N8604C

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 25,780 hrs · 23,221 cycles

DURING PREFLIGHT INSPECTION, F/O SIDE MISSING SMOKE GOGGLES. REPLACED SMOKE GOGGLES IAW AMM 25-60-00.

Part: THROTTLE CABLE — BROKEN (LT ENGINE) · airframe 25,606 hrs · 23,048 cycles

LEFT ENG UNRESPONSIVE TO REDUCING THRUST DURING CRUISE FLIGHT. NR 1 REMAINED STUCK AT 94% WHEN PULLING THRUST LEVER BACK, ALL OTHER INDICATIONS NORMAL. SHUTDOWN NR 1 ENG PRIOR TO APPROACH IAW QRH. NR 1 ENG SHUTDOWN FOR APPROXIMATELY 15 MINS PRIOR TO LANDING. LT ENG THROTTLE CONTROL CABLE FOUND BROKE IN HALF. R & R LT ENG THROTTLE CONTROL CABLE IAW AMM 76-11-09, OPERATIONS CHECKED GOOD.

Part: CONTAINER — TORN (LIFE VEST) · airframe 25,606 hrs · 23,048 cycles

OBSERVER SEAT LIFE VEST PACKAGING TORN OPEN. DEFERRED - R & R OBSERVER'S LIFE VEST IAW AMM 25-61-03. DM 019093 CLEARED. PLACARD REMOVED.

Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 25,276 hrs · 22,719 cycles

C/A SIDE SMOKE GOGGLES CRACKED. REPLACED THE SMOKE GOGGLES IAW AMM 35-11-15.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · corrosion level 2 · airframe 25,144 hrs · 22,586 cycles

PAX PRESSURE FLOOR SUPPORT HAS CORROSION IN NUMEROUS AREAS FROM FS 409+128 TO 559. REPAIRED IAW REO 601R-53-41-666.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 25,144 hrs · 22,586 cycles

FS 280 FWD AND AFT FLOORBEAM FLANGE CORRODED LBL 9 OTBD ANGLE AND RBL9 INBD AND OTBD ANGLES CRACKED. REPAIRED IAW REO 601R-53-11-926.

Part: SILL — CORRODED (BS 409-559) · corrosion level 2 · airframe 25,144 hrs · 22,586 cycles

PAX PRESSURE FLOOR RT SILL HAS CORROSION IN NUMEROUS PLACES FROM FS409+128 TO FS559. REPAIRED IAW REO 601R-53-41-666.

Part: FLASHLIGHT — NO TEST (CABIN) · airframe 25,045 hrs · 22,485 cycles

F/A FLASHLIGHT ASSEMBLY INOPERATIVE, FAILS RED LED TEST. R & R F/A FASHLIGHT ASSY IAW AMM 25-61-02. OS CHECKED GOOD.

Part: BALLAST — ODOR (CABIN) · airframe 25,008 hrs · 22,450 cycles

CREW REPORTED ELECTRICAL ODOR COMING FROM OVERHEAD BIN 13AB. FOUND ODOR COMING FROM CEILING & SIDEWALL LIGHTS POWER UNIT DIMMERS/BALLASTS. R & R CEILING & SIDEWALL BALLAST/POWER UNIT DIMMERS IAW AMM 33-21-04 & AMM 33-21-10. OPS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 24,889 hrs · 22,339 cycles

F/A FLASHLIGHT MISSING. REPLACED MISSING FLASHLIGHT IAW AMM 25-61-00. ALL CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 24,386 hrs · 21,856 cycles

ON FLIGHT 3844 (GSP TO ATL) RECEIVED "FLAPS FAIL" MSG SHORTLY AFTER TAKEOFF. WHILE MOVING THE FLAPS FROM 45-0, THE FLAPS STOPPED AT 20.F. CREW PERFORMED RESET PROCEDURES CB'S CBP1-F4 AND CBP2-F4 AND CYCLED THE FLAPS 5 TIMES WITH NO FAILURE. CURRENTLY DEFERRED UNDER DEF-005498-2013.

Part: BPSU — FAILED (TE FLAP) · airframe 24,376 hrs · 21,845 cycles

ON FLIGHT 3760 (BUF TO DTW) FLAPS FAIL AT 20 ON APPROACH WHEN SELECTING FLAPS FROM 20 TO 30. REMOVED AND REPLACED LEFT FLAP BPSU IAW AMM 27-51-10. OPS CHECK GOOD. REMOVED AND REPLACED FECU IAW AMM 27-51-05. OPERATIONS CHECK GOOD. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH(L)(6)(I) AMOC DATED DECEMBER 07, 2012 AND PA AD 27-052J.

Part: UPLOCK SENSOR — LOOSE (RT MLG) · airframe 24,285 hrs · 21,758 cycles

ON CLIMB FLIGHT 3645 (DTW TO PIT) CREW REPORTED GEAR DISAGREE AFTER GEAR SELECTED UP. ABOUT 6 SECONDS LATER "RIGHT MAIN LANDING GEAR" FOLLOWED QRH, AND GEAR WENT UP. FLIGHT CONTINUED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. COMPLIED WITH PA 05-018J RE-SECURED UPLOCK PROXIMITY SENSOR IAW RIL 2962. PERFORMED GEAR SWINGS, NO DEFECTS NOTED. OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 24,141 hrs · 21,613 cycles

ON FLIGHT 4133 (DTW TO BUF) RECEIVED A FLAPS FAIL AT 2 DEGREES ON APPROACH. AIRCRAFT LANDED SAFELY. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH (1A)(6)(I) PER AMOC DATED DECEMBER 04-2012 AND PA AD 27-052J. SEE NO ROUTINE CARD N38988 AND CONTINUATIONS CARDS FOR DETAILS OF WORK PERFORMED. MOST RECENT FECU FAULT CODES AS FOLLOWS FLIGHT LEG 6394 1) 5 1A 1)5 2B 1)C 1B 1)C 2B. REPLACED RIGHT INBOUND OUTER FLAP ACTUATOR IAW 27-50-00, INSPECTED FLAP DRIVE CABLES REPLACED LEFT AND RIGHT NR 3 FLEX CABLES. REPLACED LEFT NR 5 FLEX CABLES, IAW AMM 27-53-10. C/W LEFT AND RIGHT TORQUE CHECK NO DISCREPANCY'S NOTED.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 24,135 hrs · 21,067 cycles

ON FLIGHT 3918 (DTW - CWA) FLAPS FAIL CAUTION OCCURED WHEN FLAPS WERE SELECTED TO 30 AT APPROX 175 KIAS ON APPROACH INTO CWA). AIRCRAFT LANDED SAFELY. PERFORMED TROUBLESHOOT PER BOMBARDIER FIM REV 44 IAW AD2009-06-12 PARA H, 6, I AND PA AD27-052J. LEFT BPSU CREATING HEAT DURING STEP 6 OF TROUBLESHOOT PER FIM 27-50-00 TROUBLE 7. REMOVED AND REPLACED LEFT BPSU IAW AMM 27-51-10. ALSO RE-RIGGED RIGHT BPSU IAW AMM 27-51-10. FAIL CODES WERE 1-BINDING 2-FECU 3-FLAP CONTROL LEVER. CODES WERE 5-1B, 5-2B, 16-1A, 16-2A, 25BC, 30BC, 33BC.

Part: PSEU — MALFUNCTIONED (LANDING GEAR) · airframe 24,039 hrs · 21,518 cycles

ON FLIGHT 3792 (JFK - ROC) PERFORMED AN AIR TURNBACK AFTER RECEIVING A GEAR DISAGREE. CREW REPORTED THAT AFTER TAKEOFF RONWAY 31L IN CLIMB GEAR DID NOT RETRACT WHEN HANDLE MOVED TO "UP" POSITION. PARKING BRAKE SHUT OFF VALVE & ANTI SKID IN BD CAUTION MSG WITH HANDLE IN UP POSITION. THE QRH WAS PERFORMED AND THE AIRCRAFT RETURNED TO JFK. PERFORMED BITE TEST OF PSEU AND FOUND FAULT CODE DI-11 OFF. COMPLIED WITH SCENARIO 1 OF PA 05-018J. REMOVED & REPLACED PSEU IAW AMM 32-61-01. REMOVED & REPLACED LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,696 hrs · 21,190 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,783 hrs · 20,284 cycles

MOST FWD LT OVERWING EMER EXIT LIGHT INOP. /R NR 2 EXTERIOR EMER LIGHT ON LT SIDE IAW CRJ AMM 33-51-21. OPS CHECK NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,680 hrs · 20,179 cycles

EMERGENCY LIGHTS SWITCH INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT BULBS AND CHARGED BATTERY PACKS, PERFORMED OPS CHECK IAW AMM 33-51-01. OP CHECKED GOOD. OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 22,653 hrs · 20,154 cycles

DURING CLIMB RECEIVED SMOKE TOILET MESSAGE, OUT BEFORE QRH COULD BE ACCOMPLISHED. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR OAW AMM 26-16-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BLADE — DAMAGED (RT ENGINE FAN) · airframe 22,400 hrs · 19,922 cycles

ABORTED TAKEOFF DUE TO FAN VIBRATION ON RT ENGINE. REMOVED & REPLACED 18 FAN BLADES ON RT ENGINE IAW AMM 72-20-00.

Part: BLADES — VIBRATION (RT ENGINE FAN) · airframe 22,400 hrs · 19,922 cycles

ABORTED TAKEOFF DUE TO RT ENGINE FAN VIBRATION . REMOVED & REPLACED 18 FAN BLADES ON RT ENGINE IAW AMM 72-20-00.

Part: FLAP — MALFUNCTIONED (WING) · airframe 22,386 hrs · 19,908 cycles

FLAPS FAIL ATG 20 DEGREES ON APPROACH, (AML #2237387, DISC #1) COMPLY WITH P.A. AD27-052G FLAP FAILURE REQUIREMENTS AND PROCEDURES. C/W PA AD 27-052G. PERFORMED T/S PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARAGRAPH (H)(G) (I) AMOC DATED MARCH 27, 2009, TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA27-052G. FOUND WATER IN SEVERAL FLEX SHAFTS. REMOVED IAW FIM, OK FOR SVC.

Part: DRIVE SHAFT — CONTAMINATED (TE FLAP) · airframe 22,383 hrs · 19,904 cycles

FLAPS FAIL ON APPROACH. FOUND WATER IN FLEX DRIVE SHAFTS. REMOVED, CLEANED AND REINSTALLED FLEXDRIVE SHAFTS. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAULTY (RT COWLING) · airframe 22,161 hrs · 19,678 cycles

AIR TURNBACK RT COWL ANTI-ICE CAUTION MSG. QRH COMPLETED. MSG REMAINED ON. REMOVED AND REPLACED RT COWL ANTI-ICE VALVE IAW AMM 30-22-01. VERIFIED PARTS EFFECTIVITY.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 22,070 hrs · 19,586 cycles

THE 621.00 PRESSURE BULKHEAD HAS 6 EACH CHAFES ON FWD FACE AT LBL 18 30" ABOVE FLOOR, RBL 18 30" ABOVE FLOOR, RBL 27 30" ABOVE FLOOR, RBL 36 30" ABOVE FLOOR, RBL 36 13" ABOVE FLOOR AND RBL 42 4" ABOVE FLOOR. MAXIMUM DAMAGE IS .140" L X .140" W X .001" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 22,070 hrs · 19,586 cycles

THE 621 PRESSURE BULKHEAD FWD FACE HAS A CHAFE WITH A DENT AT LBL 24, 4 ABOVE THE FLOOR. REPAIRED IAW BOMBARDIER REO 601R-53-61-4311.

Part: POST — DAMAGED (FUSELAGE) · airframe 22,070 hrs · 19,586 cycles

FS 409+128 VERT POST FAIL NDT BL 0 UPPER AFT RT RADIUS. REPAIRED IAW BOMBARDIER REO 601R-53-41-889 REV A AND BOMBARDIER SERVICE CORPORATION EO CL600-2B19-53-L00769.

Part: STRINGER — DENTED (FUSELAGE) · airframe 22,070 hrs · 19,586 cycles

DENT RT FUSE AT FS 566 ON STRINGER 18R. REPAIRED IAW BOMBARDIER REO 601R-53-61-4316.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 21,679 hrs · 19,210 cycles

LT FLAP POSITION INDICATION ERRATIC. REMOVED AND REPLACED LT FLAP POSITION TRANSMITTER IAW CRJ AMM 27-5-01. OP CHECK GOOD, OK FOR SERVICE.

Part: SPAR — DAMAGED (RT WING) · airframe 21,396 hrs · 19,052 cycles

A NR 30 HOLE DRILLED IN RT WING LEADING EDGE SPAR AT WS 353.00 LOWER LEADING EDGE ATTACHING FLANGE 3.90" INBOARD OF WS 353. REPAIRED IAW BOMBARDIER REO 601R-57-21-1486.

Part: VALVE — MALFUNCTIONED (CABIN PRESSURE)

A/C DIVERTED TO JAN FOR PRESSURIZATION ISSUE CREW DID DECLARE EMERGENCY "NO" O2 MASK DEPLOYMENT, LANDED SAFELY. STILL IN WORK FOR CHECK VALVE REPLACEMENT.

Part: A/C PACK — OVERTEMP (AC BAY) · airframe 20,697 hrs · 18,381 cycles

APPROX 50 FEET AFTER LEAVING RUNWAY IN STL, CABIN STARTED FILLING UP WITH SMOKE. AS A PRECAUTIONARY MEASURE, CREW DEPLANED AC ON TAXIWAY BEFORE REACHING GATE. NO INJURIES REPORTED, NO EMERGENCY WAS DECLARED. MX FOUND RT PACK OVERTEMPING - DEFERRED PER MEL 21-51-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 20,674 hrs · 18,329 cycles

GEAR DISAGREE C/W PA05-18A. OPS CHECK GOOD, OK FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202) · airframe 17,018 hrs · 14,860 cycles

.75 INCH CRACK WAS FOUND ON THE FWD BULKHEAD AT FS 202.75 AT THE PARKING BRAKE CUT OUT HOLE BL 23.71 DURING A INSPECTION. CRACK WAS REPAIRED IAW GREO 601R-53-11-563.