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IFT Study Guide
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ABORT
THROTTLE - IDLE
BRAKES - AS REQUIRED
FLAPS - CRUISE
ENGINE MALFUNCTION - SUFFICIENT RUNWAY REMAINING TO LAND
AIRSPEED - 60 KIAS
FLAPS - LDG
FUEL PRESSURE LOSS
FUEL PUMP - ON
ENGINE FIRE IN FLIGHT
FUEL SHUTOFF VALVE - OFF
CABIN HEAT - OFF
ENGINE FIRE ON THE GROUND
FUEL SHUTOFF VALVE - OFF
CABIN HEAT - OFF
ELECTRICAL FIRE ON THE GROUND
GEN/BAT MASTER SWITCH - OFF
ELECTRICAL FIRE IN FLIGHT
GEN/BAT MASTER SWITCH - OFF
AIR VENTS AND WINDOWS - OPEN
CABIN FIRE IN FLIGHT
GEN/BAT MASTER SWITCH - OFF
AIR VENTS AND WINDOWS - OPEN
CABIN HEAT - OFF
Min. FL final approach speed with flaps LDG (KIAS)
55
Min. engine-out speed to sustain windmilling prop (KIAS)
60
Min. FL final approach speed with flaps T/O
60
Min. FL final approach speed with flaps CRUISE (KIAS)
65
Best glide speed at 1764 lbs (KIAS)
73
V_FE Max. Airspeed with flaps LDG (KIAS)
78
V_FE Max. Airspeed with flaps T/O (KIAS)
100
V_A Max. speed for full or abrupt control inputs at 1764 lbs (KIAS)
106
V_NO Max. structural cruising speed (KIAS)
118
Force a stopped propeller to windmill if starter inop (KIAS)
137
V_NE Never exceed speed (KIAS)
164
Max. bank in steep turns, chandelles, and lazy eights (deg)
60
Voltmeter green arc (volts)
12.5-16
Usable fuel (US gal.)
24
Max. takeoff weight (lbs)
1764
Min. “Area Idle” RPM
1400
Min. RPM during operations with fuel pump off
1400
Max. permissible continuous RPM if an IFT student is PF
2700
Max. permissible continuous RPM
2800
Oil pressure normal operating range (psi)
30-60
Max. time for oil pressure to reach 10 psi after start (sec.)
30
Max. oil pressure (psi)
100
Max. RPM after start until oil temp indication registers
1000
Oil temperature normal operating range (deg F)
170-220
Min oil temp. to begin an area SFL at area idle (deg F)
170
Min. oil quantity (US qts)
4
Max. oil quantity (US qts)
6
Max. continuous starter operation (sec.)
10
Max. cumulative starter operation before 3-5min cooling (sec.)
30
Max. tailwind dual or solo (kts)
5
Max. student solo gust spread (kts)
10
Max. student solo crosswind (kts)
10
Max. student solo total wind (kts)
20
DA20-C1 Max. demonstrated crosswind component (kts)
20