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3. Refer to DISPATCH WITH ANTISKID SYSTEM INOPERATIVE.
PROCEDURE COMPLETED
IN FLIGHT
3. ANTISKID Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
4. Landing Distance:
CAUTION
• With the antiskid off, antiskid touchdown protection is lost. Caution should
be used to make sure that the brakes are not applied while touching down.
• Apply wheel brakes lightly. Differential power braking is available. However,
since the anti-skid is inoperative, excessive pressure on the brake pedals
may cause wheel brakes to lock, resulting in tire blowout.
• When landing with STALL WARNING-NORMAL, avoid runways with a
downhill gradient. If a downhill gradient cannot be avoided, reduce
maximum landing weight by 180 lbs.
PROCEDURE COMPLETED
STALL WARNING-NORMAL MULTIPLY normal Flap LAND landing distance by 1.39.
STALL WARNING-HIGH MULTIPLY normal Flap TO/APR landing distance by 1.45.
510FM-07 AA 3-113
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
DISPATCH WITH ANTISKID SYSTEM INOPERATIVE
(ANTISKID FAIL MESSAGE DISPLAYED)
CAUTION
Differential power braking is available. However, since the antiskid system is
inoperative, excessive brake pedal pressure may cause the wheel brakes to
lock resulting in tire blowout.
• TAKEOFF
1. Takeoff Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
NOTE
• Dispatch with antiskid inoperative is prohibited if the forecast conditions for the
destination approach and landing will require the use of STALL WARNING-HIGH
(Flap TO/APR) landing data.
• HYD PRESS LO message and associated non-cancelable MASTER CAUTION
must not be displayed.
2. ANTISKID Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. Throttles . . . . . . . . . . . . . . . . . . . . . . TO DETENT (Thrust Mode Indicator – green T/O)
4. Engine Instruments. . . . . . . . . . . . . . . CHECK NORMAL (N1 matches command bug)
5. CAS Messages. . . . . . . . . VERIFY only ANTISKID FAIL caution message is displayed
6. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE
PROCEDURE COMPLETED
• LANDING
1. Landing Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
STALL WARNING-NORMAL: MULTIPLY normal Flap LAND landing distance by 1.39
2. Prior to landing . . . . . . . . . . . . . . . . . . . . Accomplish Normal Procedures APPROACH,
BEFORE LANDING, and landing.
CAUTION
• If unexpected icing conditions are encountered, appropriate “STALL WARN
HI" landing procedures and performance data must be used. Multiply
normal flap TO/APR landing distance by 1.45.
• With the antiskid system off, antiskid touchdown protection is lost. Caution
should be used to make sure brakes are not applied during touchdown.
• When landing with STALL WARNING-NORMAL, avoid runways with a
downhill gradient. If a downhill gradient cannot be avoided, reduce
maximum landing weight by 180 lbs.
PROCEDURE COMPLETED
Flaps
UP MULTIPLY appropriate takeoff distance by 1.39.
Flaps
TO/APR MULTIPLY appropriate takeoff distance by 1.44.
3-114 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
HYD PRESS LO (HYDRAULIC SYSTEM PRESSURE LOW)
Indicates that the hydraulic system pressure is low. Landing gear extension and hydraulic wheel
brakes may not work properly.
1. HYD PUMP Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . . . RESET
NOTE
If this message is displayed while the aircraft is on the ground, the associated
MASTER CAUTION cannot be cancelled and the message will continue to flash until
the fault is corrected.
• IF MESSAGE REMAINS DISPLAYED (MAY BE ACCOMPANIED BY
HYD PUMP ON MESSAGE)
2. HYD PUMP Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . PULL
3. Refer to Abnormal Procedures, LANDING GEAR WILL NOT EXTEND and Emergency
Procedures HYDRAULIC WHEEL BRAKE FAILURE as required for landing.
PROCEDURE COMPLETED
• IF MESSAGE CLEARS
PROCEDURE COMPLETED
510FM-07 AA 3-115
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
HYD PUMP ON (HYDRAULIC PUMP ON)
Indicates that power has been applied to the hydraulic pump for more than 60 seconds.
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Citation Mustang airplane flight manual 1(79)
