N257PS

Part: WARNING MESSAGE — FALSE ACTIVATION (APU FIRE) · airframe 36,305 hrs · 36,083 cycles

APU FIRE RED WARNING MESSAGE IN FLIGHT. DEFERRED APU. PER FIM VISABLY INSPECTED APU FIRE LOOP NO DEFECTS NOTED PERFORMED OPS CHECK OF APU FIRE-DETECTION SYSTEM IAW CRJ 200 AMM OPS CHECK GOOD AT THIS TIME. THIS CLEARS MEL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,529 hrs · 35,370 cycles

EMERGENCY LIGHTS WON'T STAY ON. R&R ALL 4 EMERGENCY POWER SUPPLY BATTERIES IAW CRJ 200 AMM 33-51-04-000/400-801. OPS CHECK GOOD AT THIS TIME. S/N 169577, 121949, 103966, 126070

Part: INVERTER — FAILED (CABIN) · airframe 35,270 hrs · 35,127 cycles

LH LOWER EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LH FLOOR LEVEL FLOOD EXIT SIGN IAW CRJ 200 AMM 33-51-10-000/400-801 REMOVED AND REPLACED #2 INVERTER IAW CRJ 200 AMM 33-51-07-000/400-801 OPS CHECK GOOD

Part: EXHAUST VALVE — MALFUNCTIONED · airframe 33,864 hrs · 33,839 cycles

DURING CLIMB CREW RECEIVED AN OVERBOARD COOL AMBER MSG. AFTER RUNNING THE QRH THE MSG STILL PERSISTED. CREW DECIDED TO CONTINUE TO CLT PRESSURIZED AND DECLARED AN EMERGENCY INTO CLT. MAINTENANCE DEFERRED OVERBOARD EXHAUST VALVE AND INBOARD EXHAUST VALVE.

Part: FRAME — CRACKED (BS 718) · airframe 32,099 hrs · 32,148 cycles

FRAME CRACKED AT BS 718, STRINGER 11L. REMOVED AND INSTALLED A NEW FRAME SECTION IAW SRM 51-42-06 & 51-23-16.

Part: TRUNNION — CRACKED (LT MLG) · airframe 32,099 hrs · 32,148 cycles

ONE INDICATION NOTED IN FASTENER HOLE OTBD OF MLG CUT OUT ON RT SIDE 5TH HOLE GOING FWD FROM AFT HOLE IN STEEL STRAP ON O/B AFT SIDE OF HOLE .550 INCH UP FROM LOWER SURFACE OF STEEL STRAP EXTENDING UP .100 INCH. PERFORMED EDDY CURRENT INSPECTION AT THE RT MLG TRUNNION FOUND REMAINING INDICATION TO BE 7% FSH WITH SAME LOCATION AND DIMENSIONS, FAILED NDT INSPECTION IAW REO 601R-57-21-2703, REV-P1. REPAIRED IAW REO 601R-57-21-2703 REV --.

Part: ANGLE — CRACKED (BS 484 FLOORBEAM) · airframe 32,099 hrs · 32,148 cycles

FLOORBEAM AT BS 484, LBL27 HAS A CRACKED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,099 hrs · 32,148 cycles

REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 76, ONE INCH LONG. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E, SHEET 13, SECTION 5D. THE CUTOUT IS OUTSIDE OF REO 601R-53-61-1285 REPAIR SCOPE. PERFORMED EDDY CURRENT ON REWORKED AREAS IAW REO 601R-53-61-1285, REV E, SHEET 9, NOTE 4. NO INDICATIONS NOTED. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,099 hrs · 32,148 cycles

REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATIONS, LBL 27.5, WL 130. ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1541, REV F. PERFORMED AN EDDY CURRENT OF REWORKED AREA IAW REO 601R-53-61-1541, REV F. NO INDICATIONS NOTED. REPAIRED IAW REO 601R-53-61-1541, REV F.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,099 hrs · 32,148 cycles

PAX DOOR AFT DRAG ANGLE CRACKED ADJACENT TO POWER ASSIST PULLEY BRACKET. REPAIRED THE DRAG ANGLE IAW EO 2B19-52-L05444A, PART B, AND REO 601R-52-11-513 REV B.

Part: FRAME — CRACKED (BS 718) · airframe 32,099 hrs · 32,148 cycles

FRAME CRACKED AT BS 718, STRINGER 11R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 362-409) · corrosion level 3 · airframe 32,099 hrs · 32,148 cycles

CORROSION ON LEFT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,099 hrs · 32,148 cycles

REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 9.5, WL 109, ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E. PERFORMED EDDY CURRENT OF REWORKED AREAS IAW REO 601R-53-61-1285 REV E, NO INDICATIONS NOTED. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.

Part: TRUNNION — CRACKED (LT MLG) · airframe 32,099 hrs · 32,148 cycles

ONE INDICATION NOTED IN FASTENER HOLE O/B OF MLG CUT OUT ON LT SIDE FIRST HOLE AFT OF STEEL STRAP. ON AFT SIDE OF HOLE .300 INCH UP FROM LOWER SURFACE OF PLANK EXTENDING UP .100 INCH. REPAIRED THE TRUINNION IAW REO 601R-57-21-2704 REV.

Part: ANGLE — CRACKED (BS 621-625) · airframe 32,099 hrs · 32,148 cycles

AFT EQUIPMENT BAY LEFT BS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 362-409) · corrosion level 3 · airframe 32,099 hrs · 32,148 cycles

CORROSION ON RT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.

Part: CONNECTOR — DIRTY (FIRE BOTTLE) · airframe 31,157 hrs · 31,274 cycles

CREW RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE AT FLIGHT LEVEL 290. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITH OUT INCIDENT. FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE CLEANED THE CONNECTOR PLUGS ON THE FIRE BOTTLES AND PREFORMED AN OPS CHECK OF THE SYSTEM AND EVERYTHING OPS CHECKED GOOD AND NO DEFECTS WERE FOUND.

Part: CONTROL LEVER — FAULTY (TE FLAPS) · airframe 29,538 hrs · 29,697 cycles

FLAPS FAILED DURING APPROACH AT 30 DEGREES AND 160 KNOTS. LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLAP CONTROL LEVER AND PREFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,537 hrs · 29,694 cycles

EMERGENCY FLOOR TRACK LIGHTING OUT AFTER ROW 5 TO THE BACK SIDEWALL. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM AND THE NR 4 POWER SUPPLY BATTERY FOR THE EMERGENCY LIGHTS IAW AMM, OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,534 hrs · 29,694 cycles

RIGHT LOWER FLOODLIGHT INOPERATIVE. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM, OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,222 hrs · 29,382 cycles

CAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD AND WINDSHIELD TEMP CONTROLLER. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — INOPERATIVE (WINDSHIELD TEMP) · airframe 29,222 hrs · 29,382 cycles

CAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD AND WINDSHIELD TEMP CONTROLLER. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 28,909 hrs · 29,059 cycles

DURING CLIMBOUT, THE CREW RECEIVED A RT PACK FAULT AND RT PACK HIGH PRESSURE WHEN COMPLYING WITH MEL PROCEDURES FOR THE LT PACK. MAINTENANCE INTEROGATED AND FOUND NO RELATED FAULTS FOR THE RT PACK AND COULD NOT DUPLICATE THE ISSSUE. MAINTENANCE PERFORMED CHECK IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: PLATE — CORRODED (BS 310) · corrosion level 2 · airframe 28,693 hrs · 28,838 cycles

PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE CORRODED. R & R PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE, PN 600-38061-11 IAW AMM 52-11-17-400-804.

Part: FLOOR SUPPORT — CORRODED (BS 513) · corrosion level 2 · airframe 28,693 hrs · 28,838 cycles

RIGHT PRESSURE FLOOR SILL STRAP CORRODED BEYOND LIMITS AT FS 513.00. R & R RT PRESSURE SILL STRAP IAW SRM 51-42-16, 51-42-22, AND 51-77-00.

Part: ANGLE — CORRODED (BS 310-349) · corrosion level 2 · airframe 28,693 hrs · 28,838 cycles

PAX DOOR UPPER SILL ANGLE CORRODED BETWEEN BS 310 AND 349. REPAIRED PAX DOOR UPPER SILL ANGLE, PN 601R31527-221 IAW SRM 51-42-10, 51-42-21, AND 51-42-06.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 28,682 hrs · 28,829 cycles

CREW REPORTED BACK HALF OF FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT, REPAIRED AFT CONNECTOR ON EMERGENCY LIGHT STRIP AND PERFORMED CHECKS IAW AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 28,107 hrs · 28,243 cycles

CREW REPORTED FLOOR EMERGENCY LIGHTS HAD A DISCONNECTED WIRE AND AFT HALF OF LIGHTS BEYOND ROW NINE INOPERATIVE. MAINTENANCE INSPECTED, SPLICED IN WIRE SPLICE CONNECTORS ON ROW 13 EMERGENCY FLOOR LIGHTS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — FAILED · airframe 26,799 hrs · 26,941 cycles

CREW REPORTED ANTI-ICE DUCT WARNING MESSAGE DURING CLIMB. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FUSELAGE SENSING ELEMENT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 25,572 hrs · 25,723 cycles

CREW REPORTED ENTRY LIGHT BROKEN. MAINTENANCE INSPECTED, R & R ENTRY FLOOR EMERGENCY FLOODLIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ACCESS DOOR — OUT OF ADJUST (CABIN) · airframe 24,647 hrs · 24,781 cycles

CREW REPORTED FORWARD F/A EMERGENCY EQUIPMENT ACCESS, LATCHES AND DOOR, STICKS AND HARD TO OPEN. MAINTENANCE INSPECTED, ADJUSTED EMERGENCY EQUIPMENT ACCESS DOOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 585-621) · corrosion level 2 · airframe 24,478 hrs · 24,616 cycles

DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND AROUND CARGO FLOOR SUPPORT FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO FLOOR SUPPORT WAS REPLACED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: CARGO TRACK — CORRODED (BS 559-604) · corrosion level 2 · airframe 24,478 hrs · 24,616 cycles

DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON THE CARGO TRACKS AT BS 559+80, 559.0+96 AND FS 574 - 605. THE AREA WAS INSPECTED AND CARGO FLOOR TRACKS WERE REPLACED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 23,825 hrs · 24,010 cycles

CREW REPORTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE AND COVER BROKEN. MAINTENANCE INSPECTED, R & R ROW 1 FLOOR-TRACK EMERGENCY LIGHT AND COVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 23,509 hrs · 23,705 cycles

CREW REPORTED EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROW 5 TO ROW 9. MAINTENANCE INSPECTED, R & R J391Y CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 22,875 hrs · 23,105 cycles

CREW REPORTED GEAR DISAGREE RED CAS MESSAGE. MAIN GEAR INDICATED DOWN AND LOCKED AND NOSE GEAR INDICATED UP. STEERING INOPERATIVE AMBER CAS MESSAGE ALSO REPORTED. CREW MANUALLY EXTENDED LANDING GEAR AND LANDED SAFELY. ACFT TOWED TO RAMP. MX TROUBLESHOT, R & R NLG SELECTOR VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROLLER — FAILED (ANTI-ICE SYS) · airframe 20,514 hrs · 20,995 cycles

CREW REPORTED CAPTAIN’S FRONT WINDOW CRACKED AND ELECTRICAL ARCING NOTICED. CREW RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED CAPTAIN’S FRONT WINDOW AND LEFT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,149 hrs · 19,741 cycles

CREW REPORTED LEFT AFT EXTERIOR DOOR EMERGENCY LIGHT OUT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT AFT EXTERIOR EMERGENCY LIGHT BULB AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 16,941 hrs · 17,607 cycles

CREW REPORTED FLAPS FAILURE DURING APPROACH FLAPS SELECTED FROM 0-08 WHEN FAILURE OCCURED SPEED WAS 190 IAS, ALT 6000 FT. CREW ELECTED TO DIVERT TO CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS ON THE BRAKE AND POSITION SENSOR. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPUTER — FAILED (TE FLAP) · airframe 16,938 hrs · 17,605 cycles

CREW REPORTED A FLAPS FAIL AT 10,000FT SPEED 250KNTS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS ON THE FLAP ELECTRONIC COMPUTER. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 16,935 hrs · 17,602 cycles

CREW REPORTED FLAPS FAILURE WHEN FLAPS SELECTED FROM ZERO DEGREES TO EIGHT (8) DEGREES DURING APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 16,858 hrs · 17,539 cycles

CREW REPORTED FLAPS FAIL AT 20 DEGREES WHEN FLAPS WERE SELECTED TO 30 DEGREES WHILE ON APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 16,027 hrs · 16,709 cycles

DURING SCHEDULED MAINTENANCE, THE FS 280 TRANSVERSE BEAM WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 16,027 hrs · 16,709 cycles

DURING SCHEDULED MAINTENANCE THE LEFT PRESSURE FLOOR SILL HAD CORROSION AROUND NUT PLATES FROM FS 449.85 TO 473.15. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 16,027 hrs · 16,709 cycles

DURING SCHEDULED MAINTENANCE THE FS 409+128 BULKHEAD VERTICAL POST WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 15,768 hrs · 16,450 cycles

CREW REPORTED SMOKE IN THE COCKPIT AND CABIN AFTER TURNING ON THE APU AND SWITCHING BLEEDS ON DESCENT INTO DCA. CREW LANDED IN DCA WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE APU ENCLOSURE AND THE AIR CONDITIONING COOLING DUCTS. NO DEFECTS WERE NOTED. MAINTENANCE DETERMINED THE SOURCE OF THE SMELL AND SMOKE TO BE FROM THE APU. MAINTENANCE DEFERRED THE APU PER MEL AND PERFORMED AIR CONDITIONING SYSTEM CHECKS. AIRCRAFT WAS RELEASED FOR SERVICE. APU WAS SUBSEQUENTLY REMOVED AND REPLACED TO CLEAR THE DEFERRAL. ALL WORK WAS PERFORMED USING THE AIRCRAFT MAINTENANCE MANUALS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,916 hrs · 15,598 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FS 559.00 BULKHEAD WEB. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — FAULTY (PAX DOOR) · airframe 14,322 hrs · 15,023 cycles

CREW REPORTED AN OVERBOARD COOL FAIL MASTER CAUTION EN ROUTE FROM CLT TO BHM. CABIN ALTITUDE STARTED CLIMBING AND AIRCRAFT DEPRESSURIZED. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE PASSENGER DOOR WARNING SYSTEM MICRO SWITCH AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: MANIFOLD — PUNCTURED (APU) · airframe 13,947 hrs · 14,615 cycles

CREW REPORTED FUMES IN THE CABIN FROM THE APU AT TYS. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE APU PRIMARY FUEL MANIFOLD AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 9,960 hrs · 10,329 cycles

CREW REPORTED LIGHTNING STRIKE. MAINTENANCE INSPECTED ACFT AND REPAIRED DAMAGE ON RADOME AND LT WINGLET. NO OTHER DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S)

Part: UNKNOWN — UNKNOWN (NR 2 IDG) · airframe 6,299 hrs · 6,366 cycles

CREW REPORTED A LOSS OF THE NR 2 GENERATOR ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PROPERLY SERVICED THE NR 2 IDG IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: O-RING — CRACKED (NR 2 IDG) · airframe 6,201 hrs · 6,271 cycles

CREW REPORTED THE NR 2 GENERATOR FAILED ON TAKEOFF ROLL. CREW ABORTED TAKEFOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE NR 2 IDG AND FOUND CRACKED O-RINGS AND OIL LEAKING FROM THE STANDPIPE OVERFILL. MAINTENANCE REPLACED DAMAGED O-RINGS AND SERVICED THE OIL LEVEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — BIRD STRIKE (LT WING) · airframe 4,639 hrs · 4,613 cycles

CREW REPORTED BIRD STRIKE ON LEFT INBOARD WING. BIRD STRIKE INSPECTION WAS PERFORMED. NO DAMAGE WAS FOUND AND WING LEADING EDGE WAS CLEANED. AIRCRAFT WAS RELEASED TO SERVICE.

Part: FIRE LOOP — OUT OF POSITION (RT PYLON) · airframe 3,237 hrs · 3,233 cycles

THE RT 14TH DUCT WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH, DIVERTED TO ILH, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO CLT WHERE MAINTENANCE TROUBLESHOT THE SYSTEM IAW CRJ200 FIM 36-20-00. THE RT PYLON LOOPS WERE INSPECTED AND REPOSITIONED. EXTENSIVE GROUND RUN-UP AND OPERATIONAL CHECKS WITH ALL PNEUMATIC SYSTEMS ON WERE PERFORMED. NO FAULTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (HORIZONTAL STAB) · airframe 3,198 hrs · 3,198 cycles

AFTER LANDING THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THE RT HORIZONTAL STABILIZER TIP FAIRING. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. ALL DAMAGE FOUND WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 1,999 hrs · 1,933 cycles

DURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED A DENT ON THE BOTTOM OF THE LEFT INBOARD FLAP. MAINTENANCE REMOVED & REPLACED THE FLAP IAW CRJ 200 AMM 27-54-01-000-801 AND 27-54-01-400-801. THE SYSTEM WAS RIGGED AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.