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NOSE SECTION

The nose section is an unpressurized storage
area. Various  hydraulics  components, pneu-
matic bottles, oxygen bottle, fresh-air duct,
and radar antenna are located in this com-
partment (Figure 1-15). The nose storage
compartment holds up to 20-cubic feet (320-
pounds) of baggage. It has two swing-up doors
(left and right). Each door has a mechanical
lock. Each door has a key-operated cam lock,
forward pin latch, and two independent pad-
dle latches. The pin latch shows orange when
not latched. Each latch has a switch and in-
dicates the latch position with the amber
NOSE DOOR L-R CAS message.

A manual light switch is in the compartment
(Figure 1-16). If the manual light switch is left
on, a microswitch at the left and right storage
door assembly extinguishes the storage com-
partment light when the doors are closed.

An over-center gas spring on each door holds
the door in the full open position until the
door is closed manually.

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. The 28-
VDC electrical power is supplied by two
starter-generators and one 24-volt, 28 amp-
hour sealed lead acid battery. An optional bat-
tery is a 24-volt, 28 amp-hour NiCad battery.
An external power receptacle is below the
right engine pylon.

For convenience of pilot and passengers, two
DC power outlets are provided in the cabin,
powered by the DC system through a con-
verter. One DC outlet is in the cabinet behind
the copilot seat and the other is in the aft cen-
ter console.

FUEL SYSTEM

The fuel system has two distinct, identical
halves. Each wing tank stores and supplies the
fuel to its respective engine. Fuel transfer
capability is provided. Fuel is heated through
an oil-to-fuel heat exchanger (PRIST is not
required).

ENGINES

Two pylon-mounted Pratt & Whitney PW615F
turbofan engines are on the rear fuselage, and

CITATION MUSTANG

 

OPERATING MANUAL

1-10

510OM-00

Figure 1-16. Nose Baggage Light

Figure 1-15. Nose Storage Compartment

Summary of Contents for CITATION MUSTANG

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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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