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Non # Limitations (Main) Flashcards

1
Q

Maximum Operating Altitude?

A

43,100 feet pressure altitude

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2
Q

Maximum Takeoff & Landing Altitude?

A

8,400 feet pressure altitude

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3
Q

Flight Manoeuvring Load Acceleration Limits. Flaps Up & Flaps Down?

A
  • Flaps Up
    • +2.5g to -1.0g

*Flaps Down
* +2.0g to 0.0g
* With F25 & F30, positive limits vary linearly from +2.0g at MLW to +1.5g at MTOW

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4
Q

ER Flap 1 & Flap 30 placard speeds?

A
  • F1
    * 265 kts
  • F30
    * 180 kts
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5
Q

300 Flap 1 & Flap 30 Placard Speeds?

A
  • F1
    * 255 kts
    • F30
      • 180 kts
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6
Q

VLO/VLE?

A

270 kts / 0.82M

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7
Q

MMO?

A

0.89M

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8
Q

Minimum number of cabin crew?

A

Not less than the number of main aircraft exits

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9
Q

Maximum Demonstrated Crosswind?

A

38 kts including gusts (further limited by MACTOW & runway condition)

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10
Q

RVSM operations
* Prior to takeoff the maximum allowable difference between the Capt & FO altimeter & field elevation?

A

75 feet

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11
Q

Does the standby altimeter meet the accuracy of RVSM airspace?

A

No

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12
Q

How many knots to reduce the crosswind limit on wet or contaminated runways using asymmetric rev thrust?

A

5 kts

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13
Q

Sideslip (zero crab) not recommended with a crosswind in excess of?

A

28 kts

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14
Q

Do not operate the entry or cargo doors with wind speeds at the door of?

A

More than 40 kts

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15
Q

Do not keep the doors open when wind gusts are?

A

More than 65 kts

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16
Q

300 Maximum Takeoff Weight

A

263,083 kg

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17
Q

300 Maximum Landing Weight

A

237,682 kg

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18
Q

ER Maximum Takeoff Weight

A

351,470 kg

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19
Q

ER Maximum Landing Weight

A

251,290 kg

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20
Q

Maximum differential pressure (relief valves)?

A

9.1 psi

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21
Q

Maximum allowable cabin pressure differential for takeoff and landing?

A

0.11 psi

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22
Q

What is the limitation regarding FLCH mode during takeoff after an engine has failed?

A

Do not use FLCH until flaps are up and speed is VREF30 +80 or greater

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23
Q

300 Engine model?

A

Rolls Royce Model Trent 884B

24
Q

ER Engine model?

A

General Electric GE90-115BL

25
300 freezing fog limitation?
Freezing fog & vis < 300M. There are different restrictions regarding temperature and a 45-minute limitation for run-ups. Takeoff is permitted if the total taxi time is less than 60 minutes, but a horoscope inspection is required if the 45-minute limitation has been exceeded
26
What fuel is prohibited?
JP-4 & Jet B
27
Maximum fuel temperature?
49 degrees C
28
Minimum fuel temperature for takeoff?
-40 degrees C or 3 degrees above the fuel freezing point, whichever is higher
29
Minimum fuel temperature in flight?
3 degrees above the fuel freeze point
30
Rolls Royce Model Trent 884B Max starting EGT? For how long?
700°C, momentary
31
Rolls Royce Model Trent 884B Maximum Continuous thrust EGT limit & time limit?
850°C - no time limit
32
Rolls Royce Model Trent 884B Takeoff EGT Limit & time limit?
* 900°C for 5 minutes (10 minutes with the loss of thrust to one engine during takeoff) * 920°C for 20 seconds
33
General Electric GE90-115BL Max starting EGT (ground) & time limit?
750°C - no time limit
34
General Electric GE90-115BL Max starting EGT (flight) & time limit?
825°C - no time limit
35
General Electric GE90-115BL Max Continuous Thrust EGT? Time limit?
1050°C - no time limit
36
General Electric GE90-115BL Maximum EGT (all altitudes) & time limit?
1090°C - 5 minutes (10 minutes after an engine failure)
37
General Electric GE90-115BL Maximum EGT (below 17,000 feet) & time limit?
1095°C - 30 seconds
38
What actions are required after an RTO is performed? 300 & ER?
* Maintenance control should be contacted * 300 - another takeoff is prohibited until maintenance check the aircraft
39
APU Starter cycle?
* 3 start attempts in a 60-minute period * 1 minute wait in-between starts 1 & 2 and 2 & 3
40
Which flight control mode is takeoff permitted in?
Normal only
41
Can the ground manoeuvre camera be used during takeoff, approach & landing?
No
42
ADIRU alignment shall not be attempted at latitudes greater than?
78 degrees, 14.75 minutes
43
* How are the magnetic variation limitations satisfied?
* By either installing the latest epoch of the MagVar tables (2015) or not flying within the affected regions * 2015 tables installed in ER’s and 300’s don’t fly in the affected regions
44
What is the acceptable fuel density?
0.7309 -> 0.8507 kg/litre
45
If centre tank fuel is to be loaded:
Main tanks must be scheduled to be full
46
How much fuel can the centre tanks hold if the wing tanks are not full? What is the restriction?
1360 kgs, and centre tank fuel + AZFW must not exceed Max ZFW and CG limits are observed
47
HNE - HNK & HNS - HNX. When centre tank fuel is required for the mission, what limitation is there?
An additional 320 kgs of reserve fuel must be loaded to the centre tank
48
300 * Fuel imbalance between main tanks for taxi, takeoff and landing must not exceed?
* 1,360 kg when main tank fuel exceeds 51,709 kg * 2,041 kg when total main tank fuel is less than or equal to 22,680 kg * Linear interpolation between the above values * Refer FCTM when the above limitations may be exceeded
49
ER * Fuel imbalance between main tanks for taxi, takeoff and landing must not exceed?
* 1,360 kg when total main tank fuel exceeds 55,791 kg * 2,041 kg when total main tank fuel is less than or equal to 40,823 kg * Linear interpolation between the above values * Refer FCTM when the above limitations may be exceeded
50
Can you use the terrain display for navigation?
No
51
What is the ACARS code for a hijack?
H75
52
300 Wingspan?
200 feet / 61M (rounded up)
53
ER Wingspan
213 feet / 65M (rounded up)
54
300 VMO / MMO & FL?
330KTS @ FL200 - FL320
55
ER VMO / MMO & FL?
350KTS @ FL290

CX (16 decks)

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