Gojet CRJ 550 Limitations Final study Questions and Answers Graded A+

Gojet CRJ 550 Limitations Final study Questions and Answers Graded A+ 30degrees in either direction of the airplane nose between 5 and 30 kias windspeed - 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. - 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 - 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. - Speed from Vref upto VMO and fr 0- 45%N2 What is the windmilling relight limitation from Fl250 to sea level - Speed 250 kias to vmo and 7.2 N2 minumum Motoring on ground 2 through 5 is_________followed by____________ - 30 sec, 5 minutes Motoring on ground 1 attempt is______________ followed by______________ - 90 seconds, 5 minutes Engine Start or Motoring in Flight for 2 through 5 is___________ followed by______________ - 60 seconds, 5 minutes Engine Start or Motoring during a flight for 1 attempt is ___________ followed by___________ - 120 seconds, 10 seconds cool down Engine start maximum time on ground for 3 through 5 is___________ followed by___________cool down - 90 seconds, 5 minutes la