCY EXIT OPERATION Figure 1 9 To open from the outside 1 Lift the upper cabin door handle out and rot...

Page 17: ...esigned as a plug type hatch which opens inward only and is held in the closed position by pressurization forces and the spring loaded pins The emergency exit hatch is 20 inches 51 centimeters wide by...

Page 18: ...ULL and pull it fully toward you and up retracting the hatch pins 3 While holding the emergency exit handle in the retracted position tilt the top edge of the hatch inward 4 Grasp the hatch in the arm...

Page 19: ...acard that reads EMERGENCY DOOR PUSH TO OPEN DOOR OPENS INWARD 2 Push fully inward on the latch This will retract the pins into the top of the hatch 3 While holding the latch open push the upper edge...

Page 20: ...exit handle and pull it fully inward and down This will retract the latch pins into the top of the hatch 5 While keeping the latch pins retracted push the upper edge of the emergency exit hatch into t...

Page 21: ...ens downward for access to the listed components EXTERNAL DOORS ANNUNCIATIONS Illumination of the EXTERNAL DOORS amber CAS message indicates that either the baggage compartment door or the tailcone ac...

Page 22: ...The SPPR adapter and precheck valve lever are installed behind this door The door is hinged at the bottom and is secured with two spring loaded latches near the top of the door SINGLE POINT PRESSURE...

Page 23: ...Pilot s Manual PM 132A 1 23 TURNING RADIUS Figure 1 13 37 ft 10 in 11 53 m 2 7 f t 1 0 i n 8 4 8 m NOSE WHEEL WING TIP NOTE Turning radius expressed above is based upon 60 nose wheel deflection...

Page 24: ...for idle RPM Values are approximately double for takeoff RPM 40 ft 12 19 m from tailpipe 100 F 38 C ENGINE INTAKE 12 ft 3 66 m from intake ENGINE INTAKE 12 ft 3 66 m from intake WEATHER RADAR 15 ft 4...

Page 25: ...ON ON ON ON ON ON H D X L W ARM ON 49 23 S L C T C N R OL DA TR N M8 0 CHR N OM T R OFF OFF OFF OFF O F OFF OFF C UT W RN DU3 N RM FD U H FD CAS EV C UT W ARN H l T AN MT MER 1 2 MU E M R NPH H l S E...

Page 26: ...ANTI GPWS E A R F R E E F A L L P S H D W N CLARIFIER SQUELCH VOLUME OFF STO CHANNEL FREQ KHZ PGM MODE FREQ CHAN AM USB TX PGM VHF HF PRESS FOR TEST RESET SELCAL PULL ON 15000 0 13 KING HF LAPS IDLE A...

Page 27: ...INBD SPLR PRI VOLTS L HOT RAD ALT SYSTEM L L FLAP AFCS L RUD L LEAK L L L ESS EMER L WING INSTR SYNC VIB TAIL BCN PAX L OIL PANEL SG 1 SQUAT DISC MSTR BRAKES CTRL PITCH START BUS ALT 1 VIB TEST CLOCK...

Page 28: ...AOA PITOT ICE DETECT R PRESS R BLEED R QTY R FUEL FLOW CH B PAX INFO PAX CTRLS WING INSP CHART HOLDER INSTRS R ESS PWR STBY PITOT SAT R WING STAB HT AUTO MAN CTRL PWR DET EXT FWSOV VIDEO AUDIO LOGO N...

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