DA20-C1 OPS LIMITS Flashcards

1
Q

Min. forced landing final approach speed with flaps LDG

A

55

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2
Q

Min. engine-out speed to sustain windmilling prop

A

60

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3
Q

Min forced landing final approval speed with flaps T/O

A

60

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4
Q

Min forced landing final approach speed with flaps CRUISE

A

65

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5
Q

Best glide speed (1764 lbs)

A

73

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6
Q

Vfe max airspeed with flaps LDG

A

78

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7
Q

Vfe max airspeed with flaps T/O

A

100

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8
Q

Va max speed for full or abrupt control inputs (1764 lbs)

A

106

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9
Q

Vno Mac structural cruising speed

A

118

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10
Q

Force a stopped propeller to windmill if starter is unopened

A

137

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11
Q

Vne never-exceed speed

A

164

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12
Q

Max permissible bank angle for steep turns

A

60 degrees

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13
Q

Voltmeter green arc

A

12.5-16.1 volts

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14
Q

Usable fuel ( US gal)

A

24.0

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15
Q

Max takeoff weight (lbs)

A

1764

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16
Q

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

A

1400

17
Q

Min RPM during operations with fuel pump off

A

1400

18
Q

Max permissible continuous RPM (tach redline)

A

2800

19
Q

Ooo pressure normal operating range (psl)

A

30-60

20
Q

Max old pressure (psl)

A

100

21
Q

Max RPM after start until oil temp indication registers

A

1000

22
Q

Ooo temperature normal operating range

A

170-220°F

23
Q

Min oil temp to begin an area SFL at area idle

A

170°F

24
Q

Min oil quantity (US qts)

A

4

25
Q

Max oil quantity (US qts)

A

6

26
Q

Max continuous starter operation

A

10 seconds

27
Q

Max cumulative starter operation before 3-5 min cooling

A

30 seconds

28
Q

Max tailwind dual or solo

A

5

29
Q

Max student solo gust spread

A

10

30
Q

Mac student solo crosswind

A

10

31
Q

Max student solo total wind

A

20

32
Q

DA20-C1 max demonstrated crosswind component

A

20