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DA-20 > OPS Limits > Flashcards

OPS Limits Flashcards

1
Q

INDICATED AIRSPEED

A

K I A S

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2
Q

Vs0 Stall speed with flaps LDG

A

34

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3
Q

Vs1 Stall speed with flaps CRUISE

A

42

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4
Q

VR Rotate speed

A

44

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5
Q

Lift-off Speed

A

52

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6
Q

Min. Forced landing final approach speed with flaps LDG

A

55

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7
Q

Standard pattern SFL final approach speed with flaps LDG

A

60

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8
Q

Vx Best angle of climb speed with flaps T/O

A

60

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9
Q

Normal landing final approach speed

A

60

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10
Q

Min. Engine-out speed to sustain windmilling prop

A

60

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11
Q

Min. Forced landing final approach speed with flaps T/O

A

60

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12
Q

Min. Forced landing final approach speed with flaps CRUISE

A

65

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13
Q

No-Flaps landing final approach speed

A

65

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14
Q

Vx Best angle of climb speed with flaps CRUISE

A

65

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15
Q

Vy Best rate of climb speed with flaps T/O

A

66

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16
Q

Vy Best rate of climb speed with flaps CRUISE

A

70

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17
Q

Best glide speed (1764 lbs)

A

73

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18
Q

VFE Max Airspeed with flaps LDG

A

78

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19
Q

VFE Max Airspeed with flaps T/O

A

100

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20
Q

VA Max speed for full or abrupt control inputs (1764 lbs)

A

106

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21
Q

VNO Max Structural cruising speed

A

118

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22
Q

Force a stopped propeller to windmill if starter is ions

A

137

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23
Q

VNE Never-exceed speed

A

164

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24
Q

Positive limit load factor (flaps CRUISE)

A

Plus 4.4

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25
Q

Negative limit load factor (flaps CRUISE)

A

Negative 2.2

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26
Q

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

A

Plus 2.0

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27
Q

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

A

0

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28
Q

Max. permissible bank angle for steep turns (in degrees)

A

60

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29
Q

Voltmeter lower limit red arc (volts)

A

8 to 11

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30
Q

Voltmeter caution range yellow arc (volts)

A

11 to 12.5

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31
Q

Voltmeter green arc (volts)

A

12.5 to 16.1

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32
Q

Voltmeter upper limit red lint (volts)

A

16.1

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33
Q

Approved fuel grade

A

100 LL

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34
Q

Usable fuel (US gal.)

A

24.0

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35
Q

Fuel tank capacity (US gal.)

A

24.5

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36
Q

Max. ramp weight (lbs)

A

1770

37
Q

Max. takeoff weight (lbs)

A

1764

38
Q

Max. landing weight (lbs)

A

1764

39
Q

Forward CG limit (at or below 1653 lbs)

A

7.95

40
Q

Forward CG limit (1764 lbs)

A

8.07

41
Q

Aft CG limit (1764 lbs)

A

12.16

42
Q

Aft CG limit (at or below 1653 lbs)

A

12.48

43
Q

Max. weight in baggage compartment (lbs)

A

44

44
Q

RPM normal operating range (tachometer green arc)

A

700 to 2800

45
Q

Min RPM during engine runup idle check

A

975

46
Q

Min. RPM (“area idle”) if beyond gliding range of runway

A

1400

47
Q

Min. RPM during operations with fuel pump off

A

1400

48
Q

Min. permissible full-throttle static RPM during engine runup

A

2000

49
Q

Min. permissible continuous RPM if IFT student is PF

A

2700

50
Q

Max. permissible continuous RPM (tach redline)

A

2800

51
Q

Min. RPM drop during magneto check

A

25

52
Q

Max RPM drop during magneto check

A

150

53
Q

Max RPM drop difference between magnetos

A

50

54
Q

Max permissible continuous bhp

A

125

55
Q

Min. oil pressure (PSI)

A

10

56
Q

Oil pressure normal operating range (PSI)

A

30 to 60

57
Q

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

A

30

58
Q

Max. oil pressure for full power operation if OAT

A

70

59
Q

Max. oil pressure (PSI)

A

100

60
Q

Min. oil temperature (F)

A

75

61
Q

Max. RPM after start until oil temp indication registers

A

1000

62
Q

Oil temperature normal operating range (F)

A

170 to 220

63
Q

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

A

170

64
Q

Min. oil temp. for full power operation if oil pressure norm (F)

A

100

65
Q

Max oil temperature (F)

A

240

66
Q

Min. oil quantity (US qts)

A

4

67
Q

Max. oil quantity (US qts)

A

6

68
Q

Fuel pressure lower limit red line (PSI)

A

3.5

69
Q

Fuel pressure upper limit red line (PSI)

A

16.5

70
Q

Max. continuous starter operation (sec)

A

10

71
Q

Max. cumulative starter operation before 3-5 minute cooling (sec)

A

30

72
Q

Max. time for CHT below 300F in decent (minutes)

A

5

73
Q

Min. CHT (F) takeoff and descent

A

240

74
Q

CHT normal operating range (F)

A

300 to 420

75
Q

Max. CHT (F)

A

460

76
Q

Max. OAT (C) operation w/ full winterization kit

A

0

77
Q

Max. OAT (C) operation w/ partial winterization kit

A

12.5

78
Q

Max. tailwind dual or solo

A

5

79
Q

Max. student solo gust spread

A

8

80
Q

Max. student solo crosswind

A

10

81
Q

Max. dual crosswind if IFT student is PF below 500’ AGL

A

15

82
Q

Max. Student solo total wind

A

20

83
Q

DA20-C1 Max. demonstrated crosswind component

A

20

84
Q

Max. dual total wind if IFT student is PF below 500’ AGL

A

25

85
Q

Max. Aircraft structural temperature (C)

A

55

86
Q

Propeller approx. minimum ground clearance (inches)

A

10

87
Q

Main landing gear tire pressure (PSI)

A

33

88
Q

Nose gear tire pressure

A

26

89
Q

Min. OAT (C) cabin heat not reg for 10 min before T/O

A

Negative 22

DA-20 (2 decks)

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