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NOTE: An inspection of overheated wheels, tires, brakes, and wheel
speed sensors should be accomplished before next flight. Refer to GIV
FM Appendix C for Brake Kinetic Energy and Carbon Brake Cooling
chart data. (Chart shown on QRH page PC-14.)
END
Anti-Skid Failure (Brake-By-Wire) AFM 3-02-10
FOR AIRPLANES SN 1000 THRU 1213 WITH ASC 190/266
Takeoff:
During takeoff with anti-skid inoperative or selected OFF, 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. Applied Brake Pressure Display.........................SELECT ON DU 4
3. Before gear retraction after lift-off, momentarily apply light brake
pressure (300 to 400 psi).
Approach and landing:
If anti-skid is selected OFF, braking should be performed using the
appropriate ANTI-SKID OFF BRAKING procedure, this section.
If anti-skid is not selected OFF, braking in the open loop pulsed mode
(BANG - BANG) should be performed using the following procedure:
1. ANTI-SKID.................................................................... CHECK ON
2. Applied Brake Pressure Display.........................SELECT ON DU 4
3. Maximum Reverse Thrust ....................................................APPLY
4. Braking ......................USE AS REQUIRED AT HIGHER SPEEDS
5. ANTI-SKID.......................OFF AT APPROXIMATELY 100 KNOTS
NOTE: At speeds below 100 knots, the pulsing of open loop
pulsed anti-skid causes braking action to be jerky.
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EB - 12 (BRAKE BY WIRE) May 30/02
Anti-Skid Failure (Brake-By-Wire), ctd… AFM 3-02-10
6. ANTI-SKID OFF BRAKING Procedure .......................... CONSULT
NOTE: An increase in landing distance will result if landing rollout is
made with anti-skid completely inoperative or under open loop pulsed
anti-skid control. For landing distances with anti-skid inoperative, refer to
Landing Field Length, Anti-Skid Inoperative charts in Performance
section of GIV AFM. Use of reverse thrust reduces landing distances.
END
Anti-Skid Off Braking
(Brake-By-Wire: Without ASC 190/266) AFM 3-02-20
FOR AIRPLANES SN 1000 THRU 1213 WITHOUT ASC 190/266
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. Applied Brake Pressure Display.........................SELECT ON DU 4
3. Before gear retraction after lift-off, momentarily apply light brake
pressure (300 to 400 psi).
Approach and landing:
Use the following procedure when braking with anti-skid selected
off:
1. ANTI-SKID Switch.....................................................................OFF
2. Applied Brake Pressure Display.........................SELECT ON DU 4
3. Maximum Reverse Thrust.................................................... APPLY
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, refer to Landing Field Length, Anti-Skid Inoperative
charts in Performance section of GIV AFM. Use of reverse thrust reduces
landing distances.
END
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 (BRAKE BY WIRE) Page EB - 13
Anti-Skid Off Braking
(Brake-By-Wire: With ASC 190/266) AFM 3-02-30
FOR AIRPLANES SN 1000 THRU 1213 WITH ASC 190/266
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. Applied Brake Pressure Display.........................SELECT ON DU 4
3. Prior to gear retraction after lift-off, momentarily apply light brake
pressure (300-400 psi).
Approach and landing:
Use the following procedure when braking with anti-skid selected
off:
1. ANTI-SKID Switch .................................................................... OFF
2. Applied Brake Pressure Display.........................SELECT ON DU 4
3. Maximum Reverse Thrust ....................................................APPLY
　
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