Piper PA-24-250 Comanche - Additional Placards

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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