Cessna CITATION MUSTANG Скачать руководство пользователя страница 6 | Manualshive

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Cessna CITATION MUSTANG Скачать руководство пользователя страница 6

NOTE

The water barrier is installed at the
main cabin door threshold. Crew
members should be familiar with its
location and operation; and passen-
gers should be briefed prior to flights
over water.

A monitoring system checks for safe condition
of the door (closed, pins secure, door latched).
There are eight view ports on the inside panel
of the entry door to verify that the eight lock-
ing pins are in the closed position. With the
door closed and handle latched, the pilot
should be able to see the white and green in-
dicators in each port. (Figure 1-7). Three prox-
imity switches verify that the door is closed,
latched, and locked by sensing the position of
targets on the closing mechanism of the door
and signals the condition to the CAS:

• The proximity switch on the doorway

surround structure senses the door after
it is closed.

• After the door is latched, a proximity

switch senses the door pin position.

• As the handle catch is engaged, a prox-

imity switch on the inner handle assem-
bly senses a flag.

If one of the proximity switches does not sense
its target, the CABIN DOOR message appears
on the CAS.

EMERGENCY EXIT

A plug-type emergency exit (escape hatch) is
on the aft right side of the cabin, above the
wing. It opens inboard. The emergency exit
door can be opened from outside or inside
the airplane (Figure 1-8).

The D-shaped inner door handle is recessed be-
hind a magnetic cover. The flush-mounted
outer handle is located at the top of the door.
The outer handle is not directly connected to
the inner handle. The outer handle has a green
indicator to show when the door is latched.

Because no other provisions are provided for
securing the escape hatch when the airplane
is unattended, a safety pin with a REMOVE
BEFORE FLIGHT streamer is placed on the
inside of the hatch. The pilot must ensure this
pin is removed prior to flight. The emergency
exit hatch is not connected to the door warn-
ing circuit.

CABIN

The cabin extends from the forward pressure
bulkhead to the aft pressure bulkhead and

CITATION MUSTANG

OPERATING MANUAL

1-6

510OM-00

Figure 1-7. Door Pin Indicator

Figure 1-6. Hinged Panel

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Содержание CITATION MUSTANG

Страница 1: ...accor dance with Title 14 of the Code of Federal Regulations 14CFR23 Part 23 including day night visual flight rules VFR instru ment flight rules IFR single pilot and flight into known icing condition...

Страница 2: ...pounds Maximum takeoff weight 8 645 pounds Maximum landing weight 8 000 pounds STRUCTURES The Citation Mustang Figure 1 1 is an all metal pressurized low wing monoplane with a swept T tail The interi...

Страница 3: ...CITATION MUSTANG OPERATING MANUAL 510OM 00 1 3 43 17 FT 13 0 M 11 79 FT 3 6 M 14 35 FT 4 37 M 40 56 FT 12 36 M 13 10 FT 3 99 M Figure 1 2 Exterior Three View Drawing...

Страница 4: ...FEET 8 M 0 30 60 90 120 150 0 9 18 27 36 45 DISTANCE FEET DISTANCE METERS Figure 1 4 Engine Hazard Areas CURBTO CURB 27 32 FEET 8 33 M 11 79 FEET 3 59 M 15 53 FEET 4 734 M WING TIP LIGHT TO WING TIP L...

Страница 5: ...elease but ton inside the cabin inside left of door open ing must be pushed Figure 1 5 This lets the door move freely The locking pins will contact and damage the painted surface of the fuselage if an...

Страница 6: ...itch on the inner handle assem bly senses a flag If one of the proximity switches does not sense its target the CABIN DOOR message appears on the CAS EMERGENCY EXIT A plug type emergency exit escape h...

Страница 7: ...e cabin overhead panels contain individual air vent outlets and seat lighting for passen ger comfort FLIGHT COMPARTMENT The airplane is equipped with dual controls in cluding control yokes brakes and...

Страница 8: ...58 MM FS 321 00 IN 8 153 MM FS 202 76 IN 5 150 MM A A FORWARD PRESSURE BULKHEAD FORWARD DIVIDER 0 53 IN THICK 13 MM THICK AFT PRESSURE BULKHEAD 24 00 IN 610 MM 46 00 IN 1 168 MM 54 00 IN 1 372 MM 117...

Страница 9: ...es to the bottom of the fuselage and is constructed of aluminum Each wing is also a fuel tank Electromechanical speedbrakes and flaps and hydraulically actu ated main landing gear are attached to each...

Страница 10: ...y Ensure that the keys are removed from both nose compartment doors prior to flight to pre vent possible ingestion of a key into an engine SYSTEMS ELECTRICAL SYSTEM The Mustang is an all DC aircraft T...

Страница 11: ...ional cable operated surfaces An aileron rudder interconnect provides improved lateral stability Trimming is provided by aileron elevator and rudder tabs The eleva tor trim is both mechanically and el...

Страница 12: ...If any doubt exists or if the conditions are not covered by the checklist the AFM must be consulted FAA approved Citation Mustang Abbreviated Checklist Emergency Abnormal Procedures contains emer genc...

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