Fuel Limitations; Maximum Operating Altitude Limit; Outside Air Temperature Limits; Cabin Pressurization Limit - Piper Cheyenne IIXL PA-31T2 1981 Pilot Operating Handbook

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SECTION
2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA-31T2, CHEYENNE II XL
2.25
FUEL LIMIT A TIO NS
(a) Fuel capacity when filled to tip tank
fillers (U.S. gal.)
(b) Fuel capacity when filled to nacelle
tank fillers (U.S. gal.)
(c) Unusable Fuel (total) (U.S. gal.)
2.27
MAXIMUM OPERATING ALTITUDE LIMIT
Maximum Approved Altitude
NOTE
374
336
8.0
31,000 FT
In flight above 25,000 feet, oxygen masks must
be connected to supply.
2.29
OUTSIDE AIR TEMPERATURE LIMITS
Aircraft shall not be operated when takeoff ambient temperature
exceeds ISA+ 37°C (125°F day).
Oil cooler doors must be opened for takeoff and climb when operating in
temperatures above ISA+ 17.2°C, (90°F day).
2.31
CABIN PRESSURIZATION LIMIT
Maximum Cabin Differential Pressure
Maximum Cabin Altitude
5.5 + .1-.0 PSI
11,140 FT
Do not land when airplane cabin is pressurized above .3 psi.
REPORT:
2272
2-16
ISSUED: APRIL
22, 1981
REVISED: FEBRUARY 7,
1984