N829AY

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 17,747 hrs · 15,200 cycles

ON LEFT BRAKE ONE BTMS SAYS 00 THE OTHER FOR THE LEFT BRAKE SAYS 05 DISCONNECTED AND RE-ATTACHED LEFT O/B BRAKE LINE QUICK DISCONNECT IAW AMM 32-43-26. LEFT O/B BRAKE CHECKS NORMAL. OK FOR SERVICE.

Part: COVER — UNKNOWN (CABIN SIGN) · airframe 177,190 hrs · 15,174 cycles

F/A NO SMOKING/FASTEN SEAT BELT SIGN IN GALLY NEEDS COVER REPLACED. 2LA007353-50. OPS CHECK OK. REMOVED AND REPLACED F/A GALLEY NO SMOKING LIGHT IAW CRJ200 AMM 33-24-00. THIS CLOSES OUT DM 76112.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 17,652 hrs · 15,101 cycles

ONE INFANT LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED INFANT LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,582 hrs · 15,027 cycles

MID AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BULB IAW AMM 33-21-01. OP CHECKS GOOD DM 74146 CLOSED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,188 hrs · 14,647 cycles

RIGHT EMERGENCY OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BULB NR 3 IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: PSEU — MALFUNCTIONED (LANDING GEAR) · airframe 16,080 hrs · 13,557 cycles

AIR RETURN FOR PROX SYS FAULT STATUS IN FLIGHT IN CLIMBOUT THRU 10000. FOUND PSEU CODE A06 - NVRAM. REMOVED AND REPLACED PSEU & OP CHECK GOOD IAW AMM 32-61-01. OK FOR SVC.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 14,753 hrs · 12,261 cycles

CREW DECLARED EMERGENCY DUE TO FLAPS FAILED AT ZERO EN ROUTE. REMOVED AND REPLACED LT BPSU IAW AMM 27-51-10. FLAPS OP CHECK NORMAL IAW AMM 27-54-00. OK FOR SERVICE. PART EFFECTIVELY VERIFIED.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 14,753 hrs · 12,261 cycles

FLAPS FAIL AT 18 DEG OUTBOUND OF ROC. A/C DID AIR RETURN AND DECLARED AN EMERGENCY. REMOVED AND REPLACED BPSU IAW AMM 27-51-10.

Part: FLAP — MALFUNCTIONED (WING) · airframe 14,749 hrs · 12,256 cycles

FLAPS FAIL AT 0 ON CLIMBOUT DTW CREW DECLARED AN EMERGENCY ON APPROACH TO BUF RESET AND PLACED ON DI FOR 10 CYC.

Part: FLAP — FAILED (WING) · airframe 14,715 hrs · 12,227 cycles

CREW REPORTED FLAPS FAILED AT ZERO AFTER CLIMBOUT CONTINUED ON TO DTW LANDED WITHOUT INCIDENT. PERFORMED TROUBLESHOOTING PER BOMBARDIER FCM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I), AMOC DATED MARCH 27, 2009, TR 27-012 PER AMOL DATED DECEMBER 18, 2009 AND PA AD27-052G. CODES FOUND EVENT 1, FLIGHT LEG 33, ALL THREE MOST PROBABLE’S.

Part: FLAP — MALFUNCTIONED (WING) · airframe 14,670 hrs · 12,188 cycles

CREW REPORTED FLAPS FAIL CAUTION WITH FLAPS RETRACTED TO '0' AIRSPEED 200/250. DEFERRED FLAP SYSTEM IAW MEL 27-50-00 DM-45378.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,290 hrs · 11,857 cycles

FWD FACE OF FS 621 BULKHEAD CHAFED IN 9 EACH PLACES NO DEEPER THAN 0.003 INCHES. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155 AND 601R-53-61-4042.

Part: YOKE — SCRATCHED (RT ENGINE) · airframe 14,290 hrs · 11,857 cycles

RIGHT FORWARD ENGINE MOUNT YOKE HAS FOUR SCRATCHES AT TOP FORWARD LUG ON FORWARD FACE. TWO SCRATCHES MEASURE .156 INCH LONG AND UP TO 0.025 INCH DEEP. TWO SCRATCHES MEASURE 0.375 INCH LONG AND UP TO 0.007 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-71-21-047.

Part: PANEL — OPEN · airframe 14,133 hrs · 11,710 cycles

LOUD NOISE COMING FROM THE NOSE OF THE A/C FOLLOWED BY A STALL FAIL MSG DURING INITIAL CLIMBOUT. FOUND PANEL 212BR OPEN. PERFORMED OPS CHECK ON STALL PROTECTION SYSTEM IAW 27-35-00.

Part: WEB — CANNING (PAX DOOR) · airframe 13,992 hrs · 11,572 cycles

DAMAGE WAS FOUND ON THE AFT SIDE PANEL WEB OF THE MAIN PASSENGER DOOR STAIRS (P/N 601R31701-01, S/N 8029) NEAR THE TOP OF THE 2ND STEP (AT FS 349). THE DAMAGE IS OIL CANNING WITH A DENT PROTRUDING OUTWARD. ONLY THE WEB IS DAMAGED NO INTERNAL STRUCTURE IS AFFECTED. THE DAMAGED AREA MEASURES 8 LONG X 3 WIDE X 0.166 DEEP. TEMPORARY REPAIR IAW STS ENGINEERING EA 09-2011-041. REPEAT INSPECT EVERY 150 FH. WITHIN 800 FLIGHT HOURS, ACCOMPLISH A PERMANENT REPAIR TO THE DAMAGED AREA.

Part: SKIN — CRACKED (SPOILER) · airframe 13,970 hrs · 11,553 cycles

A DENT WAS FOUND ON THE UPPER SURFACE OF THE RIGHT WING OUTBOARD GROUND SPOILER (P/N 600-10502-56, S/N 3971165). THE DENT MEASURES 0.625 X 0.625 X 0.011 DEEP; IT IS 2.8 FROM THE OUTBOARD EDGE AND 2.0 FROM THE LEADING EDGE. REPAIRED IAW STS ENGINEERING EA 09-2011-039.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 11,932 hrs · 9,640 cycles

GEN 2 OFF CAUTION SVC NR 2 IDG IAW AMM 12-13-24. OPC GOOD THIS CLEARS DM 19630. OK FOR SERVICE.

Part: FLAP — FAILED (WING) · airframe 2,498 hrs · 1,860 cycles

FLAPS FAILED AT 30 DEGREES ON APPROACH. APPROACH ABORTED QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 1,412 hrs · 1,047 cycles

FLAPS FAIL AT GATE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD98-20-01.