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510FM-07 AD 3-15
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
 MAXIMUM GLIDE - EMERGENCY LANDING (Continued)
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.
NOTE
• With no generator online and the BATT switch in EMER, the battery will supply DC
power to the emergency bus equipment for approximately 30 minutes, provided
EMER is selected within 1 minute after failure of the second generator.
• The battery switch must be moved from BATT to EMER within 1 second to
maintain adequate avionics power. If the switch is moved slowly, the PFD, AHRS,
ADC, and other devices may need to re-initialize.
• ENG CTRL SYS L-R message will display due to loss of normal aircraft DC power
to the FADEC’s. Engine operation will not be degraded and no pilot action is
required.
• Flap system will be inoperative. Plan to land with the flap position set when EMER
selected.
• Normal gear extend will be inoperative. Plan to use emergency extension and
blow-down.
• Power brakes and antiskid will be inoperative. Plan to use emergency brake
system for landing.
• Exterior lighting will be inoperative.
• Windshield anti-ice and defog will be inoperative.
• Master Warning and Master Caution lights will be inoperative. However, the pressto-
reset function will still work to acknowledge flashing EICAS messages.
• Avionics audio warnings including Altitude Alert, Decision Height (BARO only),
Marker Beacon, TAWS, and Vertical Track will be functional. Aircraft generated
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.
(Continued Next Page)
3-16 AD 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
• 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
510FM-07 AE 3-15.1
SECTION III - OPERATING PROCEDURES MODEL 510
　
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