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Ameristar > Falcon DA 20 limitations > Flashcards

Falcon DA 20 limitations Flashcards

1
Q

Max TO weight

A

28,660 lbs

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2
Q

Max taxi weight

A

28,660 lbs

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3
Q

Zero fuel weight

A

22,000 lbs

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4
Q

Max landing weight

A

27,320 lbs

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5
Q

Max pressure altitude for TO

A

10,000’

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6
Q

Max operating altitude

A

42,000’

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7
Q

Max runway slope gradient

A

+/- 2%

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8
Q

Max operating temperature

A

120° F

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9
Q

Max tailwind for TO&L

A

10 kts

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10
Q

Max X-wind for drag chute without nose on the ground

A

15 kts

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11
Q

Max speed for nose steering on the ground

A

100 kts

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12
Q

For take off without anti-skid

A

Add 1,000’

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13
Q

For landing without anti-skid

A

Add 2,000’

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14
Q

Max slush, water allowed for TO&L

A

1/2”

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15
Q

Max dry snow allowed for TO&L

A

2.36”

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16
Q

Max temp for engine and airframe anti-ice

A

+10° C

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17
Q

Temperature anti-ice must be on in visible moisture

A

+5° C

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18
Q

Max EGT for start

A

854° C (5 seconds)

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19
Q

Max EGT/N1 for TO

A

740° C @ 101.2% (5 min)

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20
Q

Max cont EGT/N1

A

724° C @ 100%

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21
Q

Max cont EGT/N1 (ameristar)

A

660° C

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22
Q

Max N2

A

105%

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23
Q

Max starting (motoring) time

A

30 sec

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24
Q

Starter cooling times between attempts

A

5/5/20/60

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25
Q

Min oil press

A

5 psi

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26
Q

Max oil press

A

65-70 psi (12 min)

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27
Q

Max oil temp

A

185° C

28
Q

Max oil consumption

A

.6 pts/hr

29
Q

Ignition limitations (min)

A

2 on/3 off, 2 on/23 off OR 5 on/25 off

30
Q

Max generator output

A

300 amps @ 28.5 volts

31
Q

Max generator amps below 170 kts

A

200 amps

32
Q

Max generator amps with OAT above 30° C (86° F)

A

150 amps

33
Q

Max generator reset attempts

A

2

34
Q

Max cabin altitude

A

10,000’

35
Q

Max differential press

A

8.3 psi

36
Q

Differential pressure relief

A

8.5 psi

37
Q

Pressure/altitude warn light “CAB” and horn

A

8.7 psi / 10,000’

38
Q

Max diff press and airspeed w/cracked windshield

A

7.5 psi / 230 kts

39
Q

Reservoir “jewel” light on

A

25,000’ max, do not use airbrake, avoid abrupt attitude changes and turbulence; no limitations below 12,000’

40
Q

Autopilot altitude limitations

A

1,000’ & 200’

41
Q

Min O2 with 2 crew <10,000’

A

600 psi

42
Q

Min O2 with 2 crew >10,000’

A

950 psi

43
Q

Min O2 with 3 crew <10,000’

A

1,100 psi

44
Q

Max altitude for gear and flap operation

A

20,000’

45
Q

Min maneuvering speed w/flaps up

A

160 kts

46
Q

Vmo

A

350 kts

47
Q

Mmo

A

.85 Mach

48
Q

Vmcg

A

120 kts

49
Q

Min O2 for 60 min duration at 14,000’ with 3 crew

A

1,100 psi

50
Q

Vmca

A

115 kts

51
Q

Mlo

A

190 kts

52
Q

Vle

A

220 kts

53
Q

Vfe (15°)

A

200 kts

54
Q

Vfe (25°)

A

190 kts

55
Q

Vfe (40°)

A

180 kts

56
Q

Va

A

200 kts

57
Q

Vllo (landing light)

A

220 kts

58
Q

Vwwo (windshield wiper)

A

180 kts

59
Q

Vab (air brake)

A

Vmo/Mmo

60
Q

Max speed for sliding window

A

160 kts

61
Q

Tire speed limit

A

186 kts

62
Q

Approx tire hydroplaning speed 6.4x√ tire pressure

A

74-78 kts

63
Q

Max Vref adjust speed

A

1/2 steady + 100% gust not to exceed Vref + 20 kts

64
Q

Max speed for braking with anti-skid inoperative

A

105 kts

65
Q

Engine oil type

A

Mobil Jet II

66
Q

Hydraulic fluid type

A

MIL 5606

Ameristar (5 decks)

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