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SW CQ 2012 Powerplan

Powerplant

QuestionAnswer
POWERPLANT: 1. When does the Air Turbine Starter (ATS) normally cutout? CRJ 200: N2 RPM exceeds 55% CRJ 700/900: N2 RPM exceeds 50%
2a. What is APR? APR provides: 1)Automatic Engine Failure Detection 2)Thrust increase upon detection CRJ200:8729->9220 2% N1 increase to good engines CRJ700:12760->13790 CRJ900:13535->14255
2b. How is the APR armed? CRJ200: 1) APR switches set to ARM 2) Engine Speed switches set to ON 3) Weight on Wheels 4) N1 RPM>79.1% (in N1 mode) 5) Operative ECU 6) 2 operating DCUs CRJ700/900: During T/O when N1 RPM of both engines are within 8% of scheduled T/O p
3. Do we have APR on Go Around? CRJ 200: No because one of the requirements to arm the APR is Weight ON wheels CRJ 700/900: Yes, APR is armed when the approach bit is set by having 1)Either engines available 2) Flaps >20 deg -or- Landing gear down
4. How is APR activated? CRJ200: when either engine <67.6% CRJ700/900: 1)FADEC determines a N1 mismatch >15% 2)Thrust levers must be in TOGA detent 3)Programmed N1 setting either norm/reduced note:APR pwr is activated when one/both thrustlevers are set in MAX PWR detent
5. You gain an additional ____% or _____ LBS thrust with APR 2% or 500 LBS
6. What do the engine speed switches do on the CRJ 200? 1) arm APR system 2) Engine speed control (N1 vs N2 mode)
6b. In the N1 mode, is it possible to control n2 RPM speeds? Yes, but the thrust lever position/angles will be mismatched (not close to aligned) for N2 speeds
6c. In the N2 mode, is it possible to control N1 RPM speeds? Yes, but the thrust lever position/angles will be mismatched for N1 speeds
6d. What should be done to automatically go from N1 mode -to- N2 mode? Select both engine speed switches OFF -or- Reduce power < 79% N1 note: this could cause a rapid increase in engine RPM and RPM or ITT limits could be exceeded
7. What would happen if the right engine speed switch was selected OFF during climb out on the CRJ 200? this could cause a rapid increase in engine RPM and RPM or ITT limits could be exceeded
8. When do you need continuous ignition? 1) T/O & LNDG contaminated RWY 2) T/O with crosswind component >10 knots (200 only) 3) moderate or heavier rain 4) moderate or heavier turbulence 5) in vicinity of T-storms
9. When will continuous ignition be automatically activated? Stall: when high AOA is approached both ignition systems are energized until the airplane attitude is corrected
10. When does the thrust lever auto-retard on the CRJ 200? Whenever Thrust Reversers in transit -or- inadvertent deployment of TRs
11. What does the UNLK light mean on the TR panel? indicates reversers not locked. A TR emergency stow system is installed to stow an unlocked thrust reverser. Selecting the UNLK switchlight directs 14th-stage bleed air to the PDU to stow unlocked reverser
12. L(R) REV UNSAFE caution message means? a)Thrust Reverser is unsafe to arm in-flight b)TR lever deploy switches have failed in a commanded deploy state but thrust reversers are not locked and are not armed
13. Normal N1 thrust is displayed on ED1 in what color? Flex Thrust? Normal N1 = Cyan Flex N1 = Magenta
14. When do we check engine oil, how much oil can you add? 3 min - 2 hours after engine shutdown you can add up to 2 qts. if any of these limits are exceeded then dry motoring is required
15. if needed, when can you add oil? 15 min - 2 hours after shutdown
16. When do you have to dry motor after adding oil? 1) you add more than 2 qts oil 2) oil has been added after 2 hours from shutdown 3) airplane has been cold soaked for >8hrs at <= -30 degC. dry motor for 60 sec
Created by: muddyairplane
 

 



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