N8797A

Part: CONTAINER — TORN (LIFE VEST) · airframe 23,474 hrs · 20,813 cycles

F/A LIFE VEST HAS HOLE IN BAG. R & R LIFE VEST IAW AMM 25-61-03.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,585 hrs · 19,938 cycles

F/A LIFE VEST BAG TORN. R & R F/A LIFE VEST IAW AMM 25-61-03.

Part: STEERING UNIT — FAULTY (NLG) · airframe 22,398 hrs · 19,753 cycles

N/W STEERING INOP CAUTION CAME ON TWICE WHILE TAXING. QRH RESETS WERE SUCCESSFUL. R & R STEERING UNIT IAW AMM 32-51-01. OPS CHECK GOOD, OK FOR SVC.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,300 hrs · 19,653 cycles

EDDY CURRENT INSPECTIONS OF FS 621 BULKHEAD REVEALED TWO CRACKS IN THE BULKHEAD WEB AROUND THE AFT MACHINED FITTING OF THE CARGO DOOR LINTEL, MEASURING 0.213" AND 0.145" LONG. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: GEARBOX — MALFUNCTIONED (THROTTLE CONTROL) · airframe 21,645 hrs · 19,015 cycles

ON FLIGHT 4320 FROM DTW TO PVD THE CREW RECEIVED LEFT TR UNLOCK MESSAGE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MDT. REPLACED LT ENGINE THROTTLE CONTROL GEAR BOX. TEST OKAY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,211 hrs · 18,590 cycles

F/A REPORTS FORWARD EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY IAW AMM 25-61-04 AND OPS CHECKS GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 21,199 hrs · 18,578 cycles

EMERGENCY FLOOR LIGHTING AFT OF EXIT ROW IS INOP. RESEATED AFT CONNECTOR & OP CHECK GOOD IAW AMM 33-51-01.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,166 hrs · 18,547 cycles

F/O EMERGENCY FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED F/O EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-60-01. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,156 hrs · 18,541 cycles

LBL 27 FLOORBEAM IN CARGO AREA IS CHAFED AND HAS CORROSION AROUND SCREW HOLES. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,031 hrs · 18,425 cycles

THIRD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERHEAD EMERGENCY FLOODLIGHT IAW AMM 33-52-00. AIRCRAFT OK FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 20,953 hrs · 18,345 cycles

FLIGHT 3918, FLAPS FAIL CAUTION WHEN SELECTED TO FLAPS 30 ON APPROACH . REMAINED AT 30 GO AROUND FLOWN OND APPROACH AND LANDING MADE AT FLAPS 30 TOUCHDOWN AT 400 FPM. PERFORMED TROUBLESHOOTING PER FIM REV 39 AD 2009-06-12. PERFORMED FLAP LEVER TEST IAW FIM 27-50-00 AND RIL 1871. FLAPS OPS CHECKED GOOD IAW AMM 27-50-00.

Part: PACKING — LEAKING (FUEL LINE) · airframe 20,688 hrs · 18,097 cycles

FUEL LEAK WITH APU RUNNING ONLY. NO ENGINES STARTED YET. REMOVED AND REPLACED APU FUEL FEED LINE PACKING IAW AMM 28-20-01. OPS AND LEAK CHECK GOOD.

Part: TARGET — LOOSE (MLG) · airframe 20,641 hrs · 18,049 cycles

RT MAIN GEAR DISAGREE MESSAGE ON RETRACTION, GEAR WAS RECYCLED OPERATION WAS NORMAL . SCENARIO 1 FOUND RT MLG UPLOCK TAGERT LOOSE USED PROPER WASHER IAW CMM 32-30-15. ADJUSTED PROXIMITY SWITCH IAW AMM 32-32-05 PSEU CODE WAS S18. CLEARED PSEU, OP CHECKED GEAR SWING IAW AMM 32-30-00. CHECK GOOD, OK FOR SERVICE.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 20,500 hrs · 17,907 cycles

1 INFANT LIFE VEST HAS HOLD IN BAG. COMPLIED WIHT PA 25-096A BY INSALLING INFANT LIFE VEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,974 hrs · 17,418 cycles

EMERGENCY FLOOR TRACK LTS AFT IF ROW 8 INOP. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT STRIP IAW AMM 33-51-01.

Part: CABLE ASSY — BINDING (THROTTLE) · airframe 19,640 hrs · 17,094 cycles

LT THRUST LEVER IS VERY STIFF. PERFORM RIGGING OF LT THROTTLE GEARBOX. GEAR BOX FAILED OPS CHECK FOUND TO BE BINDING AT MAX PWR POS. REF NON ROUTINE CARD N30910 FOR CORRECTIVE ACTION & RIGGING. LEFT ENG THROTTLE AFT PUSH PULL CABLE ASSY IS BINDING AND ROUGH. REMOVED AND REPLACED AFT PUSH PULL THROTTLE CABLE ASY IAW CRJ200 AMM76-11-07: CKS GOOD. REMOVED AND RE-INSTALLED ORIGINAL GEARBOX S/N1074 IAW CRJ200 AMM76-11-17. OPS & RIG CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (FIRE WARNING) · airframe 18,383 hrs · 15,928 cycles

ON APPROACH INTO FAR GOT APU FIRE INDICATION FOLLOWED BY APU FIRE FAIL MESSAGE FOLLOWED BY APU OVERTEMP MESSAGE CREW DECLARED EMERGENCY FOLLOWED QRH DISCHARGED APU FIRE EXTINGUISHERS. FIRE DEPT WAS CALLED FOUND "NO" ACTUAL FIRE EVIDENCE. MAINT DEFERRED APU FIRE EXT SYSTEM IAW MEL 26-22-01 DM-42579.

Part: IDG — LOW (NR 1) · airframe 17,069 hrs · 14,681 cycles

NR 1 IDG CAUTION MESSAGE DURING TAKEOFF. SERVICED NR 1 IDG IAW AMM 12-13-24. OP/C GOOD.

Part: HYDRAULIC SYSTEM — OVERSERVICED (NR 3) · airframe 16,263 hrs · 13,889 cycles

LT MAIN GEAR DISAGREE MESSAGE. QRH COMPLETED, ALL INDICATION NORMAL AFTER GEAR CYCLED, FOUND NR 3 HYD SYS TO BE OVERSERVICED. REMOVED HYD FLUID TO 60 PERCENT IAW AMM 32-30-00.

Part: APU — FLAMED OUT · airframe 8,917 hrs · 7,509 cycles

DURING APU START WHILE SITTING AT THE GATE IN YUL, THE APU OVERTEMPED AND SHUTDOWN. SMOKE ENTERED THE CABIN THROUGH THE ENVIRONMENTAL CONTROL SYSTEM. THE FLIGHT CREW CALLED FOR CFR AND DEPLANED THE PASSENGERS. CFR FOUND NO INDICATION OF FIRE. THE APU WAS DEFERRED AND THE AIRCRAFT RELEASED FOR FLIGHT. MAINTENANCE TROUBLESHOT THE APU AT MSP. THE APU WAS INSPECTED AND OPS CHECKED NORMAL. IT IS BELIEVED THAT AN INCOMPLETE APU START CAUSED THE SMOKE.

Part: APU — WARNING MESSAGE · airframe 8,763 hrs · 7,376 cycles

ON SHORT FINAL INTO ROC, THE APU FIRE WARNING ILLUMINATED, FOLLOWED SHORTLY BY THE APU FIRE FAIL MESSAGE. THE APU DID AN AUTO SHUTDOWN. UPON LANDING, MAINTENANCE PERFORMED A VISUAL INPSECTION OF THE APU AND APU COMPARTMENT. THERE WAS NO INDICATION THAT THERE HAD BEEN ANY FIRE. AS A SAFETY PRECAUTION, THE APU WAS DEFERRED PER THE MEL, UNTIL FURTHER TROUBLESHOOTING COULD BE DONE AT A MAINTENANCE BASE.