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B737-8 > Limitations > Flashcards

Limitations Flashcards

1
Q

ETOPS Max Diversion Distance (120, 138 and 180 min)

A

120 min……. 764 nm
138 min……. 879 nm
180 min…….. 1146 nm

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2
Q

60 Minute and Benign (75 minute) Max Diversion Distance

A

60 min…………… 395 nm
75 min…………… 478 nm

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3
Q

Approved One-Engine Cruise Speed

A

290 KIAS

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4
Q

Runway Slope

A

+/- 2%

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5
Q

Max Takeoff Tailwind Component

A

15 kts (demonstrated)

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6
Q

Max Operating Altitude

A

41,000’

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7
Q

Max Takeoff and Landing Altitude

A

8400’

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8
Q

Max Taxi Weight

A

82.4 T

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9
Q

Max Takeoff Weight

A

82.1 T

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10
Q

Max Landing Weight

A

69.3 T

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11
Q

Max ZFW

A

65.9 T

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12
Q

Vlo (Retract)

A

235 kts

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13
Q

Vlo (Extend)

A

270 kts / 0.82 M

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14
Q

Vle

A

320 kts / 0.82 M

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15
Q

Flap 1 or 5

A

250 kts

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16
Q

Flap 10

A

210 kts

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17
Q

Flap 15

A

200 kts

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18
Q

Flap 25

A

190 kts

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19
Q

Flap 30

A

175 kts

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20
Q

Flap 40

A

166 kts

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21
Q

Vmo

A

340 kts

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22
Q

Va (?)

A

282 - 318 kts

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23
Q

Window Heat Inop Speed

A

250 below 10,000’

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24
Q

RVSM Altimeter Limits (inflight)

A

200’

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25
Q

RVSM Altimeter Limits (on gnd)

A

Sea Level to 5000’
50’ CAPT-FO
75’ CAPT/FO-Field Elevation

5001-10000’
60’ CAPT-FO
75’ CAPT/FO-Field Elevation

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26
Q

Max Cabin Diff

A

9.1 PSI

27
Q

Packs High Limitation (for TO/APCH/LAND)

A

With 1 or both bleeds on - packs on high not allowed

28
Q

Anti Skid Inop?

A

Autobrakes not allowed

29
Q

Main Tanks 1 or 2 must be full when…

A

Center tanks contain more than 453 kgs

30
Q

When must you advise loading agent when fuel load is incorrect?

A

Greater than 300 kgs from planned fuel load

31
Q

Minimum Altitude for AP on departure

A

400 AGL

32
Q

Autoland Wind Limits

A

25 HW
15 XW
10 TW

33
Q

Cabin DIFF for Takeoff and landing

A

0.125 PSI Max

34
Q

Max Voltage with 1 Generator on Ground

A

75 KVA (215 amps)

35
Q

Minimum Oil Temp for engine Start

A

-40 degrees

36
Q

Minimum Fuel Tank Temp

A

Higher of -43 degrees
OR
3 degrees above fuel freezing point

37
Q

Engine Ignition CONT and FLT conditions

A

CONT - moderate to heavy rain, hail or sleet
FLT - Severe Turbulence

38
Q

EGT Limits Takeoff

A

Takeoff - 1038 for 5 mins
Transient - 1048 for 30 seconds

39
Q

Max continuous EGT

A

1013 degrees

40
Q

Max EGT for Engine Start (Ground/Air)

A

Ground Start - 753 degrees
Air Start - 883 degrees

41
Q

Max Oil Temp (Max and Continuous)

A

Max 155 for 15 mins
Continuous - 140 degrees

42
Q

Minimum Oil Temp for Takeoff

A

31 degrees

43
Q

Minimum Oil Pressure

A

17.4 PSI at idle

(Do not takeoff if in yellow band with TO Thrust set)

44
Q

Max Alt for APU Bleed and Elec Load

A

10,000 ft

45
Q

Max Altitude APU Bleed only

A

17,000 ft

46
Q

Max Altitude APU Electrical Only

A

41,000 ft

47
Q

APU Starter Cooldown

A

3 attempted starts then 15 min cooldown

48
Q

Cold Soaked Fuel Frost on wing is not permitted when…

A
  • Beyond permissible marked area
  • Ambient Temp below +4
  • Fuel Tank Temp Below -16
  • precipitation or visible moisture
49
Q

Rough Air Speed

A

280 KIAS or 0.76 M

50
Q

Max Altitude with Flaps extended

A

20,000 ft

51
Q

Speedbrakes in flight limitation

A

Prohibited below 1000’ AGL or with flaps 40

52
Q

Alternate Flap Duty Cycle

A
  • 15 second between down/up movement
  • after complete extend or retract movement(0-15, 15-0) , cool 5 mins
53
Q

Maximum Fuel Tank Temp

A

49 degrees

54
Q

Fuel Imbalance Limit

A

453 kg

55
Q

453 kg if fuel in Center tank means…

A

Main tanks must be full

56
Q

Max Fuel

A

20,728 kg

57
Q

T/O Alternate Distance (60/120)

A

60 min………. 343 nm
120 min (ETOPS)……… 686 nm

58
Q

Engine Clearance - Ground

A

17”

59
Q

Define Engine Run Up AND when it is required….

A

50% N1 for 5 seconds at least 5 mins prior to takeoff
————
Required when:
Engine Anti Ice ON and Temp 3 degrees or below
OR
Increased fan Vibration

60
Q

Min Altitude for AP on a single channel approach

A

50’ AGL

61
Q

Min/Max Glideslope for an Autoland

A

2.5 - 3.25 degrees

62
Q

Runway Contamination Depth - Dry Snow & Wet Snow, Slush, Standing Water

A

Dry Snow - 4 inches
Wet Snow, Slush, Standing Water - 1/2 inch

63
Q

Runway Width required (under contamination Limits) for Takeoff

A

100’

64
Q

Pressurization Panel - Land Alt at airport above 6000’ but below 8400’

A

Set 6000’ for departure then set landing elevation at TOD to destination

B737-8 (5 decks)

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