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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-25
31 May 2000
3-04-40: APU Alternator Failure:
1. An APU alternator failure (as indicated by lack of AUX PWR on Electrical Master Panel
and/or AUX AC POWER FAIL amber caution message on CAS) will have no effect as long
as both engine driven Alternator/Converters continue to function. Back up power, for
Alternator/Converter failures, has been lost.
2. Cycle Auxiliary Power Switch OFF, then ON. If condition remains same, position Auxiliary
Power Switch OFF.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3-26 FAA APPROVED
31 May 2000
3-05-00: BRAKES SYSTEM
3-05-30: Wheel Brake Failure:
If the Combined System engine-driven pump fails, the Utility System will automatically provide
power to operate brakes. If the Combined and Utility systems fail, the Auxiliary Hydraulic Pump
may be utilized to operate the brakes. Anti-skid protection is available when using Combined,
Utility, or Auxiliary System pressure.
CAUTION: TAKEOFF IS NOT PERMITTED WITH EITHER SINGLE OR DUAL
CHANNEL FAILURE OF PILOT’S OR COPILOT’S BRAKE SYSTEM.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-27
31 May 2000
3-05-40: Brake Confidence Check - Inflight (Brake-By-Wire):
1. ANTI-SKID ........................................................................................................................ ON
2. Depress and hold the BRAKE NUTCRCKR ORIDE switch for the duration of this check.
Wait minimum of ten (10) seconds then individually depress the left and right brake pedals
(pilot or copilot).
A. Confirm applied brake pressure proportionally tracks brake pedal deflection.
B. Confirm brake pedal deflection does not cause applied pressure on opposite brake.
3. Release BRAKE NUTCRCKR ORIDE Switch.
4. If check is satisfactory, proceed with normal landing.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3-28 FAA APPROVED
31 May 2000
3-05-50: Uncommanded Applied Brake Pressure - Inflight (Brake-By-Wire):
1. Perform Brake System Test (BITE) several times in an attempt to clear the uncommanded
pressure.
If pressure returns to normal, perform BRAKE CONFIDENCE CHECK this Section.
If pressure remains proceed as follows:
2. PULL BCS 1 circuit breaker (C/P OH). The ANTI-SKID FAIL message will illuminate on
CAS. Apply brake pressure for thirty (30) seconds. Open-loop pulsed (BANG-BANG)
braking will occur. Release brake pedals.
A. If brake pressure returns to normal, reset BCS 1 circuit breaker. If pressure remains
normal, perform the BRAKE CONFIDENCE CHECK this Section.
B. If applied pressure remains, PULL BCS 2 circuit breaker (C/P OH).
All four (4) brake system messages will illuminate on CAS.
C. If pressure returns to normal, leave BCS 2 circuit breaker out and perform BRAKE
CONFIDENCE CHECK. If BRAKE CONFIDENCE CHECK is satisfactory, land with
BCS 2 circuit breaker out.
D. If the uncommanded pressure remains, reset BCS 2 circuit breaker.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-29
31 May 2000
3. Select ANTI-SKID OFF. Cycle the affected brake pedal(s) in an attempt to clear the
uncommanded pressure.
A. If pressure returns to normal, land using ANTI-SKID OFF BRAKING procedure this
Section.
4. If the uncommanded applied brake pressure remains, assume that this pressure will be
present during landing.
Select ANTI-SKID............................................................................................................... ON
Refer to LANDING WITH APPLIED BRAKE PRESSURE INDICATED this Section.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3-30 FAA APPROVED
31 May 2000
3-05-60: Landing With Applied Brake Pressure Indicated (Brake-By-Wire):
1. ANTI-SKID ......................................................................................................................... ON
2. Brake Accumulator Pressure ...................................................................................... 3000 PSI
3. AUX Pump .................................................................................. ARMED (NOT RUNNING)
On Touchdown:
4. Apply Reverse Thrust as necessary.
5. Use rudder and/or Nose Wheel Steering to maintain directional control.
6. DO NOT attempt to use brakes.
7. When ground speed is less than 80 knots, use the metering parking brake to stop airplane.
　
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