B737-800 Limitations Flashcards

1
Q

Max runway slope

A

+/- 2%

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2
Q

Max allowable inflight difference between C & FO’s altitude for RVSM operations

A

200ft

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3
Q

Max Tank Fuel Temp

A

49’C

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4
Q

Engine Ignition must be on………..

A

During T/O & ldg, operting in heavy rain and anti-ice operations.

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5
Q

Max oil temp

A

155’c

operation of oil temp between 140’c-150’c is limited to 45mins

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6
Q

Max oil Temp for continuos operations

A

140’c

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7
Q

Max Flap speed 30

A

175kt

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8
Q

Max Zero Fuel Weight

A

62,731Kg

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9
Q

Minimum Altitude for single channel autopilot approach

A

50ft agl

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10
Q

During Autoland dual channel operation should occur by……

A

800ft

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11
Q

Max Flap speed 1,2 and 5 settings

A

250 kts

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12
Q

Max Operating Altitude

Max T/O and LDG Altitude

A

41000ft

8400ft

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13
Q

Max continuos EGT

A

925’C no time limit.

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14
Q

Max altitude For APU ops with Bleed and Electrical loads.

Inflight, on ground

A

Inflight 10,000ft

On Ground 15,000ft

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15
Q

Vmo

A

340kts S.L - 26000ft

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16
Q

Max Landing gear retract speed

A

235 kts

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17
Q

Mmo

A

M0.82 26000ft - 41000ft

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18
Q

Max X/W Wet/ Good rwy 45m+ and 30m T/O……. Ldg…….

A

T/O 25kts Ldg 33kts for both rwy types

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19
Q

G limits flaps up

A

+2.5g to -1.0g

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20
Q

Max Wind speeds for Auto land

H/w, X/w, T/w

A

Headwind 25kts
X/w 20kts
T/w 15kts

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21
Q

Max x/w good to medium 45m+ and 30m T/o………… Ldg…………………..

A

45m+ T/o 22kts Ldg 33kts

30m T/o 22kts ldg 25kts

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22
Q

Max x/w medium 45m+ and 30m T/o……….. Ldg…………

A

45m+30m T/o 20kts ldg 25kts

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23
Q

Max T/O weight

A

79,015Kg

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24
Q

normal cabin diff below 28000ft

A

7.45 +/- 0.1psi

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25
Q

Max and Min Glide slope angles for auto land ops.

A

Max 3.25 Min 2.5

26
Q

Max Flap speed 15

A

200kt

27
Q

Max Flap speed 10

A

210 kts

28
Q

Max X/W Dry rwy 45m+ and 30m T/o…….. Ldg……..

A

T/o 34kts Ldg 33kts for both rwy types

29
Q

severe turbulence penetration speed

A

280kts/M0.76

30
Q

Max allowable on the ground altitude display differences for RVSM operations..

5001ft to 10000ft

A

C & FO altimeters 60ft

C & FO altimeters from elevation 75ft

31
Q

Max Taxi Weight

A

79,242kg

32
Q

Max Landing gear extend speed

A

270 kts

33
Q

Max Flap speed 25

A

190kt

34
Q

Main fuel Tanks must be full if the centre tank has more than…………of fuel?

A

453kgs

35
Q

Max fuel weight- L&R wing tanks…….?
- Centre Tank……..?

   S.G 0.8507
A

4147kg
13843kg

S.G of 0.8507

36
Q

Max EGT for T/O

A

950’C for 5min*

*10mins allowed in the event of loss of thrust on one engine.

37
Q

Min oil pressure

do not t/o with oil pressure in yellow band with t/o thrust set

A

13psi

38
Q

Max N2 (High pressure compressor)

A

105%

39
Q

Max Cabin Differential pressure.

A

9.1psi

40
Q

Min inflight tank fuel temp

A

3’c above freezing point of fuel being used or -43’c whichever is higher

41
Q

Flap setting requirements for auto land ops

A

30 or 40 only

both engines must be operative

42
Q

G limits flaps down

A

+2.0 to 0.0g

43
Q

Max N1 (low pressure compressor)

A

104%

44
Q

Do not deploy speed brakes below ……….ft RA

A

1000ft radio alt

45
Q

Max flap extension altitude

A

20,000ft

46
Q

Minimum Autopilot engage altitude

A

400ft agl

47
Q

normal cabin diff above 28000ft below 37000ft

A

7.80 +/- 0.1psi

48
Q

Max Ldg Weight

A

66,360Kg

49
Q

Max altitude for APU ops Electrical load only

A

41,000ft

50
Q

During auto land Flare should arm by…..

A

500ft

51
Q

Fuel use

A

use centre tank 1st

52
Q

normal cabin diff above 37000ft

A

8.35 +/- 0.1psi

53
Q

Max altitude for APU ops Bleed only

A

17,000ft

54
Q

Max Flap speed 40

A

162 kts

55
Q

Max EGT during start

A

725’C no time limit

56
Q

Max Operating Latitude

A

82’ north and south

except between 120’E-160’E Longitude max is 60’S

57
Q

Max T/W for T/O or LDG

A

15kts

58
Q

Max fuel imbalance for Taxi , T/O, inflight or Ldg

A

453kgs

59
Q

Max allowable on the ground altitude display differences for RVSM operations..

SL to 5000ft

A

C & FO altimeters 50ft

C & FO altimeters from elevation 75ft

60
Q

Max landing gear operating speed

A

320 kts/M.82

61
Q

on Ground Do not operate wing anti ice when oat is ……

A

above 10’c