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

19
Q

V^ne Never-exceed speed

20
Q

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

21
Q

Voltmeter green arc (volts)

22
Q

Usable fuel (US gal.)

23
Q

Max. takeoff weight (lbs)

24
Q

Min. “Area Idle” RPM

25
Min. RPM during operations with fuel pump off
1400
26
Max. permissible continuous RPM if an IFT student is PF
2700
27
Max. permissible continuous RPM (tachometer redline)
2800
28
Oil pressure normal operating range (psi)
30-60
29
Max. time for oil pressure to reach 10 psi after start (sec.)
30
30
Max. oil pressure (psi)
100
31
Max. RPM after start until oil temp indication registers
1000
32
Oil temperature normal operating range (deg. F)
170-220
33
Min. oil temp. to begin an area SFL at area idle (deg. F)
170
34
Min. oil quantity (US qts)
4
35
Max. oil quantity (US qts)
6
36
Max. continuous starter operation (sec.)
10
37
Max. cumulative starter operation before 3-5min cooling (sec.)
30
38
Max. tailwind dual or solo (kts)
5
39
Max. student solo gust spread (kts)
10
40
Max. student solo crosswind (kts)
10
41
Max. student solo total wind (kts)
20
42
DA20-C1 Max. demonstrated crosswind component (kts)
20
43
MATL
I will maintain aircraft control, analyze the situation, take proper action, and land as soon as conditions permit.