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Kalitta 747-400 Systems > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Tailwind

A

15kts

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2
Q

Max Altitude

A

45,100’

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3
Q

Max Takeoff/Land Field Elevation

A

10,000’

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4
Q

Max Differential Pressure

A

9.4 PSI

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5
Q

Max Differential Takeoff/Land Differential Pressure

A

0.11 PSI

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6
Q

Minimum AP Engagement

A

400’

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7
Q

Minimum AP Disengagement Height

A

50’ below MDA

100’ AGL if on single channel

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8
Q

Minimum TCH for Auto-land

A

40 FT

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9
Q

Mimimum Fuel Temperature

Jet A Freezing Point

A

3ºC above fuel freezing point

Jet A freezing point is -40ºC

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10
Q

Maximum Fuel Temperature

A

54ºC

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11
Q

Minimum Crew O2

Minimum Passenger O2

Minimum Portable O2 Bottles

A

1400 PSI

1400 PSI

1200 PSI

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12
Q

Main Battery Switch

A

Must remain on during APU use

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13
Q

Max Difference between Altimeter and Field Elevation

A

75’

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14
Q

Max difference between CA & FO Altimeters

A

Sea Level to 5,000’ - 35’

5,000’ to 10,000’ - 40’

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15
Q

Max Wind Components for Normal Operations

A

Headwind - 25kts for auto-land

Tailwind - 15kts

Crosswind - 40kts

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16
Q

Max Wind Components for:

Takeoff?

  1. Dry Runway?
  2. Wet Runway?
  3. Standing Water/Slush?
  4. Snow?
  5. Ice?
  6. Cat 1 Auto-land
  7. Cat II/II Auto Land
A

Crosswind T/O

  1. Dry 40kts
  2. Wet 25kts
  3. Standing Water/Slush 15kts
  4. Snow 15kts
  5. Ice 15kts
  6. Cat I Auto-land N/A
  7. Cat II/III Auto-land N/A
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17
Q

Max Landing Gear Extend/Retract Vlo Speed

A

270 KIAS / .82 M

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18
Q

Max Landing Gear Extended Vle Speed

A

320 KIAS / .82 M

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19
Q

Max Speed in RVSM

A

.90 M

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20
Q

Max Turbulent Air Speed

A

290-310 KIAS / .82-.85 M

whichever is lower

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21
Q

Max Flap Speeds:

  • Flap 1
  • Flap 5
  • Flap 10
  • Flap 20
  • Flap 25
  • Flap 30
A

Flap 1 - 280

Flap 5 - 260

Flap 10 - 240

Flap 20 - 230

Flap 25 - 205

Flap 30 - 180

22
Q

Max Flap Altitude

23
Q

APU Restrictions

A

Cannot be started inflight

Cannot be used for electricity inflight

Max altitude 20,000’

Can power 1 pack up to 15,000’

Battery switch must remain on

24
Q

You are ready to taxi in N741CK. What is the maximum the aircraft can weigh?

A

873,000lbs

25
Q

You are in N745CK and have just received your weight and balance form. The zero fuel weight shows 612,754. Is any action required?

A

You must remove enough payload to return the ZFW within limits.

ZFW

610,000lbs (BCF)

611,000lbs (ERF)

26
Q

You are in Europe. It is a grey and rainy day. Your intended landing runway is not shown as grooved on the 10-9A airport chart. Braking action is reported as a “.30” on a Tapley report. What is your maximum recommended crosswind component?

27
Q

You are conducting a Category III approach. The approach chart indicates a threshold crossing height of 39 feet. What is the significance?

A

The maximum autoland threshold crossing height is 40 feet

28
Q

You are conducting an RNAV approach, using VNAV as the pitch mode. When must the autopilot be disconnected?

A

50 feet below DA

29
Q

What is the maximum permitted depth of dry snow for takeoff? For landing?

A

• Takeoff – 2.4 inches

• Landing – 4.0 inches

30
Q

You are in Amsterdam on a grey and rainy day. The runway is wet and the breaking action has been reported as “4”. What is the maximum crosswind component for landing?

31
Q

You are conducting an ILS approach to a runway with a prevailing visibility of ¾ nautical miles. Is the flight director required to be on?

32
Q

What must a person do to enter the main deck in flight?

A

He or she must carry a portable oxygen bottle to enter the main deck in flight.

33
Q

You are conducting a flight with a payload that requires ballast fuel to bring the zero fuel weight CG within limits. What is the maximum amount of required fuel that can be shown on the flight release?

A

Approximately 244,000 pounds (244,416 @ 6.7 lb.gal)

34
Q

The batteries for the emergency lighting system are charged by?

35
Q

Fully charged Emergency Lighting batteries should provide light for?

A

15 minutes

36
Q
  • What is the MGLW of the ERF?*
  • BCF?*
A
  • 653,000lbs (ERF)*
  • 652,000lbs (BCF)*
37
Q

What is the main deck cargo door open, what is the wind limit?

38
Q

The supernumerary oxygen system provides how many minutes of O2 at what cabin altitude?

A

195, 25,000’

39
Q

The PBE has a maximum duration of what?

40
Q

How many supernumeraries are we authorized to carry on the upper deck?

A

20, but no more than number of seats installed.

8-BCF

4-ERF

41
Q

What color of the PBE paper indicator signifies a failed vacuum seal, requiring the unit to be replaced?

42
Q

Maximum Runway Slope?

43
Q

Flight Manuevering Load Acceleration Limits:

Flaps Up?

Flaps Down?

A
  • Flaps Up: +2.5g to -1.0g
  • Flaps Down: +2.0g to 0.0g
44
Q

What altitude must the autopilot be disengaged for a single channel ILS?

A

100 FT AGL

45
Q

Max Crosswind Components

Landing? Takeoff?

Dry Runway?
Wet Runway?
Standing Water/Slush?
Snow?
Ice?
Cat 1 Auto-land
Cat II/II Auto Land

A

Condition - Takeoff / Landing

  • Dry Runway? 40 / 36
  • Wet Runway? 25 /30
  • Standing Water/Slush? 15 / 20
  • Snow? 15 / 25
  • Ice? 15 / 15
  • Cat 1 Auto-land? / 25
  • Cat II/II Auto-land? / 15
46
Q

Continuous ignition must be used when encountering WAITR:

A

Water or slush

Ash

Ice

Turbulence

Rain

47
Q

Max Starting temperature (Unlimited)

48
Q

Max Starting temperature (Max. Transient 40 seconds)

49
Q

Max Takeoff temperature (5 Minutes)

50
Q

Max Continuous temperature

51
Q

Max Oil temperature (Continuous)

52
Q

Max Oil temperature (Max. Transient 15 Mins)

Kalitta 747-400 Systems (18 decks)

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