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Cessna 206H - Page 44

Cessna 206H
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SOLOY TURBINE PAC SECTION 2
POHS CESSNA T206H/206H LIMITATIONS
2-22
F.A.A. Approved May 23, 2003
(27) On air oil shock strut: (Cessna placard)
(28) On forward cargo door: (Cessna placard)
CESSNA AIR OIL SHOCK STRUT
CESSNA AIRCRAFT COMPANY, WICHITA, KANSAS
FILLING INSTRUCTIONS
1. REMOVE VALVE CAP AND RELEASE ALL AIR.
2. REMOVE VALVE HOUSING ASSEMBLY.
3. COMPRESS STRUT COMPLETELY (STOPS IN
CONTACT WITH OUTER BARREL HUB).
4. OIL LEVEL
a. FLUID USED SHOULD COMPLY WITH
SPECIFICATION MIL-D-5606.
b. FILL STRUT TO BOTTOM OF VALVE
INSTALLATION HOLE.
c. MAINTAIN OIL LEVEL AT BOTTOM OF
VALVE INSTALLATION HOLE.
5. FULLY EXTEND STRUT
6. REPLACE VALVE HOUSING ASSEMBLY
7. WITH STRUT FULLY EXTENDED AND NOSE
WHEEL CLEAR OF GROUND, INFLATE STRUT
TO 80 PSI.
WARNING
RELEASE AIR AND FLUID PRESSURE BEFORE
REMOVING ANY PART OF THIS ASSEMBLY.
UNCONTROLLED
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