曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 1(30)