SECTION 8 CESSNA
HANDLING, SERVICE, AND
MAINTENANCEMODEL 2088 (675 SHP)
LANDING GEAR
NOSE WHEEL TlRE PRESSURE:
30-42 PSI on
22~8.00-8,6-Ply Rated Tire.
MAIN WHEEL TlRE PRESSURE:
53-57 PSI on 8.50-10, 8-Ply Rated Tires.
35-45 PSI on
29~11.00-10, 10-Ply Rated Tires
NOSE GEAR SHOCK STRUT:
Keep filled with MIL-H-5606 hydraulic fluid per filling instructions
placard. No air pressure is required in strut.
BRAKES:
Service brake fluid reservoir with MIL-H-5606 hydraulic fluid as
placarded on reservoir. Maintain fluid level between MIN and MAX
markings.
OXYGEN
AVIATOR'S BREATHING OXYGEN:
Spec. No. MIL-0-27210.
MAXIMUM PRESSURE (cylinder temperature stabilized after filling):
1850 PSI at 21°C (70°F).
Refer to Oxygen Supplements (Section 9) for filling pressures.
GROUND DEICEIANTI-ICE OPERATIONS
During cold weather operations, flight crews are responsible for
ensuring that the airplane is free of ice contamination. Type
I
deice, and
1
Type II, Type Ill or Type IV anti-ice fluids may be used sequentially to
ensure compliance with FAA regulations, which require that all critical
components (wings, control surfaces and engine inlets as an example)
be free of snow, ice, or frost before takeoff. The deicina
Drocess is
intended to restore the airplane to a clean
conflgurarion sothat neither
aerodvnamtc characreristics nor
mechanical
Interference from
contaminants will occur.
(Continued Next Page)
1
8-26 U.S.
Revision 23
To Next Page
Loading...
