Op Limits Flashcards

0
Q

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

A

60

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1
Q

Forced landing final approach airspeed (flaps LDG, kts)

A

55

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2
Q

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

A

60

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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

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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 control inputs above VA or overstress conditions will occur.)

A

106

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8
Q

VNO (Max. structural cruising speed, kts)

A

118

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9
Q

Force propeller to windmill if stopped, starter inop (kts)

A

137

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10
Q

VNE (Never exceed airspeed, kts)

A

164

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11
Q

Max. Permissible bank angle for steep turns (in 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 for in-flight (area) idle beyond gliding range of a runway

A

1400

16
Q

Min. rpm operations with fuel pump off

A

1400

17
Q

Max. permissible coninuous rpm

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

20
Q

Max. oil pressure (psi)

A

100

21
Q

Max. rpm after start until oil temp indication registers

A

1000

22
Q

Oil temperature normal operationg range (oF)

A

170-220

23
Q

Min. oil temp. to begin an area SFL at Area Idle (oF)

A

170

24
Q

Min. oil quantity (US qts)

A

4

25
Q

Max. oil quantity (US qts)

A

6

26
Q

Max. continuous starter operation (secs.)

A

10

27
Q

Max. cumulative starter op. before coooling 3-5min. (secs.)

A

30

28
Q

Max. total wind student dual (kts)

A

25

29
Q

Max. total wind student solo (kts)

A

20

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