OMA

Question 1

Turbulent Air Penetration Speed

Below 25,000

Answer 1

290 KIAS

Question 2

Turbulent Air Penetration Speed

25,000 and above

Answer 2

310 KIAS/.84 Mach which ever is lower

Question 3

TUIA - G-TUII, OO-JDL - PH-TFM

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

Answer 3

100 ft agl

Question 4

G-TUIJ - G-TUIM

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

Answer 4

135 ft agl

Question 5

Maximum Takeoff and Landing Tailwind Component

Answer 5

15 knots

Question 6

The autopilot must not be engaged below which minimum engage altitude after takeoff

Answer 6

200 feet AGL

Question 7

Do not use FLCH on final approach below what height?

Answer 7

1,000 feet AFE

Question 8

With LAND 2 or LAND 3 annunciated and glideslope angles greater than ?.?? degrees, the autopilot must be disengaged below what height?

Answer 8

3.25 degrees

100 feet AGL

Question 9

If the glidepath angle for approach is greater than ### degrees, the autopilot must be disengaged no later than ### feet below DH/MDA

Answer 9

3.77

50

Question 10

Do not use FLCH on final approach below ### feet AFE

Answer 10

1,000

Question 11

Low weather minima (below 125m) takeoff may only be performed #####

Answer 11

using ILS guidance

Question 12

Low Visibility (HUD) Takeoff wind limits

Answer 12

Headwind 25 knots
Tailwind 15 knots
Crosswind 20 knots

Question 13

Automatic Landing

Maximum wind component speeds

Answer 13

Headwind 25 knots
Tailwind 15 knots
Crosswind 25 knots

Question 14

Automatic Landing maximum glideslope angle

Answer 14

3.25 degrees

Question 15

Automatic Landing minimum glideslope angle

Answer 15

2.5 degrees

Question 16

Oil temperature for engine start

Answer 16

Greater than -40° C

Question 17

Intentional selection of reverse thrust in flight

Answer 17

Prohibited

Question 18

Backing the airplane with use of reverse thrust

Answer 18

Prohibited

Question 19

When is using HF radios prohibited?

Answer 19

When refuelling

Question 20

The center tank may contain up to ### kilograms of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed.

Answer 20

10,000

Question 21

Prior to takeoff the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is # feet.

Answer 21

75

Question 22

Runway slope maximum

Answer 22

+/- 2%

Question 23

Minimum Runway Width

Answer 23

Takeoff 45m; Landing 36m

Question 24

Avoid weather radar operation

Answer 24

In a hangar
Within 15.25 meters of fueling operations or a fuel spill. When personnel are within the area normally enclosed by the aircraft nose radome.

Question 25

787-8 MTW

Answer 25

228,383

Question 26

787-8 MTOW

Answer 26

227,930

Question 27

787-8 MLW

Answer 27

172,365

Question 28

787-8 MZFW

Answer 28

161,025