N254PS

Part: STRUT — CONTAMINATED (NLG) · airframe 34,329 hrs · 34,188 cycles

GEAR DISAGREE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD SERVICED NLG STRUT SUSPECTED AIR IN THE SYSTEM.

Part: SENSOR — OUT OF LIMITS (WOW) · airframe 34,231 hrs · 34,097 cycles

THE CREW RECEIVED A NOSE GEAR DISAGREE AFTER TAKEOFF. THEY RAN THE QRH WHICH TOLD THEM TO LAND AT THE NEAREST SUITABLE AIRPORT. THEY RETURNED TO SHV AFTER BURNING OFF SOME FUEL. FOUND NGL WOW SENSOR TO BE OUT OF LIMITS. ADJUSTED SENSOR IAW CRJ200AMM. OPS CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

RT SIDE FS625 OBLIQUE ANGLE IS CRACKED. C/A: REMOVED AND REPLACED RT OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: LBL 9 SEAT TRACK IS CORRODED AT VARIOUS LOCATIONS FROM FS 559-FS559+80 CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: 5 CARGO TIE DOWNS ARE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED 5 EA ANCHOR PLATES IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: CARGO SEAT TRACK IS CORRODED AT LBL9 BETWEEN FS559+80 AND 559+96. CORRECTIVE ACTION: REMOVED AT REPLACED CARGO SEAT TRACK AT LBL9 BTWN FS559+80 AND 559+96 IAW AMM 53-01-11-000-802/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

GALLEY SVC DOOR/LOWER SILL ANGLE CORRODED IN THREE LOCATIONS. C/A:. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE LOWER SILL ANGLE IAW SRM 51-40-11, 51-42-06, 51-42-13 AND 51-42-21.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: RBL9 CARGO SEAT TRACK IS CORRODED AT FS 559+112. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK AT RBL9 FS559+112 IAW AMM 53-01-11-000-802/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: CARGO SEAT TRACK IS CORRODED AT LBL18 FROM FS559+80 TO FS559+96. CORRECTIVE ACTION: REMOVED AND REPLACED CARGO SEAT TRACK AT LBL18 FROM FS559+80 TO FS559+96 IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: LBL 27 FLOORBEAM IS CORRODED BETWEEN FS 589 - FS 605 CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM CAP IAW REO 601R-53-61-6742 REV -- DATED 2018/10/16.

Part: STRAP — DAMAGED (ZONE 500) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: WHILE PERFORMING TRUNNION SB 601R-57-046 REV C, FOUND 1EA HOLE TO BE PREVIOUSLY OVERSIZED AT MOST AFT HOLE ON STEEL STRAP, LEFT SIDE. CORRECTIVE ACTION: REPAIRED DAMAGED HOLE IAW REO 601R-57-21-2879 REV -- DATED 2018/10/16.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: AFT CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: RT INBOARD CLIP AT F.S. 484 IS CRACKED CORRECTIVE ACTION: REMOVED AND REPLACED 601R31171-9 CLIP IAW SRM 53-41-43 AND 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: FS621 REAR PRESSURE BULKHEAD WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA @ LBL 27 WL 106.25 TO WL 137.25 AT 50% FSH, FAILED NDT INSPECTION. CORRECTIVE ACTION: REPAIRED REAR PRESSURE BULKHEAD AT LBL 27 IAW REO'S 601R-53-61-1285 REV E DATED 2016-10-31, REO 601R-53-61-1240 REV D DATED 2016-10-31 AND REO 601R-53-61-6735 REV -- DATED 2018-10-31

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: CARGO FLOORBEAM IS CORRODED LT SIDE FS 589.00 BETWEEN LBL 9 AND LBL 18. CORRECTIVE ACTION: REMOVED CORROSION FROM FLOORBEAM CAP STRIP AND FOUND CAP STRIP TO BE OUT OF LIMITS, REMOVED AND REPLACED FLOORBEAM CAP STRIP IAW SRM 51-40-11 (TR51-42), 51-42-06, 51-42-21 AND 51-45-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: RBL9 SEAT TRACK IS CORRODED AT VARIOUS LOCATIONS FROM FS 559 TO FS 559+80. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK @ RBL 9 FS 559-55-+80 IAW AMM 53-01-11-000/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.

Part: STRAP — DAMAGED (ZONE 600) · airframe 34,220 hrs · 34,086 cycles

DISCREPANCY: WHILE PERFORMING TRUNNION SB 601R-57-046 REV C, FOUND 1EA HOLE TO BE PREVIOUSLY OVERSIZED AT MOST AFT HOLE ON STEEL STRAP, RIGHT SIDE. CORRECTIVE ACTION: REPAIRED DAMAGED HOLE IAW REO 601R-57-21-2878 REV -- DATED 2018/10/16.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 31,778 hrs · 31,790 cycles

AFTER TAKE OFF, THE CREW TRIED TO RETRACT THE LANDING GEAR AND RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE MAIN GEAR DISPLAYED UP AND LOCKED, BUT THE NOSE GEAR WAS STILL SHOWING DOWN AND GREEN. FOLLOWED THE QRH AND SELECTED THE GEAR MANUAL RELEASE AND ALL GEAR SHOWED DOWN AND LOCKED. DIVERTED AND DECLARED AN EMERGENCY. MAINTENANCE VISUALLY INSPECTED THE GEAR AND NO DEFECTS WERE FOUND. THE LANDING GEAR RETRACTION SYSTEM WAS THEN PLACED ON MEL.

Part: PROXIMITY SENSOR — MALFUNCTIONED (PASSENGER DOOR) · airframe 30,932 hrs · 30,950 cycles

PASSENGER DOOR AMBER MESSAGE IN FLIGHT. REMOVED AND REPLACED PROXIMITY SENSOR PS9MB.

Part: LATCH — STICKING (DOOR) · airframe 30,734 hrs · 30,763 cycles

CAN NOT LATCH MAIN CABIN DOOR. CLEANED AND LUBRICATED LATCH. OPERATIONAL CHECK GOOD.

Part: SWITCH — INOPERATIVE (PAX DOOR) · airframe 30,685 hrs · 30,716 cycles

CABIN ALTITUDE AND OVERBOARD COOL CAUTION MESSAGE IN FLIGHT. AIRCRAFT WAS NOT PRESSURIZING. REMOVED AND REPLACED PASSENGER DOOR SWITCH S102MB.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,038 hrs · 30,103 cycles

CORROSION ON TOP SIDE OF STRAP AT FS 559, LBL30. MAINTENANCE REMOVED AND REPLACED STRAP AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,038 hrs · 30,103 cycles

FS 621 REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATION AT LBL27.50, WL130. MAINTENANCE REPAIRED BULKHEAD WEB AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRAP — CORRODED (BS 559) · airframe 30,038 hrs · 30,103 cycles

CORROSION FOUND ON TOP SIDE OF STRAP AT BS 559 NEAR LBL 30. MAINTENANCE REMOVED AND REPLACED STRAP IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,038 hrs · 30,103 cycles

BS 621 REAR PRESSURE BULKHEAD WEB CRACKED AT LBL 27.50 AT TOP OF CARGO DOOR AFT TRACK. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW REO.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG STEERING) · airframe 29,027 hrs · 29,094 cycles

CREW REPORTED A "STEERING INOPERATIVE" MESSAGE IN FLIGHT. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, COMPLIED WITH SYS RESET AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROL LEVER — FAILED (FLAP SYSTEM) · airframe 28,498 hrs · 28,558 cycles

CREW REPORTED FLAPS FAIL MESSAGE DURING CLIMBOUT. FLAPS AT 8 DEGREES DURING TAKEOFF. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM IAW FIM, R & R FLAP LEVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 28,104 hrs · 28,166 cycles

CREW REPORTED FLAP FAIL AT 30 DEGREES ON FINAL APPROACH. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM AND DETERMINED SYS OPERATED NORMALLY AND THAT CAUSE OF DISCREPANCY WAS OPERATOR ERROR. MAINTENANCE PERFORMED CHECKS AND ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,324 hrs · 27,385 cycles

EMERGENCY LIGHT HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 2 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,324 hrs · 27,385 cycles

EMERGENCY LIGHT HAD BEEN LT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 1 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,324 hrs · 27,385 cycles

EMERGENCY LIGHT HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 3 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,324 hrs · 27,385 cycles

EMERGENCY LIGHTS HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 4 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 26,247 hrs · 26,303 cycles

CREW REPORTED SMOKE LAV CAUTION MESSAGE AT 2,500 FT. ALARM IN LAV WENT OFF WITH F/A SMELLING SMOKY SMELL. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LAV SMOKE DETECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: COALESCER BAG — ODOR (AIR CONDITIONING) · airframe 26,247 hrs · 26,303 cycles

CREW REPORTED SMOKE LAV CAUTION MESSAGE AT 2,500 FT ALARM IN LAV WENT OFF WITH F/A SMELLING SMOKY SMELL. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT COALESCER BAG AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ADC — FAILED (NR 1) · airframe 26,038 hrs · 26,098 cycles

CREW REPORTED CAPTAIN’S PRIMARY FLIGHT DISPLAY (PFD) LOST AIRSPEED, ALTITUDE AND NAVIGATION DATA IN FLIGHT. MACH TRIM ALSO DISCONNECTED AND AUTOPILOT DISENGAGED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT. R & R NR 1 AIR DATA COMPUTER (ADC) AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FUEL NOZZLE — LEAKING (APU) · airframe 25,815 hrs · 25,883 cycles

DURING START OF APU, THE CREW REPORTED A FUEL ODOR IN COCKPIT. MAINTENANCE TROUBLSHOT FUEL ODOR AND FOUND TOP FUEL NOZZLE/FUEL LINE CHAFED AND INDICATION OF FIRE. R & R APU, OPS AND LEAKED CHECK GOOD. ACFT RELEASED FOR SERVICE.

Part: LINE — CHAFED (APU FUEL) · airframe 25,815 hrs · 25,883 cycles

WHILE STARTING THE APU, THE CREW REPORTED A FUEL ODOR IN COCKPIT. MAINTENANCE TROUBLESHOT FUEL ODOR AND FOUND TOP FUEL NOZZLE AND NOZZLE FUEL LINE CHAFED. R & R APU, OPS AND LEAKED CHECK GOOD. ACFT RELEASED FOR SERVICE.

Part: ATTACH FITTING — DAMAGED (BS 333) · airframe 25,772 hrs · 25,840 cycles

PASSENGER DOOR ATTACHMENT STRUCTURE FOR STOP PANEL 832 ET FASTENER HOLE ENLARGED. REPAIRED DAMAGED NUTPLATE AND BOTTOM ROW OF PANEL 832 ET STEP STRUCTURE IAW EO NR CL600-2B19-52-L02946.

Part: STRINGER — CRACKED (BS 379) · airframe 25,772 hrs · 25,840 cycles

STRINGER 3L IS CRACKED .750" LONG AT FS 379.00. REPAIRED CRACKED STRINGER 3L AT FS 379.0 IAW REO 601R-53-21-2582 AND SRM 53-00-03.

Part: FLOORBEAM — DAMAGED (BS 559) · airframe 25,772 hrs · 25,840 cycles

RBL 9 FLOORBEAM HAS ELONGATED HOLE AST FS 559 + 34 ON OTBD SIDE WITH SCREW STILL STUCK IN HOLE. REPAIRED FLOORBEAM AT FS 559+34, RBL 9 IAW SRM 53-00-43, REV 32, REPAIR 1, FIGURE 203, SHEET 2.

Part: STIFFENER — CRACKED (RIGHT INLET) · airframe 25,772 hrs · 25,840 cycles

THE RIGHT INLET INTERNAL STIFFENER AT 11 O'CLOCK FWD MOST HOLE IS CRACKED. CUT AND REMOVED THE DAMAGE PART OF THE INLET INTERNAL STIFFENER. FABRICATED A REPAIR ANGLE, APPROXIMATELY 3.5" LONG AND INSTALLED ANGLE.

Part: DOOR SILL — CORRODED (BS 574 - 621) · airframe 25,772 hrs · 25,840 cycles

CARGO DOOR SILL IS CORRODED AROUND NUTPLATES BS 574 - 621. REMOVED AND REPLACED THE CORRODED DOOR SILL IAW REO 601-53-61-1574, REV B.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 25,773 hrs · 25,840 cycles

FS 202.75 HAS EVIDENCE OF CRACK ON FWD AND AFT SIDE OF BULKHEAD AROUND PARKING BRAKE CABLE HOLE.

Part: STRINGER — CRACKED (BS 379) · airframe 25,773 hrs · 25,840 cycles

STRINGER 3L IS CRACKED .750' LONG AT BS 379.

Part: TARGET — OUT OF RIG (MLG) · airframe 25,559 hrs · 25,631 cycles

CREW REPORTED GEAR DISAGREE WARNING MESSAGE DURING FLIGHT. LEFT GEAR SHOWED DASHES. MANUAL RELEASE WORKED NORMALLY. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND PROXIMITY SENSOR ELECTRONIC UNIT FLAGGING LEFT LANDING GEAR UPLOCK SENSOR AND FOUND TARGET GAP OUT OF RIG. MAINTENANCE ADJUSTED SENSOR GAP AND PERFORMED CHECKS PER AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (IDG) · airframe 24,769 hrs · 24,827 cycles

CREW REPORTED LT ENGINE OIL PRESSURE RED WARNING MESSAGE AT FL320. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND IDG CARBON SEAL LEAKING. MAINTENANCE R & R LT ENGINE IDG CARBON SEAL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED · airframe 24,537 hrs · 24,607 cycles

CREW REPORTED POSSIBLE LIGHTNING STRIKE ON LT SIDE OF ACFT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R THE LOWER VHF ANTENNA AND STATIC WICKS ON HORIZONTAL STABILIZER. REPAIR PERFORMED FOR BURN MARK ON LT SIDE AFT TAIL CONE. MAINTENANCE PERFORMED CHECKS AND ACFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 23,829 hrs · 23,946 cycles

CREW REPORTED AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT POWER STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: POWER UNIT — FAULTY (LAVATORY) · airframe 21,351 hrs · 21,677 cycles

CREW REPORTED THE LAVATORY LIGHT INOP WITH A STRONG ELECTRICAL SMELL. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE LAVATORY POWER UNIT / DIMMER USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 21,038 hrs · 21,406 cycles

CREW REPORTED UPON LEVELING AT 6,000 FEET MSL IN MODERATE TURBULENCE, BOTH CAPTAIN’S PFD (PRIMARY FLIGHT DISPLAY) AND FIRST OFFICER’S PFD FAILED FOR APPROXIMATELY ONE MINUTE. BOTH WERE DARK SCREENS WITH RED ALT, A/S, ATT AND MAG HDG FLAGS. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL TEST OF AHRS (ATTITUDE AND HEADING REFERENCE SYSTEM) USING AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 20,130 hrs · 20,606 cycles

CREW REPORTED LIGHTNING STRIKE AND DAMAGE NOTED ON NOSE CONE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND PUNCTURE IN RADOME AND TWO (2) DAMAGED RIVETS ON RIGHT WINGLET. MAINTENANCE ALSO NOTED NUMBER ONE COM ANTENNA WAS CRACKED. MAINTENANCE REMOVED AND REPLACED NOSE RADOME ASSEMBLY AND NUMBER ONE VHF COM ANTENNA, REPAIRED BURNT RIVETS ON RIGHT WINGLET AND PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 19,089 hrs · 19,645 cycles

CREW REPORTED FLAP FAIL CAS MESSAGE IN FLIGHT WITH FLAPS AT ZERO DEGREES. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 19,086 hrs · 19,640 cycles

CREW REPORTED FLAPS FAIL MESSAGE IN FLIGHT WITH FLAPS AT ZERO DEGREES. CREW RAN QRH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (APU) · airframe 18,352 hrs · 18,934 cycles

CREW REPORTED APU OIL PRESSURE CAUTION MESSAGE IN FLIGHT EN ROUTE FROM CLT TO MGM. CREW SHUT DOWN APU PER QRH, RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT APU, REMOVED AND REPLACED APU LOP (LOW OIL PRESSURE) SWITCH AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,204 hrs · 18,783 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 BULKHEAD AFT J-CLIP WAS FOUND CRACKED. THE FS 280.0 THE FS 280.0 BULKHEAD AFT J-CLIP WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UPLOCK SWITCH — OUT OF ADJUST (LANDING GEAR) · airframe 17,919 hrs · 18,515 cycles

CREW REPORTED LEFT MAIN LANDING GEAR DISAGREE MASTER WARNING ON TAKEOFF FROM XNA. CREW RETURNED TO XNA AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LANDING GEAR SYSTEM, ADJUSTED LEFT AND RIGHT UPLOCK SWITCHES AND TARGETS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PSEU — FAILED (LT MLG) · airframe 17,885 hrs · 18,483 cycles

CREW REPORTED GEAR DISAGREE MASTER WARNING ON GEAR RETRACTION AFTER TAKEOFF FROM TYS. LEFT MAIN GEAR INDICATED RED. CREW RAN QRH, PERFORMED MANUAL GEAR EXTENSION, RETURNED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,292 hrs · 17,907 cycles

AT DAY, CREW REPORTED STRIP OF EMERGENCY LIGHTS BY ROW 1 (AIRCRAFT RIGHT) NOT WORKING. MAINTENANCE INSPECTED, REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT NR 1 POWER STRIP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 17,049 hrs · 17,677 cycles

CREW REPORTED A STRONG FUEL SMELL IN COCKPIT DURING CRUISE. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL TESTED THE APU FUEL CONTROL USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (LT MLG) · airframe 16,956 hrs · 17,590 cycles

AT OAJ, CREW FOUND LEFT INBOARD MAIN TIRE TREAD SEPARATED, DAMAGE TO INBOARD FLAP AT WING ROOT AND DAMAGE TO LEFT ENGINE. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED LEFT INBOARD AND OUTBOARD MAIN LANDING GEAR TIRES, LEFT INBOARD FLAP AND LEFT FLAP STUB FAIRING. FORWARD AND AFT SPINNER, VANE SPACERS AND ALL FAN BLADES WERE REMOVED AND REPLACED ON LEFT ENGINE. LEFT ENGINE ANTI-ICE RELIEF VALVE (POPPED) WAS REMOVED AND REPLACED. CHECKS WERE PERFORMED AND AIRCRAFT RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS.

Part: CONNECTOR — DIRTY (APU) · airframe 16,358 hrs · 17,026 cycles

CREW REPORTED APU OIL PRESSURE AMBER CAS MESSAGE IN FLIGHT EN ROUTE FROM CLT TO XNA. CREW DIVERTED TO TYS BECAUSE RIGHT GENERATOR WAS DEFERRED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO FAULTS IN APU ECU (ELECTRONIC CONTROL UNIT). MAINTENANCE REMOVED, CLEANED AND REINSTALLED LOP (LOW OIL PRESSURE) SWITCH CONNECTOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (APU) · airframe 16,279 hrs · 16,948 cycles

CREW REPORTED, RECEIVED AN APU OIL PRESSURE MESSAGE IN FLIGHT. BECAUSE THE RIGHT IDG WAS DEFERED THE CREW DIVERTED TO TYS LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE APU OIL SYSTEM USING THE AIRCRAFT MAITENANCE MANUALS. THE LOW OIL PRESSURE SWITCH PLUG WAS FOUND CONTAMINATED, WAS CLEANED, AND RE-INSTALLED. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (APU) · airframe 16,280 hrs · 16,949 cycles

CREW REPORTED, RECEIVED AN APU OIL PRESSURE MESSAGE IN FLIGHT. BECAUSE THE RIGHT IDG WAS DEFERRED THE CREW DIVERTED TO BHM LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE APU OIL SYSTEM USING THE AIRCRAFT MAINTENANCE MANUALS. THE LOW OIL PRESSURE SWITCH WAS REMOVED AND REPLACED. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,936 hrs · 16,594 cycles

CREW REPORTED GEAR DISAGREE RED CAS MESSAGE AND NOSE DOOR OPEN RED CAS MESSAGE AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CHECKS OF THE LANDING GEAR RETRACTION AND EXTENSION SYSTEM. NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (AIR DATA SYSTEM) · airframe 15,795 hrs · 16,449 cycles

CREW REPORTED RIGHT AOA, RIGHT PITOT, RIGHT TAT AND RIGHT STATIC AMBER MESSAGES ON TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RESET THE NR 2 AIR DATA SYSTEM CIRCUIT BREAKER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — MALFUNCTIONED (RT ENGINE) · airframe 15,599 hrs · 16,254 cycles

CREW REPORTED A RIGHT COWL ANTI-ICE CAS MESSAGE IN FLIGHT AT CLIMB POWER SETTING ON DEPARTURE FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT COWL ANTI-ICE VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUT — DAMAGED (NLG) · airframe 15,535 hrs · 16,185 cycles

CREW REPORTED THE NLG DID NOT RETRACT WHEN SELECTED. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE USING THE AIRCRAFT MANUALS REMOVED AND REPLACED THE NLG STRUT. TESTS AND SERVICING WERE DONE PER THE AIRCRAFT MANUALS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,994 hrs · 15,656 cycles

DURING SCHEDULED INSPECTION A CRACK WAS FOUND AT FS 559 BULKHEAD RIGHT SIDE. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLUID — LOW (APU) · airframe 14,807 hrs · 15,479 cycles

CREW REPORTED AN APU PRESS CAUTION MSG. CREW DIVERTED TO RIC LANDING WITHOUT INCIDENT. MAINTENANCE USING THE MANUFACTURER MAINTENANCE MANUALS INSPECTED AND FOUND APU OIL LEVEL LOW. MAINTENANCE SERVICED THE OIL. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,426 hrs · 14,020 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FS 621.00 PRESSURE BULKHEAD AT LINE FITTING. REPAIRS WERE MADE PER THE MANUFACTURERS MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 9,352 hrs · 9,718 cycles

CREW REPORTED A FLAPS FAIL AT 8 DEGREES DURING DESCENT INTO DCA. CREW ELECTED TO DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU, BITE CHECK AND SKEW DETECTOR. MAINTENANCE RESET THE FLAP CHANNELS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 9,225 hrs · 9,587 cycles

CREW REPORTED AN APU OIL CAUTION MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND VISUALLY CHECKED THE APU OIL LEVEL AND APU OIL SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OIL LEVEL CHECKED GOOD, NO VISUAL DEFECTS NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INTAKE — DAMAGED (RT ENGINE) · airframe 7,726 hrs · 7,975 cycles

CREW REPORTED A BIRD STRIKE ON APPROACH TO THE RIGHT HAND ENGINE INTAKE COWLING LEADING EDGE. MAINTENANCE INSPECTED AND FOUND THE DAMAGE TO BE 2 INCH LENGTH BY 1 INCH WIDTH BY .15 DEEP. DAMAGE WITHIN LIMITS IN ACCORDANCE WITH THE SHORTS CMA CMM 71-61-01. TEMPORARY AIRCRAFT DAMAGE AUTHORIZATION 20044 ISSUED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 6,902 hrs · 7,056 cycles

CREW REPORTED THE PLANE SUDDENLY JUMPED ON TAKEOFF ROLL AT 20-30 KTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE MAIN LANDING GEAR AND FOUND NO DEFECTS. MAINTENANCE ALSO PERFORMED A TAXI CHECK WITH THE CREW AND FOUND NO DEFECTS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-10-00-210-801. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 5,672 hrs · 5,728 cycles

CREW REPORTED A FLAPS FAIL CAS MESSAGE AFTER TAKEOFF. CREW DIVERTED AND LANDED IN ILM WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS NOTED AND OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NONE — NONE (NONE) · airframe 4,668 hrs · 4,690 cycles

CREW REPORTED A BIRD STRIKE ON RT LEADING EDGE. AREA WAS INSPECTED AND CLEANED. NO DAMAGE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 4,364 hrs · 4,379 cycles

ON APPROACH WITH FLAPS AT 20DEGREES THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND RESET THE FLAP SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,132 hrs · 4,143 cycles

ON FINAL APPROACH WITH FLAPS AT 8 DEGREES SELECTED TO 20 DEGREES, THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND RESET THE FLAP SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,936 hrs · 3,944 cycles

ON FINAL APPROACH WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES THE -FLAPS FAIL- MESSAGE ILLUMINATED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND RESET THE FLAP SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,671 hrs · 3,671 cycles

THE FLAP FAIL CAUTION MESSAGE ILLUMINATED WHEN FLAPS WERE SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW BOMBARDIER CRJ200 SL-00-001. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,590 hrs · 3,593 cycles

DURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,550 hrs · 3,562 cycles

DURING APPROACH WITH FLAPS 20 DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN FLAPS WERE SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURES. NO FAULTS WERE FOUND. THE FLAP SYSTEM WAS RESET AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 3,400 hrs · 3,415 cycles

THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE IN CRUISE AT 15000 FT WITH GEAR AND FLAPS UP. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE LT HORIZONTAL STABILIZER AND THE LOWER AFT FUSELAGE. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,158 hrs · 3,180 cycles

DURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8° SELECTED TO 20°. THE CREW FOLLOWED THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM PER THE CRJ FIM. THE FLAP SYSTEM WAS RESET IAW BOMBARDIER SL 00-001. THE FLAPS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — INTERMITTENT (PAX DOOR) · airframe 2,942 hrs · 2,949 cycles

THE PAX DOOR OUT HANDLE CAUTION MESSAGE ILLUMINATED SEVERAL TIMES DURING THE FLIGHT. THE AIRCRAFT WAS FERRIED TO CLT WHERE MAINTENANCE REMOVED & REPLACED THE PAX DOOR OUTER HANDLE PROXIMITY SWITCH IAW CRJ200 AMM 52-70-04-000(400)-803. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 2,850 hrs · 2,854 cycles

THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WITH THE FLAPS AT 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE CLEARED CODES FROM THE FECU AND RESET THE SYSTEM IAW CRJ200 FIM 27-50-00. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (TE FLAPS) · airframe 2,726 hrs · 2,732 cycles

THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS SELECTED TO 20 DEGREES AND INDICATING 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE PERFORMED FAULT ISOLATION AND RESET PROCEDURES IAW CRJ200 FIM 27-50-00. THE SYSTEM RESET AND NO FURTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 1,659 hrs · 1,615 cycles

DURING CLIMBOUT (CLT TO CAK) THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 20DEGREES. THE CREW OF FLIGHT 2560 FOLLOWED THE QRH, RETURNED TO CLT, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE INTERROGATED AND RESET THE FECU. A FLAP SYSTEM AND FLAP CONTROL LEVER TEST WAS PERFORMED IAW CRJ 200 FIM 27-50-00. THE OPERATIONAL TEST WAS NORMAL AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (AILERONS) · airframe 1,200 hrs · 1,164 cycles

DURING TAKEOFF ROLL AT PHL THE CREW OF FLIGHT 2470 RECEIVED A CONFIG AILERON WARNING WHEN THE YOKE WAS MOVED FOR CROSSWIND CORRECTION. THE CREW ABORTED THE TAKEOFF AND TAXIED BACK TO THE GATE. PSA MAINTENANCE FOUND THE AILERON TRIM SET OUT OF THE TAKEOFF RANGE. OPERATIONAL CHECKS OF THE AILERON SYSTEM WERE PERFORMED IAW CRJ 200 AMM 27-11-00-710-801. ALL CHECKS WERE GOOD WITH NO DISCREPANCIES FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 829 hrs · 819 cycles

DURING CLIMBOUT AFTER TAKEOFF FROM DCA THE CREW OF FLIGHT 2326 RECEIVED A FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 20 DEGREES. THE CREW RETURNED TO DCA AND MADE AN UNEVENTFUL LANDING. MAINTENANCE PULLED THE FAULT CODES FROM THE FLAP ELECTRONIC CONTROL UNIT. FAULT DETERMINED TO BE CAUSED BY THE FLAP HANDLE. CIRCUIT BREAKERS WERE CYCLED AND THE CAUTION MESSAGE CLEARED. THE FLAP SYSTEM WAS INSPECTED WITH NO FAULTS FOUND AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RETURNED TO SERVICE.