N262PS

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 33,084 hrs · 32,868 cycles

AFTER TAKEOFF AND GEAR UP, CREW RECEIVED A GEAR DISAGREE MESSAGE. MX COMPLIED WITH GEAR SWINGS. CHECKED ALL SENSORS AND RIGGING. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 32,943 hrs · 32,717 cycles

AFT CARGO DOOR LOWER SILL IS CORRODED AT FASTENER HOLES AND CRACKED AT FS 605. REPLACED AFT CARGO DOOR LOWER SILL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,943 hrs · 32,717 cycles

SEAT TRACKS CORRODED FROM FS 409+128 - 559+80. REPLACED FLOOR TRACKS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,943 hrs · 32,717 cycles

LBL 27 FLOORBEAM IS CORRODED AT 2 FASTENER HOLE LOCATIONS BETWEEN FS 589- FS 621. REMOVED AND REPLACED SEAT RAIL BEAM P/N 601R35031-263 BETWEEN FS 569.00 AND FS 610 AT LBL 27 IAW REO 601R-53-61-6630 REV- DATED 2018-07-08 AND SNIEO S15 DRAWING NUMBER 601R35031.

Part: POST — CRACKED (FUSELAGE) · airframe 32,943 hrs · 32,717 cycles

FS 409+128 RBL 18 INBD AND OUTBD VERTICAL POSTS HAVE INDICATIONS IN THE AFT RADIUS AT WL69 .15" LONG BY 60% FSH ON INBD VERTICAL POSTS AND .15" LONG BY 65% FSH ON OUTBD VERTICAL POST. FAILED NDT INSPECTION. C/A REMOVED AND REPLACED VERTICAL POST AT 409+128 RBL 18.0 IAW REO 601R-53-41-889 REV C DATED 2018-01-03 AND SNIEO S31 DRAWING NUMBER 601R32208.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,943 hrs · 32,717 cycles

FS 280 CROSSBEAM FWD J-ANGLE IS CORRODED AROUND RECEPTACLES. REMOVED AND REPLACED FWD J ANGLE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,943 hrs · 32,717 cycles

REAR PRESSURE BULKHEAD CRACKS LBL 36.2 WL 79, 27.5 WL 65, BL0 WL 95 & 113. PERFORMED MAJOR REPAIR TO THE FS 621 BULKHEAD IAW REO 601R-53-61-1240 REV D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,943 hrs · 32,717 cycles

LT AND RT INTERCOSTAL CLEATS ARE CRACKED AT FS 621.00 AND STR 14. REPLACED INTERCOSTAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,943 hrs · 32,717 cycles

SEAT TRACKS CORRODED FROM FS 394-529 & 559+80-559+96. REPLACED FLOOR TRACKS.

Part: ECU — FAULTY (TE FLAP) · airframe 31,176 hrs · 31,076 cycles

CREW DIVERTED TO CLT FOR A FLAPS FAIL MSG. FLAPS FAILED AT 0 DEG. DECLARED EMERGENCY INTO CLT. MX R&R FECU OPS AND FUNCTIONAL CHECK.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 29,061 hrs · 29,048 cycles

CARGO DOOR OUTER SKIN'S UPPER EDGE GOUGED. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE EXTERNAL CARGO DOOR SKIN AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (BS 235) · airframe 29,061 hrs · 29,048 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT RIGHT AFT CORNER OF THE NOSE LANDING GEAR WHEEL WELL DOOR CUTOUT AT BS 235, RBL 6.0. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT THE NOSE LANDING GEAR WHEEL WELL DOOR CUTOUT’S RIGHT HAND SIDE AFT RADIUS AT BS 235, RBL 6.0 IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POSITION SENSOR — FAILED (FLAP CONTROL SYS) · airframe 28,127 hrs · 28,126 cycles

CREW REPORTED RECEIVING A FLAP FAIL AMBER CAUTION DURING CRUISE AT FLIGHT LEVEL 090. THEY DECLARED AN EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, AND R & R THE LT BRAKE AND POSITION SENSOR UNIT. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 27,569 hrs · 27,565 cycles

CREW REPORTED GEAR DISAGREE WARNING MESSAGE WITH NOSE GEAR INDICATING RED. CREW COMPLETED QRH, RECEIVED 3 GREEN INDICATIONS AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R NLG PRIORITY VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 27,043 hrs · 27,034 cycles

CREW REPORTED GEAR DISAGREE WARNING MESSAGE WITHIN 6 SECONDS OF GEAR EXTENSION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LANDING GEAR SELECTOR HANDLE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (FLAP CONTROL SYS) · airframe 27,013 hrs · 27,005 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE WHEN FLAPS SELECTED TO 30 DEGREES DURING APPROACH. LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM, R & R FLAP ELECTRONIC CONTROL UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 379) · airframe 26,712 hrs · 26,693 cycles

STRINGER 3L IS CRACKED ON FWD SIDE OF BS 379, APPROX .5 INCHES LONG ON OTBD SIDE OF STRINGER. REPAIRED THE STRINGER IAW SRM.

Part: CONTROL UNIT — FAILED (H/S TRIM) · airframe 26,523 hrs · 26,510 cycles

CREW REPORTED STABILIZER TRIM AND MACH TRIM MESSAGES DURING CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R HORIZONTAL STABILIZER TRIM CONTROL UNIT (HSTCU) AND PERFORMED CHECKS IAW MM. ACFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 26,498 hrs · 26,485 cycles

FORWARD PRESSURE BULKHEAD CRACKED AT BS 202.75 WHERE PARKING BRAKE CABLE PASSES THROUGH. CRACK AT 1 O’CLOCK POSITION AND .3125" LONG. REPAIRED IAW REO 601R-53-11-563 REV C AND STANDARD REPAIR 601R-53-0101A.

Part: SENSING ELEMENT — BROKEN (BLEED AIR) · airframe 26,169 hrs · 26,160 cycles

CREW REPORTED ANTI-ICE DUCT RED WARNING MESSAGE IN FLIGHT. SYNOPTIC PAGE SHOWED RT FUSELAGE OVERHEAT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LOOP A18WK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERHEAT) · airframe 25,830 hrs · 25,822 cycles

CREW REPORTED LT JET PIPE OVERHEAT MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LT JET PIPE SENSING ELEMENT, CONNECTORS AND WIRES AND PERFORMED CHECKS IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.

Part: ENGINE — VIBRATION (LEFT) · airframe 25,694 hrs · 25,703 cycles

WHILE DESCENDING THROUGH 20,000 MSL, CREW REPORTED A VIBRATION AND THAT LT ENGINE INTERTURBINE TEMPERATURE (ITT) SPIKED AND ENGINE SHUTDOWN. ATTEMPT TO RELIGHT ENGINE WAS UNSUCCESSFUL. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, R & R LEFT ENGINE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. OPEN

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 24,607 hrs · 24,605 cycles

CREW REPORTED GEAR DISAGREE MASTER WARNING AND GEAR DISAGREE RED MESSAGE AFTER GEAR DOWN SELECTED. ALL MESSAGES LATER WENT AWAY AND GREEN DOWN INDICATIONS RETURNED. CREW LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH FUNCTIONAL CHECK OF GEAR EXTENSION, RETRACTION, GEAR DISAGREE TEST AND GEAR PRIORITY VALVE TEST. BLED NR 3 HYD SYS INTERROGATED PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). NO CODES FOUND. ALL CHECKS GOOD IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,555 hrs · 24,553 cycles

CREW REPORTED AFT EMERGENCY INTERNAL FLOODLIGHT OUT. MAINTENANCE INSPECTED, R & R LAMP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 21,935 hrs · 22,060 cycles

CREW REPORTED F/A EMERGENCY FLASHLIGHT INOPERATIVE. MX INSPECTED, R & R FLASHLIGHT BATTERY AND PERFORMED CHECK IAW AMM. ACFT RELEASED FOR SERVICE.

Part: THRUST REVERSER — MALFUNCTIONED (LT ENGINE) · airframe 21,734 hrs · 21,877 cycles

THE CREW REPORTED A LEFT THRUST REVERSER UNLOCK MESSAGE. THE AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LEFT THRUST REVERSER CASCADE USING THE AIRCRAFT MANUALS. CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (ANTI-ICE SYS) · airframe 20,959 hrs · 21,169 cycles

CREW REPORTED A LEFT WING ANTI-ICE CAUTION MESSAGE. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE LEFT MODULATING SHUT OFF VALVE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RELAY — MALFUNCTIONED (ELECTRICAL SYS) · airframe 19,944 hrs · 20,276 cycles

CREW REPORTED AC ESS (ESSENTIAL) BUS MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED AC ESS BUS RELAY AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,332 hrs · 18,811 cycles

CREW REPORTED LIGHTNING STRIKE ON AIRCRAFT NOSE DURING DESCENT. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REPAIRED BURN MARK ON RIGHT FUSELAGE JUST BELOW ADG (AIR DRIVEN GENERATOR) DOOR, BLENDED DAMAGED RIVETS ON RIGHT SIDE OF FUSELAGE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,036 hrs · 18,513 cycles

CREW REPORTED OVERHEAD EMERGENCY LIGHT NEAR ROW 10 INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED OVERHEAD EMERGENCY LAMP AT ROW 10 AND PERFORMED CHECKS USING AIR MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 17,407 hrs · 17,908 cycles

CREW REPORTED FLAPS FAIL AMBER MESSAGE ON APPROACH TO CLT. CREW LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT OUTBOARD FLAP OUTBOARD ACTUATOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SHAFT — LACK OF LUBE (TE FLAP) · airframe 17,379 hrs · 17,885 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE ON APPROACH TO CLT. FLAPS FAILED AT 20 DEGREES AND WOULD NOT EXTEND ANY FURTHER IN FLIGHT. AIRCRAFT LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, CLEANED AND LUBED LEFT AND RIGHT FLAP FLEX SHAFTS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS FOUND AND NEUTRAL RIG MAINTAINED. AIRCRAFT RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 16,959 hrs · 17,492 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: POST — CRACKED (FUSELAGE) · airframe 16,959 hrs · 17,492 cycles

DURING SCHEDULED MAINTENANCE THE FS FS409+128 VERTICAL POST WAS FOUND CRACKED. THE FS 409+128 VERTICAL POST WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 16,959 hrs · 17,492 cycles

DURING SCHEDULED MAINTENANCE THE FS 718 WAS FOUND CRACKED. THE FS 718 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — VIBRATION (RIGHT) · airframe 15,276 hrs · 15,816 cycles

CREW REPORTED THE RIGHT ENGINE MADE A NOISE AND INDICATED A VIBRATION 3.8. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE USING THE AIRCRAFT MAINTENANCE MANUALS COULD NOT DUPLICATE PROBLEM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 559) · airframe 15,200 hrs · 15,742 cycles

DURING SCHEDULED MAINTENANCE A CRACK TO THE FS 559 PRESSURE BULKHEAD WEB WAS FOUND. REPAIRS WERE MADE IAW MM. AIRCRAFT RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 15,200 hrs · 15,742 cycles

DURING SCHEDULED MAINTENANCE DAMAGE TO THE FS 559 FLOOR SUPPORT CHANNEL WAS FOUND. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE. REV TO VNAA2010121300000 TO ADD 04.

Part: SKIN — DENTED (RT WING) · airframe 14,618 hrs · 15,173 cycles

AT CLT, CREW REPORTED A BIRD STRIKE ON THE RIGHT WING LEADING EDGE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A DENT IN THE RIGHT WING INBOARD LEADING EDGE. THE DENT WAS DETERMINED TO BE WITHIN LIMITS PER THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 11,216 hrs · 11,614 cycles

CREW REPORTED LIGHTNING STRIKE IN CLT. MAINTENANCE REPAIRED BURN MARKS TO LT STABILIZER TIP AND FUSELAGE. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PDU — LACK OF LUBE (THRUST REVERSER) · airframe 10,506 hrs · 10,867 cycles

CREW REPORTED AN INTERMITTENT RT REV UNLOCKED MSG IN FLIGHT. FLIGHT RETURNED TODAY AND LANDED WITHOUT INCIDENT. MX INSPECTED AND LUBED PDU LOCK PLUNGER. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 9,346 hrs · 9,606 cycles

CREW RECEIVED A LT HAND STATIC HEAT CAS MSG AND ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE RE-SET THE SYSTEM AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)

Part: SKIN — DAMAGED (FUSELAGE)

CREW REPORTED A LIGHTNING STRIKE FOUND DURING PREFLIGHT INSPECTION. MAINT PERFORMED AN ENROUTE AND DETAILED LIGHTNING STRIKE INSPECTION. MAINT FOUND SEVERAL AREAS OF BURN DAMAGE. MAINT REPAIRED ALL DAMAGE IAW REO NR 601R-55-12-170 AND IAW THE AC MM. AIRCRAFT WAS RELEASED FOR SERVICE. (K)

Part: TIRE — SEPARATED (MLG) · airframe 8,916 hrs · 9,158 cycles

CREW REPORTED ON TAKEOFF ROLL FELT A BUMP. AT DESTINATION, MAINTENANCE INSPECTED AND FOUND THE LEFT INBOARD MAIN TIRE HAD SEPARATED AND CAUSED DAMAGE TO THE UNDERNEATH PORTION OF THE LEFT WING AND LANDING GEAR. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD MAIN TIRE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REPAIRED ALL OTHER DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PDU — FAILED (THRUST REVERSER) · airframe 8,218 hrs · 8,429 cycles

CREW REPORTED A LEFT HAND THRUST REVERSER UNLOCKED AMBER MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND RETURNED TO TRI WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (PAX DOOR) · airframe 7,863 hrs · 8,044 cycles

CREW REPORTED A PASSENGER DOOR TRIPLE CHIME RED WARNING AT 10,000 FEET AND CAS REPEATED MULTIPLE TIMES. CREW ALSO REPORTED HEARING A THUMP AT THE MAIN CABIN DOOR. CREW ELECTED TO DIVERT TO JAX AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR WIRING HARNESS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (LT MLG) · airframe 7,438 hrs · 7,591 cycles

CREW REPORTED DURING LANDING ROLLOUT RECEIVING A WOW INPUT CAUTION AND A PROX SYSTEM FAULT STATUS MESSAGES. MAINTENANCE INSPECTED AND FOUND THE LEFT HAND INBOARD MAIN TIRE TREAD HAD SEPARATED FROM THE WHEEL ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE MAIN TIRE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE INSPECTED AND FOUND THE AIRCRAFT SAFE FOR FERRY FLIGHT TO DAYTON. MAINTENANCE REMOVED AND REPLACED DAMAGED FLAP ASSEMBLY. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PSEU — FAILED (SERVICE DOOR) · airframe 7,167 hrs · 7,280 cycles

CREW REPORTED A SERVICE DOOR CAUTION MESSAGE AND THEN A MAIN CABIN DOOR WARNING MESSAGE IN CRUISE. DURING DESCENT CABIN ALT CAS MESSAGE CAME ON. PASSENGER O2 MASKS WERE DEPLOYED DURING CABIN ALT EPISODE. CREW FOLLOWED THE QRH AND DECLARED AN EMERGENCY AND LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A FAULTY PROXY SENSOR ELECTRONIC UNIT. MAINTENANCE REMOVED AND REPLACED THE PSEU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-61-01-000(400)-801. MAINTENANCE REPLACED DEPLETED O2 GENERATORS AND REPACKED O2 MASKS. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,412 hrs · 3,376 cycles

AFTER TAKEOFF THE FLAPS STAYED AT 20 DEGREES AND WOULD NOT RETRACT. THE CREW FOLLOWED THE QRH, DIVERTED TO ILM, AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLAP SYSTEM IAW BOMBARDIER CRJ200 SL-00-001. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — GROUND DAMAGE (FUSELAGE) · airframe 3,334 hrs · 3,297 cycles

DURING SERVICING A LAV TRUCK STRUCK THE RIGHT SIDE OF THE FUSELAGE, CAUSING A 1 X 1 PUNCTURE IN THE SKIN, APPROXIMATELY 16 AFT OF THE LAVATORY POTABLE WATER DOOR. MAINTENANCE REPAIRED THE FUSELAGE SKIN IAW BSC EO 601R-53-8002. PRESSURE LEAK CHECK OF THE REPAIR WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: STRUCTURE — BIRD STRIKE (RT WING LE) · airframe 3,278 hrs · 3,250 cycles

DURING CLIMBOUT FROM BDL THE CREW REPORTED A POSSIBLE BIRD STRIKE. THE FLIGHT CONTINUED TO PIT AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED IMPACT DAMAGE ON THE RT WING INBOARD LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE RT WING INBOARD LEADING EDGE AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WHEEL — OUT OF BALANCE (NLG) · airframe 1,496 hrs · 1,461 cycles

THE CREW OF FLIGHT 2411 REPORTED NOSE WHEEL VIBRATION AFTER TAKEOFF FROM PHL. THE FLIGHT CONTINUED TO DAY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE FOUND THE LT NLG WHEEL AND TIRE ASSEMBLY OUT OF BALANCE DUE TO FLAT SPOTS ON THE TIRE. THE LT NLG WHEEL & TIRE ASSEMBLY WAS REMOVED & REPLACED IAW CRJ 200AMM 32-42-01-000-801 AND 32-42-01-400-801. THE NLG WAS LUBRICATED IAW CRJ 200 AMM 12-20-32-640-801. BOTH NOSE WHEEL AXLE NUT TORQUES WERE VERIFIED IAW CRJ 200 SL 32-015. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: TIRE — DAMAGED (LT MLG) · airframe 455 hrs · 454 cycles

POST FLIGHT INSPECTION OF THE AIRCRAFT BY THE CREW OF FLIGHT 2293 REVEALED THE LEFT INBOARD MAIN LANDING GEAR RETREADED TIRE HAD SHED APPROXIMATELY HALF ITS TREAD DURING LANDING AT MSP. UPON FURTHER INVESTIGATION FOD WAS FOUND ON THE LEFT INBOARD FLAP AND ON THE NR 1 ENGINE FAN BLADES. PSA MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD MAIN LANDING GEAR WHEEL AND TIRE ASSEMBLY. THE AIRCRAFT AND ENGINES WERE INSPECTED AND DETERMINED TO BE AIRWORTHY. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD FLAP. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY DOOR) · airframe 215 hrs · 213 cycles

CREW REPORTED, RECEIVED A LEFT EMERGENCY DOOR CAS MESSAGE. MAINTENANCE CONTROL DEFERRED THE LEFT EMERGENCY DOOR WARNING 57-70-3 CODE C.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY DOOR) · airframe 208 hrs · 205 cycles

CREW REPORTED, RECEIVED A LEFT EMERGENCY DOOR CAS MESSAGE AT 25000 FEET. MAINTENANCE CONTROL DEFERRED THE LEFT EMERGENCY DOOR WARNING 57-70-3 CODE C.