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510FM-07 AA 3-17
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
MAXIMUM GLIDE - EMERGENCY LANDING (Continued)
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 . . . . . . . . . . . . . ZERO DIFFERENTIAL PRESSURE AT TOUCHDOWN
(use CABIN DUMP switch if required)
LANDING
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
ramp using emergency brakes.
13. Directional Control . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN with nosewheel steering
PROCEDURE COMPLETED
3-18 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
ENGINE SURGES OR UNSTABLE ENGINE OPERATION
3. Refer to Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY SHUTDOWN.
• IF ENGINE SURGING STOPS
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE CAUTIOUSLY
3. Engine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
4. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESUME NORMAL OPERATION
PROCEDURE COMPLETED
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
• IF ENGINE CONTINUES TO SURGE AND / OR ITT EXCEEDS LIMIT
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
510FM-07 AA 3-19
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
OIL PRESS LO L-R
(LOW OIL PRESSURE, RED POINTER AND DIGITS)
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
• IF POINTER AND DIGITS CHANGE TO AMBER OR GREEN
2. Throttle (affected engine) . . . . . . . . . . MAINTAIN REDUCED POWER AS REQUIRED
NOTE
Operation at reduced oil pressure may result in increased oil temperature. If an oil
temperature limit is approached, a further reduction in power may be necessary.
3. Land as soon as practical.
PROCEDURE COMPLETED
• IF POINTER AND DIGITS RETURN TO RED OR REMAIN RED FOR
MORE THAN 15 SECONDS
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
3. Accomplish Abnormal Procedures, ENGINE FAILURE / PRECAUTIONARY
SHUTDOWN.
PROCEDURE COMPLETED
3-20 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
ELECTRICAL FIRE OR SMOKE
• UNKNOWN SOURCE
9. DISPLAY BACKUP Button (pilot audio panel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
10. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
11. FUEL TRANSFER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
12. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH
13. Cockpit Curtain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN
14. Exit icing environment.
With the battery switch in EMER position and the generators OFF, power is supplied for at
least 30 minutes to the following equipment:
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Citation Mustang airplane flight manual 1(33)
