DA20-C1 Operating Information Table 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 foaps 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

V (FE) Max. Airspeed with flaps LDG (KIAS)

A

78

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7
Q

V (FE) Max. Airspeed with flaps T/O (KIAS)

A

100

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8
Q

V (A) Max. Speed for full or abrupt control inputs at 1764 (KIAS)

A

106

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9
Q

V (NO) 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

V (NE) Never Exeeded speed (KIAS)

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

Min. “Area Idle” RPM

A

1400

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15
Q

Min. RPM during Operations with fuel pump o

A

1400

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16
Q

Max. Permissible continuous RPM if an IFT student is PF

A

2700

17
Q

Max. Permissible continuous RMP (Tachometer redline)

A

2800

18
Q

Oil Pressure Normal Operating Range (psi)

A

30-60

19
Q

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

A

30

20
Q

Max. Oil Pressure (psi)

A

100

21
Q

Max. RPM after start until
oil temp indication registers

A

1000

22
Q

Oil temperature normal operating range (°F)

A

170-220

23
Q

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

A

170

24
Q

Min. Oil Quantity (US Quarts)

A

4

25
Q

Max Oil Quantity (US Quarts)

A

6

26
Q

Max. continuous starter operation (sec.)

A

10

27
Q

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

A

30

28
Q

Usable Fuel (US Gal.)

A

24

29
Q

Max Takeoff weight (lbs)

A

1764

30
Q

Max. tailwind dual or solo (kts)

A

5

31
Q

Max. Student solo gust spread (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