Operational Llmts; Flap Limitations - Piper PA-24-250 COMANCHE Pilot Operating Handbook

AircraR Publications
Piper Comanche 2 5 0 (Early Model)
Section
-
2
Limitations
OPERATIONAL LIMITS
The airplane is approved for the following operations when equipped in accordance with FAR Part
91 or FAR Part 135.
1.) VFR day and night
2.) IFR day and night
**
WARNING
** Flight into known icing conditions is prohibited
FUEL LIklITATIONS
Fuel Capacity (Two Cells,
30
US Gal ea.)
...................
. .
...................
60 US Gal - 56 Usable
**NOTE
**
The unusable he1 in this aircraft has been determined to be 2 gallons in each inboard tank in
critical flight attitudes. Minimum he1 grade is (blue) 91/96 octane
(100
LL) aviation he].
FLAP LIMITATIONS
Takeoff ................
. . . . .
............................................................................ Zero,
9
or 18 Degrees
............................................................................................ Landing Zero, 9, 18 or 27 Degrees
OTHER LIMITATIONS
1.) Maneuvers:
Normal Category: All intentional
acrobatic
maneuvers, including spins, are prohibited.
2.) Procedures:
A,) Instructions for emergency extension of landing gear:
1.)
Reduce power
-
airspeed not to exceed 100 mph.
2.) Place landing gear selector switch in center "OFF" position.
3.) Disengage motor
-
raise motor release arm and push forward through full travel
4.) ~ x t e n d gear emergency handle h l l length.
5.)
Rotate handle forward
full
travel to extend gear.
Green light on panel indicates gear down and locked.
CAUTION
Do not re-engage motor in flight.
B.) Except as noted above, all operating procedures for this airplane are normal.
\
C.) When three people are carried, both front seats must be occupied.
FAA APPROVED (November 10,1993)
Copyright: 1993
AIRPLANE FLIGHT MANUAL
Page 2-5