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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
**You are in N745CK and have just received your weight and balance form. The zero fuel weight shows 612,754. Is any action required?**
**You must remove enough payload to return the ZFW within limits.** **_ZFW_** **610,000lbs (BCF)** **611,000lbs (ERF)**
26
**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?**
**20 kts**
27
**You are conducting a Category III approach. The approach chart indicates a threshold crossing height of 39 feet. What is the significance?**
**The maximum autoland threshold crossing height is 40 feet**
28
**You are conducting an RNAV approach, using VNAV as the pitch mode. When must the autopilot be disconnected?**
**50 feet below DA**
29
**What is the maximum permitted depth of dry snow for takeoff? For landing?**
**• Takeoff – 2.4 inches** **• Landing – 4.0 inches**
30
**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?**
**30 kts**
31
**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?**
** No**
32
**What must a person do to enter the main deck in flight?**
**He or she must carry a portable oxygen bottle to enter the main deck in flight.**
33
**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?**
**Approximately 244,000 pounds (244,416 @ 6.7 lb.gal)**
34
*The batteries for the emergency lighting system are charged by?*
*DC Bus 4*
35
*Fully charged Emergency Lighting batteries should provide light for?*
*15 minutes*
36
* What is the MGLW of the ERF?* * BCF?*
* 653,000lbs (ERF)* * 652,000lbs (BCF)*
37
*What is the main deck cargo door open, what is the wind limit?*
*65kts*
38
*The supernumerary oxygen system provides how many minutes of O2 at what cabin altitude?*
*195, 25,000'*
39
*The PBE has a maximum duration of what?*
*15 mins*
40
*How many supernumeraries are we authorized to carry on the upper deck?*
20, but no more than number of seats installed. 8-BCF 4-ERF
41
*What color of the PBE paper indicator signifies a failed vacuum seal, requiring the unit to be replaced?*
*Pink*
42
Maximum Runway Slope?
+/- 2%
43
Flight Manuevering Load Acceleration Limits: Flaps Up? Flaps Down?
* Flaps Up: +2.5g to -1.0g * Flaps Down: +2.0g to 0.0g
44
What altitude must the autopilot be disengaged for a single channel ILS?
100 FT AGL
45
Max Crosswind Components Landing? Takeoff? Dry Runway? Wet Runway? Standing Water/Slush? Snow? Ice? Cat 1 Auto-land Cat II/II Auto Land
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
Continuous ignition must be used when encountering **WAITR**:
**W**ater or slush **A**sh **I**ce **T**urbulence **R**ain
47
Max Starting temperature (Unlimited)
750ºC
48
Max Starting temperature (Max. Transient 40 seconds)
870ºC
49
Max Takeoff temperature (5 Minutes)
960ºC
50
Max Continuous temperature
925ºC
51
Max Oil temperature (Continuous)
160ºC
52
Max Oil temperature (Max. Transient 15 Mins)
175ºC

Kalitta 747-400 Systems (18 decks)

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