Limitations

Question 1

ETOPS

The approved one-engine-inoperative cruise speed is ___ KIAS

Answer 1

330 KIAS

Question 2

ETOPS

Maximum diversion times and distances:
60 minutes 458 nm
75 minutes 549 nm
120 minutes 878 nm
138 minutes 1010 nm
180 minutes 1317 nm
207 minutes 1515 nm

Answer 2

60 minutes 458 nm
75 minutes 549 nm
120 minutes 878 nm
138 minutes 1010 nm
180 minutes 1317 nm
207 minutes 1515 nm

Question 3

B787-8

Maximum Taxi Weight ________kg

Maximum Take-off Weight ________

Maximum Landing Weight ________

Maximum Zero Fuel Weight ________

Answer 3

B787-8

Maximum Taxi Weight 228,383 kg

Maximum Take-off Weight 227,930

Maximum Landing Weight 172,365

Maximum Zero Fuel Weight 161,025

Question 4

B787
FINs 831-859

Maximum Taxi Weight ________kg

Maximum Take-off Weight ________

Maximum Landing Weight ________

Maximum Zero Fuel Weight ________

Answer 4

B787
FINs 831-859

Maximum Taxi Weight 254,692kg

Maximum Take-off Weight 254,011

Maximum Landing Weight 192,776

Maximum Zero Fuel Weight 181,436

Question 5

B787
FINs 860-861

Maximum Taxi Weight ____kg

Maximum Take-off Weight ____

Maximum Landing Weight ____

Maximum Zero Fuel Weight ____

Answer 5

B787
FINs 860-861

Maximum Taxi Weight 255,372kg

Maximum Take-off Weight 254,692

Maximum Landing Weight 192,776

Maximum Zero Fuel Weight 181,436

Question 6

787-8

Below 10,000 MSL, maximum indicated airspeed is ___ knots unless required to be exceeded in emergency.

Note: Applicable to 787-8 aircraft with 2Ku Taurus Antenna fitted with flight deck placard.

Answer 6

787-8]

Below 10,000 MSL, maximum indicated airspeed is

250 knots

unless required to be exceeded in emergency.

Note: Applicable to 787-8 aircraft with 2Ku Taurus Antenna fitted with flight deck placard.

Question 7

Airspeed Unreliable

When operating under conditions where AOA Airspeed is used and the 250 kt maximum airspeed red barber pole displays on the PFD airspeed tape, the 250 kt maximum indication should be disregarded and the maximum airspeeds are as follows:

ALTITUDE (FT) MAXIMUM SPEED (KIAS)

Above 40,000 ____KIAS
38,001 to 40,000 ____
35,001 to 38,000 ____
At or below 35,000 ____

Answer 7

Airspeed Unreliable

When operating under conditions where AOA Airspeed is used and the 250 kt maximum airspeed red barber pole displays on the PFD airspeed tape, the 250 kt maximum indication should be disregarded and the maximum airspeeds are as follows:

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

Question 8

Assumed Temperature Method (ATM) Reduced Thrust Take-off

ATM Reduced thrust take-off is always used except when:

• ___________
• ___________
• ___________
• ___________

Answer 8

ATM Reduced thrust take-off is always used except when:

• windshear or known temperature inversion below 1500 ft AGL.

• residual slush, extensive standing water (pooled), or more than approximately 25% snow or ice cover exists on the center 100 ft of the runway.

• ATM reduced thrust take-off is prohibited by Jeppesen Route Manual.

• ATM reduced thrust take-off is prohibited by MEL Manual.

Question 9

Derate Reduced Thrust Take-off

Derate reduced thrust take-off (i.e., TO1 and TO2) is prohibited if ___________

Answer 9

Derate reduced thrust take-off (i.e., TO1 and TO2) is prohibited if:

-windshear conditions exist below 1500 ft AGL.

Question 10

Cabin Pressure

Maximum differential pressure (relief valves): _______

Maximum allowable cabin pressure differential for take-off and landing: _______

Answer 10

Maximum differential pressure (relief valves):

9.9 psi

Maximum allowable cabin pressure differential for take-off and landing:

0.11 psi

Question 11

Autopilot/Flight Director System

The autopilot must not be engaged below a minimum engage altitude of _____’ AGL after take-off.

Answer 11

The autopilot must not be engaged below a minimum engage altitude of

200 ft AGL

after take-off.

Question 12

Autopilot/Flight Director System

[787-9]

When in direct or secondary flight control mode and flaps are extended, do not __________________________________________.

Answer 12

[787-9]

When in direct or secondary flight control mode and flaps are extended, do not:

-follow the Flight Director pitch guidance when operating in FLCH Pitch mode.

Question 13

Autopilot/Flight Director System

Autoland capability may only be used for operations into runways at or below ______’ airport field elevation.

Answer 13

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

8400 ft

airport field elevation.

Question 14

Autopilot/Flight Director System

[787-8]

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below _____ ft AGL.

Answer 14

[787-8]

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below

100 ft

AGL.

Question 15

Autopilot/Flight Director System

[787-9]

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below ______ ft AGL.

Answer 15

[787-9]

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below

135 ft

AGL.

Question 16

Autopilot/Flight Director System

With LAND 2 or LAND 3 annunciated and glideslope angles greater than _____ deg, the autopilot must be disengaged below _____ ft AGL.

Answer 16

With LAND 2 or LAND 3 annunciated and glideslope angles greater than

3.25 deg,

the autopilot must be disengaged below

100 ft

AGL.

Question 17

Autopilot/Flight Director System

Use of the Autopilot Flight Director System (autopilot coupled or using flight director guidance) at facilities with a final approach glide path angle greater than ____ degrees is prohibited.

Answer 17

Use of the Autopilot Flight Director System (autopilot coupled or using flight director guidance) at facilities with a final approach glide path angle greater than

3.77 deg

is prohibited.

Question 18

Autopilot/Flight Director System

Do not use FLCH on final approach below ______’ AFE.

Answer 18

Do not use FLCH on final approach below

1000’ AFE.

Question 19

Maximum wind component speeds when landing weather minima are predicated on autoland operations:

[787-8]

Headwind ____ kt

Tailwind ____ kt*.
* For CAT II, SA CAT II and CAT III tailwind is limited to ___ kt.

Crosswind ___ kt**
**Air Canada crosswind limitation is ____ knots in CAT II, SA CAT II and CAT III conditions.

Answer 19

[787-8]

Headwind 25 kt

Tailwind 15 kt (10 KT - CAT II, SA CAT II and CAT III).

Crosswind 25 kt (AC limit 15 knots in CAT II, SA CAT II and CAT III conditions)

Question 20

Autoland

The maximum and minimum glideslope angles are _____° and ____°, respectively.

The autoland capability may be used with flap __, __, or __, with ____ engines operative.

The Autopilot Flight Director System (AFDS) autoland annunciation must have _______________ displayed.

Answer 20

Autoland

The maximum and minimum glideslope angles are
3.25° and 2.5°.

The autoland capability may be used with
flap 20, 25, or 30, with
BOTH engines operative or with ONE engine inoperative.

The Autopilot Flight Director System (AFDS) autoland annunciation must have
LAND 2 or LAND 3
displayed.