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IFS > IFS OPS LIMITS NO RED > Flashcards

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)

A

+2.0

25
Q

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

A

0

26
Q

Max permissible bank angle for steep turns in degrees

A

60

27
Q

Voltmeter lower limit red arc in volts

A

8-11

28
Q

Voltmeter caution range yellow arc in volts

A

11-12.5

29
Q

Voltmeter green arc in volts

A

12.5-16.1

30
Q

Voltmeter upper limit red line in volts

A

16.1

31
Q

Approved fuel grade

A

100LL

32
Q

Usable fuel (US GAL)

A

24

33
Q

Fuel tank capacity (US GAL)

A

24.5

34
Q

Max ramp weight in lbs

A

1770

35
Q

Max takeoff weight lbs

A

1764

36
Q

Max landing weight lbs

A

1764

37
Q

Forward CG limit (at or below 1653 lbs)

A

7.95

38
Q

Forward CG limit (1764)

A

8.07

39
Q

Aft CG limit (1764 lbs)

A

12.16

40
Q

Aft CG limit (at or below 1653)

A

12.48

41
Q

Max weight in baggage compartment

A

44 lbs

42
Q

Min rpm during engine fun up idle check

A

975

43
Q

Min rpm during flight if beyond gliding range of runway

A

1400

44
Q

Min rpm operation with fuel pump off

A

1400

45
Q

Min permissible static rpm (fuel throttle run up)

A

2000

46
Q

Tachometer normal operating range rpm

A

700-2800

47
Q

Max continuous rpm redline

A

2800

48
Q

Min rpm drop during magneto check

A

25

49
Q

Max rpm during magneto check

A

150

50
Q

Max rpm drop difference btwn magnetos

A

50

51
Q

Max permissible continuous bhp

A

125

52
Q

Min oil pressure

A

10

53
Q

Max oil pressure for full power operation if OAT <0 C (psi)

A

70

54
Q

Min oil temp

A

75

55
Q

Min oil temperature for full power operation if oil pressure norm (‘F)

A

100

56
Q

Max oil temp

A

240

57
Q

Fuel pressure lower limit red line (psi)

A

3.5

58
Q

Fuel pressure upper limit red line in psi

A

16.5

59
Q

Max time for CHT below 300F in descent (mins)

A

5

IFS (4 decks)

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