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Pilot’s Manual

PM-132A

1-5

CABIN ENTRY DOOR

The cabin door is located in the forward left side of the fuselage. The
cabin door is a clamshell style design which consists of an upper door
section which opens upward to form a canopy while open, and a lower
door section with integral steps which opens downward. A retractable
flip step is installed on the lower cabin door which is rotated down to
form the lowest entry step. The cabin door is 30 inches (76 centimeters)
wide and provides normal entrance to and egress from the aircraft. The
upper cabin door also doubles as the left forward emergency exit.

The upper cabin door features handles on both the inside and outside
of the door. The outside upper door handle is recessed and protrudes
slightly from the door skin. Before operating the outside handle the
security keylock must be unlocked and the handle must be first lifted
out from the door, then rotated clockwise into the open position. The
inside upper door handle is readily accessible and can be rotated to lock
or unlock the upper door mechanism. The upper door is equipped with
a pair of gas struts which aid when raising the door. The gas struts will
maintain the door in the open position after it is raised. A key lock 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. The security lock can
be easily overridden from inside the aircraft.

A vent door and locking mechanism is incorporated into the upper
cabin door. If the upper cabin door is not closed with the locking pins
engaged, the vent door will remain open to prevent the airplane from
pressurizing. The vent door is connected to the upper door handle
mechanism through a series of bell cranks and link rods which will
keep the vent door closed while the upper door handle is in the closed
position. As the upper door handle is rotated out of the closed position,
the vent door will open and remain open while the handle is in
transition. When the handle is in the fully open position, the vent door
will close. The vent door will remain closed while the upper cabin door
is open to prevent ice and moisture contamination. 

The lower cabin door is equipped with a single locking handle which is
installed in the upper edge of the door as it is viewed in the closed po-
sition. The handle can be lifted out of the recess and rotated forward to
latch the door or aft to unlatch the lower cabin door. Gas struts are in-
stalled on the forward lower door structure to aid in closing and
prevent damage if the door is inadvertently allowed to drop open.

Содержание LEARJET 40

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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