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 IF ONLY ONE ENGINE STARTS
8. ENGINE ANTI-ICE (operating engine) - - - - - - - - - - AS REQUIRED
9. Refer to Abnormal Procedures, ENGINE FAILURE/
PRECAUTIONARY SHUTDOWN; Tab B1 to secure non-running
engine or Abnormal Procedures, INFLIGHT RESTART - ONE
ENGINE; Tab B2 to attempt another start.
PROCEDURE COMPLETED
 IF BOTH ENGINES START
8. ENGINE ANTI-ICE Switches - - - - - - - - - - - - - - - - - AS REQUIRED
9. AIR COND Switch- - - - - - - - - - - - - - - - - - - - - - - - - - AS DESIRED
PROCEDURE COMPLETED
(Continued Next Page)
4  EMERGENCY RESTART - TWO ENGINES
1. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -BATT
2. Throttles - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF
3. Either Engine START button - - - - - - - - - - - - - - - - - PRESS momentarily
4. Throttle (selected engine) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE A
510CLEAP-07 AA 13
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
 EMERGENCY RESTART - TWO ENGINES (Continued)
• 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
5. AIR COND Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
6. Firewall Shutoff - - - - - - - - - - - - - - - - - - - - - - - - CHECK BOTH OPEN
7. Throttles - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF, then IDLE
 IF NEITHER ENGINE STARTS
8. Throttles- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF
9. BATT Switch- - - - - - - - - - - - - - - - - - - - - RAPIDLY SELECT EMER
10. Refer to Emergency Procedures, MAXIMUM GLIDE-EMERGENCY
LANDING; Tab A6.
 IF ONE OR BOTH ENGINES START
8. GEN Switch (operating engine) - - - - - - - - - - - - - - - - - - - - - - GEN
9. ENGINE ANTI-ICE Switches - - - - - - - - - - - - - - - - -AS REQUIRED
10. AIR COND Switch- - - - - - - - - - - - - - - - - - - - - - - - - - AS DESIRED
PROCEDURE COMPLETED
C A U T I O NCAUTION
• Minimum N2 for windmill start is 4%.
• Minimum RAT for windmill start is -10°C.
• The windmill starting envelope is provided as an alternate
procedure for use in the event of a failure of the normal electric
starting system. The windmill start envelope is not a guaranteed
envelope and is provided for informational purposes only.
• Use of the windmill start procedure for training or routine airstarts is
not recommended.
5  AIRSTART ENVELOPE
14 AA 510CLEAP-07
A
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
DESCENT
1. Airspeed - PER CHART BELOW:
MAXIMUM GLIDE AIRSPEED
2. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - UP
3. Speed Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - RETRACTED
4. LANDING GEAR Handle (if desired)- - - - - - - - - - - - - - - - - - - - - - - - UP
5. Transponder - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -EMERGENCY
6. ATC - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ADVISE
7. Throttles - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -CUTOFF
8. FUEL TRANSFER - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
9. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - RAPIDLY SELECT EMER
(for a sustained descent)
10. DISPLAY BACKUP Button (pilot audio panel) - - - - - - - - - - - - - -PRESS
11. Altitude permitting and below FL200, attempt engine restart. Refer to
EMERGENCY RESTART - TWO ENGINES; Tab A4.
WARNING
Wing and tail deice systems will be inoperative. Avoid entering or exit
icing conditions as required. STALL WARNING-HIGH landing data is
provided and must be used in the event any ice remains on the wings
and/or tail during approach and landing.
BEFORE LANDING
1. Landing Data - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CONFIRM
a. Airspeed
VREF (KIAS)
b. Landing Distance:
(Continued Next Page)
6  MAXIMUM GLIDE - EMERGENCY LANDING
Weight - lbs 6000 6500 7000 7500 8000 8645
KIAS 120 125 130 135 140 145
　
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