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DA-20 > OPS Limits > Flashcards

OPS Limits Flashcards

(89 cards)

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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
Negative limit load factor (flaps CRUISE)
Negative 2.2
26
Positive limit load factor (flaps T/O or LDG)
Plus 2.0
27
Negative limit load factor (flaps T/O or LDG)
0
28
Max. permissible bank angle for steep turns (in degrees)
60
29
Voltmeter lower limit red arc (volts)
8 to 11
30
Voltmeter caution range yellow arc (volts)
11 to 12.5
31
Voltmeter green arc (volts)
12.5 to 16.1
32
Voltmeter upper limit red lint (volts)
16.1
33
Approved fuel grade
100 LL
34
Usable fuel (US gal.)
24.0
35
Fuel tank capacity (US gal.)
24.5
36
Max. ramp weight (lbs)
1770
37
Max. takeoff weight (lbs)
1764
38
Max. landing weight (lbs)
1764
39
Forward CG limit (at or below 1653 lbs)
7.95
40
Forward CG limit (1764 lbs)
8.07
41
Aft CG limit (1764 lbs)
12.16
42
Aft CG limit (at or below 1653 lbs)
12.48
43
Max. weight in baggage compartment (lbs)
44
44
RPM normal operating range (tachometer green arc)
700 to 2800
45
Min RPM during engine runup idle check
975
46
Min. RPM ("area idle") if beyond gliding range of runway
1400
47
Min. RPM during operations with fuel pump off
1400
48
Min. permissible full-throttle static RPM during engine runup
2000
49
Min. permissible continuous RPM if IFT student is PF
2700
50
Max. permissible continuous RPM (tach redline)
2800
51
Min. RPM drop during magneto check
25
52
Max RPM drop during magneto check
150
53
Max RPM drop difference between magnetos
50
54
Max permissible continuous bhp
125
55
Min. oil pressure (PSI)
10
56
Oil pressure normal operating range (PSI)
30 to 60
57
Max. time for oil pressure to reach 10 PSI after start (sec)
30
58
Max. oil pressure for full power operation if OAT
70
59
Max. oil pressure (PSI)
100
60
Min. oil temperature (F)
75
61
Max. RPM after start until oil temp indication registers
1000
62
Oil temperature normal operating range (F)
170 to 220
63
Min. oil temp. to begin an area SFL at area idle (F)
170
64
Min. oil temp. for full power operation if oil pressure norm (F)
100
65
Max oil temperature (F)
240
66
Min. oil quantity (US qts)
4
67
Max. oil quantity (US qts)
6
68
Fuel pressure lower limit red line (PSI)
3.5
69
Fuel pressure upper limit red line (PSI)
16.5
70
Max. continuous starter operation (sec)
10
71
Max. cumulative starter operation before 3-5 minute cooling (sec)
30
72
Max. time for CHT below 300F in decent (minutes)
5
73
Min. CHT (F) takeoff and descent
240
74
CHT normal operating range (F)
300 to 420
75
Max. CHT (F)
460
76
Max. OAT (C) operation w/ full winterization kit
0
77
Max. OAT (C) operation w/ partial winterization kit
12.5
78
Max. tailwind dual or solo
5
79
Max. student solo gust spread
8
80
Max. student solo crosswind
10
81
Max. dual crosswind if IFT student is PF below 500' AGL
15
82
Max. Student solo total wind
20
83
DA20-C1 Max. demonstrated crosswind component
20
84
Max. dual total wind if IFT student is PF below 500' AGL
25
85
Max. Aircraft structural temperature (C)
55
86
Propeller approx. minimum ground clearance (inches)
10
87
Main landing gear tire pressure (PSI)
33
88
Nose gear tire pressure
26
89
Min. OAT (C) cabin heat not reg for 10 min before T/O
Negative 22

DA-20 (2 decks)

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