Limitations Flashcards

(59 cards)

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

25
Max crosswind for Autoland cat II/III
15 kts
26
Max tailwind for Autoland
10 kts
27
What type of radios does not operated while refueling
HF radios
28
How many times you can reset a circuit breaker and after how long is the cooling period
Once, two minutes
29
Which circuit breaker you can reset after it tripped
Fuel pump or fuel valve
30
Trust rating for capital CF6-80C2B6F Engine
60,200 pounds
31
N1 and N2 limits for 2B6F Engines
N1 117.5% | N2 112.5%
32
Max EGT for a start | Ground/in-flight
Ground 750 Unlimited time | In flight 870 40 seconds transient
33
Max EGT for takeoff
960
34
Max EGT for Max continues
925
35
Max time at takeoff trust for aircraft N651GT
Five minutes (641GT 10 minutes)
36
Normal engine starter duty cycle
One minute on | One minute off indefinitely
37
Extended engine starter duty cycle
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
Starter re-engagement N2
0% recommended 0-20% permissible 21-30% only if on fire >30% may cause damage to starter
39
Min. engine oil pressure
10
40
Max oil temp
160°C continues | 175°C 15 minutes max
41
Minimum oil quantity for dispatch
17
42
Continue ignition on
``` Moderate to heavy rain Moderate to severe turbulence Volcanic ash Icing conditions Standing water or slush ```
43
When is continuing ignition turned on automatically
When Engine Anti-ice is on | When leading edge flaps are extended (Because require for takeoff and landings)
44
Max altitude to extend flaps
20,000 feet
45
Use of speed breaks in flight with flaps beyond_______Is not recommended
20
46
Do not use speedbrakes below
800 feet AGL
47
From engine start to engine shut down_______ | Messages are the primary means of alerting crew to non-normal conditions or improper configuration
EICAS
48
Max Allowable fuel weighed in center tank
85,200 pounds | 38,647 kg
49
Maximum allowable fuel weight in left or right tanks
43,097 pounds | 19,549 kg
50
True or false | Fuel tanks have to be filled in a specific order
False
51
Max fuel weight in center tank with wing tanks less than full
22,050 pounds | 10,000 kg
52
Max allowable fuel in balance between left and right main thanks
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
Engine Anti-ice must be on
Below 22,000 feet in icing conditions | Prior to thrust reduction for descent and icing conditions
54
Max allowable in-flight difference between captain And FO how to display in RVSM
200 feet
55
Max difference on ground between captain and FO altitude displays SL 5K 10K
40 45 50
56
Max difference on ground between captain or FO Altitude and field elevation SL 5K 10K
75 75 75
57
MMO
.86 Mack
58
Glide slope Angle for outoland | Max min
3. 25 | 2. 5
59
How many hydraulics do you need to autoland
3