AVT 417 Procedures and Limitations Quiz

During landing, application of reverse thrust is not permitted under

60 kts

Maximum airport pressure altitude for takeoff and landing is

10,000 ft

What is the maximum taxi and ramp weight of the CRJ 200

53,250 lbs

Reduced thrust cannot be used if the normal takeoff fan speed is less than

85% N1

For precision approaches (PAR or ILS), the minimum autopilot use height is

80 ft AGL

The maximum speeds at which the flaps may be extended are (flaps to 30 degrees)

185 KIAS

Maximum airspeed to operate windshield wipers is

220 KIAS

Maximum airspeed with the landing gear extended and locked is

250 KIAS

(T/F) Powered crossflow and gravity crossflow must be on for takeoff

False

During taxi, takeoff, and landing, the pressure differential must not exceed

0.1 PSI

When the low pressure air ground connection is used, the ____ must be open

Main cabin door

Flight spoilers must not be extended in flight below an altitude of _____ ft AGL

1,000

Upon departure from a wet or contaminated runway, when the SAT falls below 0 degrees C during a climb, the ailerons must be operated manually every _____ feet until the top of the climb

5000

Flight with flaps extended at altitudes above _____ feet is prohibited

15,000

Avoid unnecessary and large _____ maneuvers during low speed operations

Side-slip

Maximum airspeed for turbulence penetration is ______ KIAS or _____ Mach, whichever is lower

280/.075

Maximum airspeed to extend the landing gear is

250 KIAS

(Engine operating limitations) Core RPM N2% at idle

56.5 to 68.0

(T/F) The maximum runway slopes approved for takeoff and landing are: Uphill 2% and Downhill -2%

True

The ______ anti-ice system must be on for takeoff when the OAT is 5 degrees C (41 F) or below and the runway is contaminated with surface snow, slush, or standing water.

Wing and cowl

To ensure adequate maneuver margins, flight spoilers must not be extended in flight at airspeeds below the recommended approach/maneuvering speeds plus

17 KIAS

For visual and non-precision approaches, the minimum autopilot use height is ____ feet AGL

400

The maximum airspeed to retract the landing gear is

200 KIAS

Maximum ambient air temperature for takeoff and landing is

ISA +35

Maximum allowable crosswind component during takeoff or landing on a contaminated runway is _______ knots

15 kts

The maximum allowable crosswind component during takeoff or landing on a wet or dry runway is _______ knots

27 kts

The maximum permissible fuel imbalance between the contents of the left main and right main tank is ____ pounds

800

The maximum tailwind component is

10 kts

With regard to cabin pressure, the maximum differential pressure must never exceed

8.7 psi

Maximum operating altitude (company) is

37,000 ft

Maximum altitude with one air conditioning pack operating is

25,000 ft

Does the statement below accurately describe the role of the Pilot Monitoring? PM – Pilot Monitoring: The pilot who is not controlling the aircraft but is monitoring the PF’s actions. The PM will perform all other cockpit duties to include: In normal flight – navigates, communicates, and programs equipment, monitors flight and engine instruments, and performs other tasks as delegated by the PF During emergencies or abnormal operations – checks and assists in the interpretation of instrumentation, reads and accomplishes checklists, and takes corrective action as necessary

True