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SOP's > Limitations > Flashcards

Limitations Flashcards

1
Q

What is the min oil temp for eng start?

A

-40

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2
Q

What is the temp limit for jet A

And Jet A1

A

Jet A -40

Jet A1 -47

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3
Q

What is the MLW

A

172,365 kg

192,776

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4
Q

What is the wing length

A

197’ 3”

60.1 M

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5
Q

When cross checking waypoints with the OFP what is the tolerance for deg and distance?

A

1 degree and 2 nm

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6
Q

What is the climb speed targeted by TOGA Switch

A

2,000 fpm

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7
Q

What g forces are created with bank angle’s

A
  1. 1 G = 25 deg
  2. 3 G = 40 deg

2 G = 60 deg bank

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8
Q

During RTO when is A/T going to advance the thrust levers

A

Before 80/HOLD it will try to reset T/O thrust

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9
Q

When does auto-braking occur for RTO

A

> 85 kts

The RTO autobrake setting commands maximum braking pressure if:
the airplane is on the ground , and
groundspeed is above 85 knots, and
both thrust levers are retarded to idle

Maximum braking is obtained in this mode. If an RTO is initiated at or below 85 knots, the RTOautobrake function does not operate.

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10
Q

What is the turbulence penetration speed

A

290 < 25,000 ft
310/.84 >= 25,000 ft

PASS SIGNS ON

Climb/desk avoid VNAV or FLCH use VS
Cruise use VNAV or ALT may discon A/T
Set N1 to magenta line if required

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11
Q

What are the crew O2 requirements?

Where can you find this?

A

2 crew - 480 psi (660 L)
3 crew - 700 psi (990 L)
4 crew - 860 psi (1320 L)

(Time at 14,000 ft for each is 2 hrs)

AOM 1
Pg 1.01.35

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12
Q

What are the weight limitations for the 787-9

A

Fin 831-859/ 860-861

Max Taxi Weight - 254,692 KG / 255,372
Max T/O Weight - 254,011 / 254,692
Max Landing WT - 192,776 / 192,776
Max Zero Fuel WT -181,436 / 181,436

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13
Q

What are the weight limitations for the 787-8

A

Max Taxi Weight - 228,383 KG
Max T/O Weight - 227,930
Max Landing WT - 172,365
Max Zero Fuel WT -161,025

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14
Q

What is the flight maneuvering load limits flaps up and flaps down

A

Flaps Up: +2.5g to -1.0

Flaps Down: +2.0g to 0g

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15
Q

What is the max diff press?

Max Diff pressure on TO/Landing?

A

9.9 psi relief valves

0.11psi

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16
Q

What is the limitations for ATM

Assumed thrust method

A

Contaminated runway

Windshear below 1,500

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17
Q

What is the restriction for reduced thrust take off

TO1 TO2

A

Windshear below 1,500

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18
Q

What is the limit for autoland

Not wind limits

A

Not allowed on runways =/<8,400

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19
Q

What are the autoland wind limits for headwind, crosswind, tailwind

A

25 kts head
25 kts cross
15 kts tailwind

10 kts tail for -9

The rest are the same

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20
Q

What is the single engine airspeed

Used to calculate etops distances

A

330 kts

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21
Q

What is the min altitude for speed brake deployment

A

800 ft

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22
Q

What is the min/max fuel temp for take off

Min cruise temp

A

Ground -29/+49

3 degrees above freezing point (-40 jet A, -47 Jet A1)

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23
Q

What is the max fuel imbalance

A

.68 > 30.9 (30,980 kg)

1.13 < 19.0 (19,005 kg)

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24
Q

What is the a limitation on jettison fuel

A

[801-803]
Do not jettison fuel at Flaps 20, 25, or 30.

[804-808, 787-9]
Do not jettison fuel at Flaps 30.

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25
Q

What is the limitation of eng and wing anti ice

A

Eng
10 deg Air
10 on the ground

Wing
25 deg Air

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26
Q

On the ground or in flight what’s the max allowable difference in airspeed?

A

+/- 4

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27
Q

What’s the max allowable altitude difference on the altimeter?

A

100 ft CA-FO

200 ft CA/FO vs Stby

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28
Q

What are the RVSM limits for the altimeter

A

75 ft max difference between CA-FO’s altimeter on the ground prior to take off

(The standby altimeter does not meet RVSM altimeter accuracy requirements)

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29
Q

What is the VLO/VLE

A

270 M.82

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30
Q

What is the limitation on approaches for temp comp

A

Instrument approach operations are prohibited, unless altitude corrections are applied when the temperature at the landing elevation is below ISA.

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31
Q

What is the max oil temp

Continuous and 15 min limit

A

160 deg

177 deg

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32
Q

What is the limitation for go around when landing

A

Once reverse selected you can no longer go around

Backing the airplane up with reverse thrust is prohibited

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33
Q

What is the ground wind operating envelope

A

N1 >45 % prohibited when:

> 40 kt crosswind

> 5 kt tailwind

> 35 kt winds

No more than idle when
> 55 kts

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34
Q

What is the Engine RPM maximum operational limits

A

N1 - Low Pressure Compressor Rotor 108.5%

N2 - High Pressure Compressor Rotor 117.5%

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35
Q

What is the EGT temp limit for engine start on the ground

A

EGT 750 degrees C

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36
Q

What is the max DEMONSTRATED wind limits for take off and landing

A
  • 8 40 kt T/O 37 kts Ldg (gust included)
  • 9 33 kt T/O 40 kts Ldg (gust included)

These speeds are demonstrated and are not limiting
CP info 18-01)

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37
Q

What is the maximum approved operating altitude

What is the maximum take-off and landing altitude

A

43,100 ft

14,000ft

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38
Q

What is the max slope

A

+/- 2 %

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39
Q

What are the cold weather operation limits

A

ground ambient temperature below -30°C for a period exceeding 4 hours in the preceding 12 hours

(unless warm-up procedures are followed below -20°C)

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40
Q

What are the definition of a damp runway and how do we treat it?

A

A runway is considered to be damp, when it has a moisture layer that is non reflective.

A damp runway is considered to be wet.

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41
Q

When is a runway considered wet?

When do we treat trace and frost as a contam, and what contam

A

A runway is considered to be wet, when it appears reflective.

Reported TRACE contamination shall be considered as equivalent to WET if the coverage is more
than 25% of the area to be used.

Reported FROST runway condition shall be considered as equivalent to WET if the coverage is more than 25% of the area to be used.

42
Q

For contaminated runway what width is required

A

100ft

43
Q

What are the limitations for contamination

Slush, Wet Snow, Standing Water

Packed dry snow

Light Dry Snow

A

> 1/2 in of Slush, Wet Snow or Standing Water

> 2 in of packed dry snow

> 4 in Light Dry Snow

44
Q

How much fuel can we jettison per min

A

2,000kg per min

45
Q

What are the new holding speeds for Canada

A

holding patterns must be entered and flown at or below the following
At or below 6000 feet 200 KIAS

Above 6000 feet up to and including 14000 ft
230 KIAS

Above 14000 feet 265 KIAS

(Shuttle climbs (All altitudes) 310 KIAS)

46
Q

What types of precipitation do we have limitations for take off and landing?

A

FOM 10.6.5.1 Take-Off Restrictions Take-offs are not authorized in:

  1. Hail
  2. Heavy ice pellets
  3. Moderate or heavy freezing rain

Landing Restrictions
Landings are not authorized in moderate or heavy freezing rain.

47
Q

How many passenger seats do we have for -8

A

255

As of may 20th

48
Q

What is the max range for 787

A

7850nm

8300nm

49
Q

In Europe you can get 280 kts below 10,000 can we do it

A

Yes if assigned by ATC

From bulletin

50
Q

How can you estimate fuel required for trip

A

EET X5

8 hr X5 = 40.0 kg

TW means tail wind

51
Q

When do we require a T/O alternate

A

< 2600 RVR or 1/2 sm

Below landing minima

52
Q

What is the T/O alternate distance for the 787

-8/-9

A

60 min
Trick question, consolidated in FOM 34

-8/-9
60min. 377 nm
120(etops) 754 nm

(120 min is just double the 60)

In still Air calculated at 330 kts

53
Q

What is the fuel consumption in KG for flight and taxi per min

A

Flight 90 KG

Taxi 22 KG

54
Q

What is the operating min cabin crew

A

5

> 200 - 6
240 - 7
280 - 8

55
Q

What are the designate fuelling emergency exits

A

L1 and/or L2 + L4

56
Q

Adjustments to the TOW figure may be made by the Flight Crew without advising the load agent provided the fuel loading error is less than what for 787

A

400 KG

57
Q

What is the passenger count tolerances for

Zone

and

Total

A

No zone tolerance

  • 8 = +/- 10
  • 9 = +/- 12
58
Q

In Canada what approach category is the 787?

A

Cat D (141-165)

59
Q

Outside Canada what approach category is the 787?

What is it based on?

A

Cat D

Based on stall speed at landing config at max weight

60
Q

What is the airplane design group FAA and design code ICAO?

FAA

ICAO

How is it determined?

A

FAA group V (Wingspan/height)

ICAO group E (wingspan/main gear span)

61
Q

What is the optimum ARFF capability for 787

A

CAT 9

62
Q

What is the restrictions for EFB’s

A

No P-EFB required if 2 class 3 installed EFB’s

If only 1 class 3 installed EFB then 1 P-EFB is required

63
Q

When can we use the t/o alternate of 2 hrs

A

If aircraft is etops approved

(ETOPS approved twin-engine aircraft means that the aircraft
type is approved and capable of ETOPS for the flight, and an ETOPS Service check was completed for the flight)

64
Q

How do you convert KMS to kts

A

Divide KMH by 2 to approximate knots (e.g., 14 KMH = 7 knots).

65
Q

How do you convert MPS to kts

A

Double the value in MPS to approximates knots.

(e.g., 6 MPS = 12 knots),

66
Q

What is the weight limit for discrepancy between estimated WT and actual WT

A

-5,000 lbs

67
Q

What is economy climb speed?

A

< 10,000 ft. 250kt or Vref30 +80 which ever is higher

> 10,000 ft. 320 or M 0.85

68
Q

What is max rate climb speed?

A

Vref30 + 140 until intercepting M 0.82

69
Q

What is the procedure in the ground in icing conditions for oil temps?

A

3 - deg
4 - 40% N1
5 - sec
6 - 60 min

70
Q

What do the trend arrows indicate for airspeed and altitude?

A

A/S - speed in 10 sec

Alt - altitude in 6 sec

71
Q

PWS provides windshear alerts when an excessive windshear condition is detected ahead of the airplane

What are the dimensions of the PWS (predictive windshear )

A

PWS alerts are enabled below 1,200 feet radio altitude.

Warnings provided:

On ground 3 nm 30 deg either side (60 total)

Airborne 1.5 nm 30 deg either side

(WXR begins scanning below 2,300 ft)

72
Q

How can you set up a conference call between STATMD and Incharge FA?

A

On radio #3

CAB ON and MIC on
STAT 1 ON and MIC on

(Use of the Captains or First Officers ACP to establish a SATCOM / cabin conference is prohibited)

73
Q

How can you calculate the min hydroplaning speed?

A

The minimum speed, in knots,at which hydroplaning will commence can be calculated by multiplying the square root of the tire pressure (psi) by 9 for a rotating tire.

74
Q

When do you get a FUEL QUANTITY LOW EICAS message

A

Right or left main tank drops below 1,700 kg

4,000 kg (4.0)

This EICAS message will appear any time either left or right main tank drops to approximately 1700 kg. The additional 300 kg per tank is to account for any possible Fuel Imbalance.

If additional fuel isrequired to meet the 4000 kg requirement, the extra fuel will appear as SUPP on the OFP.

75
Q

What pitch gives you a tail strike on take off

A
  1. 2 for -8

9. 7 for -9

76
Q

What is the stabilized approach criteria

1,000 ft

500 ft

A

At 1000’ AAE the aircraft must be on correct lateral and vertical path and landing configuration (AOM) (final landing flap selected FOM)

At 500’ AAE, airspeed +10/-5, thrust stable, not more than 1000’/min, landing checks complete.

77
Q

What pitch gives you a tail strike on landing?

A

Tail strike at about 9 (-8) 7.5 (-9) degrees, struts compressed.

FCTM 8.24-27 for tailstrike avoidance technique.

78
Q

What is the minimum flying for currency for a RP?

A

In the previous 90 days one of:

  • A minimum of 5 sectors assigned to duty as a flight crewmember;
  • • A simulator LOFT Recency exercise plus one sector assigned to duty as a flight crew member; or
  • • An MT/LOFT or MTV/LOE.
79
Q

When do we have to turn the center fuel pumps on?

A

> 7.3

80
Q

What is the average APU fuel burn

A

195 kg/h average APU fuel burn on the ground.

81
Q

What is the representative surface of the 787

A

leading edge of slat to trailing edge of flap between the engine pylon and the evacuation walkway on the right hand side is the representative surface

82
Q

What is the distance we travel in 10 min for fix purposes

A

80 nm

83
Q

How often do we have to do a fuel check?

A

90 min

84
Q

Is air Canada allowed to conduct LAHSO ?

A

Not In the USA

85
Q

What is the requirements for operating Lav

A

1 lav per 55 people >9 hrs

300 people need 6 lavs out of 8

86
Q

In the QRH what does a bold upper case item mean

LOSS OF ALL DISPLAYS

Lower case?

Stabilizer

A

Unannunciated quick reference item

EICAS item

87
Q

How do you enter a time on the ND

A

Fix page under ETA-ALT

2345z

(Don’t forget the Z)

88
Q

What is the new (Oct 17 2018) distance for etops alternates at 330 kts

60 min

120 min

180 min

A

60 min - 458 nm

120 min - 878 nm

180 min - 1317 nm

(We are now using one distance for -8 and -9, and it uses a statistical average using average of
reference weights for flights when operating in the planned ETOPS area was used instead of t/o weight minus 1 hr

89
Q

What are the dimensions range of the TCAS?

A

+2,700 to -2,700 ft Norm

+2,700 to -9900 ft Below

90
Q

When is GA mode armed?

A

When flaps are extended (out of up position)

OR

GS is captured

91
Q

When auto throttle is inop, what is the procedure for setting target airspeed for a manual landing?

A

If a manual landing is planned with autothrottle disconnected, it is
recommended to add up to a maximum of VREF+15:
• 50% of the steady headwind component plus,
• Full gust

92
Q

What is the difference in NAIFR in Canada and USA

A

In USA the req is only

+/- 1hr
Ceiling 2000, VI’s 3 sm

Canada
1500 and 6 sm
100 above 2nd lowest FAF and 3 sm
No fog
Freezing precip
Or CB

2 separate runways
2 different approaches
1 runway wet landing distances

93
Q

Aft CG configurations require additional considerations to accommodate
the effects of reduced nose gear steering effectiveness.
What is the limit on aft C of G (%MAC)

A

Refer to the aft CG take-off chart when the gross weight CG (%MAC) is at
or aft of:
• 25.3 on the 787-8, or
• 23.1 on the 787-9

94
Q

Aft CG configurations require additional considerations to accommodate the effects of reduced nose gear steering effectiveness aft of:

A
  • Refer to the aft CG take-off chart when the gross weight CG (%MAC) is at
    or aft of:
  • 25.3 on the 787-8, or
  • 23.1 on the 787-9
95
Q

What is the procedure for engine start?

A

Check EICAS
“Starting right and left engines”

“Right and left engines running”

After engine start, the First Officer shall
check that the generator OFF lights on
the electrical panel are extinguished.
• If a generator OFF light is illuminated,
maintenance action is required.

96
Q

What is TAP

A

Thrust Asymmetry protection

Reduces thrust when airspeed is below V2 on takeoff.
For an eng out condition TAP reduces thrust on the operating eng to ensure sufficient rudder for directional control

97
Q

What do we have to remember when turning on the anti-ice on the ground during ground operations.

A

Confirm that “EAI” is shown on the primary engine display for both engines

98
Q

What is the crosswind limitation for wet runways?

A

25 kts

QRHN

99
Q

What is the max take off altitude for the -8 and -9?

A

[787-8]
The maximum take-off and landing altitude is 11,000 ft pressure altitude. The AFM landing limit is 14,000 ft pressure altitude but has been restricted to 11,000 ft pressure altitude due to the takeoffpressure altitude limitation.

[787-9]
The maximum take-off and landing altitude is 14,000 ft pressure altitude.

100
Q

What is the cold weather operation limit?

A

has been exposed to a ground ambient temperature below -30° C for a period exceeding 4 hours in the preceding 12 hours or if fuel temperature is - 20° C degrees or lower, unless hydraulic system warm-up procedures

101
Q

How do we treat a runway:
When it has a moisture layer that is NON reflective.

When it is covered with sufficient moisture to cause it to appear reflective.

Reported TRACE contamination

Reported FROST runway condition

A

When it has a moisture layer that is non reflective is considered to be damp, A damp runwayis considered to be WET

When covered with sufficient moisture to cause it to appear reflective, it is considered WET

Reported TRACE contamination shall be considered as equivalent to WET if the coverage is more than 25% of the area to be used.

Reported FROST runway condition shall be considered as equivalent to WET if the coverage is more than 25% of the area to be used.

(AOM 1 Limitations)

SOP's (7 decks)

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