Boeing 787 Exam Questions And Correct Answers 2024-2025
Minimum Fuel Tank Temperature
-28C or 3C warmer than fuel freezing point ( Based on bulletin ELA 48)
Runway slope
+/- 2%
Maximum TW component
15 kts
Maximum Operating Altitude
43,100 feet pressure altitude
Maxumum T/O and Landing alt
14,000' pressure altitude
Do not operate HF radios
while refueling
Max Demonstrated Crosswind
787-8 : T/O 40 kts, Land 37kts.
787-9 : T/O 33kts, Land 40 kts
Severe Turbulent Air Penetration Speed
290 kts Below 25,000'
310/0.84 mach at and above 25,000'
Wx radar
Avoid operating in a hangar and when personnel are within area enclosed by nose
radome
Max difference between Captain's or Fo's altitude and field elevation
75'
Maximum Taxi Weight
,787 - 9: 253,558 kgs
787 - 8: 228,383 kgs
Maximum Takeoff Weight
787 - 9 : 252,650 kgs
787 - 8: 227,930 kgs
Maximum Landing Weight
787 - 9 : 192,776 kgs
787 -8 : 172,365 kgs
Maximum Zero Fuel Weight
787 -9 : 181,436 kgs
787 -8 : 161,025 kgs
Minimum Autopilot Engagement Height
200' after takeoff
Maximum Autoland field elevation
8400'
Without LAND 2 or LAND 3 annunciated, the autopilot must not remain engaged below
787 - 9 : 135' AGL
787 - 8 : 100' AGL
With LAND 2 or 3 annunciated, for glideslope angles > 3.25 degrees
Auto pilot must be disengaged below 100' AGL
For glidepath angle > 3.77 degrees
Autopilot must be disengaged no later than 50' below DH/MDA
HUD TAKE OFF wind limitations
HW : 25 kts
TW: 15 kts
CW: 20 kts
Autoland wind limitations
, HW : 25 kts
TW: 15 kts
CW: 25 kts
Autoland capability may only be used with
Glideslope angles 2.50 - 3.25 degrees
Flaps setting at 20,25 or 30
2 engines or 1 engine inoperative
Land 2 or Land 3 must be announciated
Do not use FLCH on final approach below
1000' AFE
Use of Captain's or Fo's ACP to establish a SATCOM/cabin conference is
Prohibited
Minimum Oil Temperature for Start
-40 C
Reverse thrust limitations
*Intentional selection in flight prohibit
*Backing up the airplane with use of reverse thrust prohibited
Ground wind limitations
TW > 42 kts -> limit engines to taxi power
CW > 45 kts -> limit engine to taxi power
>65 kts -> do not run engines
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.
Maximum Flaps altitude
20,000 '
Maximum tank fuel temperature
Minimum Fuel Tank Temperature
-28C or 3C warmer than fuel freezing point ( Based on bulletin ELA 48)
Runway slope
+/- 2%
Maximum TW component
15 kts
Maximum Operating Altitude
43,100 feet pressure altitude
Maxumum T/O and Landing alt
14,000' pressure altitude
Do not operate HF radios
while refueling
Max Demonstrated Crosswind
787-8 : T/O 40 kts, Land 37kts.
787-9 : T/O 33kts, Land 40 kts
Severe Turbulent Air Penetration Speed
290 kts Below 25,000'
310/0.84 mach at and above 25,000'
Wx radar
Avoid operating in a hangar and when personnel are within area enclosed by nose
radome
Max difference between Captain's or Fo's altitude and field elevation
75'
Maximum Taxi Weight
,787 - 9: 253,558 kgs
787 - 8: 228,383 kgs
Maximum Takeoff Weight
787 - 9 : 252,650 kgs
787 - 8: 227,930 kgs
Maximum Landing Weight
787 - 9 : 192,776 kgs
787 -8 : 172,365 kgs
Maximum Zero Fuel Weight
787 -9 : 181,436 kgs
787 -8 : 161,025 kgs
Minimum Autopilot Engagement Height
200' after takeoff
Maximum Autoland field elevation
8400'
Without LAND 2 or LAND 3 annunciated, the autopilot must not remain engaged below
787 - 9 : 135' AGL
787 - 8 : 100' AGL
With LAND 2 or 3 annunciated, for glideslope angles > 3.25 degrees
Auto pilot must be disengaged below 100' AGL
For glidepath angle > 3.77 degrees
Autopilot must be disengaged no later than 50' below DH/MDA
HUD TAKE OFF wind limitations
HW : 25 kts
TW: 15 kts
CW: 20 kts
Autoland wind limitations
, HW : 25 kts
TW: 15 kts
CW: 25 kts
Autoland capability may only be used with
Glideslope angles 2.50 - 3.25 degrees
Flaps setting at 20,25 or 30
2 engines or 1 engine inoperative
Land 2 or Land 3 must be announciated
Do not use FLCH on final approach below
1000' AFE
Use of Captain's or Fo's ACP to establish a SATCOM/cabin conference is
Prohibited
Minimum Oil Temperature for Start
-40 C
Reverse thrust limitations
*Intentional selection in flight prohibit
*Backing up the airplane with use of reverse thrust prohibited
Ground wind limitations
TW > 42 kts -> limit engines to taxi power
CW > 45 kts -> limit engine to taxi power
>65 kts -> do not run engines
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.
Maximum Flaps altitude
20,000 '
Maximum tank fuel temperature
