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5. AIR COND Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
6. Firewall Shutoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK BOTH OPEN
7. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF then IDLE
NOTE
• Throttles must be place to CUTOFF to reset FADEC start logic.
• Aggressive and sustained nose down pitch may be required to attain desired
airspeed. 225 KIAS is a minimum demonstrated airspeed for windmill starts.
Higher airspeeds will allow N2 to accelerate more quickly. Do not exceed 250
KIAS. Use caution for rapid terrain closure rates.
IF NEITHER ENGINE STARTS
8. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
9. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RAPIDLY SELECT EMER
10. Refer to Emergency Procedures, MAXIMUM GLIDE-EMERGENCY LANDING.
PROCEDURE COMPLETED
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
510FM-07 AA 3-13
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
AIRSTART ENVELOPE
Figure 3-1
CAUTION
• 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.
3-14 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
MAXIMUM GLIDE - EMERGENCY LANDING
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
Procedures, EMERGENCY RESTART - 2 ENGINES.
*With the battery switch in EMER position and the generators OFF, power is supplied for at
least 30 minutes to the following equipment:
(Continued Next Page)
Weight - lbs 6000 6500 7000 7500 8000 8645
KIAS 120 125 130 135 140 145
• PFD 1 - Reversion Mode
• COM 1
• NAV 1 including Marker Beacon
• GPS 1
• ADC 1
• AHRS 1
• Transponder 1 (XPDR1)
• Pilot’s and Copilot’s Audio Panels
• L and R N1, N2, and ITT Indications
• L Oil Temperature
• L Fuel Flow
• Fuel Temperature
• Battery Voltage Indication
• Autopilot Control Panel (HDG, CRS, ALT
knobs only)
• Cabin Altitude and Differential Pressure
Indications
• Cabin Dump System
• Cockpit Flood Light
• Pilot’s Pitot-Static Heat
• Landing Gear Indicator Lights
• Avionics Audio Warnings
• Standby Instruments (Airspeed, Altitude,
Attitude)
• Magnetic Compass Lighting
• ELT GPS Position Interface
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