AircraR
Publications
Piper
Comanche
250
(Early
blodcl)
Section
-
1
General
ADDITIONAL PLACARDS
(Cont.)
5.)
Inside Landing Gear Motor Release Arm Access Door:
INSTRUCTIONS FOR EMERGENCY EXTENSION OF LANDING GEAR
1
REDUCE POWER
-
AIRSPEED NOT TO EXCEED
100
M.P.H.
2.
PLACE LANDING GEAR SELECTOR SWITCH IN CENTER "OFF" POSITION.
3.
DISENGAGE MOTOR
-
RAISE MOTOR RELEASE
ARM
AND PUSH FORWARD
THROUGH FULL TRAVEL.
4.
EXTEND EMERGENCY GEAR HANDLE TO FULL LENGTH.
5. ROTATE HANDLE FORWARD -TRAVEL TO EXTEND LANDING GEAR.
GREEN LIGHT ON PANEL INDICATES LANDING GEAR DOWN
AND
LOCKED.
DO NOT RE-ENGAGE MOTOR IN FLIGHT
6.)
Above Alternate Static Source Valve:
(When
Item
is
Installed)
ALTERNATE STATIC SOURCE
PULL AFT TO OPEN
IN
CASE OF STATIC PRESSURE TUBE MALFUNCTION
DUE TO ICE OR OTHER OBSTRUCTION, CLOSE WINDOW
,
'I
AND
ACTIVATE ALTERNATE STATIC SOURCE VALVE
7.)
On Brake Fluid Reservoir:
BRAKE FLUID
HYDRAULIC OIL
MIL-H-5606
8.)
Adjacent to Fuel Filler Caps:
MAIN
FUEL AUX. FUEL
91-96 OCTANE
MIN.
9 1-96 OCTANE
MIN.
TANK
CAPACITY 30 GAL.
CAPACITY
15
GAL.
USABLE CAPACITY
28
GAL.
FILLING INSTRUCTIONS
TO OBTAIN
MAXIMUM
CAPACITY, AIRPLANE
MUST
BE
APPROXIMATELY
LEVEL WITH LANDING
GEARS EQUALLY EXTENDED
Copyright:
1993
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