N8646A

Part: BRACKET — BENT (NLG) · airframe 23,360 hrs · 21,027 cycles

ON FLIGHT 4056 (DTW TO CAK) CREW RECEIVED A GEAR DISAGREE ON CLIMBOUT AFTER THE GEAR HANDLE WAS SELECTED UP. NOSE GEAR REMAINED DOWN. ON ORIGINAL PUSHBACK STRAP GOT STUCK IN NOSE GEAR. FOUND NLG CENTERING BRACKET BENT FOR NLG CENTERED/EXTENDED PROX SWITCH BRACKET. REMOVED AND REPLACED NLG CENTERED/EXTENDED PROX SWITCH BRACKET IAW MESSIER DOWTY CMM32-20-04. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED.

Part: LIFE VEST — TORN (COCKPIT) · airframe 229,767 hrs · 20,634 cycles

CAPTAIN'S LIFE VEST BACK TORN. REMOVED AND REPLACED LIFE VEST IAW AMM 25-61-03.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,721 hrs · 20,389 cycles

FIRST OFFICERS FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED BATTERY IAW AMM 25-60-00. OPS CHECKED GOOD, OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (FLT CONTROL) · airframe 22,438 hrs · 20,094 cycles

AT SPEEDS ABOVE 250 KTS OR SLOW SPEEDS WITH FLAPS OUT AILERON CONTROL IS SLOPPY. IT THEN OPTS HARD THEN CATCHES IN THE BANK CAUSING OVER CONTROLLING. PERFORMED PA 27-0660 FOR AILERON BINDING. LUBRICATED REAR QUADRANT PULLEYS HEARINGS IAW AMM 12-20-07-640-809. LUBRICATED AILERON CABLES AND PULLEYS IAW AMM 12-20-04-640-810. PERFORMED AILERON CABLE TENSION TEST. ALL WITHIN LIMITS IAW AMM 27-11-00-830-202. OPS CHECKED AILERON PCUS, NO DEFECTS NOTED IAW AMM 27-11-00-710-803.

Part: SKIN — DENTED (BS 374 S16R) · airframe 22,354 hrs · 20,006 cycles

MAINTENANCE FOUND THE SKIN TO BE DENTED AT APPROXIMATELY FS 374 JUST BELOW S16R. THE DENT MEASURES 1 15/32 X 15/16 X 0.094 DEEP. REPAIRED IAW EA CRJ253-00649 AND ASSOCIATED 8110-3.

Part: BULKHEAD — GOUGED (BS 621) · airframe 22,328 hrs · 19,984 cycles

AFT PRESSURE BULKHEAD FORWARD FACE HAS GOUGES ON WEB AT LBL 9 ABOVE THE FLOOR MEASURING 0.004 INCH DEEP. REPAIRED IAW SRM 51-12-00.

Part: CABLE — BROKEN (ANTI ICE) · airframe 22,160 hrs · 19,814 cycles

PAX DOOR ICE BREAK CABLE BROKEN. REMOVED AND REPLACED PAX DOOR ICE BREAK CABLE IAW AMM 52-11-15.

Part: WARNING SYSTEM — FALSE ACTIVATION (LAVATORY) · airframe 21,999 hrs · 19,657 cycles

SMOKE TOILET CAUTION ON FINAL APPROACH MESSAGE CAME ON AFTER STARTING APU. F/A CONFIRMED NO FIRE AND HALON BOTTLE DID NOT DISCHARGE. MESSAGE LASTED FOR APPROX A MINUTE AND THEN WENT OUT, IT DID NOT COME BACK ON. PERFORMED OP CHECK OF LAV SMOKE DET AND INSPECTED LAV IAW AMM 26-16-00. NO DEFECTS NOTED. NO MSG'S PRESENT. OK FOR SVC.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 21,976 hrs · 19,631 cycles

FLT 3759 FSD-DTW ABORTED TAKEOFF AT LESS THAN 50 KTS DUE TO HIGH LT ENGINE OIL PRESSURE CAUTION. THE CREW ONLY HAD THE ENGINE RUNNING FOR FOUR MINUTES BEFORE ATTEMPTING THE TAKEOFF. THE CREW IS GOING TO LET THE ENGINE RUN FOR LONGER TO WARM UP AND THE ATTEMPT THE TAKEOFF AGAIN. NO WRITE-UP WAS MADE SO NO MAINTENANCE ACTION WAS TAKEN.

Part: SEAT BELT — UNSECURE (CABIN) · airframe 21,584 hrs · 19,311 cycles

SEAT 9B SEAT BELT CAME OFF. RESECURED SEAT 9B SEAT BELT IAW CRJ 200 AMM 25-24-01, OPS CHECK GOOD. OK FOR SVC.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,405 hrs · 19,132 cycles

LBL 27 FLOORBEAM CAP HAS CORROSION AROUND NUT PLATES FROM FS 574-FS 621. REPAIRED IAW SRM 53-61-43.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 20,818 hrs · 18,500 cycles

CREW DECLARED AN EMERGENCY REPORTED GEAR DISAGREE ON APPROACH, NOSE GEAR WOULDN'T RELEASE FOLLOWED QRH CYCLED GEAR GOT 3 GREENS FLIGHT LANDED SAFELY WITHOUT FURTHER INCIDENT DEFERRED & PINNED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-01DM-48162.

Part: FLAP — FAILED (WING) · airframe 20,125 hrs · 17,871 cycles

FLAPS FAILED AT 20 DEGREES ON APPROACH "NO" EMERGENCY DECLARED. PERFORMED T/S PER BOMBARDIER FIM REV 34 IAW AD 2009-06-12 PARAGRAPH (N) (B) (I) AMOC DATED DEC 18 2009 AND PA AD27-052G. FOUND FAULT FOR FLAP CONT LEVER. RESET & OP CHECKED SYSTEM IAW AMM 27-51-00. OK FOR SERVICE.

Part: FLAP — FAILED (WING) · airframe 20,012 hrs · 17,764 cycles

FLAPS FAIL DEFERRED PER MEL 27-50-00 AUTH 40782.

Part: BULKHEAD — CRACKED (BS 559) · airframe 17,333 hrs · 15,234 cycles

FOUND CRACKS AT FS 559 BULKHEAD WEB HAS 2 INDICATIONS OF CRACKS NOTED ON RT SIDE WL 59.10 I/B OF RBL 18 APPROX .3 INCH IN LENGTH AND WL 58.70 O/B OF RBL 9, APPROX .2 INCH IN LENGTH AND RT FS 559 CAP ANGLE HAS INDICATION NOTE AT RBL 18 APPROX .2 INCH IN LENGTH ALL FAILED NDT INSP. AIRCRAFT IS CURRENTLY IN "C" CHECK AND REPAIR IS IN WORK.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

RECEIVED STAB/MACH TRIM CAUTION MESSAGE IN FLIGHT QRH FOLLOWED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MESSAGE CLEARED AFTER LANDING WITH NO REPEAT. ACFT WAS POWERED DOWN AND BACK ON. NO FURTHER MESSAGES RECEIVED. (S)

Part: FCU — FAILED (TE FLAPS) · airframe 10,385 hrs · 9,261 cycles

FLAPS FAILED ON TAXI OUT. RETURNED TO GATE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU) IAW AMM.