Section 3
Emergency Procedures
3.1
AIRSPEEDS FOR EMERGENCY OPERATION
If nothing is mentioned a weigh of 840 kg (1852 lbs) is valid.
Stall speed
Engine failure after takeoff
Best recommended gliding speed ( glide angle 1 : 6,2 )
-Normal
-Acro (800 kg)
Precautionary landing with engine power
Landing without engine power
Maximum demonstrated cross wind component
3.2
OPERATIONAL CHECKLIST
3.2.1
ENGINE FAILURE DURING TAKEOFF ROLL
1. Throttle
2. Brakes
3. Mixture
4. Ignition switch
5. Master switch
3.2.2
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
Stall speed: 59 KIAS (109 km/h)
1. Airspeed
2. Mixture
3. Fuel shutoff valve
4. Ignition switch
5. Master switch
6. Forced landing
3.2.3
ENGINE FAILURE DURING FLIGHT (RESTART PROCESS)
1. Airspeed
2. Fuel shutoff valve
3. Mixture
4. Boost pump
5. Ignition switch
3 - 4
WARNING
The stall warning is deactivated!
Pilot´s Operating Handbook
59 KIAS (109 km/h)
80 KIAS (148 km/h)
90 KIAS (167km/h)
80 KIAS (148 km/h)
80 KIAS (148 km/h)
80 KIAS (148 km/h)
15 Knots (27 km/h)
IDLE
APPLY
IDLE CUT OFF
OFF
OFF
80 KIAS (148 km/h)
IDLE CUT OFF
OFF (Pull & Turn)
OFF
OFF
PERFORM as practical
80 KIAS (148 km/h)
"ACRO & CENTER" tank
RICH
ON
BOTH
(or START if propeller has stopped)
Page Date: 20. April 2002
Page Date: 14. July 2008
EXTRA 200
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