A~rcraR Publications
Piper
Comnnchc
250
(Early
Modcl)
OTHER LIkIITATIONS
(Cont.)
3.)
Performance:
Section
-
2
Limitations
Loss of altitude from a power-on stall, flaps retracted, is 160 feet.
All
other normal stall
configurations result in less loss of altitude.
The Stall Warning System is inoperative with the Master Switch off
PLACARDS
1.)
In Full View of the Pilot:
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY
AIRPLANE IN COMPLIANCE
WITH
THE
AIRPLANE FLIGHT
MANUAL.
ACROBATIC MANEUVERS (INCLUDING SPINS) PROHIBITED.
2.)
On the Floor at Base of Landing Gear Manual Operating Lever:
EMERGENCY GEAR HANDLE
3.)
On Landing Gear Motor Release Arm Access Door:
EMERGENCY GEAR EXTENSION
REMOVE COVER.
EXTENSION INSTRUCTIONS
ON REVERSE SIDE.
4.)
On Baggage Compartment Door:
MAXIMUM
BAGGAGE 200 POUNDS
5.)
On Inside Top of Cabin Door:
ENGAGE LATCH BEFORE KIGHT
6.)
On Airspeed Indicator:
(If Applicable per
AD
72-22-05)
DO NOT EXCEED 203
MPH
CAS
7.)
On Tachometer:
(Applicable to 0-540-A1A Engine Only)
AVOID CONTINUOUS OPERATION
BETWEEN 2225
AND
2275
RPM
FAA
APPROVED
(November
10,
1993)
Copyright:
1993
AIRPLANE
FLIGHT
MANUAL
Page
2-6
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