N220PS

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,999 hrs · 32,800 cycles

SIDE SEAT RAIL SECTION FROM FS 409.00 PLUS 112 TO FS 455.00 ON LT SIDE IS CORRODED. INSTALLED REPLACEMENT LT SIDE SEAT RAIL P/N 601R38312-119S BETWEEN FS 409.00+112 TO 455.00 IAW AMM 53-00-11-400-802.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,999 hrs · 32,800 cycles

CRACK AT FS 333 FRAME TOOLING HOLE BETWEEN STR 1L AND STR 0. LOCATED AND DRILLED SERVICEABLE FRAME PN 601R32004-41 IAW SRM 51-40-11. INSTALLED NEW FRAME AT FS 333 IAW SRM 51-42-06 AND 51-42-21. PN 601R32004-41.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,999 hrs · 32,800 cycles

CRACKS ON THE FS 621 AFT PRESSURE BULKHEAD AND ATTACHING STRUCTURE AT LBL27.5/WL131-133, LBL18/WL74-75.5 AND WL130.5-133.5, LBL9.5/WL75-77, BL0/WL127.5-132, RBL18/WL74-75.5 AND RBL27.5/WL109-110.5. REPAIRED DAMAGED AREAS ON 621 BULKHEAD AND ATTACHING STRUCTURE IAW REO 601R-53-61-1240 REV D DATED 2016-10-31 AND REO 601R-53-61-6486 REV -- DATED 2018-03-17.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,999 hrs · 32,800 cycles

RT FS 718 FRAME IS CRACKED AT STR 11. LOCATED AND DRILLED LT FS 718 FRAME SECTOR IAW SRM 51-40-11.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,999 hrs · 32,800 cycles

STRAP AT FS 349 STR 3L IS CORRODED. REMOVED CORROSION IAW EA 43-2018-042.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,999 hrs · 32,800 cycles

SIDE SEAT RAIL SECTION FROM FS 409.00 PLUS 16 TO FS 409.00 PLUS 112 ON RT SIDE IS CORRODED. INSTALLED REPLACEMENT RT SIDE SEAR RAIL P/N 6DIR38312-29 BETWEEN FS 409 AND 16 TO 409 AND 112 IAW AMM 53-01-11-400-802.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,999 hrs · 32,800 cycles

LT FS 718 FRAME IS CRACKED AT STR 11. LOCATED AND DRILLED LT FS 718 FRAME SECTOR IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,999 hrs · 32,800 cycles

FLOOR SEAT RAIL SECTION AT RBL 9.0 FROM FS 364 TO FS 396.00 IS CORRODED. INSTALLED NEW SERVICEABLE FLOOR SEAT RAIL IAW AMM 53-01-11-400-802, 53-01-11-000-802.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,999 hrs · 32,800 cycles

RT SIDE FLOOR STRAP AT FS 559, LBL36 TO WALL IS CORRODED. REMOVED FLOOR STRAP AT FS 559 RBL 36 TO WALL IAW SRM 51-42-06-01. INSTALLED FLOOR STRAP AT FS 559 RBL 36 P/N 601R31025-29 IAW SRM 51-42-06.

Part: SKIN — CHAFED (FUSELAGE) · airframe 32,999 hrs · 32,800 cycles

EXTERIOR SKIN JUST AFT OF APU EXHAUST CUTOUT HAS 3 AREAS OF DAMAGE THAT ARE MARKED WITH RED MARKER. RECEIVED ENGINEERING ORDERS AND REPAIRED DAMAGED AREA IAW EA 25-2018-058

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,999 hrs · 32,800 cycles

FLOOR SEAT RAIL SECTION AT LBL 9.0 FROM FS 364 TO FS 396.00 IS CORRODED. INSTALLED NEW SERVICEABLE SEAT RAIL IAW AMM 53-01-11-400-802, 53-01-11-000-802.

Part: TRANSDUCER — FAULTED (ANTI SKID) · airframe 31,720 hrs · 31,643 cycles

DURING TAKEOFF AT 90 KNOTS, THE CREW RECEIVED AN INBOARD ANTI-SKID CAUTION MESSAGE AND ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT HAND INBOARD WHEEL SPEED TRANSDUCER AND CANNON PLUG AND REPAIRED WIRING TO LEFT HAND INBOARD WHEEL SPEED TRANSDUCER.

Part: WARNING LIGHT — FALSE ACTIVATION (FIRE BOTTLE) · airframe 31,713 hrs · 31,636 cycles

WHILE IN CRUISE THE CREW RECEIVED A CARGO FIRE BOTTLE LOW AMBER CAUTION MESSAGE. THE AIRCRAFT RETURNED TO FIELD. THE FIRE BOTTLE WAS FOUND TO BE WITHIN LIMITS AND THE AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 295-310) · airframe 4,675 hrs · 4,194 cycles

DENT BETWEEN BS 295-310, STRINGERS 14-15L. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE SKIN IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,807 hrs · 30,763 cycles

MIDSHIP FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE NR TWO EMERGENCY LIGHT BATTERY AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SIGN — UNSECURE (CABIN) · airframe 30,146 hrs · 30,132 cycles

EMERGENCY EXIT SIGN FELL DOWN. MAINTENANCE INSPECTED, REINSTALLED COVER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — WARNING MESSAGE (PARKING BRAKE) · airframe 29,952 hrs · 29,938 cycles

PARKING BRAKE SHUTOFF VALVE MESSAGE AFTER RETRACTION COMMAND INBD ANTI-SKID MESSAGE. MAINTENANCE TROUBLESHOT, R & R PARKING BRAKE SHUTOFF VALVE AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: TERMINAL — DAMAGED (FIRE PROTECTION) · airframe 29,924 hrs · 29,911 cycles

LEFT JET OVERHEAT FAIL CAUTION MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RING TERMINAL OF INBD WIRE AT LOOP A AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: MOUNT — CORRODED (BS 310-319) · corrosion level 2 · airframe 29,803 hrs · 29,793 cycles

GALLEY AFT MOUNT PLATE ON RT FLOOR SILL CORRODED BETWEEN FS 310-FS 319. REPLACED GALLEY AFT MOUNT PLATE, PN 601R38669-49 IAW SRM 51-40-11, 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559-569) · corrosion level 2 · airframe 29,803 hrs · 29,793 cycles

CARGO TRACK AT RBL 9 BETWEEN FS 559+91 - 569 CORRODED. REPLACED THE CARGO TRACK IAW AMM 53-01-11-000/400-802.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 29,803 hrs · 29,793 cycles

CARGO TRACK AT 27 BETWEEN FS 559+80- 559+96 IS CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11-000/400-802,

Part: CARGO TRACK — CORRODED (BS 559-597) · corrosion level 2 · airframe 29,803 hrs · 29,793 cycles

CARGO TRACK AT LBL 27, BETWEEN FS 559+80 - 567 CORRODED. REPLACED SEAT TRACKS IAW AMM 53-01-11-000/400-802.

Part: CARGO TRACK — CORRODED (BS 559-600) · corrosion level 2 · airframe 29,803 hrs · 29,793 cycles

CARGO TRACK AT LBL 9 BETWEEN FS 559+91 - 600 CORRODED. REPLACED THE CARGO TRACK IAW AMM 53-01-11-000/400-802.601R38779-5.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 27,658 hrs · 27,645 cycles

DURING EDDY CURRENT INSPECTION OF REAR PRESSURE BULKHEAD, FWD CRACK AT BL 0, WL 110.09 OF Z-MEMBER HEEL LINE. C/W REPAIRED IAW REO 601R-53-61-1285D.

Part: SKIN — DENTED (BS 635) · airframe 25,669 hrs · 25,660 cycles

DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN AT BS 635 DENTED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STIFFENER — CRACKED (BS 409) · airframe 25,669 hrs · 25,660 cycles

DURING SCHEDULED MAINTENANCE, BS 409.00 + 128 VERTICAL POST AT AFT FLANGE RADIUS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 25,089 hrs · 25,068 cycles

CREW REPORTED ABNORMAL BUMP, NOISE, & VIBRATION AFTER TAKEOFF. DECLARED AN EMERGENCY, LANDED SAFELY AT DESTINATION AIRPORT AND REPORTED LANDING NORMAL. MAINTENANCE PERFORMED GENERAL VISUAL INSPECTION OF FLAPS, SPOILERS, LANDING GEAR AND COMPONENTS, WHEELS, TIRES AND BRAKES. NO DEFECTS FOUND. MAINTENANCE PERFORMED ANTI-SKID CONTROL UNIT (ASCU) SYSTEM TEST AND WHEEL SPEED TRANSDUCER CHECK IAW AMM. OPS CHECKED GOOD. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.

Part: PUMP — LEAKING (MAIN HYDRAULIC S) · airframe 24,722 hrs · 24,720 cycles

CREW REPORTED HYD SYSTEM NR 1 PRESSURE LOW AND QUANTITY READING ZERO DURING FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND LEAK ON HYD EDP NR 1 AND HYD NR 1 PRESSURE MANIFOLD LINE. R & R NR 1 EDP, R & R NR 1 HYDRAULIC PRESSURE MANIFOLD LINE AND LINE CLAMPS AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,297 hrs · 24,326 cycles

CREW REPORTED AN APPROXIMATE 6 INCH SECTION OF FLOOR LEVEL EMERGENCY LIGHTS NOT WORKING. MAINTENANCE INSPECTED, R & R FORWARD SECTION OF EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 23,746 hrs · 23,825 cycles

CREW REPORTED FLOOR EMERGENCY LIGHTS INOPERATIVE ROW 9 AND BACK. MX INSPECTED, ATTACHED CONNECTOR TO FLOOR LIGHT STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,143 hrs · 22,381 cycles

CREW REPORTED THE CAPTAINS WINDSHIELD CRACKED DURING CRUISE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE CAPTAINS WINDSHIELD USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RVDT — FAILED (NLG STEERING) · airframe 22,109 hrs · 22,350 cycles

CREW REPORTED AIRCRAFT PULLED TO RIGHT SIDE DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT STEERING FEEDBACK RVDT (ROTARY VARIABLE DIFFERENTIAL TRANSFORMER), AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,627 hrs · 21,923 cycles

CREW REPORTED CABIN IN-FLOOR EMERGENCY LIGHTS INOPERATIVE AND NOT SECURE AT ROWS 1-3. MAINTENANCE INSPECTED, REMOVED AND REPLACED FORWARD EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (RT WING) · airframe 18,799 hrs · 19,299 cycles

AT TYS, CREW REPORTED BIRD STRIKE TO RIGHT WING, ABOUT HALFWAY ON LEADING EDGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, FOUND DAMAGE ON RIGHT WING MIDDLE LEADING EDGE TO BE WITHIN ALLOWABLE LIMITS PER SRM, FILLED DAMAGE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,610 hrs · 18,144 cycles

DURING SCHEDULED MAINTENANCE THE FS 559.0 RIGHT BULKHEAD WEB WAS FOUND CRACKED. THE FS 559.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,610 hrs · 18,144 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,610 hrs · 18,144 cycles

DURING SCHEDULED MAINTENANCE IT WAS FOUND THE FS 202.0 BULKHEAD HAD A CRACK ADJACENT TO THE HOLE WHERE PARKING BRAKE CABLE PASSES THROUGH. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DUCT — DAMAGED (RT PYLON) · airframe 17,447 hrs · 17,985 cycles

CREW REPORTED 14TH STAGE DUCT RED MESSAGE AFTER TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED DAMAGED RIGHT 14TH STAGE PYLON ANTI-ICE DUCTING AND HEAT SENSING ELEMENT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 17,177 hrs · 17,721 cycles

CREW REPORTED LIGHTNING STRIKE ON RT SIDE OF THE NOSE AREA. MAINTENANCE INSPECTED AND REPAIRED DAMAGE. THE RADOME WAS ALSO REMOVED AND REPLACED. ALL WORK WAS ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 15,620 hrs · 16,211 cycles

CREW REPORTED THE FIRST OFFICER WINDSHIELD CRACKED IN FLIGHT. CREW DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER WINDSHIELD USING AIRCRAFT MAINTENANCE MANUALS. CHECKS WERE MADE USING AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 14,366 hrs · 14,911 cycles

CREW REPORTED THE FIRST OFFICER WINDOW CRACKING. AIRCRAFT DIVERTED TO DAY WHERE MAINTENANCE USING THE AIRCRAFT MANUAL TROUBLESHOT AND REMOVED AND REPLACED THE FIRST OFFICER WINDOW. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — UNKNOWN (ENGINE) · airframe 13,456 hrs · 13,922 cycles

CREW REPORTED AT 35,000 A LOW OIL PRESSURE MESSAGE. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT USING AIRCRAFT MAINTENANCE MANUAL, REMOVED AND REPLACED CARBON SEALS ON ACCESSORY GEARBOX. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 13,232 hrs · 13,698 cycles

CREW REPORTED A LOW OIL PRESS IN FLIGHT. ENGINE WAS SHUTDOWN. AIRCRAFT DIVERTED TO RIC LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOT PER THE OEM MAINTENANCE MANUAL AND REMOVED AND REPLACED THE IDG ATS & HYD PUMP AGB CARBON SEAL ASSEMBLY. OPERATIONAL CHECKS AND LEAK CHECKS WERE DONE PER THE OEM MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (AC SYSTEM) · airframe 12,084 hrs · 12,512 cycles

CREW REPORTED AFTER TAKEOFF, TRIED TO TRANSFER RIGHT ENG BLEED CONTROL & WERE UNABLE TO GET THE RIGHT PACK TO FUNCTION OFF THE RIGHT ENG BLEED. CREW ELECTED TO RETURN TO DAY BECAUSE OF RESTRICTION OF 10,000 FT (LT PACK DEFERRED). MAINTENANCE INSPECTED ALL DUCTING, VALVES IN AFT EQUIP BAY NO DEFECTS NOTED. RAN ENGINES & COULD NOT DUPLICATE ON GROUND. ALL BLEEDS & VALVES OPERATE NORMALLY PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRANSMITTER — FAILED (TE FLAP)

CREW REPORTED IN DESCENT AT 290 KTS W/ AUTOPILOT ON, UCA AND FLAP INDICATORS DEPLOYED ON EICAS PAGE. FLAP INDICATOR SHOWED GREEN BAR MOVEMENT AND READOUT MOVED TO 2 DEG. ACFT HAD PITCH OSCILLATIONS OF APPROX 3 DEG NOSE UP AND DOWN. MAINT REMOVED AND REPLACED THE FLAP TRANSMITTER. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. (K)

Part: TRANSMITTER — FAILED (T/E FLAP) · airframe 11,119 hrs · 11,488 cycles

CREW REPORTED IN DESCENT AT 290KTS W/AUTOPILOT ON, UCA AND FLAP INDICATORS DEPLOYED ON EICAS PAGE. FLAP INDICATOR SHOWED GREEN BAR MOVEMENT AND READOUT MOVED TO 2 DEG. AIRCRAFT HAD PITCH OSCILLATIONS OF APPROX 3 DEG NOSE UP AND DOWN. MAINTENANCE REMOVED AND REPLACED THE FLAP TRANSMITTER. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPUTER — FAILED (FUEL QTY) · airframe 10,588 hrs · 10,932 cycles

CREW REPORTED A FUEL IMBALANCE AMBER MSG INFLIGHT. THE RT FUEL AND TOTAL FUEL QUANTITY INDICATORS SHOWED "DASHED". CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND CHANGED THE FUEL QUANTITY COMPUTER. MAINTENANCE CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (A)

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 10,538 hrs · 10,879 cycles

CREW ABORTED TAKEOFF BETWEEN 90-95 KIAS FOR FMS NAV RED FLAG AND MAP AMBER MSG ON PDF AND MFD. MAINTENANCE INSPECTED FMS AND FOUND NO DEFECTS AND ACCOMPLISHED AN ABORTED TAKEOFF INSPECTION WITH NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE. (A)

Part: COMPUTER — FAILED (FUEL QTY) · airframe 10,345 hrs · 10,663 cycles

CREW REPORTED THE RT FUEL QUANTITY AND TOTAL FUEL QUANTITY SHOWED DASHED LINES ON CLIMBOUT. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL QUANTITY GAUGE COMPUTER IN ACCORDANCE WITH THE ACFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. ACFT WAS RELEASED FOR SERVICE. (S)

Part: CONNECTOR — LOOSE (LT ENGINE) · airframe 9,845 hrs · 10,134 cycles

CREW REPORTED A LEFT ENGINE MISCOMPARE MESSAGE DURING CRUISE. CREW REDUCED THRUST PER THE QRH AND CONTINUED TO STL AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED AND THE EQUIPMENT DID RESPOND. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINES LEFT HAND THERMOCOUPLE HARNESS ELECTRICAL CONNECTOR LOOSE. MAINTENANCE CLEANED AND RE-TIGHTENED THE CONNECTOR. MAINTENANCE PERFORMED OPERATIONAL CHECKS PER CRJ 200 77-11-07-710-001. ALL INDICATIONS NORMAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 8,776 hrs · 8,979 cycles

WHILE BEING MARSHALED ON TO GATE E19 DURING TAXI, THE LEFT WING STRUCK A STATIONARY TUG. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEADING EDGE OF THE LEFT WING. AIRCRAFT WAS FERRIED TO AIR CENTER FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD LEADING EDGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (APU OIL TEMP) · airframe 6,527 hrs · 6,591 cycles

CREW REPORTED AN APU OIL TEMP CAUTION MESSAGE IN FLIGHT. CREW PERFORMED AN UNSCHEDULED LANDING IN CMH WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE APU OIL LEVEL. OPERATIONAL CHECKS WERE PERFORMED AND NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: HANDLE — POPPED (CARGO DOOR) · airframe 5,921 hrs · 5,971 cycles

THE CREW REPORTED A CARGO DOOR CAS MESSAGE ON LANDING. MAINTENANCE FOUND CARGO DOOR HANDLE POPPED. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE AFT CARGO DOOR PROX SYSTEM. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — LACK OF LUBE · airframe 5,684 hrs · 5,716 cycles

CREW REPORTED RT ENGINE RED CAS MESSAGE -LOW OIL PRESSURE-. CREW ELECTED TO DIVERT TO BNA. LANDING WAS NORMAL AND WITHOUT INCIDENT. MAINTENANCE SERVICED ENGINE OIL AND PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 5,314 hrs · 5,326 cycles

AFTER LANDING THE CREW REPORTED THE NR 2 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 20-30 PSI. MAINTENANCE SERVICED THE ENGINE WITH 4.25 QTS OF OIL. NO VISUAL EVIDENCE OF LEAKAGE WAS FOUND. AN OIL CONSUMPTION RUN WAS PERFORMED WITH NO LOSS NOTED AND PRESSURE WAS STABLE. THE AIRCRAFT WAS RELEASED FOR SERVICE AND THE NR 2 ENGINE WAS PUT ON AN OIL WATCH. AFTER FURTHER TROUBLESHOOTING THE NR 2 ENGINE IDG CARBON SEAL WAS FOUND TO BE LEAKING. THE SEAL WAS REPLACED AND LEAK CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FUEL CONTROL — FLUCTUATES (RT ENGINE) · airframe 4,836 hrs · 4,820 cycles

CLIMBING OUT OF CAE FROM 10,000 FT TO FL 210 THE RIGHT ENGINE N1, N2, AND FUEL FLOW WERE FLUCTUATING RAPIDLY .8 - 1 PERCENT. THE FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. THE CREW REPORTED THE FLUCTUATION CEASED WHEN THE THROTTLES WERE RETARDED FOR LANDING. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE FUEL CONTROL. ALL OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 4,651 hrs · 4,630 cycles

DURING CLIMBOUT THE -CARGO DOOR- CAUTION MESSAGE ILLUMINATED. PRESSURIZATION WAS STABLE. THE CREW FOLLOWED THE QRH AND ELECTED TO RETURN TO XNA. MAINTENANCE FOUND THE CARGO DOOR HANDLE POPPED OUT. THE HANDLE WAS INSPECTED AND OPERATIONALLY CHECKED. NO DEFECTS WERE FOUND. THE DOOR HANDLE WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PEDAL — OBSTRUCTED (FOD IN COCKPIT) · airframe 4,031 hrs · 4,043 cycles

THE TAKEOFF WAS REJECTED DUE TO BINDING IN THE RUDDER PEDALS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND A COCKPIT SUN VISOR JAMMING THE RT RUDDER PEDALS. THE SUN VISOR WAS REMOVED AND THE RUDDER SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-21-00-710-801. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: HOSE — RUPTURED (OXYGEN SYSTEM) · airframe 3,809 hrs · 3,810 cycles

CLIMBING THRU FL120, THE CREW HEARD A HISSING SOUND AND REPORTED THAT THE CREW OXYGEN QUANTITY WAS DEPLETED. THE QRH WAS FOLLOWED AND THE FLIGHT DIVERTED TO PIT. MAINTENANCE FOUND THE OXYGEN HOSE UNDER THE FIRST OFFICER'S MASK STOWAGE BOX RUPTURED. THE HOSE WAS REMOVED AND REPLACED IAW CRJ200 AMM 35-11-15-000(400)-801. THE CREW OXYGEN BOTTLE WAS ALSO REMOVED AND REPLACED IAW CRJ200 AMM 35-11-03-000(400)-801. THE OXYGEN SYSTEM WAS SERVICED AND LEAK CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (AILERON SYS) · airframe 3,411 hrs · 3,390 cycles

DURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. THE CREW PERFORMED A REJECTED TAKEOFF. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AILERON TRIM SYSTEM IAW CRJ200 AMM 27-11-00-710-801 AND A REJECTED TAKEOFF INSPECTION IAW CRJ200 AMM 05-51-27. NO DISCREPANCIES WERE FOUND. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (LT WING TIP) · airframe 3,123 hrs · 3,097 cycles

AFTER LANDING MAINTENANCE DISCOVERED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WING TIP. A DETAILED LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-05-220-801. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 2,080 hrs · 2,010 cycles

AFTER TAKEOFF FROM DCA FLIGHT 2445 WAS CLIMBING THRU 8000 FT WHEN THE CARGO DOOR CAUTION MESSAGE ILLUMINATED. THE CREW DECIDED TO RETURN TO DCA TO HAVE MAINTENANCE INSPECT THE CARGO DOOR. NO EMERGENCY WAS DECLARED. NO LOSS OF PRESSURIZATION WAS REPORTED. THE FLIGHT LANDED WITHOUT INCIDENT. UPON INSPECTION THE CARGO DOOR HANDLE WAS FOUND UNSTOWED. CONTRACT MAINTENANCE AT DCA OPS CHECKED THE CARGO DOOR HANDLE AND RESECURED THE DOOR IAW CRJ 200 AMM 52-31-03-710-801 AND AMM 52-31-03-710-002. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 1,886 hrs · 1,832 cycles

THE PILOTS OF FLIGHT 2434, DCA TO YYZ, REPORTED A PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ON THE EICAS PRIMARY DISPLAY. THE AIRCRAFT DIVERTED TO PIT AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE TROUBLESHOT THE PASSENGER DOOR SYSTEM IAW CRJ200 FIM 52-70-04. NO DEFECTS WERE FOUND. THE DOOR OPERATIONALLY TESTED GOOD IAW CRJ200 AMM 52-70-04-710-801. THE AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: SKIN — BIRD STRIKE (FUSELAGE) · airframe 1,549 hrs · 1,510 cycles

AFTER LANDING AT CLT THE PILOT OF FLIGHT 2421 REPORTED A BIRD STRIKE BELOW THE CAPTAIN'S WINDSHIELD. A BIRD STRIKE INSPECTION WAS PERFORMED AND TWO DENTS WERE FOUND ON THE FORWARD FUSELAGE AT FS 589 & FS 202. THE AIRCRAFT WAS FERRIED TO CAK WHERE PSA MAINTENANCE PERFORMED TEMPORARY REPAIRS IAW BOMBARDIER REO 601R-53-61-1193 AND REO 601R-53-11-828. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: DOOR — FAILED (EMERGENCY EXIT) · airframe 1,046 hrs · 1,001 cycles

THE CREW REPORTED RECEIVING A RIGHT HAND EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL MEL'D THE EMERGENCY DOOR IN ACCORDANCE WITH MEL 52-70-3 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: FLAP — OUT OF RIG (LEFT) · airframe 481 hrs · 436 cycles

AFTER TAKEOFF, FLAPS FAILED AT 8. FLIGHT 2270 RETURNED TO PHL. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND RIGGED LEFT HAND AND RIGHT HAND FLAPS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 27-54-00-803-801. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.