Memory Limitations

Question 1

Max Operating Pressure Altitude
(787-8, 787-9)

Answer 1

43,100 feet

Question 2

Max Operating Pressure Altitude
(787-10)

Answer 2

41,100 feet

Question 3

Max Takeoff and Landing Tailwind Component

Answer 3

15 knots

Question 4

Turbulent Air Penetration Speed
Severe Turbulence at or above 25,000 feet

Answer 4

310 knots/ .84 mach which is lower

Question 5

Turbulent Air Penetration Speed
Severe turbulence below 25,000 feet

Answer 5

290 knots

Question 6

Takeoff Crosswind Component
>430,000 lbs Dry Rwy, CG < 20

Answer 6

40 knots

Question 7

Takeoff Crosswind Component
350,000 lbs Dry Rwy, CG < 20

Answer 7

40 knots

Question 8

Takeoff Crosswind Component
< 270,000 lbs Dry Rwy, CG < 20

Answer 8

40 knots

Question 9

Landing Crosswind Component
RWY Dry

Answer 9

40 knots

Question 10

AUTOFLIGHT LIMITATIONS
Autopilot/ Flight Director System
(5)

Answer 10

1. Do not engage the autopilot below a minimum altitude of 200 feet AGL after takeoff.
2. Auto land capability may only be used for operations to runways at or below 8,400 airport field elevation.
3. Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged above 135feet AGL.
4. With LAND 2 or LAND 3 annunciated and glidepath angles greater than 3.25, the autopilot
   must be disengaged above 100 feet AGL.
5. Do not use FLCH on final approach below 1000 feet AFE

Question 11

Max wind component Low Vis HUD Takeoff

Answer 11

Headwind 25 knots
Tailwind 15 knots
Crosswind 15 knots

Question 12

SA CAT I Approach Max Crosswind

Answer 12

15 knots

Question 13

ILS Automatic Landing Max Glideslope Angle

Answer 13

3.25

Question 14

ILS Automatic Landing Min Glidepath Angle

Answer 14

2.5

Question 15

Communication/Fueling Limitation

Answer 15

Do not operate the HF radio during fueling operations

Question 16

Minimum Oil Quantity Prior to Start

Answer 16

18 quarts

Question 17

Minimum Oil temp prior to start

Answer 17

The oil temp must be greater than -40C for engine start

Question 18

Reverse Thrust Limitations

Answer 18

1. Intentional selection of reverse thrust in flight is prohibited
2. Backing the plane with use of reverse thrust is prohibited

Question 19

Control Inputs

Answer 19

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA