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limitations and checkride Q's > #L Limitations > Flashcards

#L Limitations Flashcards

1
Q 
#Maximum Taxi Weight
[8-1000C] [8-1000CE] [8-1000L]
A

A 503,500lb
B 464,900lb
C 427,400lb

*Weight limits to be applied are established in Chapter WB, WB-50 Application of MTOW to International Airplane

AOM L.2.1

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2
Q 
#Maximum Takeoff Weight
[8-1000C] [8-1000CE] [8-1000L]
A

A 502,500lb
B 462,900lb
C 425,400lb

*Weight limits to be applied are established in Chapter WB, WB-50 Application of MTOW to International Airplane

AOM L.2.1

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3
Q 
#Maximum Landing Weight
[8-1000C] [8-1000CE] [8-1000L]
A

380,000lb

AOM L.2.1

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4
Q 
#Maximum Zero Fuel Weight
[8-1000C] [8-1000CE] [8-1000L]
A

355,000lb

AOM L.2.1

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5
Q

Runway Slope Limit

A

+/- 2%

AOM L.2.13

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6
Q

Maximum Operating Pressure Altitude

A

43,100 ft

AOM L.2.13

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7
Q

Maximum Takeoff and Landing Pressure Altitude

A

8000 ft

AOM L.2.13

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8
Q

Maximum Takeoff and Landing Tail Wind

A

15 kt

AOM L.2.13

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9
Q

What must you verify with Flight deck access system？

A

Check access system test operational once each flight day

AOM L.3.1

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10
Q

how must main door be configured when passengers are carried？

A

Must be in armed position

Windows clear state prior to towing, pushback, taxi, takeoff, and landing

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11
Q

what must the pic verify before there are any occupants in the Overhead crew rest？

A

Pic has determined occupants trained on emergency procedures and rapidly can use evac routes
AOM L.3.1

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12
Q

who can use the Overhead fa rest?

A

Restricted to members trained in emergency procedures, evacuation routes, firefighting procedures and depressurization procedures
OFAR during taxi, takeoff and landing prohibited

AOM L.3.2

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13
Q

When must you have engine anti ice on?

A

ON during all flight operations when icing conditions exist or are anticipated, except when the temperature is below -40 C OAT.

Do not use engine anti ice if OAT (on the ground) exceeds 10C or displayed TAT (in Flight) exceeds 15C

AOM L.3.2

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14
Q

Above what temperature should you not use wing anti ice？

A

When TAT is above 15C

AOM L.3.2

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15
Q

Autopilot Minimum Engage Altitude After Takeoff

A

200 feet AGL

AOM L.3.3

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16
Q

Autoland capability may only be used for operations into runways at or below what altitude？

A

at or below 8400feet airport field elevation

AOM L.3.3

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17
Q

Without LAND 2 or LAND 3 annunciation, the autopilot must be disengaged below the following altitudes:

A

[787-8] - 100 feet AGL
[787-9] - 135 feet AGL

AOM L.3.4

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18
Q

With LAND 2 or LAND 3 annunciation and glideslope angles greater than ____ degrees, the autopilot must be disengaged below _____feet AGL

A

3.25, 100

AOM L.3.4

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19
Q

If the glide path angle is greater than ____ the autopilot must be disengaged no later than ____ feet below the DA(DH)/MDA.

A

3.77 degrees, 50 feet

AOM L.3.4

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20
Q

When in direct or secondary Flight control mode and flaps are extended, Do not follow the _______________________________when operating in FLCH Pitch mode

A

flight director pitch guidance

AOM L.3.4

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21
Q

What is the Max headwind, tailwind and crosswind speed for automatic landing？

A

Headwind 25 knots
Tailwind component 15
Crosswind 25 knots

AOM L.3.4

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22
Q

Maximum glideslope angle for automatic landing

A

3.25 degrees

AOM L.3.4

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23
Q

Minimum glideslope angle for automatic landing

A

2.5 degrees

AOM L.3.4

24
Q

What are the approved flap settings, number of engines required and required autoland annunciation for autolanding?

A

Flaps 20,25,30
Both engines or one engine
LAND 2 or LAND 3

AOM L.3.4

25
Q

Datalink messages sent from Company format or annunciation with a com or printer on Eicas are limited to messages which will not create an unsafe condition if:

A

The messages or parts of the message are delayed or not received

Message is delivered to the wrong recipient

The message content may be frequently corrupted

They can be in the company format if they are verified per approved operational procedures

AOM L.3.4

26
Q

Do not operate HF radios during ___________.

A

Refueling operations

AOM L.3.5

27
Q

Oil temperature must be greater than ___for engine start

A

-40 c

AOM L.3.5

28
Q

Engine must be run or at idle or taxiing power for at least ____ prior to takeoff

A

1 minute

AOM L.3.6

29
Q

When is reverse thrust prohibited

A

Intentional selection of reverse thrust in Flight
Backing the airplane with reverse thrust

AOM L.3.6

30
Q

Maximum duration for takeoff thrust rating and go around thrust

A

Both engines operating - 5 minutes

One engine thrust loss - 10 minutes

AOM L.3.7

31
Q

Takeoff is permitted in which mode?

A

Normal mode

AOM L.3.8

32
Q

Max flap Altitude

A

20,000 feet

AOM L.3.8

33
Q

＃Avoid what sort of control movements？

A

Large and rapid alternating control inputs especially in combination with large changes in pitch, roll, yaw as it may result in structural failure at any speed, including below Va

AOM L.3.8

34
Q

When do icing conditions exist on the ground, takeoff and in ｆｌｉｇｈｔ？

A

When:
Ground and for takeoff:OAT is 10C or below
In flight: TAT is 20C and below

          and

Visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals)

or when operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freezes on engines, nacelles or engines sensor probes

AOM L.3.3

35
Q 
What are engine Temperature Limits for:
Ground starting 
Flight starting 
Maximum Continuous 
Takeoff
A

Ground starting - 700C
Flight starting - 900C
Maximum Continuous - 850C
Takeoff - 900C (5 minutes 2 engines, 10 minutes single engine)

AOM L.3.5

36
Q

When crosswinds greater than _________, limit thrust to a setting normally used for taxi.

A

45 knots

AOM L.3.7

37
Q

In the even of loss of primary air data, standby system corrections must be provided to, and applied by the flight crew. Correction charts are located in which chapter？

A

Performance Chapter

AOM L.3.8

38
Q

Do not fly in _______ airspace on ISFD alone. The standby altimeter does not meet ______ altimeter accuracy requirements.

A

RVSM

AOM L.3.8

39
Q

When should you set step size to zero in the FMC?

A

When required to cruise at altitudes below optimum and no further step climbs are planned.

AOM L.3.9

40
Q

the use of VNAV and/or LNAV with ____ selected is prohibited

A

QFE

AOM L.3.9

41
Q

A QFE altitude reference for the PFD must be selected in the FMS whenever QFE is used instead of ______.

A

QNH

AOM L.3.9

42
Q

Fuel density must be between _____________ lb/gallon

A

6.3 and 7.1lb/gallon

AOM L.3.11

43
Q

Fuel tanks may be loaded individually, simultaneously, or in any sequence and load main tanks equally to the desired fuel quantity or until _______.

A

Fully

AOM L.3.10

44
Q

main tanks must be scheduled to be full if ___________fuel is loaded

A

center tank

AOM L.3.10

45
Q

For the 787-9, when alternate gear extension is used what are the limitations associated with this？

A

Speedbrakes must be retracted when alternate gear extension is used, and when extending the landing gear using the alternate gear system at flap 20, speed limit during gear extension is 190 KIAS.

AOM L.3.13

46
Q

What should you not use terrain display for❓

A

navigation

within 15NM of takeoff, approach or landing at an airport or runway not contained in the GPWS terrain database.

AOM L.3.13

47
Q

When are pilots authorized to deviate from their current ATC clearance?

A

to comply with a tcas resolution advisory.

AOM L.3.13

48
Q 
# Max crosswind 
dry
A

787-8 35 takeoff, 33 landing
787-9 29 takeoff, 35 landing

AOM L.4.1

49
Q 
# Max crosswind 
wet grooved
A

25kt

AOM L.4.1

50
Q 
# Max crosswind 
Wet non-grooved
A

20 knots

AOM L.4.1

51
Q 
# Max crosswind 
Flooded
A

10kt

AOM L.4.1

52
Q 
# Max crosswind 
ICE or SNOW
breaking action good, medium good, medium poor, poor
A 
good 20kt
medium good 20(15) *
medium 20 (15) *
medium poor 15 (10) *
poor 10

*landing less than 2500Ⓜ️

AOM L.4.1

53
Q

Max crosswind
slush depth 2mm or less
3-12mm

A

2mm or less - 15kt
3-12mm - 10kt

AOM L.4.1

54
Q

What are the restriction depths for takeoff and landing?

water or slush, wet snow, dry snow

A

water or slush 13mm deep or more
wet snow 51mm deep or more
dry snow of 71mm deep or more (takeoff)
dry snow of 153mm deep or more (landing)

L.4.3

55
Q

What breaking action is takeoff and landing not permitted?

A

Very poor, 0.19 and below

L.4.3

56
Q

in flight, if it is at or below 15 degrees and there is visible moisture and anti ice is in auto and anti ice is not shown automatically on, what should you do?

A

select to on

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limitations and checkride Q's (8 decks)

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