Chapter 1 - Limitations Flashcards

1
Q

Maximum Runway Slope

A

​+/–​ 2%​

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2
Q

Company​ limit:​ Minimum​ runway​ width​

A

30 meters

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3
Q

Company​ limit:​ Minimum​ taxiway​ width​

A

15 meters

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4
Q

​ Maximum Takeoff​ and Landing Tailwind Component​

A

15 knots

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5
Q

Maximum​ speeds

A

Observe gear​ and flap​ ​placards​, or 340 knots or Mach .82

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6
Q

Max operating altitude

A

41.000 feet

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7
Q

Max landing altitude

A

8.400 feet

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8
Q

Do not operate HF radios…

A

…during fueling operations.

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9
Q

Max landing weight

A

66.360 kg

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10
Q

Max takeoff weight

A

78.999 kg

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11
Q

Max Zero Fuel weight

A

62.731 kg

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12
Q

Wingtip turn radius

A

75.2 feet / 22.9 meters

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13
Q

FLIGHT MANOEUVRING​ LOADS

A

Flaps up +2.5G to -1.0G

Flaps down +2.0G to 0.0G

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14
Q
Maximum Wind (including gusts)
Ground operations
Tailwind
Autoland headwind
Autoland crosswind
A
Ground operations: 60kts 
# Max tailwind: 15 kts 
# Max headwind for autoland: 25 kts 
# Max crosswind for autoland: 20 kts
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15
Q

Recommended Maximum Crosswind (incl gusts)
Dry RWY
Wet Rwy

Contaminated
BA Good
BA Medimum
BA Poor

A

Dry Runway: 34 kts
Wet Runway: 34 kts

Contaminated:
BA Good: 34 kts
BA Medium: 20 kts
BA Poor: 5 kts

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16
Q

Takeoff in standing water/slush or equivalent, depth greater than ….. mm is not allowed

A

13 mm

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17
Q

Fuel System temp limits

A

Max fuel tank temp: 49°C

Min fuel tank temp: 3°C above freezing point or -43°C, whichever higher.

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18
Q

Max main tanks imbalance

A

453 kg

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19
Q

Max takeoff engine EGT

20
Q

Max N1 and N2 engine RPM

A

104% and 105%

21
Q

Max continuous engine EGT

22
Q

Engine temp limit during start

23
Q

Minimum engine oil pressure

A

13 PSI

if engine oil pressure is in the yellow band with takeoff thrust set: DO NOT TAKEOFF!

24
Q

Max engine oil temp, continuous operation

25
Max engine oil temp
155°C | operation between 140-155°C is limited to 45 minutes
26
Engine starter duty cycles limits
First attempt: 2 minutes on, 10 seconds off | Second and subsequent attempts: 2 min on, 3 min off.
27
APU max operating altitude with electrical load
41.000 feet
28
APU load, both bleed only, bleed+electrical
Bleed only: do not use above 17.000 feet | Bleed AND electrical: do not use above 10.000 feet
29
When should you not operate the onboard weather radar?
When in a hangar, or within 50 feet of fueling operations of fuel spills.
30
Use of aileron trim is prohibited...
...with the autopilot​ engaged.
31
During takeoff, when can you engage autopilot?
When passing 400​ feet​ AGL.​ ​
32
The Minimum​ Use Height​ (MUH)​ for​ single channel autopilot​ operation is​ ​defined as​ ...
...158 feet​ AGL.​
33
Maximum and minimum​ glideslope angles​ for​ autoland​ are...
3.25 degrees​ ​and 2.5 degrees​ respectively.​ ​
34
Autoland capability may​ only​ be used with...
...flaps​ 30 or​ 40 and both engines​ ​operative
35
Max flap extension altitude
20.000 feet
36
Under what condition is it prohibited to hold with flaps extended?
In icing conditions.
37
Do not​ deploy​ the speed brakes​ in flight​ at​ radio altitudes​ less​ than...
...1.000 feet.
38
The maximum​ allowable in-flight​ difference between Captain and First​ Officer​ ​altitude displays​ for​ RVSM​ operations​ is​...
...200 feet.
39
The maximum​ allowable on-the-ground altitude display​ differences for RVSM​ ​operations​ are...
Capt/FO: 50 feet | Capt or FO and field elevation: 75 feet.
40
Minimum HYDRAULIC OIL level before flight is ...
76% (triggers REFILL indication)
41
Minimum ENGINE OIL quantity is ...
... 60% before flight. (if less than 70%, notify MOC) | ... 80% before a long flight (4 hours).
42
If during ENGINE START there is a fuel leak from the engine drain ...
... continue on IDLE for up to 5 minutes. If the leak continues, shut down for maintenance.
43
Name and power of the 737-800 engines
Two CFM56-7B26 Turbofan engines, producing 26,000 lbf thrust.
44
When is Cold Soaked Fuel Frost (CSFF) allowed?
- Ambient temperature > 4°C - There is no precipitation or visible moisture (rain, snow, drizzle, ​or fog with less than 1 mile visibility) - Tank fuel temperature is at or above -16°C - Frost within CSFF area on upper wing and not more than 3mm thick CSFF on lower wing surfaces
45
Speed Brakes should not be extended ...
... with flaps 15 or more.