N8665A

Part: CONNECTOR — LOOSE (CABIN) · airframe 27,158 hrs · 23,978 cycles

EMERGENCY EXIT LIGHTS ON FLOOR ROW 2 - 5 INOPERATIVE. FOUND LOOSE CONNECTION AT ROW 5. RECONNECTED PLU. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,068 hrs · 23,892 cycles

FLOOR PATH EMER LIGHTS INOPERATIVE FROM ROW 2 - 5. CYCLE BREAKER CBP 4 C2. OPERATIONS CHECKED GOOD IAW AMM 33-51-03.

Part: POWER STRIP — INOPERATIVE (CABIN) · airframe 27,001 hrs · 23,823 cycles

EMERGENCY FLOOR TRACK LIGHT INOPERATIVE AT ROWS 5 THROUGH 2. R & R EMER LIGHT POWER STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: SMOKE GOGGLES — SCRATCHED (COCKPIT) · airframe 26,319 hrs · 23,143 cycles

FIRST OFFICER`S SMOKE GOGGLES BIG SCRATCH. SWAP FIRST OFFICER`S SMOKE GOGGLES WITH OBSERVERS. DEFER OBSERVERS SMOKE GOGGLES IAW MEL 25-12-11. OK FOR SERVICE. INSTALLED SERVICEABLE SMOKE GOGGLES IAW AMM 35-11-15.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 26,222 hrs · 23,052 cycles

LEFT OVERWING MOST REARWARD EMER EXIT LIGHT INOPERATIVE. ALL OTHER EMERGENCY EXIT LIGHTS WORK. DEFERRED LT WING EMER LIGHT IAW 33-51-22 CAT C IAW KM MOC AUTH 003787. PLACARD INSTALLED, MORE INFORMATION TO COME.

Part: WIRE HARNESS — BROKEN (NLG) · airframe 26,207 hrs · 23,034 cycles

ON CLIMB OUT, A NOSE WHEEL STEERING INOPERATIVE. CAUTION MSG DISPLAYED. RAN QRH STILL INOPERATIVE. ACARSED DX & MX. CHECKED CB'S ALL IN. WENT MEM, LANDED NORMALLY & DECLARED EMER. JUST IN CASE, SET PARKING BRAKE & WAITED. FOUND BROKEN WIRE IN NLG HARNESS. R & R NLG HARNESS IAW AMM 32-61-25. SEE AML 2453677 FOR REPLACEMENT & ADJUSTMENT OF LT RVDT. OPERATIONS CHECKED GOOD.

Part: STRUT — LOW (NLG) · airframe 26,139 hrs · 22,972 cycles

AT SELECTION OF LG HANDLE UP, BOTH MAIN GEARS WENT UP BUT NOSE GEAR STAYED DOWN. STEERING INOPERATIVE CAUTION MSG, WOW INPUT CAUTION MSG & WOW OUTPUT FAIL LIGHT ALL ILLUMINATED. RAN QRH, BOTH MAIN GEARS EXTENDED NORMALLY & NOSE GEAR REMAINED EXTENDED. COMPLETED PA05-018K, SCENARIO 1. FOUND NOSE STRUT TO BE LOW ON FLUID. SERVICED NLG STRUT IAW AMM 12-12-32, NO LEAKS NOTED. SWUNG GEAR, OPERATIONS CHECKED GOOD. TAXIED ACFT, NO ISSUES NOTED. STRUT EXTENSION IS GOOD. NWS OPERATIONS CHECKED GOOD.

Part: CONNECTOR — FAULTY (CABIN) · airframe 26,058 hrs · 22,892 cycles

EMERGENCY FLOOR LIGHTS AT ROW 8 INOPERATIVE. R & R FAULTY CONNECTOR FOR EMERGENCY FLOOR LIGHTS AT ROW 8. EMERGENCY LIGHTS TESTED GOOD IAW AMM 33-51-01.

Part: FLAP — OBSTRUCTED (WING) · airframe 25,793 hrs · 22,623 cycles

FLAPS FAIL PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I, AMOC DATED JULY 22, 2013 & PA AD 27-052N. REMOVED SNOW & ICE CONTAMINATION FROM FLAPS. OPERATIONS CHECKED GOOD IAW AMM 27-54-00, NO DAMAGE FOUND.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,447 hrs · 22,313 cycles

NUMBER 2 EMERGENCY LIGHT BATTERY PACK INOPERATIVE. R & R NR 2 EMERGENCY BATTERY PACK IAW AMM 33-51-04, OPERATIONS CHECKED GOOD.

Part: DOOR — INOPERATIVE (OXYGNE DEPLOY) · airframe 25,146 hrs · 22,019 cycles

PASSENGER OXYGEN MASKS AT SEATS 7AB AND 8AB FAILED TO DEPLOY. R & R HATCHES AT 7AB AND 8AB IAW AMM 35-21-05-000-801 AND 400-801, OPS CHECKED GOOD IAW AMM 35-20-00-00-710-801.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 25,146 hrs · 22,019 cycles

EMERGENCY LIGHT FOUND TO HAVE MULTIPLE CONNECTORS DAMAGED. R & R DAMAGED CONNECTORS ON EMERGENCY LIGHT IAW ESPM 20-16-00. COMPLIED WITH OPS CHECK OF EMERGENCY LIGHT IAW AMM 33-51-00-710. NO DEFECTS NOTED.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,818 hrs · 25,028 cycles

VERTICAL BEAM INBD SIDE AT LBL 27 BS 409+128 IS CRACKED AT LOWEST FASTENER HOLES. REPAIRED IAW REO 601R-53-41-056.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 25,134 hrs · 22,009 cycles

RT WING LOWER PLANK ACCESS HOLE 650AB CORRODED AND PITTED IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 25,134 hrs · 22,009 cycles

RT WING LOWER PLANK ACCESS HOLE 640FB CORRODED AND PITTED IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 25,134 hrs · 22,009 cycles

RIGHT WING LOWER PLANK ACCESS HOLE 650BB CORRODED AND PITTED IN CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: FLOOR SUPPORT — CORRODED (BS 574) · corrosion level 2 · airframe 25,134 hrs · 22,009 cycles

CARGO BAY FLOOR SUPPORT HAS CORROSION NEAR FS 574, LBL 27. REPAIRED IAW REO 601R-53-61-3778.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 25,134 hrs · 22,009 cycles

RT WING LOWER PLANK ACCESS HOLE 640AB CORRODED AND PITTED IN CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: RIB — CRACKED (WING) · airframe 25,134 hrs · 22,009 cycles

RIGHT BATTERY RIB AT WS 53.6 CRACKED. REPAIRED IAW REO 601R-57-51-046.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 25,134 hrs · 22,009 cycles

RIGHT WING PLANK LOWER ACCESS HOLE 640BB AT WS 54.897 CORRODED. REPAIRED IAW REO 601R-57-21-030.

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 25,134 hrs · 22,009 cycles

MX FOUND THE UPPER FLANGE OF FLOORBEAM AT BS 349 TO BE CORRODED RBL 32.75 - 36. 100 PERCENT MATERIAL LOSS. REPAIRED IAW CRJ253-01774 .

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,134 hrs · 22,009 cycles

OTBD ANGLE AT FS 280 ON RBL 9 AND LBL 9 CRACKED. REPAIRED IAW REO 601R-53-11-171.

Part: RIB — CRACKED (WING) · airframe 25,134 hrs · 22,009 cycles

RIGHT BATTERY RIB AT WS53.60 IS CRACKED. REPAIRED IAW REO 601R-57-51-046.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 24,188 hrs · 21,097 cycles

CO-PILOT LIFE VEST BAG TORN. REMOVED AND REPLACED CO-PILOT LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,944 hrs · 20,864 cycles

SECOND FROM REAR CEILING EMERGENCY LIGHT INOPERABLE. RELAMPED CEILING EMERGENCY LIGHT PER CRJ AMM 33-51-14. OPS TEST GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 23,827 hrs · 20,744 cycles

1 EA INFANT LIFE VEST HAS HOLE IN BAG. REMOVED & REPAIRED 1 INFANT LIFE VEST IAW PA 25-096A.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,795 hrs · 20,717 cycles

OBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 23,656 hrs · 20,579 cycles

CAPTAINS OXYGEN MASK HARNESS HAS A LEAK. REPLACED CAPTAINS O2 MASK PER AMM 35-11-12. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,319 hrs · 20,096 cycles

FORWARD OVERHEAD CEILING EMERGENCY FLOODLIGHT INOP. REPLACED BULB P/N WL-1317 IAW AMM 33-51-16. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 23,099 hrs · 19,990 cycles

CAPTAIN'S AND FIRST OFFICER’S EMERGENCY FLASHLIGHT FAILS "RED" LED TEST. REMOVED AND REPLACED CAPTAIN'S AND FIRST OFFICER’S FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW AMM 25-60-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 23,036 hrs · 19,925 cycles

FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLIGHT ATTENDANT BATTERY IN FLASHLIGHT IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,964 hrs · 19,852 cycles

CAPTAIN`S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN`S LIFE VEST IAW AMM 25-61-03.

Part: UNKNOWN — UNKNOWN (THRUST REVERSER) · airframe 22,928 hrs · 19,822 cycles

LEFT THRUST REVERSER WOULDN'T DEPLOY. OPS CHECKED LEFT THRUST REVERSER SEVERAL TIMES IAW AMM 78-30-00. NO DEFECTS NOTED, OK FOR SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (THRUST REVERSERS) · airframe 22,733 hrs · 19,627 cycles

ON LANDING, LEFT THRUST REVERSER LEVER DIFFICULT TO UNLOCK TO SPOOL REVERSE THRUST. MUST RELEASE BUTTON AFTER THRUST REVERSER UNLOCKS THEN PULL LEAVER UP WHICH IS ABNORMAL. OPS CHECKED GOOD OF LT THRUST REVERSER IAW AMM 78-30-00. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,590 hrs · 19,492 cycles

CAPTAIN AND FIRST OFFICER'S FLASHLIGHTS DEAD. REMOVED AND REPLACED CAPTAIN AND FIRST OFFICER'S FLASHLIGHTS IAW AMM 25-61-02.

Part: LIGHT — UNSERVICEABLE (CABIN) · airframe 22,118 hrs · 19,045 cycles

ROW 1 FLOOR EMERGENCY LIGHTS ARE UNSERVICEABLE. REPLACED FWD FLEXIBLE LAMP & ORANGE OVERLAY IAW AMM 33-51-01. OPS TEST OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,069 hrs · 18,991 cycles

EXTERIOR FUSELAGE EMERGENCY LIGHT ON LT - 2, 3, 4 RT - 1, 2, 3 INOP. REMOVED AND REPLACED EXTERIOR FUSELAGE EMERGENCY LIGHTS 2, 3, 4 ON THE LT SIDE AND 1, 2 & 3 ON THE RIGHT SIDE IAW CRJ200 AMM 33-51-21. OPC GOOD. OK FOR SVC.

Part: RELAY — DEFECTIVE (FUEL SYSTEM) · airframe 21,746 hrs · 18,746 cycles

XFLOW/APU PUMP CAUTION. REPEAT. REMOVED AND REPLACED RELAY UQ4B IQ OB10 IAW ESPM 20-17-10 OPS CHECK OK. REMOVED AND REPLACED APU POWER FUEL PUSH BUTTON IAW CRJ ESPM 20-24-00. THIS CLEARS DM 56040. PLACARD REMOVED OK FOR SERVICE.

Part: TRANSDUCER — DEFECTIVE (APU) · airframe 21,656 hrs · 18,588 cycles

APU SHUTOFF AND RT FUEL PUMP FAIL DURING PUSH BACK. REMOVED AND REPLACED APU MOTION PICK-UP TRANSDUCER AND ECU AS A PRECAUTIONARY STEP IN T/S APU. COULD NOT REPRODUCE DISCREPANCY. OP CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM) · airframe 21,494 hrs · 18,436 cycles

AT 25,000 RIGHT X-FLOW CAUTION STAYED ON FOR APPROX 2 MIN THEN WENT OUT. X-FLOW MSG CLEARED W/POWER RESET PER AMM 28-20-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,326 hrs · 18,282 cycles

EMERGENCY LIGHTS NR 3 INVERTER INOP. REMOVED AND REPLACED NR 3 INVERTER IAW AMM 33-51-00. OPS CHECK GOOD. VERIFIED PART NUMBER EFFECTIVITY.

Part: INDICATION SYS — ACTIVATED (COCKPIT) · airframe 21,007 hrs · 17,988 cycles

ON APPROACH INTO DTW CREW DECLARED CLASS II EMERGENCY DUE TO LEFT ENGINE THRUST REVERSER UNLOCKED INDICATION, A/C LANDED WITHOUT INCIDENT.

Part: A/C PACK — FAULTY (RIGHT) · airframe 20,860 hrs · 17,857 cycles

CREW & PAX REPORTED SMELLING SMOKE DURING TAXI OUT. A/C RETURNED TO GATE. OUTSTATION MAINTENANCE INVESTIGATED AND FOUND THE RT PACK AT FAULT, DEFERRED PER MEL.

Part: ISIS UNIT — MALFUNCTIONED (COCKPIT) · airframe 20,104 hrs · 17,186 cycles

REJECTED T/O FOR ISIS INOP. REMOVED AND REPLACED ISIS AMM 34-14-01. OK FOR SERVICE. GOOD FOR RVSM.

Part: LINE — LEAKING (APU) · airframe 19,797 hrs · 16,897 cycles

WHILE SITTING AT GATE C15 IN DTW THE APU PERFORMED AN AUTO SHUTDOWN. THE FLIGHT CREW SMELLED SMOKE AND SAW IT COMING FROM THE GASPERS. THE PASSENGERS WERE EVACUATED AND CFR RESPONDED. NO FIRE OR HOT SPOTS WERE FOUND. MAINTENANCE FOUND THAT THE APU ENCLOSURE WAS SOAKED IN OIL. FURTHER INVESTAGATION FOUND A RUPTURED OIL LINE ON THE APU. THE ENCLOSURE WAS CLEANED, THE APU DEFERRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BUSHING — MIGRATED (RT MLG TRUNNION) · airframe 19,629 hrs · 16,761 cycles

RT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED. REMOVED AND REPLACED RT MLG AFT TRUNNION BUSHING IAW CRJ 20O AMM 20-26-00, BOMBARDIER RIL 1115 REV B AND GREO 601R-57-21-003.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,629 hrs · 16,761 cycles

CRACKED FS 559.00 BULKHEAD WEB REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB LAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B, DEVIATION "E".

Part: RECEPTACLE — DAMAGED (EXTERNAL POWER) · airframe 19,628 hrs · 16,759 cycles

THE GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE WAS DAMAGED. THE DAMAGE CONSISTS OF THE POWER RECEPTACLE BEING PULLED FROM THE INSTALLED POSITION IN THE RECESSED PAN AREA. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-280. REPEAT INSPECTIONS DAILY, FLY ON FOR 10 DAYS WITHIN WHICH TIME REPLACE THE DAMAGED P/N 600-33283-33 PAN SUPPORT MEMBER WITH A NEW, SERVICEABLE PART.

Part: ECU — FAILED (TE FLAP) · airframe 17,004 hrs · 14,295 cycles

FLAPS FAIL CAUTION MESSAGE AFTER START WITH ZERO DEGREE INDICATION. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I) PER AMOC DATED MARCH 27-2009 AND PA 27-052C. REMOVED FECU, CODES-51A REPLACED WITH SERVICEABLE FECU IAW AMM 27-51-05, OPS CHECK OK.

Part: BULKHEAD — CRACKED (BS 202) · airframe 16,715 hrs · 14,028 cycles

3 CRACKS FOUND ON FWD PRESSURE BULKHEAD FS 202.75 AT BL 23.71 AT THE PARKING BRAKE CABLE CUT OUT DURING AN "A" CHECK INSPECTION. THE CRACKS MEASURES IN LENGTH .50 INCH AT THE 5:00 POSITION, .250 INCH AT 7:00 POSITION AND .625 INCH AT 11:00 POSITION. MAJOR REPAIR IS UNDERWAY IAW GREO 601R-53-11-563.

Part: ENGINE — FLAMED OUT (RIGHT)

ON APPROACH, ATC ISSUED DESCENT CLEARANCE TO 9000. BOTH THRUST LEVERS WERE REDUCED TO IDLE AT WHICH POINT THE FLIGHT CREW NOTICED A SEVERE YAW IN THE ACFT AND RT ENG OIL PRESSURE MASTER WARNING. ECIAS INDICATED A FLAMEOUT OF THE RT ENGINE. THE FLIGHT CREW DECLARED AN EMERGENCY, PERFORMED THE QRH FOR SINGLE ENGINE APPROACH. AN OTHER WISE NORMAL APPROACH AND LANDING WAS MADE. CFR MET THE ACFT AND SOC CLEARED IT TO THE GATE. MX INSPECTED THE ENGINE AND PERFORMED A GROUND RUN WITH ACCELERATION AND DECELERATION CHECKS. NO REPEAT OF THE FLAMEOUT OCCURRED AND THE ACFT WAS RELEASED FOR SERVICE. NO FURTHER PROBLEMS OCCURRED UNTIL MARCH 2, 2009. ON THAT DATE THE ACFT WAS TAXIING TO THE GATE AND THE RT ENGINE FLAMED OUT WHEN THE THRUST LEVER WAS BROUGHT TO IDLE. MX FOUND THE THROTTLE ROD TO BE OUT OF RIG. THE THROTTLE WAS RIGGED, THE ENGINE RUN UP AND THE ACFT WAS RELEASED FOR SERVICE. (K)

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL ON APPROACH. RESET FLAPS AND PLACED ON 72 HOUR MONITORING PER AD 2006-12-21.

Part: COMPUTER — MALFUNCTIONED (SKEW DETECTION) · airframe 10,246 hrs · 8,872 cycles

FLAP FAILURE MESSAGE. SYSTEM TROUBLESHOT DETERMINE TO BE THE SKEW DETECTION COMPUTER FAILURE. COMPUTER CHANGED PER BOMBARDIER AMM, OPERATIONAL CHECKED GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 10,007 hrs · 8,666 cycles

FLAPS FAIL AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. RESET SYSTEM AND PLACED ON 72 HOUR MONITORING PER AD 2006-12-21.

Part: FCU — FAILED (TE FLAPS) · airframe 10,008 hrs · 8,667 cycles

FLAPS FAILED AT 8 DEGREES ON APPROACH. LANDING UNEVENTFUL. REMOVED AND REPLACED FECU PER BOMBARDIER AEROSPACE AIRCRAFT MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD.

Part: PUMP — DEFECTIVE (HYDRAULIC SYS) · airframe 8,785 hrs · 7,567 cycles

UPON CLIMBOUT WHEN SELECTING GEAR UP RECEIVED GEAR DISAGREE MESSAGE. QRH FOLLOWED, RETURNED TO MEM WITH UNEVENTFUL LANDING. MAINT FOUND NR 3 HYDRAULIC PUMP LOW PRESSURE, REMOVED AND REPLACED PUMP OPERATIONAL CHECK PER AMM.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 7,748 hrs · 6,725 cycles

DURING ROUTINE INSPECTION TASK, CREW ESCAPE HATCH OUTER HANDLE DID NOT EJECT WHEN OPENING ESCAPE HATCH WHEN UTILIZING INSIDE HANDLE. OUTER HANDLE IS RECESSED INTO HATCH FOR AERODYNAMIC PURPOSES. UPON INSPECTION, OUTER HANDLE WAS FOUND FROZEN IN PLACE (FLUSH) DUE TO CORROSION.