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Limitations/knowledge Flashcards

(78 cards)

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1
Q

Max taxi weight
AOM 1.01.20 p2

A

228,383 kg -8
254,962 kg -9

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2
Q

Max takeoff weight
AOM1.01.20 p2

A

227,930 kg -8
254,011 kg -9

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3
Q

Max Landing Weight
AOM 1.01.20 p2

A

172,365 kg -8
192,776 kg -9

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4
Q

Max ZFW
AOM 1.01.20 p2

A

161,025 kg -8
181,436 kg -9

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5
Q

Passenger oxygen for level off FL250 in minutes?
AOM 45 1.01.35 P 3

A

-8 min 23 minutes
-9 min 59 minutes

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6
Q

G limits?
AOM 1.01.20 p3

A

Flaps up 2.5 to -1.0g
Flaps down 2.0 to 0.0g

Flap 25 and 30 +limit linear from 2.0 mlw to 1.5 mtow

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7
Q

Mmo Vmo

AOM 1.01.20 p3

A

350 kias sea level linear* to 16,500’
360 kias @ 16,500’ to fl280
M 0.9 from fl280 to fl431

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8
Q

Etops engine out speed
AOM 1.01.20 p1

A

330kias

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9
Q

Maximum takeoff alternate distance and speed

FOM 8.1.7.3

A

377nm 60minutes
814nm 120 minutes etops
330kts

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10
Q

Max Airspeed unreliable AoA speed used
AOM 1.01.20 P 4

A

ALTITUDE (FT) MAXIMUM SPEED (KIAS)
Above 40,000 250
38,001 to 40,000 260
35,001 to 38,000 270
At or below 35,000 290

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11
Q

Length and wingspan
AOM 2.20.10 P 1-2

A

Length:
183’ 5” for -8
203’ 5” for -9

Wingspan:
197’ 3”

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12
Q

Minimun altitude for FLCH and V/S
AOM 1.04.00 P 8

A

1000’ agl

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13
Q

Minimum altitude for speedbrake use
AOM 1.01.27 P 1

A

800’ agl

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14
Q

Min engine oil qty for dispatch
AOM 1.04.02 P 2

A

Flight less then 4hrs 13L
Otherwise 18L

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15
Q

Minimum crew oxygen

AOM 1.04.02 P 2

A

1200 psi otherwise reference charts AOM 1.01.35 P 1

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16
Q

Onboard library
AOM 45 1.04.02 P 2

A

Pax evac card
2 metric flat lvl cards
2 qrh
2 qrh normal
2 tailored enroute charts
ASR
Reclearance info card
Permit to proceed
A/C cabin odour reporting sheet
Flight deck observer seat card
Logbook
MEL

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17
Q

Cockpit emergency equipment
AOM 1.04.02 P 5

A

Escape hatch and descent devices
Fire extinguisher
Crash axe
Gloves
PBE
2 flashlights
4 life vest
2 reflective vests
Supplemental survival kit
Doc pouch
Elementary work pouch

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18
Q

OFCR safety equipment

AOM 45 1.04.02 P 5

A

1 flashlight
2 portable O2 (1000psi)
1 halon fire extinguisher
1 life vest
2 pbe
2 polar suits
Escape hatch

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19
Q

Wind manual entry requirements

AOM 1.04.02 P 18

A

Variations greater than:
30° and/or 30kt
Temp. -/+5°
Altitude change

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20
Q

When is engine clearing required

AOM 1.04.02 P 7
AOM 1.04.03 P 6
AOM 1.01.30 P 1

A

Oat is 3°c or below and Visible moisture or fog 1sm/1600M or less, rain, snow…..

Within 5min of t/o
Max 60 min interval
Max 120min taxi

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21
Q

Max engine vibration for t/o

AOM 1.04.04 P7

A

Below 4 units at up to 55% N1

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22
Q

Minimum fuel tank temp for takeoff

AOM 1.04.04 P 8

A

-29°c

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23
Q

Limitation to start both engines at once?

AOM 45 1.04.03 P 4

A
  • 40°c
  • Simultaneous engine starts are only allowed when the APU is running and both APU generators are operating.
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24
Q

Minimum engine oil temp for start

AOM 1.04.03 P 4

A

-40°c

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25
Tail strike pitch attitude AOM 1.04.05 P4
-8 11.2° -9 9.7°
26
When do autobrakes arm on t/o AOM 2.32.10 P 1 AOM 1.04.06 P 2
85kts
27
When do automatic rudder inputs activate on takeoff for engine failure AOM 1.04.06 P 2
65kts
28
When does the a/p become available on takeoff? AOM 45 1.01.22 P 1
200’ agl
29
When will vnav engage on t/o? AOM 45 1.04.05 P 1
400’ agl if armed
30
Maximum rate of climb speed AOM 1.04.07 P6
Vref 30 plus 140 until M.82 for -8 M.84 for -9
31
Econ climb speeds AOM 1.04.07 P6
Below 10,000’ 250kts/vref +80 whichever is higher Above 10,000’ -8 320kts/M.85 -9 330kts/M.85
32
When can APP mode be selected?
Within 18nm for ils/loc 23nm for gls 120° intercept angle Both pointers showing Cleared approach
33
Turbulence speed AOM 1.04.18 P1
below 25,000’ 290kts Above 25,000’ 310kts/M.84 whichever is lower
34
Icing conditions exist at what temp AOM 1.04.18 P 4
Icing conditions exist when OAT (on the ground) or TAT (in-flight) is 10°C or below and any of the following exists: • visible moisture (clouds (in-flight), fog with visibility of one statute mile (1600 m) or less, rain, snow, sleet, ice crystals, and so on) is present, or • ice, snow, slush or standing water is present on the ramps, taxiways, or runways.
35
%mac for aft c/g considerations AOM 45 1.03.20 P 1
If a run up is required: -8 25.3% -9 23.1% Or greater weight depending as weight increases
36
When is a runway considered contaminated? AOM 45 1.01.90 P 2
When the coverage is more than 25% of area to be used
37
What contaminants prohibit takeoff? AOM 1.01.90 P 2
Combined coverage of more than 25% of length and 100’ width to be used: •Wet ice •Water, slush, wet snow, or dry snow over ice •Water over compacted snow
38
Max contamination depths and equivalency? AOM 1.01.90 P 2
Less than 1/8” or 3mm is not contaminated Max 4” or 102mm light dry snow Max 2” or 51mm packed dry snow Max 1/2” or 12.7mm slush, wet snow or standing water Half or less of above =1/4” slush t/o wat Greater than half of above = 1/2” t/o wat
39
Engine anti ice use AOM 1.01.30 P 1
OAT 10°c or less with visible moisture or contaminated surface Do not use above 10°c or below -40°c, or in flight with TAT exceeding 15°c
40
Minimum time from engine start to takeoff AOM 1.01.71 P 2
3 minutes
41
Maximum flap operation altitude AOM 45 1.01.27 P 1
20,000 feet
42
Maximum fuel imbalance AOM 1.01.28 P 2 FCTM 8.25
Fuel imbalance between main tanks for taxi, take-off and landing must not exceed: • 680 kg when total main tank fuel exceeds 30,980 kg. • 1133 kg when total main tank fuel is less than or equal to 19,005 kg. • A linear interpolation between 680 kg and 1133 kg when main tank fuel is less than or equal to 30,980 kg and greater than 19,005 kg, respectively. Simply for structural life in normal operations.
43
Maximum gear speed? AOM 1.01.32 P 1
270 kias/M.82
44
Maximum approved operating altitude AOM 1.01.90 P 1
43,100’
45
Crosswind limits AOM 45 1.01.90 P 1
-8 40kts t/o and 37kts ldg -9 33kts t/o and 40kts ldg
46
Maximum tire speed? QRH 18 PI-QRH.11.55/PI-QRH.21.55
Printed on tire sidewall? 204 kts normal? 226 kts non normal temp/weight chart limits
47
When is ATM reduced thrust take off prohibited? AOM 1.01.20 P 8
•Windshear •Known temp inversion below 1500’ agl •Residual slush, standing water, OR approx more than 25% snow or ice cover exists on 100’ centre line • prohibited jeppesen route manual • prohibited by MEL
48
When is a derate reduced trust takeoff prohibited AOM 1.01.20 P 8
If windshear conditions exist below 1,500’ AGL
49
Maximum cabin differential pressure AOM 1.01.21 P 1
9.9 psi
50
Maximum allowable cabin pressure for takeoff and landing AOM 1.01.21 P 1
0.11 psi
51
When must the autopilot be disengaged WITHOUT land2 or land3 annunciated? AOM 1.01.22 P 1
-8 Below 100’ agl -9 Below 135’ agl
52
When must the autopilot be disengaged WITH land2 or land3 annunciated AOM 1.01.22 P 1
Below 100’ on glideslope angles greater then 3.25°
53
What is the maximum glide path angle for use of auto pilot or flight director AOM 1.01.22 P 1
3.77°
54
When should centre fuel tank pumps be used? AOM 1.01.28 P 2
7,300 kg or more, or Fuel in center msg
55
Max flight instrument allowable deviations? AOM 1.01.31 P 1
+/- 4 kts +/- 10° Cpt vs fo 100’ Cpt or fo vs stby 200’ RVSM cpt vs fo field elevation 75’
56
Entry and cargo door wind limits AOM 1.01.52 P 1
40kts gusting 65kts at the door
57
Autoland wind limits? AOM 45 1.01.22 P 1
AC max CATii/iii crosswind 15kts -8 Hw 25kts Tw 15kts Xwind 25kts -9 Hw 25 kts Tw 10 kts Xwind 25kts
58
Maximum runway slope? AOM 1.01.90 P 1
+/- 2%
59
Maximum takeoff and landing altitude? AOM 1.01.90 P 1
-8 11,000’ * -9 14,000’
60
When are hydraulic system warm-up procedures required? AOM 1.01.90 P 1 AOM 1.04.18 P 7
Fuel temp is -20°c or lower, Or Ground ambient temp below -30°c for more then 4hrs in last 12hrs Note: If the fuel temperature is less than or equal to -17°C and if the electric hydraulic pump selectors are in the AUTO or OFF position for more than 10 min prior to engine hydraulic pump operation, notify maintenance personnel.
61
Max fuel loading error before advising load FOM 8.2.15.5
400kg
62
Pax count tolerance FOM 8.2.29
-8 +/- 10 -9 +/- 12 Adjust tow by 80kg per extra pax
63
Heavy weight landing weights? QRH normal P26
-8 200,000kg -9 215,000kg
64
One minute fuel increments? FOM 8.1.6.3
90kg/min in flight 22kg/min on ground
65
Etops diversion times and distances? AOM 45 1.01.20 P1 FOM 43 9.3.3
60min 458nm 75min 549nm 120min 878nm 139min 1010nm 180min 1317nm 207min 1515nm Distances are based on still air
66
Apu fuel burn on ground and 35,000 feet?
195kg/hr ground 120kg/hr FL350
67
How many minutes of cargo fire suppression available? AOM 45 2.26.20 P 5
240 minutes
68
RNP RF legs speed restrictions?
IAF/IF to FAF 250kts FAF/FAP to DA 165kts DA to missed hold 265 As published
69
Main wheel span AOM 2.20.10 P 1
38’4” -8 39’2” -9
70
Minimum pavement width for 180°turn AOM 2.20.10 P 3
138’ 4” -8 154’ -9
71
787 categories: Approach ARFF ICAO design TC/FAA group FOM 8.11.2 FOM 12.4.18.3 FOM 8.11.2
Approach D ARFF cat9 ICAO design E TC/FAA group 5
72
Break away power? AOM 1.04.04 P 1
35% N1
73
When is a slat drive operation check required? AOM 1.04.14 P 1
• the outside air temperature on the ground at the destination airport is 10°C or below, and operating on the ground with ice, snow, slush, or standing water or • an accumulation of airframe ice is observed or suspected (for example, indicated by wing anti-ice active during the approach).
74
Fuel capacity AOM 2.28.20 P 4
101,330 kg -8 101,451 kg -9
75
When would TOGA not be available to set take off thrust? AOM 45 2.22.20 P 13
- When the autothrottle is not active by 50 knots, it cannot be activated until above 400 feet. - or due to a 50 head wind component
76
Static wick count? MEL 38 23-61-01
- Wing 10 plus 2 on tip - Horizontal stab 8 plus 2 on tip - Vertical stab 7 plus 3 on tip
77
Ground wind engine operating envelope? AOM 45 1.01.71 P 1
- for crosswinds greater than 40 kt, limit thrust to a setting normally used for taxi (45% N1) - with a tailwind component greater than 5 kt and winds greater than 35 kt, limit thrust to a setting normally used for taxi (45% N1) - for winds greater than 55 kt, limit engine thrust to idle
78
After LOC and G/S capture, the localizer and glideslope modes can be deactivated by? AOM 45 2.22.20 P 2
- disengaging the autopilot and turning both flight directors off - selecting the go–around mode - if above 1,500agl, by reselecting APP (roll and pitch revert to default modes).

787 (3 decks)

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