Limitations Flashcards

1
Q

Max Ramp Weight

A

768,000lbs

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2
Q

Max Takeoff Weight

A

766,000lbs

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3
Q

Max Landing Weight

A

575,000lbs

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4
Q

Max Zero Fuel Weight

A

547,000lbs

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5
Q

Taxi Speed - Normal

A

20kts

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6
Q

Taxi Speed - Long, Straight

A

30kts

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7
Q

Taxi Speed - Approaching a Turn

A

slow

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8
Q

Turn Speed Speed - Dry Surface

A

10kts

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9
Q

Max Turbulent Air Penetration Speed Below FL250

A

270

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10
Q

Max Turbulent Air Penetration Speed FL250 and Above

A

280 or 0.82M, whichever is lower

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11
Q

Maintain ___ above min man speed when below 0.82M

A

15kts

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12
Q

Flaps 1

A

265

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13
Q

Flaps 5

A

230

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14
Q

Flaps 20

A

225

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15
Q

Flaps 25

A

200

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16
Q

Flaps 30

A

180

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17
Q

Landing Gear Operating Speed

A

270 / 0.82M

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18
Q

Landing Gear Extended Speed

A

270 / 0.82M

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19
Q

Max Crosswind - TO

A

38

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20
Q

Max Crosswind - Landing

A

38

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21
Q

Max Crosswind - Autoland

A

25

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22
Q

Max Crosswind - Autoland (CAT II/III)

A

15

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23
Q

Max Crosswind Good to Medium BA

A

35

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24
Q

Max Crosswind Medium to Poor BA

A

20

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25
Q

Max Crosswind Poor BA

A

17

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26
Q

Max Tailwind - TO

A

10

27
Q

Max Tailwind - Landing

A

10

28
Q

Max Tailwind - Autoland

A

10

29
Q

Max Headwind - Autoland

A

25

30
Q

Runway Slope

A

+/- 2%

31
Q

Takeoff and landing altitude

A

9800ft

32
Q

Max Field Elevation

A

9650ft

33
Q

Max Operating Altitude

A

43,100ft

34
Q

Max Cabin Differential Relief Valves

A

9.1psi

35
Q

Max Cabin Differential TO/Landing

A

0.11psi

36
Q

APU to Pack takeoffs prohibited above

A

6900ft

37
Q

Minimum AP engagement alt

A

500ft AGL

38
Q

Without Land2 or Land3, AP must be disengaged below

A

200ft AGL

39
Q

CATII and CATIII NA with these messages

A

SGL SOURCE DISPLAYS, SGL SOURCE RAD ALT, SINGLE SOURCE ILS, SLATS DRIVE

40
Q

CATII and CATIII NA with flaps

A

25

41
Q

Max EGT Ground Start

A

750

42
Q

Max EGT Flight Start

A

825

43
Q

Max EGT all altitudes, no time limit

A

1050

44
Q

Takeoff and GA thrust time limit, 2 Eng

A

5 min

45
Q

Takeoff and GA thrust time limit, Single Eng

A

10 min

46
Q

Minimum Oil Pressure

A

10 psid

47
Q

Max Oil Temp - continuous

A

132

48
Q

Max Oil Temp - 15 min

A

143

49
Q

Max Flaps/Slats Altittude

A

20,000ft

50
Q

Captains and FO’s Altimeter difference

A

75ft

51
Q

Fuel Types

A

Jet A, Jet A-1, JP-5, JP-8

52
Q

Max Fuel Temp

A

49

53
Q

Min Fuel Temp

A

-40 or 3 degrees above the fuel freezing poing.

54
Q

Min Fuel Temp in Flight

A

3 degrees above fuel freezing point

55
Q

Left Main Fuel Tank Volume

A

10,300 gallons

56
Q

Right Main Fuel Tank Volume

A

10,300 gallons

57
Q

Center Fuel Tank Volume

A

27,290 gallons

58
Q

Left Main Fuel Tank Limit

A

73,170

59
Q

Right Main Fuel Tank Limit

A

73,170

60
Q

Center Fuel Tank Limit

A

193,759

61
Q

Max Fuel Imbalance when total is > 123,000

A

3000lbs

62
Q

Max Fuel Imbalance when total is < 90,000

A

4500lbs

63
Q

May have 3000lbs fuel in center tank with less than full mains, if

A

Center Tank + Actual ZFW does not exceed MZFW and CG and fuel useage limits are observed