Limitations Flashcards

1
Q

Max Taxi Weight

A

207,014 lbs

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2
Q

Max Takeoff Weight

A

206,132 lbs

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3
Q

Max Landing Weight

A

174,606 lbs

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4
Q

Max Zero Fuel Weight

A

166,669 lbs

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5
Q

Minimum Weight

A

102,075 lbs

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6
Q

Fuel Feed Sequence

A

Wing tanks feed fuel to the engines

  1. ACT2 into center
  2. ACT1 into center
  3. Center tank into wing tanks
  4. Wing tanks
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7
Q

Doors…go

A
4 pax doors
4 emer exit doors
2 cockpit windows
3 cargo doors
4 avionics compartment doors
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8
Q

Oxygen System

A

2 cylinders 4 masks
Captain + 3rd occupant
FO + 4th occupant
2 solenoid valves

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9
Q

Autopilot use after takeoff

A

100ft AGL or 5 sec after liftoff

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10
Q

Autopilot on Non Precision Approach using F-LOC or F-GS

A

Down to 200ft AGL

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11
Q

Autopilot on circling approach

A

500ft AGL CAT C

600ft AGL CAT D

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12
Q

Autopilot use on Non Precision Approach using FINAL APP, NAV FPA, NAV V/S, TRK FPA, HDG V/S

A

250ft AGL

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13
Q

Autopilot ILS CAT 1

A

160ft AGL

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14
Q

ILS with CAT2 or CAT3 (single or dual)

A

0ft if autoland

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15
Q

Autopilot after a manual GO AROUND

A

100ft AGL

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16
Q

Autoland Limitations

A

Config 3 or Full
Glide slope between -2.5 and -3.15 deg
Airport elevation at or below 2500ft

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17
Q

G LOADING CLEAN

A

-1g to +2.5g

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18
Q

G LOADING DIRTY

A

0 to +2g

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19
Q

Max runway slope

A

+/- 2%

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20
Q

Max runway altitude

A

9200 FT

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21
Q

Nominal runway width

A

45m

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22
Q

Max demonstrated crosswind

A

38kt (gust included)

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23
Q

Max tailwind for takeoff

A

15kt

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24
Q

Max tailwind for landing

A

10kt

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25
Q

Max wind for passenger doors

A

65kts

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26
Q

Max wind for FWD and AFT cargo doors

A

40kt windward side

50 kt leeward side

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27
Q

Max crosswind (brake action good)

A

38kt

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28
Q

Max crosswind (brake action good to medium)

A

29kt

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29
Q

Max crosswind (brake action medium)

A

25kt

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30
Q

Max crosswind (brake action medium to poor)

A

20kt

31
Q

Max crosswind (brake action poor)

A

15kt

32
Q

Max GEAR extended VLE

A

280kt / M 0.67

33
Q

Max Gear VLO extension

A

250kt / M 0.60

34
Q

Max Gear VLO retraction

A

220kt / M 0.54

35
Q

Max Tire speed

A

195kt Groundspeed

36
Q

Taxi weight limitation

A

Over 167,500lb:

Do not exceed 20 kt in a turn

37
Q

Avionics ventilation limits (OAT)

A

Up to 49C no time limit on election power. See chart after that

38
Q

Max positive diff press

A

9.0 psi

39
Q

Max negative diff press

A

-1.0 psi

40
Q

Safety relief valve setting

A

8.6psi

41
Q

APU started limits

A

After 3 consecutive attempts, wait 60 min

42
Q

APU max N speed

A

107%

43
Q

APU start max EGT

A

1,090 *C below FL350

1,120 *C above FL350

44
Q

Max APU EGT running

A

675*C

45
Q

Max fuel imbalance at takeoff

A

882

46
Q

Max fuel imbalance in flight

A

2910lb (then check the chart)

47
Q

Min takeoff fuel

A

3300

And no “low level” alerts

48
Q

Icing conditions definition

A

OAT (on ground) or TAT (in flight) at or below 10*C and visible moisture present

(visible moisture can be surface snow, standing water, or slush that might adhere or be ingested into the engines)

49
Q

Definition of Severe Ice Accretion

A

Airframe ice approx 5mm or .2 Incest thick.

50
Q

Rain Repellent

A

Only use in Moderate to Heavy rain

51
Q

Max brake temp for takeoff

Brake Fans off/on

A

300C / 150C

52
Q

NWS limit for towbarless ops

A

85*

53
Q

Max turn speed with one tire per gear deflated ???WTF.

A

7kt

54
Q

Max Taxi speed 2 2 deflated tires on same main gear

A

3kt

55
Q

Max NWS angle with a deflated tire

A

30*

56
Q

IRS alignment latitude

A

Possible between 73* north and 73* south

Look in the manual beyond that

57
Q

Minimum oxygen pressure

A

800psi

Less than 800 refer to FCOM

58
Q

ROPS may be inhibited (how and if):

A
  • TERR pb OFF. On GPWS panel
  • specific approaches that have been identified to produce undue ROW alerts
  • NOTAM shortened landing distance available
59
Q

Predictive GPWS should be inhibited when:

A

Operating on rwys not incorporated in PRED GPWS database

Approached identified as causing false terrain alerts

60
Q

Cabin alt warning

A

9550 +/- 350ft

61
Q

APU altitude limits

A

FL410 max

FL250 batt only start

62
Q

NAV may be used after takeoff if:

A

GPS primary available or

Crew checked FMGS takeoff updating

63
Q

Max norm cabin ALT

A

8000

64
Q

Engine EGT limit takeoff and go around

A

1083*c

65
Q

Engine EGT limit at MCT

A

1043*c

66
Q

Engine EGT start limit temp

A

1018*c

67
Q

Engine MAX N1 (N2) normal

A

100%

68
Q

Engine MAX N1 (N2) permitted

A

105%

69
Q

Engine oil temps
Max:
Min starting:
Min takeoff:

A

151c
-40
c
52*c

70
Q

Engine min oil press

A

65 psi

71
Q

Engine starter limits

A

Auto start 3 attempts/3 cycles

Ground start 35sec pause Bren attempts

15min cooling after 3 cycles or 15 min crank

Starter engagement 20% or below

72
Q

Engine start crosswind limit

A

35 kt

73
Q

Max alt with slats / flaps extended

A

20,000