Piper PA-24-250 Comanche User Manual

AircraR Publicalions
Piper Comanche
250 (Early Model)
Section
- 1
General
PERFORMANCE (Cont.)
P
'I
i 6.) Short Field Performance:
Takeoff Distance, Ground Run (18 Degrees of Flap) 1,095 A:
Total Over a SO ft Obstacle ................... .. .... .. ....................................................... 1,575 ft
Landing Distance, Ground Roll (Full Flaps)
Total Over a
SO ft Obstacle ..........................
7.) Service Ceiling:
At 2,800 lbs Gross Weight
........................ 20,000 ft
At 2,200 lbs Gross Weight ........................... ............. .............................................. 27,000 ft
8.) Absolute Ceiling:
At 2,800 lbs Gross Weight ............................. .... ............................................. 22,000 ft
At 2,200 lbs Gross Weight ............................... ........ ................................................ 29,000 ft
**NOTE **
The maximum approved altitude for the Comanche 250 is FL 220.
Unless otherwise specified, all performance figures are based on standard day, standard
atmosphere, gross weight, sea level, no wind conditions.
Copyright: 1993
Page 1-6
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Piper PA-24-250 Comanche Specifications

General

Brand	Piper
Model	PA-24-250 Comanche
Category	Aircrafts
Language	English