Table of Contents
Advertisement
SECTION 8
HANDLING, SERVICE, AND MAINTENANCE
LANDING GEAR
NOSE WHEEL TIRE PRESSURE:
30-42 psi on 22x8.00-8, 6-Ply Rated Tire.
MAIN WHEEL TIRE PRESSURE:
53-57 psi on 8.50-10, 8-Ply Rated Tires.
35-45 psi on 29x11.00-10, 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-O-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 DEICE/ANTI-ICE OPERATIONS
During cold weather operations, flight crews are responsible for making
sure that the airplane is free of ice contamination. Type I deice, and
Type II, Type III, 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 deicing process is
intended to restore the airplane to a clean configuration so that neither
aerodynamic
characteristics
contaminants will occur.
U.S.
8-24
nor
mechanical
(Continued Next Page)
CESSNA
MODEL 208B G1000
interference
from
208BPHBUS-00
Advertisement
Chapters
Table of Contents
