N230PS

Part: SWITCH — MALFUNCTIONED (ANIT-ICE SYS) · airframe 34,672 hrs · 34,589 cycles

DURING CLIMB CREW BECAME AWARE THE WING ANTI-ICE WAS NOT WORKING. FOLLOWED QRH. CONTACTED ATC AND DECLARED AN EMERGENCY AS THEY WERE IN ICING CONDITIONS AND REQUESTED AN EXPEDITED DECENT TO FL100. UPON REACHING FL100, EMERGENCY CANCELLED. LANDED WITHOUT INCIDENT. PAX WERE ADVISED PRIOR TO DECENT AND DID NOT BRACE. R&R WING ANTI-ICE HEAT SWITCH.

Part: SELECTOR PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,018 hrs · 33,972 cycles

AS THE AIRCRAFT CLIMBED THROUGH FLIGHT LEVEL 230, THE CREW RECEIVED A CABIN ALTITUDE PRESSURIZATION MESSAGE. THE CREW RAN THE IMMEDIATE ACTION LIST AND BEGAN IMMEDIATE DECENT. THE CREW DEPLOYED OXYGEN MASKS AND DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT INCIDENT AND MAINTENANCE WAS DISPATCHED TO INSPECT AND POSSIBLY FERRY TO A MAINTENANCE BASE. MX REMOVED & REPLACED CABIN PRESSURE SELECTOR PANEL OPS & LEAK CHECK NORMAL.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 32,366 hrs · 32,375 cycles

FOUND RIB AT ES 14.47 CRACKED. REMOVED THE DAMAGED RIB. AND INSTALLED A REPLACEMENT IAW SRM 51-42-06, 51-42-13, AND EO SNIEO S06.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,366 hrs · 32,375 cycles

FOUND THE REAR PRESSURE BULKHEAD WEB WITH MULTIPLE CRACK INDICATIONS AT RBL 18, WL 103, TWO INCHES LONG 50% FSH. FAILED NDT INSPECTION. PERFORM INTERIM REPAIR IAW REO 601R-53-61-1285, REV E.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,366 hrs · 32,375 cycles

FOUND THE REAR PRESSURE BULKHEAD WEB BS 621, HAD MULTIPLE CRACK INDICATIONS NOTED AT RBL 27.5, WL 103, TWO INCHES LONG AND 100% FSH. PERFORMED AN INTERIM REPAIR THE BULKHEAD IAW REO 601R-53-61-1285, REV E.,

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LEFT HAND SIDE SEAT TRACK FS 499 - 544 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 499 - 544 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-131 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LEFT HAND SIDE SET TRACK FS 364 - 409+16 SEGMENT IS CORRODED. REMOVED LT SIDE SEAT TRACK FROM FS 364-406+16 IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE LT SIDE SEAT TRACK FROM FS 364-409+16 P/N 601R38312-31 IAW AMM 53-01-11-400-802. FABRICATED NEW SERVICEABLE LT SIDE SEAT TRACK FROM STOCK P/N N126-2075 IAW REO 601R-53-00-055.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LEFT HAND FLOOR SILL IS CORRODED FROM FS 559+80 TO FS 621. REMOVED CARGO FLOOR SILL IAW SRM 51-42-06 & 51-42-21. LOCATE, DRILL & INSTALL NEW CARGO DOOR SILL P/N 601R3501263 IAW SRM 51-40-11 & REO 601R-53-61-1574 REV B DATED 2012-04-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

ALL CARGO BAY FLOOR SEAT TRACKS ARE CORRODED FROM FS 559+80 TO FS 621. REMOVED ALL CARGO BAY FLOOR SEAT TRACKS FROM FS 559+79 TO FS 621 IAW AMM 53-01-11-000-802. INSTALLED 7 EA NEW SERVICEABLE CARGO FLOOR SEAT TRACKS IAW AMM 53-01-11-400-802 P/N 601R31032-51, LBL 9 FS 621. INSTALLED 4 EA NEW SERVICEABLE FITTING ASSY (P/N CDSP1900-509) IAW SRM 51-41-04.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

RIGHT HAND FLOOR SILL IS CORRODED FROM FS 559+80 TO FS 559+112. REMOVED AND INSTALLED RT FLOOR NEW SILL PLATE PN 601R31133-102 FROM FS 559+80 TO FS 559+112 IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

RIGHT HAND SIDE SEAT TRACK FS 409+16 - 409+112 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 409+16 – 409+112 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-29 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LEFT HAND SIDE SEAT TRACK FS 449 - 499 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 449 - 499 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-115 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

FUSELAGE FRAME FS 589 IS CORRODED FROM STR 27L TO STR 26R. REMOVED AND INSTALLED NEW LOWER FRAME SECTOR PN 601R36025-61 AT FS 589 A IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LEFT HAND SIDE TRACK FS 409+16 - 409+112 SEGMENT CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 409+16 - 409+112 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-29 IAW AMM TASK 53-01-11-400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 399 TO FS 409+128. LOCATED, FABRICATED, DRILLED AND COUNTERSUNK SEAT TRACK RBL 9 FS 399 TO FS 409+128 PER REO 601R-53-00-485 REV B DATED 2016-04-01. REMOVED AND INSTALLED FABRICATE SEAT TRACK PN 601R31032-27 AT RBL 9 AND LBL 9 FS 399 - FS 409+128 IAW AMM 53-01-11-946-003 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

RIGHT HAND SIDE SEAT TRACK FS 364 - 409+16 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 364 - 409+16 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-31 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

FUSELAGE FRAME FS 605 IS CORRODED FROM STR 26L TO 24R. REMOVED AND INSTALLED FS 605 FRAME SECTOR PN 601R36026-27 IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LEFT HAND SIDE SEAT TRACK FS 544 - 559+80 SEGMENT IS CORRODED. REMOVED & REPLACED SIDE SEAT TRACK FS 544 - 559+80 PN: 601R38312-25 IAW AMM TASK 53-01-11-400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 364 TO FS 399. REMOVED AND INSTALLED NEW SERVICEABLE SEAT TRACK P/N 601R31032-15 & SCREW NAS517 IAW AMM 53-01-11-000/400-802.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

DRAIN MAST DOUBLER BETWEEN FS 605 AND FS 621 AND STR 25R - STR 26R IS CORRODED. REMOVED AND INSTALLED DRAIN MAST DOUBLER PN: 601R43216-9 IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

RIGHT HAND SIDE SEAT TRACK FS 409+112 - 449 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS FS 409+112 - 449 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-119 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

RIGHT HAND SIDE SEAT TRACK FS 559-499 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 559-499 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-115 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

RIGHT HAND SIDE SEAT TRACK FS 499-544 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 499-544 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-131 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,366 hrs · 32,375 cycles

FS 621 BULKHEAD FLOOR SILL ANGLE IS CRACKED AT LBL 43. REMOVED AND INSTALLED SERVICEABLE FLOOR SILL ANGLE P/N 601R-53-61-004-1 FROM LBL 36-43 FS 621 IAW SRM 51-42-06 & SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

LEFT HAND SIDE SEAT TRACK FS 409+112 - 449 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 409+112 - 449 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-119 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,366 hrs · 32,375 cycles

RIGHT HAND SIDE SEAT TRACK FS 544-559+80 SEGMENT IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 544-559+80 WITH A NEW SERVICEABLE SEAT TRACK SEGMENT P/N 601R38312-25 IAW AMM TASK 53-01-11-000/400-802 AND REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: THRUST REVERSER — WARNING LIGHT (LEFT) · airframe 28,795 hrs · 28,877 cycles

CREW REPORTED INTERMITTENT LT REVERSER UNLOCKED CAUTION MESSAGE IN FLIGHT. MESSAGE WENT FROM INTERMITTENT TO STEADY. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LT THRUST REVERSER IAW MEL. ACFT RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 461-473) · corrosion level 2 · airframe 28,765 hrs · 28,846 cycles

LT PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF MINOR CORROSION BETWEEN FS 461 - 473. REMOVED APPROXIMATELY .004" OF DAMAGE FROM SILL ANGLE.

Part: FLOOR SUPPORT — CORRODED (BS 461-513) · corrosion level 2 · airframe 28,765 hrs · 28,846 cycles

RT PRESSURE FLOOR SILL ANGLE IS CORRODED AT FS 513 AND BETWEEN FS 461 AND FS 473. REMOVED APPROXIMATELY .004" OF DAMAGE FROM SILL ANGLE, APPROXIMATELY .076" MATERIAL REMAINING.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 28,752 hrs · 28,831 cycles

CREW REPORTED LT REVERSER UNLOCKED CAUTION MESSAGE APPEARED INTERMITTENTLY SEVERAL TIMES DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LT THRUST REVERSER IAW MEL. ACFT RELEASED FOR SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 28,632 hrs · 28,717 cycles

CREW REPORTED EMERGENCY EXIT FLOOR LIGHTING STRIP WIRES PULLED LOOSE AT LAVATORY. MAINTENANCE INSPECTED AND FOUND LIGHTING STRIP CONTACT ENDS PULLED OUT. MAINTENANCE CRIMPED NEW CONTACT ENDS ON, SECURED LIGHT STRIP TO FLOOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ACTUATOR — BINDING (TE FLAPS) · airframe 28,191 hrs · 28,280 cycles

CREW REPORTED FLAPS FAIL MESSAGE AT 160 KNOTS AND 40/39 DEGREE ASYMMETRY ON EXTENSION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R RT INBD FLAP OTBD ACTUATOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DAMAGED (FLAP SYS) · airframe 28,160 hrs · 28,250 cycles

CREW REPORTED FLAPS FAIL MESSAGE WHILE SELECTING FLAPS FROM 8 TO 20 DEGREES. FLAPS REMAINED AT 8 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R MATING CONNECTOR PLUG FOR LT BRAKE AND POSITION SENSOR UNIT DUE TO BENT PINS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — DAMAGED (FLAP SYS) · airframe 28,160 hrs · 28,250 cycles

CREW REPORTED FLAPS FAIL MESSAGE WHILE SELECTING FLAPS FROM 8 TO 20 DEGREES. FLAPS REMAINED AT 8 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R LT BRAKE AND POSITION SENSOR UNIT DUE TO BENT ELECTRICAL CONNECTOR PINS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 27,530 hrs · 27,625 cycles

CREW REPORTED FLAPS FAIL AMBER MESSAGE ON APPROACH. FLAPS FAILED AT ZERO DEGREES. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM IAW ACFT FAULT ISOLATION MANUAL, FIM, R & R FLAP ELECTRONIC CONTROL UNIT, FECU, AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (PROX SENSOR) · airframe 27,370 hrs · 27,462 cycles

CREW REPORTED WOW INPUT CAUTION, WOW OUTPUT CAUTION, WOW OUTPUT STATUS AND PROXIMITY SYS FAULT STATUS MESSAGES. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RERACKED PROXIMITY SENSOR ELECTRONIC UNIT (PSEU) AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 27,258 hrs · 27,356 cycles

CREW REPORTED PASSENGER DOOR EMERGENCY EXIT SIGN ON FORWARD CLOSET OUT. MAINTENANCE INSPECTED, FOUND BROKEN WIRE AT CONNECTOR, R & R CONNECTOR AND MULE PIN AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 26,427 hrs · 26,534 cycles

CREW REPORTED EMERGENCY LIGHTS AFT OF ROW 8 WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED, R & R CONNECTOR PINS, SOCKETS, JUMPER AND 1 LIGHT STRIP AND PERFORMED CHECKS AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,427 hrs · 26,534 cycles

AFT EMERGENCY LIGHT PIN BROKEN. MAINTENANCE INSPECTED, R & R LAST LIGHT STRIP OF EMERGENCY FLOOR LIGHTS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 24,529 hrs · 24,678 cycles

CREW REPORTED GEAR DISAGREE WARNING MESSAGE AFTER LANDING GEAR SELECTED UP. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R MLG SELECTOR VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 24,302 hrs · 24,457 cycles

CREW REPORTED STABILIZER CHANNEL 2 INOPERATIVE STATUS MESSAGES IN FLIGHT. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R MOTOR CONTROL UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (APU OIL) · airframe 23,498 hrs · 23,729 cycles

CREW REPORTED APU OIL PRESSURE MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED, REMOVED AND REPLACED APU LOW OIL PRESSURE SWITCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: TIRE — FAILED (RT INBOARD) · airframe 23,159 hrs · 23,408 cycles

CREW REPORTED TREAD SEPARATION ON RT INBD TIRE, DAMAGING RT FLAP. MX INSPECTED, R & R BOTH RT MLG WHEEL/ TIRE ASSEMBLIES AND COMPLIED WITH REPAIR DISPOSITION FOR DENT TO RT INBD FLAP LOWER SKIN IAW AMM AND REO. ACFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 22,185 hrs · 22,518 cycles

CREW REPORTED GEAR DISAGREE RED MESSAGE UPON GEAR SELECTED DOWN. THE QRH WAS ACCOMPLISHED CYCLING GEAR AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED AN OPERATION CHECK OF THE LANDING GEAR RETRACTION AND EXTENSION SYSTEM PER AIRCRAFT MANUALS WITH NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,459 hrs · 20,980 cycles

DURING SCHEDULED MAINTENANCE THE REAR PRESSURE BULKHEAD WEB HAS INDICATION OF CRACK. THE REAR PRESSURE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 20,459 hrs · 20,980 cycles

DURING SCHEDULED MAINTENANCE A VERTICLE STIFFENER AT BL 0 AT FS 409.0+128 WAS CRACKED. THE VERTICLE STIFFENER FS 409.0 + 128 AT BL 0 WAS INSPECTED, REMOVED, AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 20,459 hrs · 20,980 cycles

DURING SCHEDULED MAINTENANCE A DENT WAS FOUND AT FS 635.0. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 20,459 hrs · 20,980 cycles

DURING SCHEDULED MAINTENANCE FOUND A DENT AT FS 183.0. STRINGER BL 0 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — DAMAGED (RT MLG) · airframe 20,293 hrs · 20,822 cycles

CREW REPORTED ON LANDING THE RIGHT MAIN OUTBOARD TIRE WAS SHREDDED. MAINTENANCE INSPECTED, REPAIRED, REMOVED AND REPLACED THE FOLLOWING. RIGHT MAIN OUTBOARD WHEEL ASSEMBLY, RIGHT FLAP ASSEMBLY, DOOR BELLCRANK, AND RIGHT DOOR STRUT. CHECKS WERE PERFORMED USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 19,132 hrs · 19,715 cycles

CREW REPORTED BIRD STRIKE ON NUMBER TWO (2) ENGINE. NO CHANGE IN ENGINE VIBRATION NOTED. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED RIGHT ENGINE AND NOTED FAN BLADE DAMAGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, REMOVED AND REPLACED THREE (3) CRACKED FAN GUIDE VANE SPACERS AND MULTIPLE BENT FAN BLADES ON RIGHT ENGINE. REPAIR OR REPLACEMENT OF DENTED RIGHT ENGINE UPPER TRANSLATING COWL WAS DEFERRED BY MAINTENANCE. AIRCRAFT RELEASED FOR SERVICE. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED RIGHT UPPER TRANSCOWL AND CLEARED DEFERRAL. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.

Part: PACKING — LEAKING (APU) · airframe 19,022 hrs · 19,607 cycles

CREW REPORTED STRONG SMELL OF OIL COMING FROM PACKS AND APU EXHAUST. MAINTENANCE CLEANED AND INSPECTED APU AREA AND FOUND FUEL LEAK. MAINTENANCE REMOVED AND REPLACED PACKING AT FUEL SOLENOID ELBOW ON APU FUEL CONTROL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,831 hrs · 18,451 cycles

CREW REPORTED SMOKE / FUMES SMELLED VIA LEFT PACK SYSTEM ON DESCENT INTO TYS. AIRCRAFT LANDED IN TYS WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT DUCTS, APU COMPARTMENT AND AVIONICS BAY AND RAN APU AND ENGINES. NO DEFECTS OR SMELL NOTED. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 17,648 hrs · 18,278 cycles

CREW REPORTED HYDRAULIC LOW PRESSURE AMBER MESSAGE FOLLOWED BY WOW INPUT AMBER MESSAGE DURING CLIMBOUT OF TYS. WHEN GEAR SELECTED UP, CREW RECEIVED RED GEAR DISAGREE MESSAGE. AFTER ABOUT 10 SECONDS, MESSAGES WENT AWAY. CREW CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND AIR IN NUMBER 3 HYDRAULIC SYSTEM. MAINTENANCE BLED AND RE-SERVICED NUMBER 3 HYDRAULIC SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (LT MLG) · airframe 17,321 hrs · 17,981 cycles

CREW REPORTED THAT THE LEFT INBOARD MAIN LANDING GEAR TIRE THREAD SEPERATED. USING THE AIRCRAFT MAINTENANCE MANUAL, MAINTENANCE INSPECTED, REMOVED, TESTED, AND REPLACED THE TIRES ON THE LEFT MAIN LANDING GEAR AND LEFT FLAP ASSEMBLY. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — CHAFED (LT ENGINE) · airframe 16,443 hrs · 17,149 cycles

CREW REPORTED LEFT ENGINE UNCOMMANDED ACCELERATION AND N1 RED, WITH INDICATION WELL ABOVE 100 PERCENT DURING CLIMBOUT FROM CLT. ALL OTHER LEFT ENGINE INDICATIONS WERE TRACKING HIGHER PRIOR TO THRUST REDUCTION. CREW FOLLOWED QRH, RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED LEFT ENGINE BROWN W9 HARNESS (FOUND CHAFED) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PIN — NOT SEATED (CONNECTOR) · airframe 16,428 hrs · 17,133 cycles

CREW REPORTED UNCOMMANDED LEFT ENGINE ACCELERATION DURING CLIMBOUT FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESEATED AN UNSEATED PIN ON FUEL CONTROL UNIT TORQUE MOTOR CIRCUIT HARNESS CONNECTOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRANSFER PUMP — CLOGGED (FUEL TANK) · airframe 15,755 hrs · 16,423 cycles

CREW REPORTED FUEL IMBALANCE DURING CRUISE FLIGHT EN ROUTE FROM DCA TO BNA. CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT TRANSFER EJECTOR PUMP AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 15,748 hrs · 16,417 cycles

CREW REPORTED A FUEL IMBALANCE IN CRUISE FLIGHT EN ROUTE FROM CLT TO XNA. CREW SHUT DOWN THE RIGHT ENGINE PER THE QRH, DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. NO FAULTS WERE FOUND. THE FUEL IMBALANCE CORRECTED ITSELF ON THE GROUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 15,710 hrs · 16,384 cycles

CREW RECEIVED A FUEL IMBALANCE CAS MSG. CREW DIVERTED TO MGM LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING THE AIRCRAFT MAINTENANCE MANUAL AND NO DEFECTS WERE FOUND. MAINTENANCE ALSO RESET THE FUEL SYSTEM CONTROL COMPUTER. OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,723 hrs · 15,457 cycles

DURING INSPECTION CRACKS WERE FOUND ON THE FS 559.00 CAP ANGLE PRESSURE BULKHEAD. REPAIRS WERE MADE USING MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: SCREEN — OBSTRUCTED (LT ENGINE) · airframe 14,282 hrs · 14,984 cycles

CREW REPORTED LEFT ENGINE OIL TEMPERATURE HIGH AND OIL PRESSURE LOW ON CLIMBOUT FROM CAK EN ROUTE TO CLT. AIRCRAFT DIVERTED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, CLEANED DEBRIS FROM THE LEFT ENGINE LUBE AND SCAVENGE PUMP SCREEN AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — DAMAGED (LT ENGINE) · airframe 14,280 hrs · 14,981 cycles

CREW REPORTED A LEFT ENGINE OIL PRESSURE WARNING IN FLIGHT EN ROUTE FROM CLT TO CAK. AIRCRAFT LANDED IN CAK WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT ENGINE’S CARBON SEALS FOR THE INTEGRATED DRIVE GENERATOR (IDG), AIR TURBINE STARTER (ATS) AND ENGINE DRIVEN PUMP (EDP). CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS.

Part: UPLOCK — OUT OF ADJUST (RT MLG) · airframe 14,017 hrs · 14,687 cycles

ON GEAR RETRACTION DURING TAKEOFF FROM HSV, THE CREW REPORTED A RED GEAR DISAGREE, TRIPLE CHIME AND A RED BOX FOR THE RT MAIN LANDING GEAR ON EICAS. AIRCRAFT RETURNED TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND ADJUSTED THE RT MAIN LANDING GEAR UPLOCK AND THE NOSE LANDING GEAR UPLOCK USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — DEFECTIVE · airframe 13,994 hrs · 14,661 cycles

CREW REPORTED AN ANTI-ICE DUCT RED CAS MESSAGE AFTER DEPARTURE FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REMOVED AND REPLACED A HEAT SENSING ELEMENT USING THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL AND NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRANSFER VALVE — FAILED (FUEL SYSTEM) · airframe 13,249 hrs · 13,870 cycles

CREW REPORTED A FUEL IMBALANCE. AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE RIGHT FUEL TRANSFER SHUT OFF VALVE AND TESTED PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,102 hrs · 13,715 cycles

CREW REPORTED A BIRD STRIKE ON NOSE OF AIRCRAFT AT TRI. MAINTENANCE INSPECTED AND REPAIRED DENT TO AIRCRAFT. INSPECTIONS AND REPAIRS WERE DONE PER AIRCRAFT MAINTENANCE MANUALS AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPUTER — FAILED (FUEL SYSTEM) · airframe 13,028 hrs · 13,633 cycles

CREW REPORTED A FUEL IMBALANCE AND DIVERTED TO TYS WHERE THE LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE FUEL COMPUTER. TROUBLESHOOTING AND CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE BOTTLE — EMPTY (CARGO BAY) · airframe 5,315 hrs · 5,303 cycles

CREW RECEIVED A CARGO BOTTLE LOW CAS MESSAGE. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CARGO FIREX BOTTLE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (RT A/C PACK) · airframe 4,634 hrs · 4,629 cycles

AFTER TAKEOFF WITH THE RT PACK DEFFERED, THE CREW REPORTED CABIN PRESSURIZATION WAS INOPERATIVE IN AUTO AND MANUAL MODES. THE FLIGHT RETURNED TO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT PACK PRESSURE REGULATING SHUTOFF VALVE. THE PRESSURIZATION SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: VALVE — FAILED (RT A/C PACK) · airframe 3,227 hrs · 3,234 cycles

DURING CLIMBOUT WITH THE RT PACK DEFERRED PER MEL 21-51-01(C), THE LT PACK TEMP CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED & REPLACED THE DUAL POSITION VALVE IAW CRJ200 AMM 21-21-10-400-801. OPERATIONAL CHECKS WERE GOOD. THE MELS WERE CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — FAILED (NR 2 ENG TEMP) · airframe 3,087 hrs · 3,093 cycles

NR 2 ENGINE N1 STARTED FLUCTUATING +/-10% WHILE CLIMBING THROUGH 21,000 FT. THE AIRCRAFT RETURNED TO PHL WHERE MAINTENANCE REMOVED AND REPLACED THE T2C COMPRESSOR INLET TEMPERATURE SENSOR IAW CRJ200 AMM 73-21-09-000(400)-801. ALL GROUND OPERATIONAL CHECKS WERE GOOD. A SATISFACTORY OPERATIONAL CHECK FLIGHT WAS PERFORMED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAPS) · airframe 1,907 hrs · 1,890 cycles

DURING CRUISE FLIGHT WITH FLAPS SELECTED TO ZERO DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLLUMINATED. THE CREW OF FLIGHT 2292 (YOW TO PHL) DIVERTED THE FLIGHT TO YUL AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE LT FLAP BRAKE AND POSITION SENSOR UNIT IAW CRJ 200 AMM 27-51-10-000-801 AND 27-51-10-400-801. RIGGING/OPERATIONAL CHECKS WERE GOOD IAW CRJ200 AMM 27-51-10-830-801 AND 27-54-00-710-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 1,852 hrs · 1,832 cycles

WHILE IN CRUISE FLIGHT AT 29,000 FEET THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2286 FOLLOWED QRH PROCEDURES AND CONTINUED THE FLIGHT TO CAK, DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ 200 AMM 27-51-05-000-801. OPERATIONAL CHECKS OF THE FLAP SYSTEM WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 1,827 hrs · 1,810 cycles

DURING CLIMBOUT FROM BHM, AS THE FLAPS WERE RETRACTED TO ZERO DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2276 FOLLOWED THE QRH, CONTINUED THE FLIGHT TO PHL, AND MADE AN UNEVENTFUL LANDING. THE CREW DID DECLARE AN EMERGENCY AND THE CABIN WAS PREPPED FOR AN EMERGENCY LANDING. PSA MAINTENANCE IN PHL INSPECTED AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ 200 FIM 27-50-00. ALL FLAP SYSTEMS CHECKED GOOD AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.