DA20-C1 Boldface/Ops Limits Flashcards

1
Q

Abort

A

Throttle - Idle
Brakes - As Required
Flaps - Cruise

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2
Q

Engine malfunction - sufficient runway remaining to land

A

Airspeed - 60 kias
Flaps - Ldg

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3
Q

Fuel pressure loss

A

Fuel pump - On

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4
Q

Engine fire in flight

A

Fuel shutoff valve - Off
Cabin heat - Off

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5
Q

Engine fire on the ground

A

Fuel shutoff valve - Off
Cabin heat - Off

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6
Q

Electrical fire on the ground

A

Gen/bat master switch - Off

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7
Q

Electrical fire in flight

A

Gen/bat master switch - Off
Air vents and windows - Open

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8
Q

Cabin fire in flight

A

Gen/bat master switch - Off
Air vents and windows - Open
Cabin heat - Off

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9
Q

Min. FL final approach speed with flaps LDG

A

55 KIAS

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10
Q

Min. FL final approach speed with flaps T/O

A

60 KIAS

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11
Q

Min. FL final approach speed with flaps CRUISE

A

65 KIAS

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12
Q

Min. engine-out speed to sustain windmilling prop

A

60 KIAS

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13
Q

Best glide speed at 1764 lbs

A

73 KIAS

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14
Q

V^fe Max. Airspeed with flaps LDG

A

78 KIAS

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15
Q

V^fe Max. Airspeed with flaps T/O

A

100 KIAS

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16
Q

V^a Max. speed for full or abrupt control inputs at 1764 lbs

A

106 KIAS

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17
Q

V^no Max. structural cruising speed

A

118 KIAS

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18
Q

Force a stopped propeller to windmill if starter inop

A

137 KIAS

19
Q

V^ne Never-exceed speed

A

164 KIAS

20
Q

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

A

60

21
Q

Voltmeter green arc (volts)

A

12.5-16

22
Q

Usable fuel (US gal.)

A

24

23
Q

Max. takeoff weight (lbs)

A

1764

24
Q

Min. “Area Idle” RPM

A

1400

25
Q

Min. RPM during operations with fuel pump off

A

1400

26
Q

Max. permissible continuous RPM if an IFT student is PF

A

2700

27
Q

Max. permissible continuous RPM (tachometer redline)

A

2800

28
Q

Oil pressure normal operating range (psi)

A

30-60

29
Q

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

A

30

30
Q

Max. oil pressure (psi)

A

100

31
Q

Max. RPM after start until oil temp indication registers

A

1000

32
Q

Oil temperature normal operating range (deg. F)

A

170-220

33
Q

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

A

170

34
Q

Min. oil quantity (US qts)

A

4

35
Q

Max. oil quantity (US qts)

A

6

36
Q

Max. continuous starter operation (sec.)

A

10

37
Q

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

A

30

38
Q

Max. tailwind dual or solo (kts)

A

5

39
Q

Max. student solo gust spread (kts)

A

10

40
Q

Max. student solo crosswind (kts)

A

10

41
Q

Max. student solo total wind (kts)

A

20

42
Q

DA20-C1 Max. demonstrated crosswind component (kts)

A

20

43
Q

MATL

A

I will maintain aircraft control, analyze the situation, take proper action, and land as soon as conditions permit.