TM 55-1510-215-10
Section VII. ENVIRONMENTAL RESTRICTIONS
5-28. Altitude Limitations.
crewmember in compliance with AR95-1 for planned
flight above 10,000 feet.
The maximum altitude that the aircraft may be
operated at is 26,150 feet. The single engine service
5-31. Flight Under IMC (Instrument Meteorological
ceiling is 12,000 feet.
Conditions).
5-29. Auto Ignition During Night Operation.
This aircraft is approved for flight under instrument
conditions.
Auto ignition shall be used during night operations at
or above 14,000 feet.
5-32. Wind Limitations.
5-30. Oxygen Requirements.
The maximum demonstrated crosswind for landing is
25 knots. Refer to chapter 7 for wind limitations.
One oxygen mask and an adequate supply of
aviators breathing oxygen shall be provided each
Section VIII. OTHER LIMITATIONS
5-33. Passenger Seats.
an approved seat faces aft, the occupant shall not weigh
more than 170 pounds. The headrest and seat back,
The forward passenger seat on each or either side
when occupied, must be in the fully upright position for
of the aircraft may face aft, but only seats approved for
takeoff and landing.
aft facing installation may be installed facing aft. When
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