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Limitations 767 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max runway slow

A

+/- 2%

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2
Q

Max operating Altitude

A

43,100 feet

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3
Q

Max takeoff and landing altitude

A

8,400 feet

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4
Q

Turbulent penetration airspeed

A

290 kts/ .78 Mack

Whichever is lower

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5
Q

Max takeoff and landing tail wind

A

10 kts

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6
Q

Ground wind limits for doors

A

40 kts while opening or closing

65 kts while open

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7
Q

Max crosswind for takeoff braking action good

A

40 KTS

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8
Q

True or false

Crosswind guidelines are considered limitation

A

False

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9
Q

Max taxi weight (MTW)

A

409,000 lbs

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10
Q

Max takeoff weight

A

408,000 lbs

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11
Q

Max landing weight (MLW)

A

320,000 lbs

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12
Q

Max zero fuel weight

A

295,000 lbs

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13
Q

MIN oxygen ETOPS

A

1350 PSI

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14
Q

MIN oxygen non ETOPS

A

1250 PS

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15
Q

MAX cabin pressure difference

A

9.10 Psi (Red tick on cabin DIFF indicator)

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16
Q

MAX Cabin difference for T/O and landing

A

0.125 psi (236 feet below airport Px Alt.)

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17
Q

APU starter duty cycle

A

Max 3 attempts in 60 mins

1 min cooling between attempts.

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18
Q

Max Altitude to use APU Bleed Air

A

17,000 feet

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19
Q

Min Altitude for Autopilot engagement for TOGA

A

250 feet

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20
Q

Min. Altitude for Autopilot engagement for ILS Approach

A

50 feet below MDA(H)/DA(H)

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21
Q

Min. Altitude for Autopilot engagement for single channel ILS Approaches

A

100 feet AGL

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22
Q

Minimum altitude for auto pilot engagement for Autoland (2 or 3 Autopilots)

A

Touchdown/roll out

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23
Q

Flaps setting for Autoland

A

Flaps 25/30

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24
Q

Max crosswind or headwind for Autoland

A

25 kts

25
Q

Max crosswind for Autoland cat II/III

A

15 kts

26
Q

Max tailwind for Autoland

A

10 kts

27
Q

What type of radios does not operated while refueling

A

HF radios

28
Q

How many times you can reset a circuit breaker and after how long is the cooling period

A

Once, two minutes

29
Q

Which circuit breaker you can reset after it tripped

A

Fuel pump or fuel valve

30
Q

Trust rating for capital CF6-80C2B6F Engine

A

60,200 pounds

31
Q

N1 and N2 limits for 2B6F Engines

A

N1 117.5%

N2 112.5%

32
Q

Max EGT for a start

Ground/in-flight

A

Ground 750 Unlimited time

In flight 870 40 seconds transient

33
Q

Max EGT for takeoff

A

960

34
Q

Max EGT for Max continues

A

925

35
Q

Max time at takeoff trust for aircraft N651GT

A

Five minutes (641GT 10 minutes)

36
Q

Normal engine starter duty cycle

A

One minute on

One minute off indefinitely

37
Q

Extended engine starter duty cycle

A

0 to 5 minutes on,Then off until 0% N2
5 to 10 Minutes on, then 20 minutes off
10 to 15 Minutes on, then 30 minutes off

38
Q

Starter re-engagement N2

A

0% recommended
0-20% permissible
21-30% only if on fire
>30% may cause damage to starter

39
Q

Min. engine oil pressure

A

10

40
Q

Max oil temp

A

160°C continues

175°C 15 minutes max

41
Q

Minimum oil quantity for dispatch

A

17

42
Q

Continue ignition on

A 
Moderate to heavy rain
Moderate to severe turbulence
Volcanic ash
Icing conditions
Standing water or slush
43
Q

When is continuing ignition turned on automatically

A

When Engine Anti-ice is on

When leading edge flaps are extended (Because require for takeoff and landings)

44
Q

Max altitude to extend flaps

A

20,000 feet

45
Q

Use of speed breaks in flight with flaps beyond_______Is not recommended

A

20

46
Q

Do not use speedbrakes below

A

800 feet AGL

47
Q

From engine start to engine shut down_______

Messages are the primary means of alerting crew to non-normal conditions or improper configuration

A

EICAS

48
Q

Max Allowable fuel weighed in center tank

A

85,200 pounds

38,647 kg

49
Q

Maximum allowable fuel weight in left or right tanks

A

43,097 pounds

19,549 kg

50
Q

True or false

Fuel tanks have to be filled in a specific order

A

False

51
Q

Max fuel weight in center tank with wing tanks less than full

A

22,050 pounds

10,000 kg

52
Q

Max allowable fuel in balance between left and right main thanks

A

2500 pounds when main tank fuel is 48,000 pounds or less

1500 pounds when main tank fuel is greater than 79,800 pounds

53
Q

Engine Anti-ice must be on

A

Below 22,000 feet in icing conditions

Prior to thrust reduction for descent and icing conditions

54
Q

Max allowable in-flight difference between captain And FO how to display in RVSM

A

200 feet

55
Q

Max difference on ground between captain and FO altitude displays
SL
5K
10K

A

40
45
50

56
Q

Max difference on ground between captain or FO Altitude and field elevation
SL
5K
10K

A

75
75
75

57
Q

MMO

A

.86 Mack

58
Q

Glide slope Angle for outoland

Max min

A
  1. 25

2. 5

59
Q

How many hydraulics do you need to autoland

A

3

Limitations 767 (1 decks)

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