747-400 Initial/Transition Systems Final Exam Questions with 100% Correct Answers
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Course
747-400 Initial/Transition Systems
Institution
747-400 Initial/Transition Systems
Where is Cabin ALT and Rate, Landing ALT, Differential Pressure indications located? Correct Answer Primary EICAS Display
What is the Temperature Range (C) for the Flight Deck? Correct Answer 18-29 degrees celsius
When do FMC's revert to Split IRS operation? Correct Answer Passing 84 degrees ...
747-400 Initial/Transition Systems Final
Exam Questions with 100% Correct Answers
Where is Cabin ALT and Rate, Landing ALT, Differential Pressure indications located?
Correct Answer Primary EICAS Display
What is the Temperature Range (C) for the Flight Deck? Correct Answer 18-29 degrees
celsius
When do FMC's revert to Split IRS operation? Correct Answer Passing 84 degrees
North or South
How many positive pressure relief valves are installed? Correct Answer 2 forward of the
left wing
The body gear will activate when speed decreases through 20 knots ground speed
Correct Answer False
Upon touchdown, what happens to the outflow valves? Correct Answer Open as
scheduled
How many Halon fire extinguishers are there? Correct Answer 3
EEC control switch, what are the modes? Correct Answer Normal and Alternate
How many fire bottles are in each wing? Correct Answer 2
What is the maximum altitude the APU can operate? Correct Answer None of the above
(15,000 ft air, 20,000 ft unloaded
The Maximum Crosswind Component for Autoland is: Correct Answer 25 knots
Flap lever movement from UP to Flaps 1 causes Correct Answer The INBOARD and
MID SPAN leading edge to extend and the trailing edge flaps to remain retracted
Which of the below occurs when an engine fire switch is pulled? Correct Answer Arms a
squib in each bottle (2 bottles)
To what altitude can the APU generator be used? Correct Answer It is not to be used in
flight.
, What is the maximum ground wind limit while a cargo door is open? Correct Answer 65
knots
The turbulent air penetration speed is Correct Answer 290 to 310 KIAS / 0.82 to 0.85
Mach, whichever is lower
The EICAS alert message BLEED is displayed for: Correct Answer All of the above
(-Engine bleed air overpressure
-HP bleed valve failed to close when commanded
-PRV failed to close when commanded)
When does Starter Cutout occur? Correct Answer 50% of N2
How is the APU STBY bus normally powered? Correct Answer Captain's Transfer Bus
What is the Maximum Landing Weight? Correct Answer 302,092 Kgs.
The RTO activates below 80 knots Correct Answer False
(85 kts)
The ALTN mode of the EEC provides thrust limiting Correct Answer False
What is the minimum oil pressure? Correct Answer 10 psi
What powers Emergency Lighting? Correct Answer Remote Batteries
What item is on the Main Standby Bus? Correct Answer Standby Ignition
The EICAS Alert message CONFIG is displayed in all the following except Correct
Answer Doors not closed and locked.
The Expanded Localizer Deviation Scale appears when: Correct Answer The airplane is
close to the localizer center line
What would cause the illumination of a generator DRIVE light? Correct Answer IDG low
oil pressure & IDG high oil temperature
What is the maximum allowable cabin differential pressure for takeoff and landing?
Correct Answer 0.11 psi
The Pitch Limit indication is displayed when flaps are not up Correct Answer True
What does the GEN OFF light indicate? Correct Answer Generator Control Breaker
open
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