曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
(ENG FIRE LIGHTS should both illuminate)
IF BOTH ENGINE FIRE LIGHTS ILLUMINATE
3. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
NOTE
Consider reduced power on affected engine as required to keep the fire light out.
4. Land as soon as practical.
PROCEDURE COMPLETED
(Continued Next Page)
3-10 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
ENGINE FIRE L OR R
(ENGINE FIRE WARNING LIGHT ILLUMINATED) (Continued)
IF ENGINE FIRE LIGHT ON AFFECTED SIDE DOES NOT
ILLUMINATE (POSSIBLE DAMAGE TO FIRE SENSOR)
3. Illuminated ENGINE FIRE Switch . . . . . . . . . . . . . . . . . . . . LIFT COVER and PUSH
4. Illuminated BOTTLE ARMED Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
5. Throttle (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
6. FUEL BOOST Switch (affected side) . . . . . . . . . . . . . . . . . . . . . . . OFF then NORM
O IF SECONDARY FIRE INDICATIONS ARE PRESENT
7. Land as soon as possible.
8. Accomplish Abnormal Procedures SINGLE-ENGINE APPROACH AND
LANDING.
O IF SECONDARY FIRE INDICATIONS ARE NOT PRESENT
7. Land as soon as practice.
8. Refer to Abnormal Procedures ENGINE FAILURE / PRECAUTIONARY
SHUTDOWN.
PROCEDURE COMPLETED
510FM-07 AA 3-11
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
EMERGENCY RESTART - TWO ENGINES
(Refer to Figure 3-1 for Airstart Envelope)
• EMERGENCY RESTART - STARTER ASSIST
(ALTITUDE 20,000 FEET OR LOWER)
NOTE
Throttles must be placed to CUTOFF to reset FADEC start logic.
5. ENGINE ANTI-ICE Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
6. AIR COND Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
7. Opposite Engine (after first start complete or aborted). . . . . . . . . . . . . . . . . . . . START
(repeat steps 4-5)
WARNING
• Emergency battery 30-minute duration is based on a maximum of two
starter-assist start attempts. Additional starter-assist start attempts
will cause battery power to be depleted prematurely.
• The battery switch may remain in the BATT position for a maximum of
2 minutes while attempting restarts. Exceeding 2 minutes will reduce
the battery capacity available to power the emergency bus items.
IF NEITHER ENGINE STARTS
8. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RAPIDLY SELECT EMER
9. Refer to Emergency Procedures, MAXIMUM GLIDE - EMERGENCY LANDING.
PROCEDURE COMPLETED
IF ONLY ONE ENGINE STARTS
8. ENGINE ANTI-ICE (operating engine) . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
9. Refer to Abnormal Procedures, ENGINE FAILURE / PRECAUTIONARY
SHUTDOWN to secure non-running engine or Abnormal Procedures, INFLIGHT
RESTART - ONE ENGINE to attempt another start.
PROCEDURE COMPLETED
(Continued Next Page)
1. BATT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT
2. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
3. Either Engine START button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS momentarily
4. Throttle (selected engine). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
3-12 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
EMERGENCY RESTART - TWO ENGINES (Continued)
IF BOTH ENGINES START
8. ENGINE ANTI-ICE Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
9. AIR COND Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
PROCEDURE COMPLETED
• EMERGENCY RESTART - WINDMILL (AIRSPEED 225 KIAS
MINIMUM, ALTITUDE 15,000 FEET OR LOWER, 4% N2 MINIMUM,
RAT -10°C OR WARMER)
1. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT
2. L and R FUEL BOOST Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
3. L and R GEN Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
4. ENGINE ANTI-ICE Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Citation Mustang airplane flight manual 1(29)
