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PIPER AIRCRAFT CORPORATION
P A-31 T2, CHEYENNE
II XL
(g) Inter Turbine Temperature
Green Arc (Normal Operating Range)
Radial Red Line (Maximum)
(h) Engine Torque
Green Arc (Normal Operating Range)
Radial Red Line
Red Diamond (max. multi-engine climb
power)
(i) Engine Deice Ammeter
Green Arc (Normal Operating Range)
2.13 WEIGHT LIMITS
(a) Maximum Ramp Weight
(b) Maximum Takeoff Weight
(c} Maximum Landing Weight
(d) Maximum Zero Fuel Weight
(e) Maximum Weights in Baggage
Compartments
Forward
Aft
NOTE
SECTION 2
LIMIT A TIO NS
400° C to 805° C
805°C
0 to 1714 LB-FT
1714 LB-FT
(1900 RPM Max.)
1382 LB-FT
22 to 26 AMPS
9540 LBS ,
9474 LBS
9000 LBS
7600 LBS
I
300 LBS
200 LBS
IT IS THE RESPONSIBILITY OF THE
AIRPLANE OWNER AND PILOT TO
ASSURE THAT THE AIRPLANE IS
PROPERLY
LOADED.
MAXIMUM
ALLOWABLE GROSS
WEIGHT IS
9474 POUNDS. SEE "WEIGHT AND
BALANCE SECTION" FOR LOADING
INSTRUCTIONS.
When carrying 8 occupants, load front baggage first and locate heaviest
occupants forward. Fuel and/or baggage may have to be reduced to keep
total weight within 9540 lbs. Ramp Weight limit. Observe Maximum Zero
Fuel Weight limit of 7600 lbs.
ISSUED: APRIL 22, 1981
REVISED: SEPTEMBER 18, 1981
REPORT: 2272
2-9
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