Limitations (Aircraft General) Flashcards
The wingspan of the Challenger 300 is _____.
63 ft 10 in.
The wingspan of the Challenger 350 is _____.
69ft
_____ is the minimum pavement width for a 180° turn.
58 ft with a 5 ft safety margin
The Challenger 300 requires a wing tip clearance of _____ for a 180° turn.
95 ft 5 in.
The Challenger 350 requires a wing tip clearance of _____ for a 180° turn.
101 ft
While towing, the maximum rotational travel on each side of center of the nose gear is _____° without disconnecting the torque links.
120
The nose landing gear swivel pins might shear at a nose angle of _____.
beyond 123°
With torque links disconnected, _____ is the minimum nose gear strut extension required in order to rotate the nose gear beyond the travel limits.
3.5 inch
The main entry door is normally closed _____.
electrically, by inside switch or external switch
When the main entry door electric switch or door motor is inoperative, closing of the door is accomplished _____.
manually, by the ratcheting pull handle on the lower-left side of the door entry
On the ground, if an amber Cargo Door (caution) CAS message is displayed, it is because _____.
the cargo door is not fully closed, and the Left Engine switch is in RUN
In fight, if an amber Passenger Door (caution) CAS message is displayed, it is because _____.
the passenger door rollers are not fully en-gaged into fitting guides, door handle is not down and locked, or vent flap is not closed
On the ground, if an amber Passenger Door (caution) CAS message is displayed, it is because _____.
the door is not closed, and the Left Engine run
switch is placed to RUN
The purpose of the vent flap in the cabin door is to _____.
equalize cabin pressure before the door locks
are released
The 5 doors monitored by the door warning system.
Main Passenger
Emergency Exit
Cargo
Aft Equipment
Battery Bay
