IFS OPS LIMITS RED Flashcards

0
Q

Min. Engine out airspeed to sustain windmilling prop

A

60

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1
Q

Forced landing final approach airspeed (flaps LDG)

A

55

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2
Q

Forced landing final approach airspeed (flaps T/O)

A

60

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3
Q

Forced landing final approach airspeed (flaps CRUISE)

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) (max airspeed with flaps extended)

A

78

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6
Q

Vfe (flaps TO) (max airspeed with flaps extended)

A

100

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7
Q

Va (1764 lbs) (no abrupt mvmts, over stress conditions occur)

A

106

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8
Q

Vno (max structural cruising speed)

A

118

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9
Q

Force propellor to windmill if stopped, starter inop

A

137

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10
Q

Vne (never exceed airspeed)

A

164

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11
Q

Max permissible bank angle for steep turns

A

60 degrees

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12
Q

Voltmeter green arc (volts)

A

12.5 - 16.1

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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 runway (area idle)

16
Q

Min rpm operations with fuel

pump off

17
Q

Max permissible continuous rpm (redline)

18
Q

Oil pressure normal operating range (psi)

19
Q

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

20
Q

Max oil pressure (psi)

21
Q

Max rpm after start until oil temp indication registers

22
Q

Oil temperature normal operating range

23
Q

Min oil temp to begin area SFL at area idle

24
Min oil quantity (US qts)
4
25
Max oil quantity (US qts)
6
26
Max continuous starter operation (secs)
10
27
Max cumulative starter op before cooling 3-5 min
30
28
Max total wind student dual (kts)
25
29
Max total wind student solo (kts)
20
30
DA20 max demonstrated crosswind component
20
31
Max crosswind component student solo
10
32
Max tailwind component
5