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时间:2010-06-12 21:59来源:蓝天飞行翻译 作者:admin
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14. ENGINE (NP), ROTOR (Nr) INDICATOR
15. ENGINE TORQUE INDICATOR
16. SELECTABLE DIGITAL DISPLAY PANEL
17. FIRE CONTROL PANEL
18. CANOPY JETTISON HANDLE
19. ARM SAFE INDICATOR
20. ENGINE INSTRUMENT DIM/TEST PANEL
21. FUEL TRANSFER INDICATOR (UNMODIFIED
CAUTION/WARNING PANEL)
Figure 2-10. CPG Instrument Panel
Change 2 2-13
TM 1-1520-238-10
1.
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4.
5.
6.
7.
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REMOTE TRANSMITTER INDICATOR/SELECTOR PANEL
COMM SYSTEM CONTROL PANEL
BLANK PANEL
BLANK PANEL
DIRECTIONAL PEDAL ADJUSTMENT CONTROL
BLANK PANEL
BLANK PANEL
ARC-164 UHF AM RADIO CONTROL PANEL
AN/ARC-186 VHF FM-AM RADIO CONTROL PANEL
KY-58 SECURE VOICE CONTROL (PROVISIONS)
AN/APX-100 IFF TRANSPONDER CONTROL PANEL
C-7392A/ARN-89B ADF CONTROL PANEL OR
C-12192/ARN-149 (V) ADF CONTROL PANEL
APU/FIRE TEST PANEL
ANTI-ICE CONTROL PANEL
lNTR/EXT LIGHTING CONTROLS PANEL
FUEL CONTROL PANEL
FREE AIR TEMPERATURE (FAT) GAUGE
POWER LEVER QUADRANT
ENGINE OVERSPEED TEST CONTROL PANEL
COLLECTIVE SWITCH BOX
ELECTRICAL POWER CONTROL BOX
ENVIRONMENTAL CONTROL SYSTEM (ECS) PANEL
STORES JETTISON CONTROL PANEL
ROCKET CONTROL PANEL (ARCS)
MISSILE CONTROL PANEL
CONDITIONED AIR OUTLET
AUTOMATIC STABILIZATION EQUIPMENT (ASE) PANEL
PARKING BRAKE
Figure 2-11. Pilot Control Consoles
2-14
TM 1-1520-238-10
Figure 2-12. CPG Control Consoles
Change 3 2-15
WARNING
WARNING
TM 1-1520-236-10
2.12 CREW COMPARTMENTS.
The crew compartments are arranged in tandem and
are separated by a ballistic shield (fig 2-13). The pilot
sits aft of the CPG. Handholds and steps permit both
crewmembers to enter and exit at the right side of the
helicopter. A canopy covers both crew stations. The
canopy frame and the transparent ballistic shield form
a rollover structure. To provide for maximum survival
and minimum vulnerability, armored seats are
installed in both crew compartments.
2.13 CREWMEMBER SEATS.
Seats stroke downward during a
crash and any obstruction may increase
the possibility of injury. Items
should not be placed beneath seats.
The pilot and CPG seats (fig 2-14) provide ballistic
protection and can be adjusted for height only. They are
one-piece armored seats equipped with back, seat, and
lumbar support cushions. Each seat is equipped with a
shoulder harness lap belt, crotch belt, and inertial reel.
The shoulder harness and belts have adjustment fittings
and come together at a common attachment point.
This provides a single release that can be rotated either
clockwise or counterclockwise to simultaneously release
the shoulder harness and all belts.
2.13.1 Seat Height Adjustment. Vertical seat adjustment
is controlled by a lever on the right front of the
seat bucket. When the lever is pulled out (sideways),
the seat can be moved vertically approximately 4 inches
and locked at any 3/4-inch interval. Springs counterbalance
the weight of the seat. The lever returns to
the locked position when released.
With the collective in other than fulldown
position, the inertia reel control
handle may be inaccessible.
2.13.2 Shoulder Harness Inertia Reel Lock Lever. A
two-position shoulder harness inertia reel lock lever is
installed on the lower left side of each seat (fig 2-14).
When the lever is in the aft position, the shoulder harness
lock will engage only when a forward force of 1-1/2
to 2Gs is exerted on the mechanism. In the forward
position, the shoulder harness lock assembly is firmly
locked. Whenever the inertia reels lock because of deceleration
forces, they remain locked until the lock lever
is placed in forward and then aft position.
2.13.3 Chemical, Biological, Radiological (CBR) Filter/
Blower Mounting Bracket. The left side armored
wing of each seat has a mounting bracket (fig 2-14)
with an electrical interface connector for a CBR filter/
blower.
2-16
TM 1-1520-238-10
Figure 2-13. Armor Protection
2-17
TM 1-1520-238-10
Figure 2-14. Crewmember Seat (Both Crew Stations)
2-18
WARNING
TM 1-1520-236-10
Section Il. EMERGENCY EQUIPMENT
2.14 GENERAL.
Emergency equipment on the helicopter consists of fire
extinguishing equipment and two first aid kits (fig 9-1).
Exposure to high concentration of
 
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