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tones including Overspeed, Landing Gear, and Stall Warning will be inoperative.
• The AP button on the autopilot control panel may be pressed two times to cancel
the autopilot disconnect tone if required.
• IF ONLY ONE GENERATOR COMES ON LINE
4. Electrical Load . . . . . . . . . . REDUCE AS REQUIRED (300A FL300 / 280A > FL300)
5. Land as soon as practical.
PROCEDURE COMPLETED
• IF BOTH GENERATORS COME ON LINE
PROCEDURE COMPLETED
3-36.3 AO 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
DUAL GENERATOR FAILURE
(RED GEN OFF L-R CAS MESSAGE) (Continued)
BEFORE LANDING
1. Landing Data. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
a. Airspeed
VREF (KIAS)
b. Landing Distance:
CAUTION
• Avoid landing with a tailwind.
• Landing above 8000 feet MSL with flaps UP may exceed brake energy
limits.
2. Crew Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
3. Seats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST and SECURE
4. Avionics and Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
5. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PAX SAFETY
6. Passenger Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
7. Passenger Seats. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FULL UPRIGHT
(Continued Next Page)
FLAPS STALL
WARNING
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
UP or
UNKNOWN
NORMAL
HIGH
98
110
102
114
106
118
109
122
113
126
117
131
TO/APR NORMAL
HIGH
87
98
91
102
95
105
98
109
101
112
105
117
LAND NORMAL 82 85 88 91 94 98
*Use in an emergency which requires landing at weights in excess of 8000 lbs
FLAPS UP or UNKNOWN MULTIPLY appropriate STALL WARNING-NORMAL or HIGH landing
distance by 2.31.
FLAPS TO/APR MULTIPLY appropriate STALL WARNING-NORMAL or HIGH landing
distance by 2.10.
FLAPS LAND MULTIPLY appropriate landing distance by 1.83.
510FM-07 AA 3-37
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
DUAL GENERATOR FAILURE
(RED GEN OFF L-R CAS MESSAGE) (Continued)
8. LANDING GEAR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY EXTEND
a. LDG GEAR CONT Circuit Breaker (left circuit breaker panel) . . . . . . . . . . . . PULL
b. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
c. EMERGENCY GEAR RELEASE Cover . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE
d. EMERGENCY GEAR RELEASE T-Handle . . . . . . PULL AND ROTATE TO LOCK
e. EMERGENCY GEAR RELEASE Knob PULL TO BLOW DOWN (for positive lock)
f. 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 full aft before turning counter-clockwise to lock.
9. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VREF
10. Pressurization . . . . . . . . . . . . . . . . . . . . . CHECK ZERO DIFFERENTIAL at touchdown
(use CABIN DUMP switch if required)
11. Brake Pedals . . . . . . . . . . . . . . . . . . . . . . . . REMOVE FEET FROM BRAKE PEDALS
12. EMERGENCY BRAKE Handle . . . . . . . . . . . . . . . . . . SMOOTH PULL AS REQUIRED
CAUTION
• Antiskid system does not function during emergency braking. Excessive
pressure on emergency brake handle can cause both wheel brakes to lock,
resulting in blowout of both tires.
• Repeated application and release of the emergency brake handle may
cause premature loss of pneumatic pressure.
• After landing, clear the runway and stop. Do not attempt to taxi onto the
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Citation Mustang airplane flight manual 1(45)
