Piper PA-24-250 Comanche - Section 2 - Limitations

Aircraft Public3t1oos
Piper Commchc 250 (Enrly Model)
Section
- 2
Limitations
SECTION 2 - LIMITATIONS
PA-24-250 * 2800 LBS GROSS WEIGHT
1958 THROUGH 1960 MODEL
APPLICABLE TO AIRPLANES WITH SERIAL
NUMBERS:
24-103 THROUGH 24-2298 EXCEPT 24-2003
Table of Contents
Introduction
.. ...... ...... . .. . .....
... ... . .... .... . , . ..... . . . . . . . . 2-2
.. .
Airspeed Llmtatlons 2-2
Power Plant Instrument Markings 2-3
Tachometer 2-3
Oil Temperature 2-3
Oil Pressure 2-3
Fuel Pressure 2-3
Cylinder Head Temperature 2-3
Instrument Vacuum 2-3
Airspeed Indicator Markings
.... .... ........ . ... ..............., ,, ... ........ . 2-3
.. .
Power Plant Llmtatlons ............................................................. 2-4
. .
Engine Operating L~mts ..................... .. ................................ 2-4
.. .
Propeller L~mtatlons ............ . ...
....................... . . . . . . . 2-4
. .
Weight Llmts 2-4
. .
Center of Gravity Llmts .................................................................... 2-4
Structural Load Factors 2-4
. .
Operational Llmts ......... .... ..
... ..................................... 2-5
.. .
Fuel Lmutat~ons .................................................................... 2-5
Flap Limitations
.................................................................... 2-5
.. .
Other L~mtatlons .................................................................. 2-5
Placards ....................................................................... 2-6
FAA APPROVED (November 10, 1993)
Copyright: 1993
AIRPLANE FLIGHT MANUAL
Page 2-1