FAA APPROVED 4-30-76 3-45
REISSUED 2-25-81, CHANGE 11
EMERGENCY BRAKING
In the event of failure of the normal brake system, emergency brakes can
be used to stop the airplane. When using emergency braking, anti-skid pro-
tection is not available, and the anti-skid OFF corrections presented in Sec-
tion V will be applicable.
1. Pull EMER BRAKE handle out of recess.
2. Push downward on handle to apply brake pressure.
• The EMER BRAKE handle must be pushed down ap-
proximately 2 inches before braking action begins.
To realize the optimum benefit from the emergency
braking system, the following technique should be
employed:
a. Apply the brakes smoothly with small movements
to produce improved feel and reduce the probabil-
ity of tire skid. Do not pump the brake handle.
b. Avoid taxiing if sufficient brake pressure is not
available.
• An emergency air bottle charged to the lower end of
the green segment (1800 psi) will provide for landing
gear extension using the abnormal procedure and
approximately 10 brake applications.
3. Rudder and/or nose wheel steering — As required for directional
control.
EMERGENCY EVACUATION
1. Stop the aircraft.
2. PARKING BRAKE — Set.
3. Thrust Levers — CUTOFF.
4.• If an engine fire is suspected:
a. Applicable FIRE PULL or ENG FIRE PULL T-Handle —
Pull.
b. Either ARMED Light — Depress.
c. Other FIRE PULL or ENG FIRE PULL T-Handle — Pull.
• If engine fire is not suspected:
a. Both FIRE PULL or ENG FIRE PULL T-Handles — Pull.
5. Both Battery Switches — OFF.
6. Evacuate the aircraft:
a. Cabin Entry Door — Open and exit aircraft. The upper door is
openable with the landing gear retracted.
b. Aft Cabin Emergency Exit — Open and exit using the wing
step area.
NOTE
FAA APPROVED 4-30-76 3-45
REISSUED 2-25-81, CHANGE 11
EMERGENCY BRAKING
In the event of failure of the normal brake system, emergency brakes can
be used to stop the airplane. When using emergency braking, anti-skid pro-
tection is not available, and the anti-skid OFF corrections presented in Sec-
tion V will be applicable.
1. Pull EMER BRAKE handle out of recess.
2. Push downward on handle to apply brake pressure.
• The EMER BRAKE handle must be pushed down ap-
proximately 2 inches before braking action begins.
To realize the optimum benefit from the emergency
braking system, the following technique should be
employed:
a. Apply the brakes smoothly with small movements
to produce improved feel and reduce the probabil-
ity of tire skid. Do not pump the brake handle.
b. Avoid taxiing if sufficient brake pressure is not
available.
• An emergency air bottle charged to the lower end of
the green segment (1800 psi) will provide for landing
gear extension using the abnormal procedure and
approximately 10 brake applications.
3. Rudder and/or nose wheel steering — As required for directional
control.
EMERGENCY EVACUATION
1. Stop the aircraft.
2. PARKING BRAKE — Set.
3. Thrust Levers — CUTOFF.
4.• If an engine fire is suspected:
a. Applicable FIRE PULL or ENG FIRE PULL T-Handle —
Pull.
b. Either ARMED Light — Depress.
c. Other FIRE PULL or ENG FIRE PULL T-Handle — Pull.
• If engine fire is not suspected:
a. Both FIRE PULL or ENG FIRE PULL T-Handles — Pull.
5. Both Battery Switches — OFF.
6. Evacuate the aircraft:
a. Cabin Entry Door — Open and exit aircraft. The upper door is
openable with the landing gear retracted.
b. Aft Cabin Emergency Exit — Open and exit using the wing
step area.
NOTE
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