DA20-C1 Operating Information Table (Required) Flashcards

1
Q

Min FL final approach speed with flaps LDG (KIAS)

A

55

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2
Q

Min engine-out speed to sustain windmilling prop (KIAS)

A

60

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3
Q

Min FL final approach speed with flaps T/O (KIAS)

A

60

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4
Q

Min FL final approach speed with flaps CRUISE (KIAS)

A

65

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5
Q

Best glide speed at 1764 lbs (KIAS)

A

73

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6
Q

Vfe Max Airspeed with flaps LDG (KIAS)

A

78

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7
Q

Vfe Max Airspeed with flaps T/O (KIAS)

A

100

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8
Q

Vs Max speed for full or abrupt control inputs at 1764 lbs (KIAS)

A

106

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9
Q

Vno Max Structural cruising speed (KIAS)

A

118

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10
Q

Force a stopped propeller to windmill if starter inop (KIAS)

A

137

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11
Q

Vne never exceed speed

A

164

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12
Q

Max bank in steep turns, chandelles, and lazy eights (deg)

A

60

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13
Q

Voltmeter green arc (volts)

A

12.5-16

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14
Q

Usable fuel (US gal)

A

24

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15
Q

Max takeoff weight (lbs)

A

1764

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16
Q

Min “Area Idle” RPM

A

1400

17
Q

Min RPM during operations with fuel pump o

A

1400

18
Q

Max permissible continuous RPM if an IFT student is PF

A

2700

19
Q

Max permissable continuous RPM (tachometer redline)

A

2800

20
Q

Oil pressure normal operating range (psi)

A

30-60

21
Q

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

A

30

22
Q

Max oil pressure (psi)

A

100

23
Q

Max RPM after start until oil temp indication registers

A

1000

24
Q

Oil temperature normal operating range (°F)

A

170-220

25
Q

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

A

170

26
Q

Min oil quantity (US qts)

A

4

27
Q

Max oil quantity (US qts)

A

6

28
Q

Max continuous starter operation (sec)

A

10

29
Q

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

A

30

30
Q

Max tailwind dual or solo (kts)

A

5

31
Q

Max student solo gust spreads (kts)

A

10

32
Q

Max student solo crosswind (kts)

A

10

33
Q

Max student solo total wind (kts)

A

20

34
Q

DA20-C1 Max demonstrated crosswind component (kts)

A

20