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3-6 FAA APPROVED
31 May 2000
3-02-20: Anti-Skid Off Braking (Brake-By-Wire):
FOR AIRPLANES SN 1000 THRU 1213 WITHOUT ASC 190/266
Selecting ANTI-SKID OFF, using the ANTI-SKID ON/OFF Switch located on the center
pedestal, will be indicated by illumination of the ANTI-SKID FAIL amber message on EICAS.
With ANTI-SKID Selected OFF, normal ANTI-SKID and open loop pulsed control is not
available. Applied brake pressure is proportional to brake pedal deflection.
TAKEOFF
During takeoff with ANTI-SKID inoperative or selected OFF, wheel spindown function will be
disabled.
Perform the following Steps for takeoff with ANTI-SKID inoperative or OFF:
1. ANTI-SKID Switch ............................................................................................................OFF
2. Select Applied Brake Pressure Display on DU 4.
3. Before gear retraction after lift-off, momentarily apply light brake pressure (300 to 400 psi).
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-7
13 September 2000
APPROACH AND LANDING
Use the following procedure when braking with ANTI-SKID Selected OFF:
1. ANTI-SKID Switch ............................................................................................................OFF
2. Select Applied Brake Pressure Display on DU 4.
3. Apply Maximum Reverse Thrust.
4. Allow speed to decrease to approximately 100 knots before applying light braking.
Gradually increase to moderate braking as speed decreases.
NOTE: An increase in landing distance will result if landing rollout is made with Anti-Skid
completely inoperative. For landing distances with Anti-Skid inoperative see Landing
Field Length Anti-Skid Inoperative Chart, Performance Section. Use of Reverse Thrust
reduces AFM landing distances.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3-8 FAA APPROVED
31 May 2000
3-02-30: Anti-Skid Off Braking (Brake-By-Wire):
FOR AIRPLANES SN 1000 THRU 1213 WITH ASC 190/266
Selecting the anti-skid OFF, using the anti-skid ON/OFF switch located on the center pedestal,
will be indicated by the illumination of the ANTI-SKID FAIL amber message on the EICAS.
With anti-skid selected OFF, normal anti-skid and open loop pulsed control is not available.
Applied brake pressure is proportional to brake pedal deflection.
TAKEOFF
During takeoff with the Anti-skid inoperative or selected OFF, the wheel spindown function will
be disabled. Perform the following steps for takeoff with the Anti-skid inoperative or OFF:
1. ANTI-SKID Switch ............................................................................................................OFF
2. Select Applied Brake Pressure Display on DU 4.
3. Prior to gear retraction after lift-off, momentarily apply light brake pressure (300-400 psi).
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3-9
13 September 2000
APPROACH AND LANDING
The following procedure should be used when braking with anti-skid selected OFF:
1. ANTI-SKID Switch ............................................................................................................OFF
2. Select Applied Brake Pressure Display on DU 4.
3. Apply Maximum Reverse Thrust.
4. The pilot should smoothly apply brakes to approximately 300 psi as advised by the copilot.
In an anti-skid inoperative situation, the pilot should devote his attention to airplane control
and the copilot should monitor applied brake pressure and advise the pilot of corrections
needed to maintain 300 psi.
CAUTION: IT IS NORMAL FOR DECELERATION TO INCREASE AS THE STOP
PROGRESSES. IT IS EXTREMELY IMPORTANT TO MAINTAIN 300 PSI TO
AVOID LOCKED WHEELS AND BLOWN TIRES. THERE WILL BE A
SIGNIFICANT INCREASE IN LANDING DISTANCE WITH ANTI-SKID
INOPERATIVE.
NOTE: Brake pedal position in relation to brake pressure can be observed and practiced
airborne with the anti-skid system selected OFF, and the landing gear up or down.
An increase in landing distance will result if a landing rollout is made with anti-skid
inoperative. For landing distances with Anti-skid inoperative see Landing Field Length
Anti-Skid Inoperative Chart, Performance Section. Use of Reverse Thrust reduces
AFM landing distances.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3-10 FAA APPROVED
31 May 2000
3-02-40: Anti-Skid Failure (HMAB):
FOR AIRPLANES SN 1183, 1214 AND SUBS
A failure occurring in the brake system which renders the anti-skid inoperative will be indicated
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(52)
