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
Max and Min Glide slope angles for auto land ops.
Max 3.25 Min 2.5
26
Max Flap speed 15
200kt
27
Max Flap speed 10
210 kts
28
Max X/W Dry rwy 45m+ and 30m T/o........ Ldg........
T/o 34kts Ldg 33kts for both rwy types
29
severe turbulence penetration speed
280kts/M0.76
30
Max allowable on the ground altitude display differences for RVSM operations.. 5001ft to 10000ft
C & FO altimeters 60ft C & FO altimeters from elevation 75ft
31
Max Taxi Weight
79,242kg
32
Max Landing gear extend speed
270 kts
33
Max Flap speed 25
190kt
34
Main fuel Tanks must be full if the centre tank has more than............of fuel?
453kgs
35
Max fuel weight- L&R wing tanks.......? - Centre Tank........? S.G 0.8507
4147kg 13843kg S.G of 0.8507
36
Max EGT for T/O
950'C for 5min* *10mins allowed in the event of loss of thrust on one engine.
37
Min oil pressure | do not t/o with oil pressure in yellow band with t/o thrust set
13psi
38
Max N2 (High pressure compressor)
105%
39
Max Cabin Differential pressure.
9.1psi
40
Min inflight tank fuel temp
3'c above freezing point of fuel being used or -43'c whichever is higher
41
Flap setting requirements for auto land ops
30 or 40 only both engines must be operative
42
G limits flaps down
+2.0 to 0.0g
43
Max N1 (low pressure compressor)
104%
44
Do not deploy speed brakes below ..........ft RA
1000ft radio alt
45
Max flap extension altitude
20,000ft
46
Minimum Autopilot engage altitude
400ft agl
47
normal cabin diff above 28000ft below 37000ft
7.80 +/- 0.1psi
48
Max Ldg Weight
66,360Kg
49
Max altitude for APU ops Electrical load only
41,000ft
50
During auto land Flare should arm by.....
500ft
51
Fuel use
use centre tank 1st
52
normal cabin diff above 37000ft
8.35 +/- 0.1psi
53
Max altitude for APU ops Bleed only
17,000ft
54
Max Flap speed 40
162 kts
55
Max EGT during start
725'C no time limit
56
Max Operating Latitude
82' north and south except between 120'E-160'E Longitude max is 60'S
57
Max T/W for T/O or LDG
15kts
58
Max fuel imbalance for Taxi , T/O, inflight or Ldg
453kgs
59
Max allowable on the ground altitude display differences for RVSM operations.. SL to 5000ft
C & FO altimeters 50ft C & FO altimeters from elevation 75ft
60
Max landing gear operating speed
320 kts/M.82
61
on Ground Do not operate wing anti ice when oat is ......
above 10'c