Citation Mustang airplane flight manual 1(78)

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5. LDG GEAR CONT Circuit Breaker (L circuit breaker panel). . . . . . . . . . . . . . . . . PULL
6. EMERGENCY GEAR RELEASE Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE
7. EMERGENCY GEAR RELEASE T-Handle . . . . . . . . . PULL AND ROTATE TO LOCK
8. EMERGENCY GEAR RELEASE Knob. . . . PULL TO BLOW DOWN (for positive lock)
9. Landing Gear . . . . . . . . . . . . . . . . . . . . CHECK DOWN and LOCKED (3 green lights)
CAUTION
• Prior to using the emergency extension system, the landing gear handle
must be down and/or the gear control circuit breaker pulled to prevent
possible energizing of the gear hydraulic system to the retract position.
• Once the emergency gear extension system has been used, do not
attempt to retract the landing gear.
NOTE
• The emergency gear release handle must be pulled straight aft. Pulling upwards
or sideways on the handle will increase the force required to fully extend the
handle. Pull the handle fully aft before turning counter-clockwise to lock.
• Increased airspeed and some yawing may be required to achieve green lights on
all gear.
 IF LANDING GEAR HANDLE REMAINS UP
10. Land as soon as practical.
CAUTION
• With the gear handle up, antiskid touchdown protection is lost. Caution
should be used to make sure that the brakes are not applied while touching
down.
• Once the airplane is on the ground, power brakes and antiskid will function
normally.
PROCEDURE COMPLETED
 IF LANDING GEAR HANDLE IS DOWN
PROCEDURE COMPLETED
• IF LANDING GEAR HANDLE MOVES AND GEAR EXTENDS
PROCEDURE COMPLETED
510FM-07 AA 3-111
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 LANDING GEAR WILL NOT RETRACT
(RED GEAR UNLOCK LIGHT REMAINS ON)
1. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BELOW 140 KIAS
2. Rudder Input. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMIZE
3. LDG GEAR CONT Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . . . CHECK
4. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE DOWN then UP
• IF LANDING GEAR DOES NOT RETRACT AND NO GREEN DOWN
LOCK LIGHTS ARE ILLUMINATED
5. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
6. Landing Gear . . . . . . . . . . . . . . . . . . . . CHECK DOWN and LOCKED (3 green lights)
7. Land as soon as practical.
PROCEDURE COMPLETED
• IF LANDING GEAR DOES NOT RETRACT AND AT LEAST ONE
GREEN DOWN LOCK LIGHT REMAINS ILLUMINATED
5. AIRSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 150 KIAS OR ABOVE
6. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
7. LDG GEAR CONT Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . PULL
8. EMERGENCY GEAR RELEASE Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE
9. EMERGENCY GEAR RELEASE T-Handle . . . . . . . . . PULL AND ROTATE TO LOCK
10. EMERGENCY GEAR RELEASE Knob . . . PULL TO BLOW DOWN (for positive lock)
11. Landing Gear . . . . . . . . . . . . . . . . . . . . CHECK DOWN and LOCKED (3 green lights)
12. Land as soon as practical.
CAUTION
• Prior to using the emergency extension system, the landing gear handle
must be down and/or the gear control circuit breaker pulled to prevent
possible energizing of the gear hydraulic system to the retract position.
• Once the emergency gear extension system has been used, do not
attempt to retract the landing gear.
NOTE
The emergency gear release handle must be pulled straight aft. Pulling upwards or
sideways on the handle will increase the force required to fully extend the handle. Pull
the handle fully aft before turning counter-clockwise to lock.
PROCEDURE COMPLETED
• IF LANDING GEAR RETRACTS
5. Continue flight normally.
PROCEDURE COMPLETED
3-112 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 ANTISKID FAIL
This message indicates that the anti-skid system is inoperative.
1. ANTISKID Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF then ON
2. SKID CONTROL Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . . . . . CHECK
• IF MESSAGE DOES NOT CLEAR
ON GROUND
　
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