N206PS

Part: OIL SYSTEM — LEAKING (APU) · airframe 33,795 hrs · 33,566 cycles

THE CREW REPORTED THE APU HAD AN AUTOSHUT DOWN AND SMOKE FILLED THE CABIN. MAINTENANCE INSPECTED AFT E/E BAY AND FOUND APU LEAKED OIL EVERYWHERE. CLEANED AREA.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,890 hrs · 32,757 cycles

FOUNDTHE BS 621 PRESSURE BULKHEAD WEB WITH MULTIPLE CRACK INDICATIONS, LBL 36.20, WL 95, 1 INCH LONG, 80% FSH, LBL 18, WL 75, 1 INCH LONG, 80% FSH, BL 0, WL 112, 3 INCHES LONG, 60% FSH, RBL 9.5, WL 85, ONE INCH LONG, 80% FSH, RBL 9.5, WL 82, 1 INCH LONG, 100% FSH, RBL 27.5, WL 102, 1 INCH LONG, 60% FSH, BL 0, WL 128, 8 INCHES LONG, 50% FSH, AND LBL 18, WL 130, 2 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD IAW REO 601R-53-61-1240, REVISION D.

Part: ANGLE — CRACKED (BS 621) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

BS 621, FWD FACE CARGO DOOR SUPPORT LINTEL ANGLE CRACKED. DRILLED, LOCATED AND INSTALLED NEW LINTEL ANGLE IAW SRM 51-42-21, AND 51-77-00.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

FOUND THE RT FLOOR SUPPORT FROM BS 559+85 TO 559+108 TO BE CORRODED AND OUT OF LIMITS IAW REO 601R-53-00-526. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559-621) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

CARGO TRACK IN THE CARGO BAY IS CORRODED FROM BS 559+78 TO 621. REMOVED THE CARGO TRACK IAW SRM 51-41-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. INSTALLED A NEW CARGO TRACK IAW SRM 53-00-49, AND SRM 53-61-49.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

LEFT FLOORBEAM STRAP AT BS 559, LBL 27 - 42 IS CORRODED. REMOVED & REPLACED THE STRAP IAW SRM 51-42-06, AND 51-42-22.

Part: FLOOR SKIN — CORRODED (BS 499-513) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

PRESSURE FLOOR HAS FRETTING CORROSION AROUND THE HOLES THAT THE FUEL LINES PASS THROUGH. REMOVED THE CORROSION IAW SRM 51-12-00. REPAIRED THE DAMAGED AREA IAW REO 601R-53-41-2234

Part: STRAP — CORRODED (BS 559 FLOORBEAM) · corrosion level 3 · airframe 32,890 hrs · 32,757 cycles

RIGHT FLOORBEAM STRAP AT BS 559 RBL 27-42 IS CORRODED. REMOVED & REPLACED THE STRAP IAW SRM 51-42-06, AND 51-42-22.

Part: FRAME — CRACKED (BS 333) · airframe 32,890 hrs · 32,757 cycles

BS 333 FRAME ABOVE PASSENGER DOOR IS CRACKED. INSTALLED A NEW FRAME IAW SRM 51-42-21, 51-42-06, AND 51-42-13.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

FUSELAGE FRAME BS 605 IS CORRODED FROM STRINGER 24L TO 23R. REMOVED CORROSION ON FRAME IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW 53-00-00 2. LOCATED AND DRILLED THE FRAME SECTOR IAW SRM 51-40-11. INSTALLED THE FRAME IAW SRM 51-42-21, AND 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

LBL 9 SEAT TRACK IS CORRODED, BS 559 TO 559+80. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49. REMOVED, FABRICATED & INSTALLED A NEW SEAT TRACKS IAW AMM 53-01-11-400-802, & REO 601R-53-00-485.

Part: ANGLE — CORRODED (BS 621 FLOORBEAM) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

BS 621 FLOORBEAM ANGLE IS CORRODED BETWEEN LBL 9 AND LBL 27, RBL 9 AND RBL 27. THE FLOORBEAM ANGLE. COMPLIED WITH EO 2B19-53-L05325.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 32,890 hrs · 32,757 cycles

FLOOR PANEL 231ALF IS CRACKED IN THE CENTER. INSTALLED A NEW FLOOR PANEL IAW AMM 53-01-01-400-802.

Part: FRAME — CORRODED (BS 589) · corrosion level 2 · airframe 32,890 hrs · 32,757 cycles

FUSELAGE FRAME BS 589 IS CORRODED FROM STRINGERS 19R TO 20L. LOCATED, DRILLED AND INSTALLED A NEW FRAME IAW SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 31,124 hrs · 31,084 cycles

DURING SCHEDULED MAINTENANCE, THE HORIZONTAL STABILIZER’S ANTI – ROTATION FITTING WAS FOUND CRACKED. THE AIRCRAFT WAS FERRIED TO A SUITABLE MAINTENANCE FACILITY, MAINTENANCE REMOVED AND REPLACED THE FITTING AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

GEAR DISAGREE, NLG WARNING. MAINTENANCE COMPLIED WITH PSEU SYSTEM TEST INITIATION IAW AMM. GEAR DISAGREE WITH NLG GEAR DOWN. TECHNICIANS REMOVED AND REPLACED NLG NR 1 DOOR AND OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (AVIONICS COOLING) · airframe 29,872 hrs · 29,813 cycles

CREW REPORTED THAT ON INITIAL CLIMB THE ACFT WOULD NOT PRESSURIZE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OVERBOARD EXHAUST SHUTOFF VALVE WAS NOT DEACTIVATED IN THE CLOSED POSITION. MAINTENANCE DEACTIVATED OVERBOARD EXHAUST SHUTOFF VALVE, PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 29,698 hrs · 29,640 cycles

EMERGENCY LIGHT COVER NEAR MAIN CARGO DOOR WILL NOT STAY ATTACHED. MAINTENANCE INSPECTED, REPLACED EMERGENCY LIGHT COVER, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,013 hrs · 25,974 cycles

CREW REPORTED LAST SECTION OF FLOOR EMERGENCY LIGHTING INOPERATIVE NEAR 12D AND 12F. MAINTENANCE INSPECTED, CLEANED AND SECURED AFT EMERGENCY LIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DOUBLER — CORRODED (MOUNT) · corrosion level 2 · airframe 25,814 hrs · 2,775 cycles

DURING SCHEDULED MAINTENANCE, BOTH AFT WARDROBE MOUNT DOUBLERS WERE FOUND CORRODED. THE AREA WAS INSPECTED IAW AMM. AFT WARDROBE MOUNT DOUBLERS WERE R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 25,814 hrs · 25,775 cycles

DURING SCHEDULED MAINTENANCE, THE LT SIDE FLOOR SUPPORT WAS FOUND CORRODED. AREA INSPECTED IAW AMM. THE FLOOR SUPPORT WAS R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: DOUBLER — CORRODED (GALLEY MOUNT) · corrosion level 2 · airframe 25,814 hrs · 25,775 cycles

DURING SCHEDULED MAINTENANCE, THE AFT GALLEY MOUNT DOUBLER WAS FOUND CORRODED. THE AREA WAS INSPECTED USING AMM. THE AFT GALLEY MOUNT DOUBLER WAS R & R USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 24,814 hrs · 25,775 cycles

DURING SCHEDULED MAINTENANCE, THE STRAP AT BS 559 RBL 39 WAS FOUND CORRODED. AREA WAS INSPECTED IAW AMM. THE STRAP WAS R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 379) · airframe 25,814 hrs · 25,775 cycles

DURING SCHEDULED MAINTENANCE, STRINGER 3L BS 379 WAS FOUND CRACKED. AREA INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,823 hrs · 24,846 cycles

CREW REPORTED MAIN CABIN DOOR EMERGENCY FLOODLIGHT (FLOOR LEVEL) HAD ONLY 4 OF 5 BULBS ILLUMINATED. MAINTENANCE INSPECTED, R & R LIGHT BULB AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: TRANSDUCER — FAILED (OIL SYSTEM) · airframe 22,772 hrs · 23,020 cycles

CREW REPORTED HIGH LEFT ENGINE OIL PRESSURE AND ABORTED TAKEOFF. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE TRANSDUCER PER AIRCRAFT MANUALS. OPERATION CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 21,706 hrs · 22,077 cycles

CREW REPORTED EMERGENCY FLOOR PATH LIGHTING INOPERATIVE AROUND ROW SIX (6). MAINTENANCE INSPECTED, CLEANED CONNECTION AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,306 hrs · 21,706 cycles

DURING SCHEDULED MAINTENANCE THE FS 621.0 REAR PRESSURE BULKHEAD WEB WAS INDICATING CRACKED. THE FS 621.0 REAR PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 20,897 hrs · 21,351 cycles

CREW REPORTED FLAPS FAIL CAS MESSAGE WHEN SELECTING FLAPS 20 DEGREES. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM AND PERFORMED CHECKS OF FLAP CONTROL LEVER USING AIRCRAFT FIM. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,758 hrs · 21,227 cycles

CREW REPORTED 2ND OF 4 EMERGENCY FLOOD LIGHTS DOES NOT ILLUMINATE (NEAR ROW 5). MAINTENANCE INSPECTED, RELAMPED POSITION 2 EMERGENCY CEILING FLOOD LIGHT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 20,311 hrs · 20,778 cycles

CREW REPORTED RIGHT WINDSHIELD HEAT CAS MESSAGE IN FLIGHT. BASE OF WINDSHIELD COULD BE SEEN ARCING BEFORE FAILURE. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT WINDSHIELD AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: HYDRAULIC LINE — BROKEN (HYDRAULIC SYS) · airframe 18,640 hrs · 19,181 cycles

CREW REPORTED HYD 2 LO PRESS MESSAGE IN FLIGHT EN ROUTE FROM SDF TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED, REPAIRED AND REINSTALLED BROKEN TUBING, REMOVED AND REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP 2A AND REMOVED AND REPLACED WORN HYDRAULIC SYSTEM 2 AFT EQUIPMENT BAY FAIR LEAD BLOCKS. CHECKS WERE PERFORMED AND AIRCRAFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,972 hrs · 17,583 cycles

DURING SCHEDULED MAINTENANCE LIGHTNING STRIKE DAMAGE WAS FOUND ON THE FUSELAGE SKIN AT STR 25L AND FS 409. ALSO, AT STR 16 FS 319.17. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 16,972 hrs · 17,583 cycles

DURING SCHEDULED MAINTENANCE THE FS 409+128 VERTCLE POST WAS FOUND CRACKED. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 16,972 hrs · 17,583 cycles

DURING SCHEDULED MAINTENANCE THE LT INBOARD FLAP SKIN WAS DENTED. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (LEFT) · airframe 16,623 hrs · 17,245 cycles

CREW REPORTED A LT COWL ANTI-ICE CAUTION MESSAGE. ACFT RETURNED AND LANDED WITHOUT INCIDENT. MX USING THE ACFT MM REMOVED, REPLACED, AND TESTED THE LT ANTI-ICE VALVE. ACFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 15,391 hrs · 16,065 cycles

AT CAK, CREW REPORTED SOME EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED, RECONNECTED A LOOSE CONNECTION UNDER THE FLOORBOARDS AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: MOTOR — FAULTY (WINDSHIELD) · airframe 14,803 hrs · 15,439 cycles

CREW REPORTED A LIGHTNING STRIKE UNDER THE CAPTAIN’S WINDSHIELD WIPER DURING CRUISE FLIGHT EN ROUTE TO PGV. AIRCRAFT LANDED IN PGV WITHOUT INCIDENT. MAINTENANCE INSPECTED, TROUBLESHOT AND REPAIRED THE AIRCRAFT. THE LEFT WINDSHIELD WIPER MOTOR, LEFT FLUX DETECTOR UNIT AND LEFT REMOTE COMPENSATOR UNIT WERE REMOVED AND REPLACED. THE LEFT WINGLET TIP DAYTON-GRANGER MOD WAS REMOVED AND REPLACED. DAMAGE TO THE FUSELAGE, AVIONICS BAY DOOR AND LEFT WINGLET TIP WAS REPAIRED. STATIC DISCHARGERS WERE REPLACED. CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS, VENDOR DOCUMENTATION AND REO.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,753 hrs · 15,389 cycles

CREW REPORTED THE LEFT WINDSHIELD CRACKED IN FLIGHT EN ROUTE FROM LGA TO DAY. AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE LEFT WINDSHIELD AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,549 hrs · 15,187 cycles

DURING SCHEDULED MAINTENANCE AT FS 559 BULKHEAD WEB, RBL 18 WL 59.10, A CRACK WAS FOUND. MAINTENANCE REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND RELEASED THE AIRCRAFT FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,236 hrs · 14,845 cycles

CREW REPORTED AT CRUISE THE OUTER PANE OF THE CAPTAINS WINDSHIELD SHATTERED. THE AIRCRAFT DIVERTED TO MGM LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED PER THE AIRCRAFT MAINTENANCE MANUAL, REMOVED AND REPLACED THE CAPTAINS WINDSHIELD. CHECKS WERE MADE PER THE AIRCRAFT MANUAL AND THE AIRCRAFT WAS RELEASED FOR FLIGHT.

Part: WINDSHIELD WIPER — SEPARATED (WINDSHIELD) · airframe 12,497 hrs · 12,956 cycles

CREW REPORTED WINDSHIELD WIPER PIECE BROKE OFF IN FLIGHT. AIRCRAFT DIVERTED TO ILM AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPT'S WIPER BLADE ASSY. CHECKS WERE PERFORMED PER AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 11,606 hrs · 12,023 cycles

CREW REPORTED AFTER SWITCHING BLEEDS TO THE ENGINES, HAD STRANGE ODOR IN THE COCKPIT AND CABIN. CREW ELECTED TO RETURN TO DAY. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND GROUND RAN THE AIRCRAFT AT HIGH POWER SETTING IN ACCORDANCE WITH AMM 71-00-00-868-806. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. SUSPECT SMELL CAUSED BY RESIDUE FROM ENGINE WASH PERFORMED DURING PREVIOUS OVERNIGHT MAINTENANCE. THERE HAVE BEEN NO SUBSEQUENT WRITE-UPS FOR THIS CONDITION.

Part: INVERTER — FAILED (CABIN) · airframe 11,241 hrs · 11,622 cycles

DURING SCHEDULED MX, FORWARD EMERGENCY TRACK LIGHTING AND EXIT OVER LT WING FAILED. MX R&R THE NR 2 INVERTER. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.

Part: NONE — NONE (NO DAMAGE) · airframe 10,634 hrs · 10,990 cycles

CREW REPORTED A BIRD STRIKE TO THE CAPTAIN`S WINDSHIELD. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 10,172 hrs · 10,513 cycles

CREW REPORTED A CABIN ALTITUDE CAUTION MESSAGE ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PRESSURIZATION SYSTEM. MAINTENANCE REMOVED AND REPLACED THE PRIMARY OUTFLOW VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 10,046 hrs · 10,366 cycles

CREW REPORTED ON APPROACH A LIGHTNING STRIKE TO THE NOSE AREA. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RADOME AND OTHER AREAS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED · airframe 10,011 hrs · 10,330 cycles

CREW REPORTED THE STAB TRIM & MACH TRIM WILL NOT ENGAGE ON CLIMBOUT. CREW ELECTED TO RETURN TO LEX AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED THE HSTCU CIRCUIT BREAKERS, PERFORMED A MEMORY RESET AND PERFORMED AN OPS CHECK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. BITE AND OPS CHECKS BOTH WERE GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SELECTOR VALVE — FAILED (NR 2) · airframe 9,772 hrs · 10,080 cycles

CREW REPORTED A GEAR DISAGREE MESSAGE ON APPROACH. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MLG SELECTOR VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (NR 2 NACELLE) · airframe 7,609 hrs · 7,741 cycles

CREW REPORTED A NR 2 COWL ANTI-ICE CAS MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ANTI-ICING VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED · airframe 7,166 hrs · 7,271 cycles

CREW REPORTED A LIGHTNING STRIKE ON DESCENT. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION. MAINTENANCE REPAIRED ALL DAMAGE AND REPLACED A STATIC DISCHARGER. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (LT WINGLET) · airframe 4,785 hrs · 4,810 cycles

LIGHTNING DAMAGE WAS DISCOVERED ON THE LEFT WINGLET TIP DURING PERFORMANCE OF A ROUTINE INSPECTION. MAINTENANCE PERFORMED DETAILED LIGHTNING STRIKE INSPECTIONS AND FOUND NO OTHER DAMAGE. THE WINGLET WAS REPAIRED IAW BOMBARDIER REO 601R-57-31-065 AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRIKER — DAMAGED (PAX DOOR SEAL) · airframe 4,279 hrs · 4,329 cycles

THE CREW REPORTED A LOUD SQUEAL FROM THE PASSENGER DOOR DURING CLIMBOUT. THE AIRCRAFT RETURNED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO THE PASSENGER DOOR FORWARD AND AFT SEAL STRIKERS. A TEMPORARY REPAIR WAS PERFORMED IAW BOMBARDIER REO 601R-53-22-059. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: PITOT HEAD — BIRD STRIKE (FUSELAGE) · airframe 4,236 hrs · 4,285 cycles

AFTER LANDING THE CREW REPORTED A BIRD STRIKE TO THE RT SIDE OF THE RADOME AND RT PITOT TUBE. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION. THE RT PITOT TUBE WAS FILLED WITH BIRD DEBRIS. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REMOVED & REPLACED THE RT PITOT PROBE. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 3,187 hrs · 3,188 cycles

DURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED TWO HOLES PUNCTURED IN THE FUSELAGE SKIN BELOW AND AFT OF THE CARGO DOOR. THE HOLES WERE TEMP REPAIRED AND THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE REPAIRED DAMAGED STRINGERS 22L & 23L IAW CRJ 200 SRM 53-00-03 AND REPAIRED THE FUSELAGE SKIN AT FS 605-654.50 STR 20L-24L IAW BOMBARDIER REPAIR ENGINEERING ORDER 601R-53-61-1391. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: FLAP SYSTEM — UNKNOWN · airframe 3,184 hrs · 3,186 cycles

INBOUND TO DCA THE FLAPS FAILED AT 20 DEGREES. THE CREW ELECTED TO DIVERT TO IAD. MAINTENANCE TROUBLESHOT THE SYSTEM IAW CRJ 200 FIM 27-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 2,084 hrs · 2,113 cycles

AFTER TAKEOFF THE CREW OF FLIGHT 2401 NOTED THAT THE AIRCRAFT WAS NOT PRESSURIZING. THE AIRCRAFT RETURNED TO PHL AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AT PHL MEL'D THE PRESSURIZATION SYSTEM. THE AIRCRAFT FLEW TO CAK WHERE PSA MAINTENANCE FOUND THE PRIMARY OUTFLOW VALVE FAILED IN THE OPEN POSITION. THE VALVE WAS REMOVED AND REPLACED IAW CRJ 200 AMM 21-32-01-000-801 AND AMM 21-32-01-400-801. THE PRESSURIZATION SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 1,653 hrs · 1,710 cycles

CREW REPORTED A CARGO DOOR MESSAGE IN FLIGHT. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW 52-70-04 CAT-C.

Part: CONNECTOR — FAILED (RT ENGINE) · airframe 464 hrs · 518 cycles

DURING FLIGHT, THE RIGHT HAND ENGINE WAS SURGING AND FLIGHT 2216 RETURNED TO DAY. MAINTENANCE INSPECTED AND CLEANED THE RIGHT HAND ENGINE CONNECTOR IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.