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2.
AUX tank ........................... monitor quantity
3.
MAIN tank .......................... monitor quantity
NOTE
AUX tank quantity must not be less than 1 US gal and MAIN tank quantity must not be more than 15 US gal.
4. Emergency fuel valve.................. NORMAL
Doc. No. 6.01.05-E Revision 1 03-Mar-2003 Page 3 - 17
3.3 SMOKE AND FIRE
3.3.1 SMOKE AND FIRE ON GROUND
(a) Engine fire when starting on the ground
1.
Emergency fuel valve.................. OFF
2.
Fuel transfer pump .................... OFF
3.
ENGINE MASTER .................... OFF
4.
ELECTRIC MASTER .................. OFF
after standstill:
5.
Canopy............................. open
6.
Airplane ............................ evacuate immediately
(b) Electrical fire with smoke on the ground
1. ELECTRIC MASTER .................. OFF
if the engine is running:
2.
Power lever ......................... IDLE
3.
ENGINE MASTER .................... OFF
when the engine has stopped:
4.
Canopy............................. open
5.
Airplane ............................ evacuate immediately
Doc. No. 6.01.05-E Revision 1 03-Mar-2003 Page 3 - 18
3.3.2 SMOKE AND FIRE DURING TAKE-OFF
(a) If take-off can still be aborted
1.
Power lever ......................... IDLE
2.
Cabin heat .......................... OFF
3.
Brakes ............................. apply - bring the airplane to a stop
4.
After stopping ........................ proceed as in 3.3.1 - SMOKE AND FIRE ON GROUND
(b) If take-off cannot be aborted
1.
Cabin heat .......................... OFF
2.
If possible, fly along a short-cut traffic circuit and land on the airfield.
WARNING
If, in the event of an engine problem occurring during take-off, the take-off can no longer be aborted and a safe height has not been reached, then a straight-ahead emergency landing should be carried out. Turning back can be fatal.
3. Airspeed............................ 73 KIAS (1150 kg, 2535 lb)
68 KIAS (1000 kg, 2205 lb)
60 KIAS (850 kg, 1874 lb)
Doc. No. 6.01.05-E Revision 1 03-Mar-2003 Page 3 - 19
after climbing to a height from which the selected landing area can be reached safely:
4.
Emergency fuel valve.................. OFF
5.
Fuel transfer pump ................... OFF
6.
Cabin heat .......................... OFF
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