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Gojet CRJ 550 Limitations Questions with Correct Answers | Updated (100% Correct Answers)

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Gojet CRJ 550 Limitations Questions with Correct Answers | Updated (100% Correct Answers)

Institution
Gojet
Course
Gojet

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Gojet CRJ 550 Limitations Questions with
Correct Answers | Updated (100% Correct
Answers)
>30degrees in either direction of the airplane nose between 5 and
30 kias windspeed Answer: Apply up to 75%N1 before brake
released then set TOGA thrust by 60kias

Within 30degree on either direction of the airplane nose no
windspeed limit or >30 in either direction of the airplane nose; <5
knots windspeed. Answer: No limitations-TOGA thrust may be
applied before brakes released, butmust be set by 60 kias

What is All engine out rapid relight is from 10000to sea level
Answer: Fadec rapid relight capability has been demonstrated at
200kias for up to 15 second fuel interruptions.

What is starter assisted relight limitation from FL210 to SL. Answer:
Speed from Vref upto VMO and fr 0-45%N2

What is the windmilling relight limitation from Fl250 to sea level
Answer: Speed 250 kias to vmo and 7.2 N2 minumum

Motoring on ground 2 through 5 is_________followed by____________
Answer: 30 sec, 5 minutes




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, 2
Motoring on ground 1 attempt is______________ followed
by______________ Answer: 90 seconds, 5 minutes

Engine Start or Motoring in Flight for 2 through 5 is___________
followed by______________ Answer: 60 seconds, 5 minutes

Engine Start or Motoring during a flight for 1 attempt is ___________
followed by___________ Answer: 120 seconds, 10 seconds cool down

Engine start maximum time on ground for 3 through 5 is___________
followed by___________cool down Answer: 90 seconds, 5 minutes la

Engine start maximum time on ground for 1& 2 is________ followed
by_________cool down. Answer: 90 seconds, 10 seconds

The use of Reduced/Flex thrust for takeoff is not authorized when;
Answer: -Wing and/or cowl anti-ice bleeds are in use

-Runway is contaminated with standin water,slush snow or ice

-Warnings or forecast of windshear or downdrafts exist(including
LLWAS advisories)

- Antiskid system is inoperative

- The engine cannot achieve full rated thrust

Continues engine ignition must be used during the following:
Answer: -takdeoff and landings on contaminated

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