KV SKYWEST EXAM QUESTIONS WITH 100% VERIFIED ANSWERS

KV SKYWEST EXAM QUESTIONS WITH 100% VERIFIED
ANSWERS 2024-2025


1 - CRJ 200 memory item: - ANSWER HOT START, INTERRUPTED START,
N2 STAGNATION.
Affected Thrust Lever..................Shutoff
IGNITION...........................................OFF

Dry Motor.................................. UNTIL ITT is dropped to 120°C, while following
the starter time limit.

Stop the affected engine.


2 - CRJ 200 memory item: ANSWER NO LIGHT OFF

Shut off the affected thrust lever.

IGNITION...........................................OFF

Dry motor till the startup time restriction.

Affected Engine........................... STOP


CRJ 200 memory item: ANSWER DOUBLE ENGINE FAILURE.

IGNITION, CONTINUATION, ON

Airspeed: at least 240 KIAS.


CRJ 200 stabilizer trim runaway memory item: ANSWER STABILIZER TRIM
RUNAWAY.

Assume manual control and override the runaway.

STAB TRIM DISC: PRESS, HOLD, and RELEASE.

,Transfer airplane control to the pilot's (left) side.

STAB CH 1 and CH 2 HSTCU circuit breakers.

OPEN (2F5 and 4A1).


Excessive asymmetry or loss of braking memory item: - ANSWER DURING
LANDING -

Release the wheel brakes temporarily.

ANTI-SKID........................................OFF

Reapply the brakes as needed.


What is the starting time limit? - Answer in 60 seconds.

What indicators would be seen when the light was turned off? - Answer: ITT will
not grow.


How do these indicators vary from N2 stagnation? - ANSWER During N2
stagnation, N2 will progressively build and then stagnate.


Why do you reach the starter time limit during a No Light Off? To guarantee that
fuel has been motored out of the engine.


Where's the STAB TRIM DISC? - ANSWER At the rear of the control wheel


Why are the controls moved to the pilot's (LH) side? - ANSWER Because both
circuit breakers are on the right side.


Where is the anti-skid switch? - ANSWER: Upper centre pedestal, left side.

,What happens if the brakes are reapplied heavily? - Answer: The brakes would lock
up.


What is the maximum takeoff weight of the CRJ 200? - ANSWER: 53,000 pounds


- ANSWER


What is the maximum takeoff weight of the CRJ 200? - ANSWER 53,000 pounds.


What is the maximum zero-fuel weight of the CRJ 200? - ANSWER 44,000
pounds.


What is the maximum landing weight of the CRJ 200? - ANSWER 47,000 pounds.


Where can the maximum aft cargo weight be found? - ANSWER Regarding the
release


What is the maximum altitude for the CRJ 200? - ANSWER FL370


What is the VMO for the CRJ 200? - Answer: 335 KIAS.


What is MMO on the CRJ 200? - ANSWER: 0.85 M


What is the CRJ 200's minimum spoiler speed? - ANSWER Approach speed: +20
knots


What is the maximum wiper speed for the CRJ 200? - Answer: 220 KIAS.

, What are VFO flaps 8 on the CRJ 200? - ANSWER 200 KIAS


What is the maximum runway contamination depth for dry snow while landing the
CRJ 200? - Answer: 3.75 inches.


What is the maximum altitude authorized for single-pack operations in the CRJ
200? - ANSWER FL 250


What is the CRJ 200 APU's maximum altitude for bleed air use? - Answer: 15,000
feet.


What is the fuel capacity of the CRJ 200? - ANSWER Pressure: 14,518 pounds

Gravity: 13,906 pounds.


What constraints apply while leaving with fuel in the center tank? - ANSWER A.
Takeoff with more than 500 pounds of gasoline in the middle tank is not allowed
unless:

I. Each main wing tank weighs about 4400 pounds: or

II. Each main wing tank weighs about 2000 pounds, and:

_____1. The weight of the fuel in the center tank exceeds 500 pounds, which
reduces the permitted zero fuel weight:

_____2. - The permitted CG in the configuration is confirmed to be within the
acceptable CG envelope.



b. Alternative fuel loading procedure: When there is fuel in the center tank and the
two main tanks are not full, the allowable fuel load must be determined using
Fliteview.