OPS/LIMS Flashcards

0
Q

Min. Engine-out airspeed to sustain windmilling prop (kts)

A

60 knots

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1
Q

Forced landing final approach airspeed (flaps LDG, kts)

A

55 Knots

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2
Q

Forced landing final approach airspeed (flaps T/O, kts)

A

60 knots

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3
Q

Forced landing final approach airspeed (flaps cruise, kts)

A

64

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4
Q

Best Glide airspeed (1764 lbs) (L/D Max)

A

73 knots

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5
Q

Vfe (flaps LDG, kts) (Max airspeed with flaps extended)

A

78

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6
Q

Vfe (flaps T/O, kts) (Max airspeed with flaps extended)

A

100

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7
Q

Va (kts, 1764 lbs) (No full or abrupt inputs above Va or over stress conditions will occur)

A

106 knots

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8
Q

Vno (Max. Structural cruising speed, kts)

A

118 knots

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9
Q

Force Propeller to windmill if stopped, starter inop (knots)

A

137 knots

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10
Q

Vne (Never exceed airspeed)

A

164 knots

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11
Q

Max. Permissible bank angle for steep turns (degrees)

A

60

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12
Q

Voltmeter green arc (volts)

A

12.5-16

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13
Q

Usable fuel (US gal)

A

24.0

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14
Q

Max. Takeoff weight (lbs)

A

1764

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15
Q

Min. RPM during flight if beyond gliding range of a runway (are idle)

A

1400

16
Q

Min. RPM operations with fuel pump off

A

1400

17
Q

Max. Permissible continuous rpm (redline)

A

2800

18
Q

Oil pressure normal operating range (psi)

A

30-60

19
Q

Max time for oil pressure to reach 10 psi after start (secs)

A

30 secs

20
Q

Max oil pressure (psi)

A

100

21
Q

Max rpm after start until oil temp indication registers

A

1000

22
Q

Oil temp normal operating range (degrees F)

A

170-220

23
Q

Min oil temp to begin an area SFL at area idle (degrees F)

A

170

24
Q

Min. Oil quantity (US quarts)

A

4

25
Q

Max. Oil quantity (US quarts)

A

6

26
Q

Max. Continuous starter operation (secs)

A

10

27
Q

Max cumulative starter operation before cooling 3-5 min (secs)

A

30

28
Q

Max total wind students dual (kts)

A

25 knots

29
Q

Max total wind student solo (kts)

A

20 knots

30
Q

DA20 Max demonstrated crosswind component (kts)

A

20

31
Q

Max crosswind component student solo (kts)

A

10

32
Q

Max tailwind component (kts)

A

5

33
Q

VsubY (flaps cruise, knots) (best rate of climb)

A

70

34
Q

VsubY (flaps T/O, knots) (best rate of climb)

A

66