1
Q
Maximum takeoff weight
A
1230 kg
2712lb
2
Q
Maximum landing weight
A
1230 kg
2712lb
3
Q
Maximum zero wing fuel weight
A
1195 kg
2635 lb
POH P2006T
flashcards
Decks in class (32)
# Cards
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Section 2 - Limitations 213
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Section 2 - Limitations 4,5,6,7,8,9,1023
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Section 2 - Limitations 2 1321
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Section 2 - Limitations 143
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Section 2 - Limitations 154
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Section 7 - Airframe and Systems description - 2 - Airframe & Flight Controls31
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Section 7 - Airframe and Systems description - 3 - Powerplant31
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Section 7 - Airframe and Systems description - 4. Pedestal Controls3
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Section 7 - Airframe and Systems description - 6 - Internal Lights8
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Section 7 - Airframe and Systems description - 7 - External Lights6
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Section 7 - Airframe And Systems Description - 8 - Fuel System9
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Section 7 - Airframe And Systems Description - 9 Landing Gear System22
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Section 7 - Airframe And Systems Description - 10 - Brakes6
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Section 7 - Airfram And Systems Description - 11 Ventilation1
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Section 7 - Airframe And Systems Description - 12 - Cabin Heat5
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Section 7 - Airframe and Systems description - 13 - Seats And Safety Belts3
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Section 7 - Airframe and System s descrip - 14 - Doors11
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Section 7 - Airframe And Systems Description - 15 - Baggage Compartment4
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Section 7 - Airframe and Systems description - 16 - MD302 Alternative Stand-by-Instrument3
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Section 7 - Airframe and Systems description - 17 - Placards19
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Section 7 - Airframe and Systems description - 19 - Electrical System24
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Section 3 ENGINE SECURING6
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Section 3 6.3 ENGINE FAILURE DURING T/O RUN26
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Section 3 6.4 ENGINE FAILURE DURING CLIMB13
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Section 3 6.5 ENGINE FAILURE IN FLIGHT4
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Section 3 8.1 ENGINE FIRE ON THE GROUND7
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Section 3 ENGINE FIRE DURING T/O RUN28
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Section 3 8.3 ENGINE FIRE IN FLIGHT12
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Section 3 8.4 ELECTRICAL SMOKE IN CABIN ON THE GROUND7
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Section 3 8.5 ELECTRICAL SMOKE IN CABIN DURING FLIGHT17
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Section 3 9 UNINTENTIONAL SPIN RECOVERY3
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Section 3 11 AIRCRAFT EVACUATION7
