N8516C

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,553 hrs · 24,400 cycles

CAPTAIN`S SIDE EMERGENCY FLASHLIGHT NOT BLINKING, SUSPECT DEAD BATTERY. R & R CAPTAIN`S SIDE EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-61-00, OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 27,548 hrs · 24,395 cycles

CABIN FLIGHT DECK FLASHLIGHT SEAL BROKEN. R & R SEAL IAW CRJ200 AMM 25-61-01, OK FOR SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 27,356 hrs · 24,219 cycles

EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. , PERFORMED OP CHECK OF EMERGENCY LIGHT IAW AMM 33-51-01. ALL EMERGENCY LIGHT OPERATE NORMALLY WITH COCKPIT AND F/A PANEL SWITCHES. THIS CLEARS DI 17501.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,863 hrs · 19,120 cycles

ONE OVER-WING EXTERIOR EMERGENCY LIGHT INOPERATIVE ON EACH SIDE OF THE FUSELAGE. R & R SHORTED BULB IAW AMM 33-51-14. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,831 hrs · 22,719 cycles

FLIGHT ATTENDANT FLASHLIGHT FAILED TEST. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-02. OPC GOOD. OK FOR SERVICE.

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 25,795 hrs · 22,683 cycles

ON FLIGHT 3887 FROM PIT TO MEM RECEIVED GEAR DISAGREE WITH NOSE DOOR OPEN AND WOW INPUT MESSAGE. THE GEAR THEN SHOWED DOWN 3 GREEN WITH WOW INPUT CAUTION MESSAGE STILL PRESENT AND WOW OUTPUT FAIL STATUS. AIRCRAFT PERFORMED AIR RETURN TO PIT. FOUND THE GEAR DISAGREE WAS DUE TO THE TORQUE LINKS BEING DISCONNECTED. FOUND THE UPPER TORQUE LINK WAS DAMAGED .015" DEEP AND 7/8" IN DIAMETER. COMPLIED WITH PA 05-018J SCENARIO 1. FORWARDED ALL INFORMATION TO BOMBARDIER AND GOT RELIEF PER REO 601R-32-20-060 TO CHANGE THE UPPER TORQUE LINK AND DAMAGED T- HANDLE WITHIN 10 FLIGHT CYCLES, SCHEDULED TO RON IN CWA TONIGHT TO HAVE THE TORQUE LINK CHANGED AND SCHEDULED IN DTW TO HAVE THE T- HANDLE CHANGED OUT. AIRCRAFT IS OK FOR SERVICE.

Part: TORQUE LINK — UNSECURE (NLG) · airframe 25,910 hrs · 22,687 cycles

ON FLIGHT 4223 RECEIVED GEAR DISAGREE MESSAGE 6 SECONDS AFTER TAKEOFF OUT OF PVD AND GEAR SELECTED UP. MAIN GEAR SHOWED UP AND LOCKED AND NOSE GEAR SHOWED DOWN. THE CREW OPERATED THE MANUAL RELEASE SYSTEM AND THE NOSE SHOWED LOCKED DOWN. AIRCRAFT PERFORMED AIR RETURN TO PVD FOR THE GEAR DISAGREE. UPON LANDING AROUND 80 KTS AND LOWER THE CREW REPORTED THE NOSE SHAKING A LOT. WHEN ALMOST STOPPED THE CREW HEARD WHAT THEY DESCRIBED AS THE SOUND OF THE TORQUE LINK HITTING THE GROUND. ONCE THE AIRCRAFT STOPPED THEY HAD NO NLG STEERING. THE AIRCRAFT WAS TOWED FROM THE TAXIWAY TO THE GATE. C/W PA 05-018I SCENARIO 1. FOUND NLG TORQUE LINKS NOT PROPERLY SECURED. A/C OK FOR SERVICE.

Part: HINGE — WORN (FUSELAGE) · airframe 25,701 hrs · 22,583 cycles

IN HEAVY CHECK, PAX DOOR HINGE IS WORN (AIRCRAFT SIDE). REMOVED AND REPLACED PAX DOOR HINGE (AIRCRAFT SIDE) IAW CRJ 200 SRM 53-21-23.

Part: HINGE — WORN (PAX DOOR) · airframe 25,701 hrs · 22,583 cycles

IN HEAVY CHECK, PAX DOOR HINGE IS WORN (DOOR SIDE). REMOVED AND REPLACED DOOR SIDE HINGE ON PASSENGER DOOR IAW CRJ 200 SRM 52-10-31.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 25,697 hrs · 22,581 cycles

RIGHT NR 3 FLOOR SEAT TRACK GOUGED. REPAIRED AIW SRM 53-21-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,697 hrs · 22,581 cycles

LEFT NR 2 SIDE SEAT TRACK IS CORRODED. REPLACED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,697 hrs · 22,581 cycles

RIGHT NR 6 SEAT TRACK CORRODED AND GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,697 hrs · 22,581 cycles

RIGHT NR 4 SEAT TRACK CORRODED AND GOUGED. REPAIRED IAW AMM 53-01-11.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 25,697 hrs · 22,581 cycles

AFT PRESSURE BULKHEAD AT FS 621 HAS AREAS OF SCREW CHAFES. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,697 hrs · 22,581 cycles

RIGHT NR 7 SEAT TRACK CORRODED AND GOUGED. REPAIRED IAW AMM 53-01-11.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 25,135 hrs · 22,011 cycles

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

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 25,068 hrs · 21,947 cycles

ON LANDING, USED THRUST REVERSER, STOWED IT, THE LEFT UNLOCK MESSAGE CAME ON. LEFT ENGINE THEN SHUTDOWN WITH THRUST REVERSER LEVER AT IDLE. LEFT INDICATIONS NORMAL EXCEPT REVERSER AND UNLOCK LIGHTS ON. PERFORMED ENGINE RUN IAW AMM 71-00-00 AND OPS CHECKED BOTH THRUST REVERSERS IAW AMM 78-30-00. NO DEFECTS NOTED, FOUND LEFT THRUST REVERSER UNSTOWED. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (THRUST REVERSER) · airframe 24,600 hrs · 21,481 cycles

LEFT TR WOULD NOT DEPLOY ON LANDING. LEFT TR CHECKS GOOD IAW AMM 78-30-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 24,440 hrs · 21,320 cycles

LEFT SEAT RAIL AFT OF FS 409+128 GOUGED, NICKED, AND CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 24,440 hrs · 21,320 cycles

LEFT NR 3 SEAT TRACK AT LBL 9 CORRODED AND GOUGED. REPAIRED IAW BOMBARDIER REO 601R-53-00-005.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,440 hrs · 21,320 cycles

RIGHT SIDE SEAT RAIL FORWARD OF FS 409+128 GOUGED AND CORRODED. REPAIRED IAW SRM 53-21-49.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 24,440 hrs · 21,320 cycles

LEFT SIDE NR 2 SEAT TRACK AT LBL 9 CORRODED AND GOUGED. REPAIRED IAW SRM 53-21-49.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,390 hrs · 21,275 cycles

F/A'S FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHILGHT BATTERY IAW AMM 25-61-02.

Part: UNKNOWN — MALFUNCTIONED (SPOILER SYS) · airframe 23,986 hrs · 20,927 cycles

WITH ALL HYDRAULICS ON RECEIVED FLT SPLRS AND SPOILERONS CAUTION MESSAGE. RESET A/C POWER PER AMM 20-00-00. MSG CLEARED.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 23,694 hrs · 20,588 cycles

OVERHEAD EMERGENCY LIGHTS OVER ROW 8, FLIGHT ATTENDANT NOTIFICATION LIGHTS INTERMITTENT IN FLIGHT (LOWER LEFT CORNER). COULD NOT DUPLICATE DISCREPANCY. FLT ATT CALL LIGHTS OP TEST OK IAW AMM 33-22-03. OK FOR SERVICE.

Part: SWITCH — OUT OF POSITION (COCKPIT) · airframe 23,075 hrs · 20,048 cycles

AFTER CREW DEPLANED, GROUND CREW NOTICED FLAMES IN APU EXHAUST. FIRE CREW NOTIFIED. FLIGHT CREW ALERTED AND RETURNED TO AIRCRAFT. SMALL FLAME WAS OBSERVED IN THE APU EXHAUST WITH EVIDENCE OF FUEL ON THE RAMP BELOW THE APU. PWR FUEL SWITCH FOUND IN ON POSITION WITH EXTERNAL POWER ACTIVE. CREW SELECTED PWR FUEL SWITCH TO OFF. FLAME SELF EXTINGUISHED. MAINTENANCE INSPECTED. NO DAMAGE REPORTED BUT FUEL SMELL WAS PRESENT. APU DIFFERED PER MEL 49-10-11.

Part: SHUTOFF VALVE — LOOSE (APU) · airframe 23,062 hrs · 19,997 cycles

CREWS REPORTED FUEL SMELL IN COCKPIT INBOUND "NO"EMERGENCY DECLARED LANDED WITHOUT INCIDENT NSP'D - FOUND APU FUEL FEED S/O VALV OUTLET CONNECTION LOOSE. TIGHTENED AND LEAK CHECKED GOOD IAW AMM 49-30-00.

Part: PUMP — LEAKING (RT ENGINE) · airframe 22,360 hrs · 19,349 cycles

FLIGHT DIVERTED DUE TO RIGHT ENGINE LOW OIL PRESSURE INDICATION ENGINE WAS SHUT DOWN IN FLIGHT EMERGENCY WAS DECLARED FOUND RT ENGINE EDP LEAKING. DEFERRED EDP IAW MEL 29-11-01 DM-39183.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,028 hrs · 19,035 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: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 20,792 hrs · 17,884 cycles

FOUND LEVEL 2 CORROSION ON AVIONICS DOOR, AFT SEAL RETAINERS. REMOVED AND REPLACED TWO AFT AVIONICS DOOR SEAL RETAINERS, P/N CC670-38675-3 AND CC670-38662-5 IAW CRJ200 SRM 51-42-06.

Part: FLAP SYSTEM — OUT OF RIG (TE FLAPS) · airframe 19,683 hrs · 17,260 cycles

MAY 25, 2009, CREW RECEIVED "FLAP FAILURE" MESSAGE ON CLIMBOUT WHEN SELECTING FLAPS TO UP. MX INSPECTED THE ACFT AND TROUBLESHOT IAW MFG FAULT ISOLATION MANUAL, FLAPS FOUND TO BE OUT OF RIG. FLAPS RIGGED IAW MM WITH OPS CHECKS PERFORMED WITH NO DEFECTS.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 11,073 hrs · 9,678 cycles

ON CLIMBOUT UPON GEAR SELECTED UP RECEIVED GEAR DISAGREE. QRH FOLLOWED RETURNED TO MEMPHIS, UNEVENTFUL LANDING. GEAR SWINGS PERFORMED AND TROUBLESHOT TO AN OUT OF ADJUSTMENT PROX SENSOR. ADJUST PROX SENSOR IAW AMM, OPERATIONAL CHECKS GOOD.