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dow on each side is a bubble window to allow the hoist operator/crew to observe the hoist pick up point as well as the area behind the aircraft, without opening the cabin/cargo door.
2.9.3 Door Locks. Key door locks are installed on each of the cabin, cockpit and avionics compartment doors. A common key is used to lock and unlock the doors from the outside to secure the helicopter.
2.10 CREW SEATS.
2.10.1 Pilots’ Seats.

Do not store any items below seats. Seats stroke downward during a crash and any obstruction will increase the probability and severity of injury.
The pilots’ seats provide ballistic protection and can be adjusted for the pilots’ leg length and height. The pilot’s seat is on the right side, and the copilot’s is on the left.
Change 4 2-13

TM 1-1520-253-10

11 10 1011

SA

Each seat has a one-piece ceramic composite bucket at-and occupant to move vertically as single unit. Occupant tached to energy absorption tubes. Each seat is positioned restraint is provided by a shoulder harness, lap belts, and a on a track with the bucket directly above a recess in the crotch belt. cockpit .oor. Crash loads are reduced by allowing the seat
Change 4 2-14.1/(2-14.2 Blank)

1.
RADAR ALTIMETER

2.
BAROMETRIC ALTIMETER

3.
VERTICAL SPEED INDICATOR

4.
VERTICAL SITUATION INDICATOR

5.
HORIZONTAL SITUATION INDICATOR

6.
MASTER WARNING PANEL

7.
AIRSPEED INDICATOR

8.
PILOT’S DISPLAY UNIT

9.
CLOCK

10.
 RADIO CALL PLACARD

11.
 GPS / TACAN SELECT BUTTON

12.
 VSI / HSI MODE SELECTOR

13.
 MULTIFUNCTION DISPLAY

14.
 RADAR WARNING INDICATOR

15.
 NVG DIMMING CONTROL PANEL

16.
 CENTRAL DISPLAY UNIT

17.
 STORMSCOPE

18.
 STABILATOR INDICATOR

19.
 STABILATOR POSITION PLACARD

20.
 VOR / TACAN SELECT BUTTON

21.
 CIS MODE SELECTOR

22.
 PERSONNEL LOCATOR DISPLAY

23.
 LOWER CONSOLE DIMMING CONTROL PANEL

24.
 INDICATOR LIGHTS CONTROL / TEST PANEL

AB0698_2
SA

Figure 2-8. Instrument Panel (Sheet 2 of 2)

To prevent injury to personnel, do not release either the normal or emergency vertical adjust levers unless someone is sitting in the seat. The extension springs are under load at all times. With seat at lowest position, the vertical preload on the seat could be as high as 150 pounds. If no one is in the seat and vertical adjust lever(s) is released, the seat will be snapped to the highest stop. Anyone lean-ing over the seat or with hands on guide tubes above linear bearings, will be seri-ously injured.
a.
Seat Height Adjustment. Vertical seat adjustment is controlled by a lever on the right front of the seat bucket. Springs are installed to counterbalance the weight of the seat. The lever returns to the locked position when released.

b.
Forward and Rear Adjustment. The seat is adjusted for leg length by a locking lever on the left front of the seat bucket. The lever is spring-loaded and returns to the locked position when released.

c.
Emergency Tilt Levers. The emergency tilt release levers are on each side of the seat support frame. The seat may be tilted back into the cabin for removal or treatment of a wounded pilot. Seat tilting can be done from the cabin, only with the seat in the full down and aft position by pushing in on the tilt handles, and pulling the seat top rear-ward.

d.
Emergency Vertical Release Lever. The emergency vertical release permits the seat to drop to the lowest adjust-ment point for tilting. The release lever is on the upper center back of the seat, and is actuated by pulling right on the lever.
　
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