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IFS > BOLDFACE AND OPS LIMITS > Flashcards

BOLDFACE AND OPS LIMITS Flashcards

1
Q

Min. rpm operations with fuel pump off

A

1400

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2
Q

Max. permissible continuous rpm (redline)

A

2800

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3
Q

Oil Pressure normal operating range (psi)

A

30-60

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4
Q

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

A

30

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5
Q

Max. oil pressure (psi)

A

100

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6
Q

Max. rpm after start until oil temp indication registers

A

1000

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7
Q

Oil temperature normal operating range (F)

A

170-220

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8
Q

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

A

170

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9
Q

Max. tailwind component (kts)

A

5

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10
Q

Max. total wind student solo (kts)

A

20

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11
Q

Max. crosswind component student solo (kts)

A

10

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12
Q

Engine Malfunction in Flight (Sufficient Runway Remaining to Land)

A

AIRSPEED - 60 KIAS

FLAPS - LDG

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13
Q

Vfe (flaps LDG, kts) (Max. Airspeed with flaps extended)

A

78

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14
Q

Va (kts, 1764 lbs) (No full or abrupt control inputs above Va or overstress conditions will occur.)

A

106

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15
Q

Engine Fire on the Ground

A

FUEL SHUTOFF VALVE - OFF

CABIN HEAT - OFF

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16
Q

Cabin Fire in Flight

A

GEN/BAT MASTER SWITCH - OFF
AIR VENTS AND WINDOWS - OPEN
CABIN HEAT - OFF

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17
Q

Forced landing final approach airspeed (flaps T/O, kts)

A

60

18
Q

Electrical Fire During Flight

A

GEN/BAT MASTER SWITCH - OFF

AIR VENTS AND WINDOWS - OPEN

19
Q

Best glide airspeed (1764 lbs) (L/D Max)

A

73

20
Q

Forced landing final approach airspeed (flaps LDG, kts)

A

55

21
Q

Vne (Never exceed airspeed, kts)

A

164

22
Q

Max. total wind student dual (kts)

A

25

23
Q

Force propeller to windmill if stopped, starter inop (kts)

A

137

24
Q

Min. engine-out airpseed to sustain windmilling prop (kts)

A

60

25
Q

Max. takoff weight (lbs)

A

1764

26
Q

Voltmeter green arc (volts)

A

12.5 - 16

27
Q

Vno (Max structural cruising speed, kts)

A

118

28
Q

Max permissible bank angle for steep turns (in degrees)

A

60

29
Q

Min. rpm during flight if beyond gliding range of a runway (area idle)

A

1400

30
Q

Electrical Fire on the Ground

A

GEN/BAT MASTER SWITCH - OFF

31
Q

Abort

A

THROTTLE - IDLE
BRAKES - AS REQUIRED
FLAPS - CRUISE

32
Q

Usable fuel (US gal.)

A

24.0

33
Q

Forced landing final approach airspeed (flaps CRUISE, kts)

A

64

34
Q

Max. oil quantity (US qts)

A

6

35
Q

Engine Malfunction in Flight (Fuel Pressure Loss)

A

FUEL PUMP - ON

36
Q

Max. cumulative starter op. before cooling 3-5 min (secs.)

A

30

37
Q

Vfe (flaps T/O, kts) (Max. Airspeed with flaps extended)

A

100

38
Q

Engine Fire During Flight

A

FUEL SHUTOFF VALVE - OFF

CABIN HEAT - OFF

39
Q

Max. continuous starter operation (secs)

A

10

40
Q

DA20 max. demonstrated crosswind component (kts)

A

20

41
Q

Min. oil quantity (US qts)

A

4

IFS (2 decks)

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