N228PS

Part: FLOOR SUPPORT — CORRODED (BS 647-621) · corrosion level 2 · airframe 38,086 hrs · 37,652 cycles

FLOOR BEAM CAP CORRODED AT LBL 27 FS 617 TO 621. REMOVED LBL 27 FLOORBEAM FITTING AT FS 617 - 621 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. PN 601R35289-1. INSTALLED NEW SERVICEABLE LBL 27 FLOORBEAM FITTING IAW REO 601R-53-61-3778 REV B DATED 12/19/16.

Part: BRACKET — CRACKED (ASSIST MOTOR) · airframe 38,086 hrs · 37,652 cycles

PAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET IS CRACKED. REMOVED DAMAGED PAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE. IAW CRJ200 SRM 51-40-11, 51-42-06, AND 51-42-13.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 2 · airframe 38,086 hrs · 37,540 cycles

FLOOR BEAM CAP CORRODED AT RBL 9.00 BETWEEN FS 559+80 TO FS 559+96. FABRICATED, LOCATED, DRILLED AND INSTALLED, FABRICATED FLOORBEAM CAP IAW CRJ 200 SRM 51-24-36 AND 51-40-11.

Part: FLOOR SUPPORT — CRACKED (BS 574-621) · airframe 38,086 hrs · 37,540 cycles

FLOOR BEAM CAP CORRODED AND CRACKED AT LBL 27 BETWEEN FS 574.00 TO FS 621.00. INSTALLED NEW SERVICEABLE FLOOR BEAM CAP IAW REO 601R-53-61-3778 REV B DATED 12/19/16.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 2 · airframe 38,086 hrs · 37,540 cycles

FLOOR BEAM CAP CORRODED AT RBL 27 BETWEEN FS 559+80 TO FS 559+96. LOCATED,DRILLED, AND INSTALLED FLOORBEAM CAP AT RBL27 ON FS 559+80-559+96 IAW CRJ 200 SRM 51-40-11 AND 51-42-21 AND S+SEA 72-2020-163 REV P1 DATED 03/06/20.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 37,720 hrs · 37,336 cycles

HYD 2 LOW PRESS IN FLIGHT 0PSI. - AT FL2200, CREW RECEIVED A HYDRAULIC PUMP #2 LOW PRESSURE CAUTION MESSAGE FOLLOWED BY THE HYDRAULIC GAUGE SHOWING 0 PSI. CREW RAN QRH, DECLARED EMERGENCY AND LANDED RDU WITHOUT ISSUE. R&R #2 EDP IAW AMM. PERFORMED OPS CHECK AND LEAK CHECK. OPS CHECK GOOD AND LEAK CHECK GOOD.

Part: CONTROL UNIT — FAILED (TE FLAP SYSTEM) · airframe 36,584 hrs · 36,281 cycles

ON TAKEOFF CREW SELECTED FLAPS 20. ONCE AIRBORNE SELECTED FLAPS 8 AND RECEIVED A FLAPS FAIL CAUTION MSG. CREW CONTINUED CLIMB TO 7000. RAN QRH, DECLARED AN EMERGENCY AND LANDED NORMALLY. MX REMOVED AND REPLACED FECU. OPS CHECK GOOD.

Part: SKIN — CRACKED (RT WING) · corrosion level 2 · airframe 36,097 hrs · 35,804 cycles

CORROSION AND CRACK AROUND RT WING LOWER PLANK AROUND DRAIN HOLE AT WS 85.5 BETWEEN STRINGER14R-15R. CA ACCOMPLISHED REPAIR IAW REO 601R-57-21-3024.

Part: FLAP SYSTEM — MALFUNCTIONED (WING) · airframe 34,820 hrs · 34,676 cycles

DURING LANDING THE CREW DECIDED TO DO A GO AROUND DUE TO WINDS AND SELECTED THE FLAPS UP AND RECEIVED A FLAP FAIL AT 8 DEGREES. THE AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX C/W TO 27-050-004-09 REV Q,IAW TO INST. FLAPS SYS OPS CHECKS GOOD IAW CRJ200 AMM 27-54-00-710-801.

Part: FLAP — MALFUNCTIONED (WING) · airframe 34,801 hrs · 34,658 cycles

ON SHORT FINAL CREW RECEIVED A FLAPS FAIL CAUTION MSG. CREW THEN DECLARED AND EMERGENCY AND LANDED WITHOUT INCIDENT. ONCE AT THE GATE THEY WERE ABLE TO RESET THE SYSTEM, RUN THE FLAPS THROUGH 5 FULL CYCLES AND DEFER THE FLAP SYSTEM.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 34,730 hrs · 34,585 cycles

DURING CLIMB THE CREW RECEIVED A FLAPS FAIL 20-8 FAIL MESSAGE. THE AIRCRAFT WAS AROUND 160 KNOTS. THE AIRCRAFT DIVERTED AND DECLARED AN EMERGENCY AND LANDEDWITHOUT FURTHUR INCIDENT. THE AIRCRAFT FERRIED TO A MAINTENANCE BASE AND REPLACED THE FLAP ECTRONIC CONTROL UNIT.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 34,712 hrs · 34,570 cycles

AFTER DEPARTURE AT 17000 FEET THE CREW RECEIVED A FLAPS FAIL MESSAGE AT ZERO. THE CREW RETURNED TO FIELD AND DECLARED AN EMERGENCY AND LANDED ON THE LONGEST RUNWAY. MAINTENANCE REMOVED AND REPLACED LEFT HAND BRAKE POSITION SENSING UNIT AND WAS RETURNED TO REVENUE SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,683 hrs · 34,543 cycles

ON CLIMBOUT THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE AT FLIGHT LEVEL 190. THE FLAPS CURRENT POSITION WAS ZERO SETTING. ONCE ON THE GROUND THE CREW PERFORMED FIVE FULL EXTENSION/RETRACTION OF THE FLAPS WITH NO FAILURES. THE CAT II SYSTEM WAS DEFERRED.

Part: ECU — FAILED (TE FLAP) · airframe 34,623 hrs · 34,490 cycles

THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE ON CLIMB OUT. THE CREW RAN THE QUICK REFERENCE HANDBOOK AND RETURNED TO FIELD. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY AND TAXIED TO THE GATE. MX REPLACED THE FECU. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 34,390 hrs · 34,244 cycles

DURING CRUISE FLIGHT AT FLIGHT LEVEL 260, THE CREW RECEIVED A RIGHT HAND WINDSHIELD HEAT CAUTION MESSAGE. THE CREW CYCLED THE WINDHIELD TOGGLE SWITCH AND WHEN SELECTED BACK ON, THE FIRST OFFICER WINDSHIELD SHATTERED. THE CREW DECLARED AN EMERGECNY AND DIVERTED. REMOVED & REPLACED RH WINDSHIELD. OPS AND LEAK CHECKS GOOD. REMOVED & REPLACED THE RT WINDSHIELD HEAT CONTROLLER. OPS CHECKS GOOD

Part: ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 34,230 hrs · 34,080 cycles

RIGHT WING TO FUSE ATTACH ANGLE WAS CRACKED AT BS 439. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, 51-42-15, AND 51-45-00.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 34,230 hrs · 34,080 cycles

FLOORBEAM STRAP AT BS 559, LBL 38 WAS CORRODED. LOCATED, AND DRILLED A NEW FLOORBEAM STRAP IAW SRM 51-40-11.

Part: FLOOR SUPPORT — CRACKED · airframe 34,230 hrs · 34,080 cycles

WHILE PERFORMING EA 45-2018-109 P1, STEP 6, AND NDTM PART 1, 51-20-06, FOUND MULTIPLE CRACK INDICATIONS APPROXIMATELY .15 INCH LONG FROM CUTOUT HOLE. REPAIRED THE LT PRESSURE FLOOR SILL IAW EA 45-2018-109.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 34,230 hrs · 34,080 cycles

PASSENGER DOOR INTERCOSTAL INSIDE DOOR BELOW THE LOCK, LATCH BOX WAS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: ANGLE — CRACKED (LT WING) · airframe 34,230 hrs · 34,080 cycles

LH WING, WING TO FUSE ATTACHMENT ANGLE IS CRACKED AT FS 449.85. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE LH WING TO FUSELAGE ANGLE IAW SRM 51-42-06, 51-42-15, AND 51-45-00.

Part: WINDOW — SCRATCHED (EMERGENCY EXIT) · airframe 34,230 hrs · 34,080 cycles

LEFT EMERGENCY EXIT WINDOW SEVERLY SCRATCHED AND HAS TWO POSSIBLE CRACKS. INSTALLED A NEW OUTER PLY & SEAL WINDOW ASSY IAW CMM 56-20-00.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,230 hrs · 34,080 cycles

BS 621 PRESSURE BULKHEAD WEB WAS CRACKED. REPAIRED THE PRESSURE BULKHEAD IAW REO 601R-53-61-1240, REV D.

Part: ANGLE — CORRODED (BS 349 FLOORBEAM) · corrosion level 2 · airframe 34,230 hrs · 34,080 cycles

SERVICE DOOR FLOORBEAM ANGLE BS 349 WAS CORRODED. LOCATED, DRILLED, AND INSTALLED A NEW FLOORBEAM ANGLE IAW SRM 51-42-06, 51-42-21, AND 51-40-11.

Part: MOUNT — CORRODED (BS 310) · corrosion level 2 · airframe 34,230 hrs · 34,080 cycles

FLOOR SUPPORT STRUCTURE BS 310 WAS CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11, AND 51-42-13.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 34,230 hrs · 34,080 cycles

HORIZONTAL STABILIZER ANTI-ROTATION FITTING WAS CRACKED. INSTALLED A NEW ANTI-ROTATION FITTING IAW SB 601R-55-007.

Part: SEAT TRACK — GOUGED (BS 559) · airframe 34,230 hrs · 34,080 cycles

LEFT SEAT TRACK, BS 559+56, LBL 9, WAS HEAVILY GOUGED. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-1-400-802.

Part: UNKNOWN — ODOR · airframe 32,656 hrs · 32,667 cycles

BURNING SMELL COMING FROM LT PACK ON TAXI OUT. A/C RETURNED TO GATE FOR MAINTENANCE INSPECTION. CLT MX RAN PACK FOR 30 MINUTES. INSPECTED PACK AND FOUND NO DEFECTS.

Part: RELEASE PIN — BROKEN (PASSENGER DOOR) · airframe 31,483 hrs · 31,527 cycles

PASSENGER DOOR HANDLE RELEASE PIN BROKEN. REMOVED AND REPLACED RELEASE PIN.

Part: DOOR SEAL — DAMAGED (SERVICE DOOR) · airframe 30,244 hrs · 30,334 cycles

SERVICE DOOR SQUEALED AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FERRIED ACFT TO NEAREST MAINTENANCE FACILITY. MAINTENANCE INSPECTED AND REPAIRED THE SERVICE DOOR SEAL. OPS CHECK GOOD. CLEARED FERRY AND CW O/S INSPECTION.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,986 hrs · 30,071 cycles

BS 559+91 TO 559+96 , 559+110 TO 569, 583, 600 AND 612 TO 617 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT LBL 9. MAINTENANCE R & R CARGO COMPARTMENT RAIL FITTINGS AT LBL 9 IAW AMM 20-21-00-910-801.

Part: CARGO TRACK — CORRODED (BS 559-569) · corrosion level 2 · airframe 29,986 hrs · 30,071 cycles

BS 559+91 TO 559+96 AND BS 559+110 TO 569 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT RBL 9. MAINTENANCE R & R CARGO COMPARTMENT RAIL FITTINGS AT RBL 9 IAW AMM 20-21-00-910-801.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,986 hrs · 30,071 cycles

BS 559+80 TO 559+96 , 559+104 , 559+110 AND 567 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT LBL 27. MAINTENANCE R & R CARGO COMPARTMENT RAIL FITTINGS AT LBL 27 IAW AMM 20-21-00-910-801.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,986 hrs · 30,071 cycles

BS 559+91 TO FS 559+96 , 559+110 TO 569, 583, 600 AND 612 TO 617 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT LBL 9. MAINTENANCE. R & R CARGO COMPARTMENT RAIL FITTINGS AT LBL 9 IAW AMM 20-21-00-910-801.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 29,986 hrs · 30,071 cycles

F.S. 559.00+80 TO F.S. 559.00+96 CARGO COMPARTMENT CARGO TRACK IS CORRODED AT RBL 27. MAINTENANCE R & R CARGO COMPARTMENT RAIL FITTING AT RBL 27 IAW AMM 20-21-00-910-801.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 29,726 hrs · 29,802 cycles

EXIT LIGHT COVER MISSING ON SIDE PANEL NEXT TO MAIN CABIN DOOR. MAINTENANCE INSPECTED, INSTALLED AN EMERGENCY EXIT FLOOD LIGHT COVER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,600 hrs · 29,677 cycles

CREW REPORTED 5" OF EMERGENCY LIGHT INOPERATIVE NEAR ROW 12. MAINTENANCE TROUBLESHOT, R & R FLOOR EMERGENCY LIGHT, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE AGB) · airframe 28,188 hrs · 28,248 cycles

CREW REPORTED LT ENGINE OIL PRESSURE WARNING MESSAGE AND OIL PRESSURE OSCILLATION. CREW RAN QRH, INTENTIONALLY SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND DIVERTED. MAINTENANCE INSPECTED, R & R LT ENGINE AGB CARBON SEAL FOR ENGINE DRIVEN PUMP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE AGB) · airframe 28,188 hrs · 28,248 cycles

CREW REPORTED LT ENGINE OIL PRESSURE WARNING MESSAGE AND OIL PRESSURE OSCILLATION. CREW RAN QRH, INTENTIONALLY SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND DIVERTED. MAINTENANCE INSPECTED, R & R LT ENGINE ACCESSORY GEARBOX CARBON SEAL FOR INTEGRATED DRIVE GENERATOR, IDG AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE AGB) · airframe 28,188 hrs · 28,248 cycles

CREW REPORTED LT ENGINE OIL PRESSURE WARNING MESSAGE AND OIL PRESSURE OSCILLATION. CREW RAN QRH, INTENTIONALLY SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND DIVERTED. MAINTENANCE INSPECTED, R & R LT ENGINE ACCESSORY GEARBOX, AGB, CARBON SEAL FOR AIR TURBINE STARTER,ATS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — DIRTY (MLG) · airframe 26,956 hrs · 27,027 cycles

CREW REPORTED GEAR DISAGREE RED WARNING ON SELECTION OF GEAR DOWN. CREW LANDED WITHOUT INCIDENT AFTER GEAR WAS VERIFIED DOWN. MAINTENANCE PERFORMED OPS TEST OF MLG EXTENSION AND RETRACTION. OPS CHECK WAS GOOD AND NO CODES IN HISTORY. MAINTENANCE CLEANED EXCESSIVE SAND AND GREASE FOUND ON MLG SENSORS AND PERFORMED OPS CHECK OF GEAR EXTENSION AND RETRACTION. ACFT RELEASED FOR SERVICE.

Part: OXYGEN SYSTEM — LOW PRESSURE · airframe 25,949 hrs · 26,027 cycles

CREW REPORTED OXYGEN LOW PRESSURE IN FLIGHT. OXYGEN AT 1,330 PSI CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYS FOR LEAKS. NO LEAKS NOTED. MAINTENANCE SERVICED OXYGEN AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (RT NACELLE) · airframe 25,814 hrs · 25,887 cycles

DURING SCHEDULED MAINTENANCE, THE RT ENGINE TRANSLATING COWL HAD TWO DENTS. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 379) · airframe 25,814 hrs · 25,887 cycles

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

Part: LENS — DAMAGED (EXTERIOR LIGHT) · airframe 25,299 hrs · 25,357 cycles

CREW REPORTED LIGHTNING STRIKE ON NOSE OF ACFT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R UPPER REAR NAVIGATION LENS, GASKET AND HARDWARE DUE TO VERTICAL STABILIZER UPPER NAVIGATION LIGHT ASSEMBLY BURNED. LT WINGLET UPPER AND MIDDLE STATIC DISCHARGE WICKS AND LT HORIZONTAL STABILIZER TIP OTBD STATIC WICK R & R DUE TO FAILING RESISTANCE CHECK. MAINTENANCE PERFORMED CHECKS AND ACFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM.

Part: UNKNOWN — MALFUNCTIONED (FLT CONTROLS) · airframe 24,979 hrs · 25,075 cycles

CREW REPORTED UNCOMMANDED YAW AFTER TAKEOFF. RUDDER TRIM REQUIRED TO MAINTAIN CONTROL. RUDDER TRIM WAS TURNING TOWARDS FULL LEFT. CREW DECLARED EMERGENCY, DIVERTED AND LANDED SAFELY. PERFORMED OPS TEST OF RUDDER CONTROL SYS IAW AMM 27.21.00.710.801. OPS CHECK GOOD. PERFORMED OPS CHECK OF RUDDER TRIM IAW 27.21.00.710.802. OPS CHECK GOOD.

Part: DIODE — OPEN (THRUST REVERSER) · airframe 24,614 hrs · 24,736 cycles

CREW REPORTED LEFT THRUST REVERSER UNLOCK MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, FOUND A DIODE WITH AN OPEN CIRCUIT, R & R DIODE TERMINAL BLOCK AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: TERMINAL BLOCK — FAILED (THRUST REVERSER) · airframe 24,534 hrs · 24,649 cycles

CREW REPORTED LT THRUST REVERSER UNLOCKED MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, & FOUND A DIODE WITH AN OPEN CIRCUIT, REMOVED AND REPLACED DIODE TERMINAL BLOCK AND PERFORMED CHECKS MM. AIRCRAFT RELEASED FOR SERVICE.

Part: PISTON — LACK OF LUBE (THRUST REVERSER) · airframe 24,330 hrs · 24,451 cycles

CREW REPORTED A LEFT THRUST REVERSER UNLOCK CAS MESSAGE IN FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, LUBRICATED THE PDU LOCK PISTON AND OPS CHECKED THE LT THRUST REVERSER USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — MALFUNCTIONED (ANTI ICE DUCT) · airframe 24,115 hrs · 24,261 cycles

CREW REPORTED RED ANTI-ICE DUCT WARNING MESSAGE ON TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT, FOUND LT FUSELAGE SENSING ELEMENT A41WK TO HAVE HIGH RESISTANCE, R & R SENSING ELEMENT A41WK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSING ELEMENT — MALFUNCTIONED (ANTI ICE DUCT) · airframe 24,115 hrs · 24,261 cycles

CREW REPORTED RED ANTI-ICE DUCT MESSAGE DURING CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ANTI-ICE SENSING ELEMENTS, FOUND LOOP A15WK BROKEN UNDER CABIN FLOORBOARDS, R & R SENSING ELEMENT A15WK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 23,581 hrs · 23,764 cycles

CREW REPORTED RT SIDE BOTTOM WALL EXIT SIGN AND FLOOR EMERGENCY LIGHT BETWEEN ROW 5 AND ROW 8 WILL NOT LIGHT. MX INSPECTED, R & R POSITION NR 3 POWER SUPPLY INVERTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: TRACK — LACK OF LUBE (THRUST REVERSER) · airframe 23,269 hrs · 23,483 cycles

CREW REPORTED LEFT THRUST REVERSER UNLOCKED AMBER CAS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED, LUBED THRUST REVERSER TRACKS AND PDU. PLUNGER AND PERFORMED CHECKED IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SOLENOID VALVE — FAULTY (APU) · airframe 22,807 hrs · 23,067 cycles

IT WAS REPORTED AFTER APU SHUTDOWN FLAMES WERE COMING FROM APU EXHAUST AREA. WHEN POWER WAS SWITCHED OFF FLAMES EXTINGUISHED. MAINTENANCE TROUBLESHOT, INSPECTED, REMOVED AND REPLACED THE APU FUEL SELONOID VALVE AFTER INSPECTING FOR FIRE DAMAGE. NO DAMAGE NOTED. USING THE AIRCRAFT MANUALS. CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: DOOR SEAL — DEFECTIVE (SERVICE DOOR) · airframe 22,067 hrs · 22,402 cycles

CREW REPORTED CLIMBING THROUGH 17,000 FT A POP AND HISSING AROUND SERVICE DOOR. CREW RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE SERVICE DOOR SEAL USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 22,066 hrs · 22,401 cycles

DURING SCHEDULED MAINTENANCE BETWEEN FS 589 AND FS 605 WAS FOUND DENTED, NICKS, AND GOUGES. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 22,066 hrs · 22,401 cycles

DURING SCHEDULED MAINTENANCE FS 409+128 POST AT LBL 18 HAD INDICATION OF CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 22,066 hrs · 22,401 cycles

DURING SCHEDULED MAINTENANCE FS 409+128 POST AT BL 0 HAD INDICATION OF CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OVERHEAT LOOP — DEFECTIVE (FUSELAGE) · airframe 21,119 hrs · 21,550 cycles

CREW REPORTED RIGHT FUSELAGE ANTI-ICE DUCT WARNING MESSAGE EN ROUTE. CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT LOOP (HEAT SENSING ELEMENT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 19,089 hrs · 19,646 cycles

CREW REPORTED AIRCRAFT BEGAN TO FILL WITH SMOKE AND A SMOKE TOILET CAS MESSAGE ON TAKEOFF ROLL ON DEPARTURE FROM CLT. CREW FOLLOWED QRH, RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED COALESCER BAGS ON LEFT AND RIGHT ACM WATER SEPARATORS, REMOVED AND REPLACED LAVATORY SMOKE DETECTOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. NO SMOKE OR SMOKE TOILET MESSAGE OCCURRED DURING MAINTENANCE CHECKS. AIRCRAFT RELEASED FOR SERVICE.

Part: LINE — DETACHED (APU) · airframe 19,089 hrs · 19,646 cycles

WHILE BOARDING AND AT THE GATE IN CLT, CREW REPORTED SMOKE AND FUMES IN CABIN. PASSENGERS DEPLANED THROUGH MAIN CABIN DOOR. CREW REPORTED APU SHUT DOWN AUTOMATICALLY AND NOTED OIL ON GROUND UNDER AFT EQUIPMENT BAY. MAINTENANCE INSPECTED AND FOUND APU OIL COOLER LINE NOT ATTACHED. MAINTENANCE REMOVED AND REPLACED APU AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 18,424 hrs · 18,999 cycles

UPON SELECTION OF GEAR UP ON TAKEOFF FROM OAJ, CREW REPORTED ANTI-SKID OUTBOARD CAS MESSAGE, FOLLOWED BY RED MASTER WARNING GEAR UNSAFE, WITH LEFT MAIN LANDING GEAR IN AN UNKNOWN POSITION. BOTH MESSAGES WENT AWAY WITHIN 20 SECONDS. CREW COMPLIED WITH QRH. GEAR WAS MANUALLY EXTENDED AND AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LANDING GEAR SYSTEM, REMOVED AND REPLACED MLG (MAIN LANDING GEAR) SELECTOR VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RELIEF VALVE — LEAKING (HYDRAULIC SYS) · airframe 18,355 hrs · 18,935 cycles

CREW REPORTED GEAR DISAGREE AND RED INDICATION FOR BOTH MAIN GEAR UPON SELECTION OF GEAR DOWN ON APPROACH INTO BNA. CREW RAN QRH AND RECEIVED THREE (3) GREEN INDICATIONS AND HYD 3 LOW PRESS CAUTION. AIRCRAFT LANDED IN BNA WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT HYDRAULIC SYSTEM NUMBER THREE (3), REMOVED AND REPLACED PRESSURE RELIEF VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RELIEF VALVE — STICKS (HYDRAULIC SYS) · airframe 18,349 hrs · 18,931 cycles

CREW REPORTED ANTI-SKID INBOARD AMBER MESSAGE UPON WOW (WEIGHT-OFF-WHEELS) ON DEPARTURE FROM DAY. AFTER GEAR UP SELECTION, MESSAGE EXTINGUISHED, FOLLOWED BY GEAR DISAGREE WARNING. LEFT MAIN GEAR WAS SLOW IN COMING UP. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED HYDRAULIC SYSTEM NUMBER THREE (3) BLEED VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,533 hrs · 18,146 cycles

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

Part: HINGE PIN — CHAFED (TE FLAP) · airframe 17,533 hrs · 18,146 cycles

DURING SCHEDULED MAINTENANCE IT WAS FOUND THE LEFT FLAP STUB FAIRING HINGE PIN CHAFED AND CAUSED A HOLE ON ADJACENT STRUCTURE. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,533 hrs · 18,146 cycles

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

Part: FILTER ELEMENT — POPPED (APU) · airframe 16,983 hrs · 17,604 cycles

CREW REPORTED AN APU OIL TEMP CAUTION IN FLIGHT EN ROUTE FROM CLT TO STL. CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE DELTA-P POPPED ON THE APU OIL FILTER. MAINTENANCE REMOVED AND REPLACED THE APU OIL FILTER ELEMENT, SERVICED THE APU OIL AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BALLAST — DEFECTIVE (CAABIN) · airframe 15,025 hrs · 15,654 cycles

AT CLT, CREW REPORTED AN ELECTRICAL SMELL COMING FROM THE CABIN AROUND ROWS EIGHT (8) AND NINE (9). MAINTENANCE INSPECTED, REMOVED AND REPLACED TWO (2) LIGHT BALLASTS AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 14,759 hrs · 15,354 cycles

CREW REPORTED MACH TRIM AND STAB TRIM CAUTION MESSAGES IN FLIGHT EN ROUTE FROM CLT TO PGV. AIRCRAFT DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, CLEANED THE PILOT AND COPILOT TRIM DISCONNECT SWITCHES AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,722 hrs · 15,316 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FS 559 LT CAP ANGLE AND RT BULKHEAD WEB. REPAIRS WERE MADE USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAP) · airframe 12,854 hrs · 13,305 cycles

CREW REPORTED FLAPS FAILED AT 20 DEGREES. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU AND CHECKED FLAPS SYSTEM. NO PROBLEMS WERE FOUND. TROUBLESHOOTING AND CHECKS WERE DONE USING THE AIRCRAFT MAINTENANCE MANUAL AND FIM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,216 hrs · 12,631 cycles

AFTER DEPARTURE FROM DAY, THE CREW REPORTED A LEFT WINDSHIELD CAS MESSAGE RIGHT BEFORE THE CAPTAIN’S FRONT WINDSHIELD SHATTERED AT FL250. THE AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT WINDSHIELD AND THE LEFT WINDSHIELD CONTROLLER IAW THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL AND LEAKS CHECKS WERE PERFORMED. NO FURTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: IDG — LOW (NR 2) · airframe 11,451 hrs · 11,812 cycles

CREW REPORTED ON TAKEOFF ROLL FROM CLT, IDG 2 CAUTION MSG CAME ON, ABORTED TAKEOFF. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. A RESET OF GEN 2 WAS ACCOMPLISHED & ALL MSG'S WERE CLEARED. MAINTENANCE SERVICED THE NR 2 IDG. NO DEFECTS NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — FAILED (NLG) · airframe 8,104 hrs · 8,201 cycles

CREW REPORTED ON TAKEOFF ROLL THE RIGHT HAND NOSE TIRE WENT FLAT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 32-42-01. MAINTENANCE FOUND DAMAGE TO THE NOSE GEAR DOOR AND COMPLIED WITH TEMP REPAIR PER REO 601R-52-81-132. MAINTENANCE ALSO FOUND NUMEROUS DENTS ON FUSELAGE AND COMPLIED WITH TEMP REPAIR PER REO 601R-53-11-1192. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LANDING GEAR — UNDAMAGED · airframe 5,560 hrs · 5,529 cycles

CREW REPORTED BIRD STRIKE TO LEFT MAIN LANDING GEAR. BIRD STRIKE INSPECTION WAS PERFORMED AND AREA WAS CLEANED. NO DAMAGE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 4,074 hrs · 4,070 cycles

THE STAB TRIM FAILED IN FLIGHT. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED & REPLACED THE HORIZONTAL STAB TRIM CONTROL UNIT IAW CRJ200 AMM 24-41-01-000(400)-801. THE STAB TRIM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG STEERING) · airframe 3,829 hrs · 3,805 cycles

THE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER TAKEOFF FROM DCA. THE CREW FOLLOWED THE QRH, DIVERTED TO BTV, AND MADE AN UNEVENTFUL LANDING. THE STEERING SYSTEM OPERATED NORMAL ON LANDING. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE NOSE WHEEL STEERING SYSTEM IAW CRJ200 AMM 32-51-00-710-802. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 2,327 hrs · 2,293 cycles

INBOUND TO DCA THE HYD 2 LOW PRESS MESSAGE ILLUMINATED. WHILE FOLLOWING THE QRH THE MESSAGE WENT OUT AND THE HYD EDP 2A MESSAGE APPEARED. THE CREW OF FLIGHT 2344 CONTINUED TO DESTINATION AND MADE AN UNEVENTFUL LANDING AT DCA. PSA MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ 200 AMM 29-11-01-400-801. OPERATIONAL TESTS AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 2,032 hrs · 1,999 cycles

ON SHORT FINAL INTO PHL THE FLAPS STUCK AT 30 DEGREES WHEN THE CREW OF FLIGHT 2304 SELECTED FLAPS 45. THE FLIGHT LANDED UNEVENTFULLY. PSA MAINTENANCE RESET CIRCUIT BREAKERS AND CYCLED THE FLAPS IAW BOMBARDIER SERVICE LETTER RJ-SL-00-001. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 1,319 hrs · 1,315 cycles

DURING CRUISE THE CREW REPORTED A CARGO DOOR CAS MESSAGE WITH NO CHANGE IN CABIN PRESSURE. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW 52-70-04 CODE C

Part: ODOR — DETECTED (CABIN) · airframe 1,224 hrs · 1,213 cycles

THE CREW REPORTED A BURNING PLASTIC ODOR TOWARDS THE AFT CARGO BAY. MAINTENANCE RAN THE AIRCRAFT, INSPECTED, AND RAN THE ENVIRONMENTAL CONTROL SYSTEM IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 36-00-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.