FAA APPROVED 4-30-76
2-55
REISSUED 2-25-81, CHANGE 10
OXYGEN SYSTEM (CONT)
d.
To obtain 100% oxygen at any time, depress 100% lever on
mask pressure regulator.
e.
For emergency operation, select EMERGENCY (rotate PRESS
TO TEST button/knob to
●
). With the mask pressure regula-
tor controls in this position the crew mask will deliver 100%
oxygen at all cabin altitudes and maintain a positive pressure in
the mask cup at all times for respiratory protection from smoke
or fumes.
BRAKE SYSTEMS
The primary brake system utilizes hydraulic system pressure for power
boost and incorporates an anti-skid system to prevent tire skid and/or tire
blow-out during landing or aborted takeoff. The brakes are operated by de-
pressing the upper portion of the rudder pedals.
Large temperature differences between wheels after
landing may indicate improper brake operation.
A parking brake is installed. The parking brake is operated by depressing
and holding the toe brakes (hydraulic system pressurized) and then pulling
the PARKING BRAKE handle to set the brakes. Some aircraft have a PARK
BRAKE light installed on the instrument panel which illuminates whenever
the PARKING BRAKE handle is not fully in.
An emergency air braking system is installed to provide emergency braking
in the event of a hydraulic system failure. Refer to EMERGENCY PROCE-
DURES (Section III) for emergency braking procedures.
NORMAL BRAKING
Anti-skid On Operation:
1. ANTI-SKID Switch — On. Check ANTI-SKID GEN lights
extinguished.
2. Apply brakes as required. Maximum braking pressures can be main-
tained when anti-skid is operative.
The takeoff and landing distances with anti-skid On,
presented in Section V of this manual, are based on full
anti-skid braking from first brake application to com-
plete stop.
NOTE
NOTE
FAA APPROVED 4-30-76
2-55
REISSUED 2-25-81, CHANGE 10
OXYGEN SYSTEM (CONT)
d.
To obtain 100% oxygen at any time, depress 100% lever on
mask pressure regulator.
e.
For emergency operation, select EMERGENCY (rotate PRESS
TO TEST button/knob to
●
). With the mask pressure regula-
tor controls in this position the crew mask will deliver 100%
oxygen at all cabin altitudes and maintain a positive pressure in
the mask cup at all times for respiratory protection from smoke
or fumes.
BRAKE SYSTEMS
The primary brake system utilizes hydraulic system pressure for power
boost and incorporates an anti-skid system to prevent tire skid and/or tire
blow-out during landing or aborted takeoff. The brakes are operated by de-
pressing the upper portion of the rudder pedals.
Large temperature differences between wheels after
landing may indicate improper brake operation.
A parking brake is installed. The parking brake is operated by depressing
and holding the toe brakes (hydraulic system pressurized) and then pulling
the PARKING BRAKE handle to set the brakes. Some aircraft have a PARK
BRAKE light installed on the instrument panel which illuminates whenever
the PARKING BRAKE handle is not fully in.
An emergency air braking system is installed to provide emergency braking
in the event of a hydraulic system failure. Refer to EMERGENCY PROCE-
DURES (Section III) for emergency braking procedures.
NORMAL BRAKING
Anti-skid On Operation:
1. ANTI-SKID Switch — On. Check ANTI-SKID GEN lights
extinguished.
2. Apply brakes as required. Maximum braking pressures can be main-
tained when anti-skid is operative.
The takeoff and landing distances with anti-skid On,
presented in Section V of this manual, are based on full
anti-skid braking from first brake application to com-
plete stop.
NOTE
NOTE
Summary of Contents for 35A
Page 26: ...1 8 Center of Gravity Envelope Figure 1 3 FAA APPROVED 4 30 76 REISSUED 2 25 81 ...
Page 47: ...1 24 111 111 INTENTIONAlLY LEFf BlANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 ...
Page 115: ...2 58 INTENTIONALLY LEFT BLANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 ...
Page 117: ...2 60 INTENTIONALLY LEFT BlANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 ...
Page 158: ...INTENIlONAlLY LEFT BlANK FAA APPROVED 4 30 76 REISSUED 2 25 81 CHANGE 12 3 13 ...