IFS OPS LIMITS NO RED Flashcards

1
Q

Vso (Stall speed in LDG config, kts)

A

34

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2
Q

Vs1 (Stall speed in CRUISE config, kts)

A

42

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3
Q

Vr (rotate speed, kts)

A

44

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4
Q

Lift-off airspeed (kts)

A

52

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5
Q

Forced landing final approach airspeed (flaps LDG, kts)

A

55

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6
Q

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

A

60

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7
Q

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

A

60

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8
Q

Forced landing final approach airspeed (flaps CRUISE, kts)

A

64

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9
Q

Normal landing final approach airspeed (kts)

A

60

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10
Q

No-flap landing final approach airspeed (kts)

A

65

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11
Q

Vx (flaps T/O, kts) (Best angle of climb)

A

60

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12
Q

Vx (flaps CRUISE, kts) (Best angle of climb)

A

65

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13
Q

Vy (flaps T/O, kts) (Best rate of climb)

A

66

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14
Q

Vy (flaps CRUISE, kts) (Best rate of climb)

A

70

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15
Q

Best glide airspeed (1764lbs) (L/D max)

A

73

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16
Q

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

A

78

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17
Q

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

A

100

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18
Q

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

A

106

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19
Q

Vno (Max structural cruising speed, kts)

A

118

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20
Q

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

A

137

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21
Q

Vne (never exceed)

A

164

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22
Q

Positive limit load factor (flaps CRUISE)

A

+4.4

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23
Q

Negative limit load factor (flaps CRUISE)

A

-2.2

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24
Q

Positive limit load factor (flaps T/O or LDG)

25
Negative limit load factor (flaps T/O or LDG)
0
26
Max permissible bank angle for steep turns in degrees
60
27
Voltmeter lower limit red arc in volts
8-11
28
Voltmeter caution range yellow arc in volts
11-12.5
29
Voltmeter green arc in volts
12.5-16.1
30
Voltmeter upper limit red line in volts
16.1
31
Approved fuel grade
100LL
32
Usable fuel (US GAL)
24
33
Fuel tank capacity (US GAL)
24.5
34
Max ramp weight in lbs
1770
35
Max takeoff weight lbs
1764
36
Max landing weight lbs
1764
37
Forward CG limit (at or below 1653 lbs)
7.95
38
Forward CG limit (1764)
8.07
39
Aft CG limit (1764 lbs)
12.16
40
Aft CG limit (at or below 1653)
12.48
41
Max weight in baggage compartment
44 lbs
42
Min rpm during engine fun up idle check
975
43
Min rpm during flight if beyond gliding range of runway
1400
44
Min rpm operation with fuel pump off
1400
45
Min permissible static rpm (fuel throttle run up)
2000
46
Tachometer normal operating range rpm
700-2800
47
Max continuous rpm redline
2800
48
Min rpm drop during magneto check
25
49
Max rpm during magneto check
150
50
Max rpm drop difference btwn magnetos
50
51
Max permissible continuous bhp
125
52
Min oil pressure
10
53
Max oil pressure for full power operation if OAT <0 C (psi)
70
54
Min oil temp
75
55
Min oil temperature for full power operation if oil pressure norm ('F)
100
56
Max oil temp
240
57
Fuel pressure lower limit red line (psi)
3.5
58
Fuel pressure upper limit red line in psi
16.5
59
Max time for CHT below 300F in descent (mins)
5