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|  MIL-M-81260A(AS)
grounding and prevention of fire hazards. Instructions concerning access to
remote and emergency service points shall also be included.
be A graph showing the tire pressure versus airplane
gross takeoff weight relationship for both main and auxiliary wheel tires shall
be included. Tire pressure shall be plotted against gross takeoff weights, and
the curve shall extend from the minimum gross weight condition to the maxi-
mum gross weight condition. If a change of tire pressure is required for spe-
cific operation, a statement to this effect shall be made, giving the correct tire
pressure.
3.4.3.4
Emergency Procedures. - A brief description of the proper
action to be taken by maintenance and crash rescue personnel and the safety pre-
cautions to be observed during and following emergencies shall be given. In-
structions and appropriate illustrations shall include, but shall not be limited
to the following:
a. General identification of mission, crew, engines, ar-
maments and ordnance, and ejection systems.
b.
Location and capacity of:
Fuel, oil, hydraulic fluid, compressed air and
10
liquid oxygen
2.
Armament and ordnance
c.
Danger Areas
1.
Engines - intakes and exhausts
2.
Wheels
3. Canoies and ejection seats
4.
Weapons
d.
Cockpit for normal and manual conditions and
forcible entry
e.
Prevention
of
crew
suffocation
f.
Crew release from seats for automatic, manual and
cut or emergency conditions
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