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KA-400 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max N1

A

117.5%

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2
Q

Max N2

A

112.5%

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3
Q

Engine EGT Starting Unlimited

A

750 C

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4
Q

Engine EGT Starting 40 sec

A

870 C

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5
Q

Engine EGT Takeoff 5 minutes

A

960 C

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6
Q

Max Continuos EGT

A

925 C

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7
Q

Min Oil Pressure

A

10 PSI

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8
Q

Min Oil Quantity

A

16 Qts

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9
Q

Max Continuous Oil Temperature

A

160 C

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10
Q

Max Transient Oil Temperature

A

175 C

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11
Q

When must Engine Continuous Ignition be selected ON?

A

Water or Slush, Standing
Ash, Volcanic
Icing Conditions
Turbulence, Severe
Rain, Heavy

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12
Q

Min Fuel Temp

A

3 C above fuel freezing point

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13
Q

Max Fuel Temp

A

+54 C

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14
Q

Jet-A Freezing Point

A

-40 C

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15
Q

Limiting of ballast and Mission fuel in CWT

A

Cannot carry ballast and mission fuel
CWT Scavenge must be deactivated when ballast is being carried

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16
Q

Max Runway Slope

A

+/-2%

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17
Q

Max Autoland headwind component

A

25 kts

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18
Q

Max Tailwind component

A

15 kts

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19
Q

Max Crosswind Component

A

40 kts

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20
Q

Max Crosswind Component T/O and Landing DRY

A

T/O: 40
Landing: 36

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21
Q

Max Crosswind Component T/O and Landing WET

A

T/O: 25 kts
Landing: 30 kts

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22
Q

Max Crosswind Component T/O and Landing Standing Water/Slush

A

T/O: 15 kts
Landing: 20 kts

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23
Q

Max Crosswind Component T/O and Landing SNOW

A

T/O: 15 kts
Landing: 25 kts

24
Q

Max Crosswind Component T/O and Landing ICE

A

T/O: 15 kts
Landing: 15 kts

25
Q

Max Crosswind Component CAT I Autoland

A

25 kts

26
Q

Max Crosswind Component CAT III Autoland

A

15 kts

27
Q

Max Operating Altitude

A

45,100’

28
Q

Max T/O and Landing Altitude

A

10,000’

29
Q

Max Contaminated Runway Depth - Standing Water/ Slush/ Wet Snow

A

.5”

30
Q

Max Contaminated Runway Depth - Dry Snow Takeoff

A

2.4”

31
Q

Max Contaminated Runway Depth - Dry Snow Landing

A

4.0”

32
Q

Flaps Speed Limits

A

1 - 280 kts
5 - 260 kts
10 - 240 kts
20 - 230 kts
25 - 205 kts
30 - 180 kts

33
Q

Max Flap Extension Altitude

A

FL200

34
Q

Crew Oxygen Limitations

A

1,400 PSI

35
Q

PAX Crew Oxygen Limitations

A

1,400 PSI

36
Q

Bottles Oxygen Limitations

A

1,200 PSI

37
Q

Cargo Door Wind Limits

A

Door Operating - 40 kts
Door Opened - 65 kts

38
Q

Anti-Ice Use

A
  • Prior to reducing thrust for descent in icing conditions, the Nacelle Anti-Ice switches must be in the ON
    position. When icing conditions are no longer present,
    place the NAi switches in the OFF (or AUTO) position
  • In addition to Nacelle Anti-Ice, in icing conditions at
    or below 22,000 ft, the Wing Anti-Ice selector must be
    in the ON position. When icing conditions are no
    longer present, or when extending flaps, place the
    wing anti-ice selectors to the OFF (or AUTO) position
39
Q

Max Weights BCF

A

T/O - 870
Land - 652
0 Fuel - 610

40
Q

Max Weights ERF

A

T/O - 910
Land - 653
0 Fuel - 611

41
Q

Max Weights 400 F

A

T/O - 875
Land - 652
0 Fuel - 610

42
Q

Max Weights N700CK

A

T/O - 875*
Land - 666
0 Fuel - 635

43
Q

Min Alt for AP Engagement

A

400’

44
Q

AP Disengagment

A

50’ below MDA

45
Q

AP Single Channel ILS Disengagement

A

100 AGL

46
Q

Min TCH for Auto-Land

A

40’

47
Q

Max Differenctial Pressure

A

9.4 PSI

48
Q

Max Diff Press - T/O and Land

A

.11 PSI

49
Q

Vloe

A

270 KIAS/.82M

50
Q

Vle

A

320 KIAS/.82M

51
Q

Max speed in RVSM

A

.90M

52
Q

Turbulence penetration

A

290 - 210/ .82 - .85

53
Q

Tire Speed Limit

A

235 MPH / 204 KIAS

54
Q

Flight Maneuvering Load Factors Flaps Up

A

+2.5g to -1.0g

55
Q

Flight Maneuvering Load Factors Flaps Down

A

+2.0 to 0.0g

56
Q

APU limitations

A

-Cannot be started inflight
-Cannot be used for electrical power in flight
-Batt switch must be ON
-Operate up to FL200
-1 pack up to 15,000’

KA-400 (33 decks)

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