Limitations Flashcards

1
Q

Alternate Flap Duty Cycle

A

when extending or retracting flaps, allow 15 seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to ALTERNATE FLAP motor clutch

After a complete extend and retract cycle 0-15 and back to 0 allow 5 mins for cooling before trying again

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2
Q

Maximum scheduled lateral fuel imbalance is?

A

0

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3
Q

(800) Extended Engine Motoring

A

Starter usage is limited to 15 mins for the first two extended engine motorings. a minimum of 2 mins is needed between each attempt.

For the third and subsequent extended motorings, starter usage is limited to 5 mins. a minimum of 10 mins is needed between each attempt

AFM or FCOM Vol 1 L.10.9

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4
Q

The Use of what Fuel is prohibited

A

JP-4 and JET B

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5
Q

Maximum generator drive oil temp

A

157C

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6
Q

For single channel operating during approach, when shall the autopilot be disengaged

A

50ft AGL

AFM or FCOM Vol 1 L.10.5

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7
Q

On revenue flights what must be installed regarding L1 Door

A

The escape slide retention bar (grit bar), taxi, takeoff, landing

FCOM Vol 1 L.10.3

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8
Q

In flight do not extended the speed brakes past what point?

A

Flight Detent

AFM or FCOM Vol 1 L.10.10

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9
Q

Use what VHF # for primary communications the ground

A

VHF-1

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10
Q

Autoland flap and engine requirements

A

Flaps 30 or 40 // both engines operative

AFM or FCOM Vol 1 L.10.5

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11
Q

Maximum Tank fuel Temp

A

49C

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12
Q

Use of Aileron trim with the autopilot engaged is

A

Prohibited

AFM or FCOM Vol 1 L.10.5

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13
Q

Maximum takeoff and landing tailwind component

A

10 knots

FCOM Vol. 1 L.10.2

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14
Q

(800) Do not engage the autopilot below what ALT

A

400ft AGL

AFM or FCOM Vol 1 L.10.5

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15
Q

MAX and MIN glideslope angle for for autoland

A

2.5 to 3.25 degrees

AFM or FCOM Vol 1 L.10.5

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16
Q

Weight Limitations (800) Max Taxi

A

174,700lbs

AFM or FCOM Vol 1 L.10.4

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17
Q

Operation with Assumed temperature reduced takeoff is not permitted with what INOP

A

Anti-skid inoperative

AFM or FCOM Vol 1 L.10.8

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18
Q

MAX start EGT

A

(800) red line but equates to 725C

AFM or FCOM Vol 1 L.10.8

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19
Q

Holding in ICE conditions with flaps extended is ?

A

Prohibited

AFM or FCOM Vol 1 L.10.10

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20
Q

Weight Limitations (800) Min Operating

A

80,800lbs

AFM or FCOM Vol 1 L.10.4

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21
Q

Do not open the main deck cargo door in actual or anticipated winds exceeding?

A

45kts

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22
Q

Weight Limitations (800) Max Landing

A

146,300lbs

AFM or FCOM Vol 1 L.10.4

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23
Q

Do not use what VHF # for ATC communications with ACARS operational

A

VHF-3

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24
Q

Do not deploy speedbreaks below what ALT ?

A

1000ft RA

AFM or FCOM Vol 1 L.10.11

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25
Maximum time limit for takeoff thrust
5 mins AFM or FCOM Vol 1 L.10.7
26
Intentionally dry running the center tank fuel pump (low pressure light illuminated) is?
prohibited
27
(800) Normal Starter duty cycle
Multiple consecutive start attempts are permitted, each start attempt limited to 2 minutes of starter usage minimum of 10 seconds is needed between start attempts AFM or FCOM Vol 1 L.10.9
28
Weight Limitations (800) Max Zero Fuel
138,300lbs AFM or FCOM Vol 1 L.10.4
29
If a fuel pump circuit break trips, can you reset it?
NO
30
What fuel is allowed
JET A, JET A-1, JP-5, JP-8
31
After 3 consecutive APU aborted start attempts, how long is the cooling period required (800)
15 mins AFM or FCOM Vol 1 L.10.10
32
APU Max config ALT's
APU bleed + electric load = 10,000ft APU bleed = 17,000ft APU Electrical Load = 800 - 41000ft AFM or FCOM Vol 1 L.10.9
33
Maximum operating altitude
-800 = 41000ft FCOM Vol. 1 L.10.2
34
Avoid WX radar operation in what or around what
In a hanger / within 50ft of fueling operations or fuel spill
35
When can you not use LVL Change on approach?
Do not use below 1000 AFE AFM or FCOM Vol 1 L.10.5
36
What must not be operated during refueling operations
HF Radios FCOM Vol 1 L.10.3
37
When can yo not operate one or both engine bleed air switch on HIGH
Takeoff, Approach, Landing AFM or FCOM Vol 1 L.10.5
38
Reverse Thrust is not permitted when
in-flight AFM or FCOM Vol 1 L.10.8
39
Main tanks must have how much fuel if the center tank contains more than ?
full / 1000lbs
40
Random later fuel imbalance is ? Taxi, T/O, Flight, Landing
1000lbs / 453KGs
41
Engine Ignition must on AUTO/CONT for what phases
T/O Landing Anti-ice operation and (800) operation in heavy rain AFM or FCOM Vol 1 L.10.8
42
Max differential pressure (800)
9.1 PSI AFM or FCOM Vol 1 L.10.4
43
Max Runway Slope
+/- 2% - FCOM Vol. 1 L.10.2
44
MAX Oil Temp
165C 160C-165 Allowable for 15 mins 160C maximum continuous AFM or FCOM Vol 1 L.10.8
45
Maximum Speeds
Observer VMO Pointer and gear / flap placards FCOM Vol. 1 L.10.2
46
Weight Limitations (800) Max Takeoff
174,200lbs AFM or FCOM Vol 1 L.10.4
47
Maximum flight operational latitude
-800 = 82N and 82S FCOM Vol. 1 L.10.2
48
Maximum demonstrated T/O and Landing crosswind
-800 = 33kts FCOM Vol. 1 L.10.2
49
inflight tank fuel temp must be what in flight?
3C must be maintained above the freezing point of the fuel used or -43C (800) whichever is higher
50
APU bleed valve must be closed when? Can APU bleed valve be open during engine start?
- Ground air connected and isolation valve is open - engine no.1 bleed valve open - isolation and engine no.2 bleed valve open APU bleed valve may be open during engine start, but avoid engine power above idle AFM or FCOM Vol 1 L.10.10
51
Maximum allowable on the ground altitude display differences for RVSM operations
-400: Sea level = 40ft for Captain/FO 5000ft = 45ft for Captain/FO 10000ft = 50ft for Captain/FO -800: Sea level to 5000ft = 50ft 5000ft to 10,000ft = 60ft Maximum difference between Capt/FO/Ground for all = 75ft FCOM Vol 1 L.10.3
52
MAX Wind Component for Autoland (800)
Headwind: 25kts Tailwind: 10kts Crosswind: 20kts Crosswind CAT2/3: 15kts AFM or FCOM Vol 1 L.10.5
53
Maximum T/O and LDG Altitude
8,400 FCOM Vol. 1 L.10.2
54
Engine limit display markings (What colors)
``` Red = max and min limits Amber = caution limits ``` AFM or FCOM Vol 1 L.10.7
55
The max alt for flaps extended is ?
20,000ft AFM or FCOM Vol 1 L.10.10
56
Rapid and large alternating control inputs may result in what?
Structural failure at any speed, including below VA AFM or FCOM Vol 1 L.10.10
57
Severe Turbulent Air Penetration Speed (whatever is lower)
-800 = 280KIAS or .76M In cruise: SP.16 Supplementary Chart FCOM Vol. 1 L.10.2
58
Max allowable in-flight difference between captain and FO altitude display for RVSM
200ft FCOM Vol 1 L.10.3
59
what operational check must be done once each flight day?
Flight Deck Door Access System Check FCOM Vol. 1 L.10.2
60
Minimum Oil Pressure
13 psi AFM or FCOM Vol 1 L.10.8