N226JS

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 36,706 hrs · 36,425 cycles

DURING ROUTINE OVERNIGHT MAINTENANCE, MAINTENANCE NOTED THAT THE AFT DRAG ANGLE HAS A CRACK MEASURING 0.50Ï¿½ LONG WHICH IS LOCATED IN THE RADIUS OF THE DRAG ANGLE. THE CRACK IS LOCATED NEXT TO THE PULLEY SUPPORT BRACKET. THE AFT DRAG ANGLE (P/N 600-31907) IS FABRICATED FROM 60-10229 EXTRUDED 2024-T3511 ALUMINUM. APPLIED EA69-2019-273. 1000 FH TILL PERMANENT REPAIR IS DUE. SUPPLEMENTAL INFORMATION: REMOVED, FABRICATED, AND INSTALLED PAX DOOR AFT DRAG ANGLE. THIS IS A PERMANENT REPAIR AND THIS CLEARS TEMP REPAIR REO 601R-52-11-513

Part: DOOR SEAL — FAILED (SERVICE DOOR) · airframe 36,654 hrs · 36,367 cycles

FLT 5511 TOOK OFF FROM DCA-ALB AT APPROX 2000 FEET AT A SPEED OF APPROX 200 KTS CREW HEARD A LOUD POP AND THEN WIND NOISE FROM THE GALLEY SERVICE DOOR. THE AIRCRAFT DID NOT PRESSURIZE THE CAPT THEN DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE PAX WHERE INFORMED OF THE SITUATION BUT DID NOT BRACE. MX REPLACED THE SERVICE DOOR SEAL. LEAK AND PRESSURE CHECK GOOD.

Part: SHUTOFF VALVE — LEAKING (APU FUEL) · airframe 36,506 hrs · 36,228 cycles

STRONG FUEL SMELL IN WHOLE ACFT. MX FOUND APU SOLENOID SHUTOFF VALVE LEAKING. REMOVED AND REPLACED APU FUEL SHUTOFF SOLEINOID VALVE IAW AMM PERFORMED LEAK CHECK OF APU IAW AMM NO LEAKS NOTED, NO FUEL SCENT IN CABIN. REPLACED PRSOV. OPS CHECK GOOD.

Part: BPSU — FAILED (ZONE 100) · airframe 36,167 hrs · 35,898 cycles

REPEAT FLAPS FAIL CAUT MSG WHEN FLAP SELECTED TO 20 FLAPS FAILED AT ZERO. FERRY TO DAY. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE ISSUE AT THIS TIME.

Part: BPSU — FAILED (TE FLAP) · airframe 36,167 hrs · 35,898 cycles

REPEAT FLAPS FAIL CAUTION MSG WHEN FLAP SELECTED TO 20 FLAPS FAILED AT ZERO. MX REPLACED LH BPSU. OPS CHECK GOOD.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 34,995 hrs · 34,845 cycles

RH WING AT WS53.60 BATT RIB IS CRACKED. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED RH BATT RIB AND DOUBLER IAW SRM 51-24-21, 51-40-11, 51-42-06, 51-25-16, AND BOMBARDIER DWG NO 601R10203.

Part: BULKHEAD WEB — CORRODED (BS 621) · airframe 34,995 hrs · 34,845 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18 WL 110 2 INCHES LONG 100% FSH FAILED NDT. CORRECTIVE ACTION: REPAIRED IAW BOMBARDEIR REO 601R-53-61-1285 AND 601R-53-61-6801.

Part: BULKHEAD WEB — CORRODED (BS 621) · airframe 34,995 hrs · 34,845 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 WL 130 2 INCHES LONG 100% FSH FAILED NDT. CORRECTIVE ACTION: REPAIRED IAW BOMBARDEIR REO 601R-53-61-6792 REV. -- DATED 12/02/2018

Part: STIFFENER — CORRODED (BS 409) · airframe 34,995 hrs · 34,845 cycles

FOUND INDICATION BL 0 L/H FLANGE RADIUS APPROX 70%FSH .250 LONG FAILS NDT LOCATION F.S. 409+128 VERTICAL POST. CORRECTIVE ACTION: REMOVED AND REPLACED WITH NEW SERVICEABLE PARTS IAW CRJ200 SRM 51-42-06 AND 51-42-22. PN: 601R32208-132, 601R32208-131, 601R32208-229, AND 601R32208-230.

Part: DOUBLER — CORRODED (BS 317) · airframe 34,995 hrs · 34,845 cycles

DISCREPANCY: BOLT HOLE DOUBLERS AT LBL20 FS288, LBL20 FS308, AND RBL5 FS317 ARE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED DOUBLER AT RBL5 FS317 IAW CRJ-200 SRM 51-42-06 AND 51-42-13. REMOVED CORROSION ON DOUBLERS AT LBL20 FS288, AND LBL20 FS308 IAW CRJ-200SRM 51-21-06, 53-00-00, AND 53-21-16.

Part: BULKHEAD WEB — CORRODED (BS 621) · airframe 34,995 hrs · 34,845 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 00 WL 113 3 INCHES LONG 50% FSH FAILED NDT. CORRECTIVE ACTION: REPAIRED IAW BOMBARDEIR REO 601R-53-61-1285.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 34,995 hrs · 34,845 cycles

DISCREPANCY: CABIN SEAT TRACKS CORRODED AT THE FOLLOWING LOCATIONS: LBL9 & RBL9 F.S. 364-399 AND 399-409+128, L/H SIDE TRACK F.S. 546-559+80, RH SIDE TRACK F.S. 364-409+16, RH SIDE TRACK F.S. 409+112-449, RH SIDE TRACK F.S. 500-546, AND RH SIDE TRACK F.S. 546-559+80. CORRECTIVE ACTION: REMOVED AND REPLACED AFFECTED SEAT TRACKS IAW BOMBARDEIR REO 601R-53-00-055, REO 601R-53-00-485, AND CRJ200 AMM 53-01-11-400-802.

Part: TRUNNION — CRACKED (RT MLG) · airframe 34,995 hrs · 34,845 cycles

FOUND INDICATION R/H TRUNNION 2ND HOLE FROM AFT SIDE OF STRAP FWD SIDE OF HOLE 80% FSH APPROX .5 UP TRUNNION FAILS NDT, 4TH HOLE FROM AFT OF STRAP AFT SIDE OF HOLE 80% FSH APPROX .5 UP TRUNNION FAILS NDT, 8TH HOLE FROM AFT OF STRAP AFT SIDE OF HOLE 80% FSH APPROX .75 UP TRUNNION FAILS NDT. C/A: REMOVED AND REPLACED RH TRUNNION IAW BBD RIL # 3690.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,994 hrs · 34,844 cycles

DURING CLIMB PHASE, AROUND 10000', CREW RECEIVED A DISPLAY COOL FAN FAIL MESSAGE. CREW FOLLOWED THE QRH AND TRIED FANS. CREW DECLARED AN EMERGENCY AND RETURNED TO PHL. AROUND 600' THE MESSAGE WENT AWAY. CREW CANCELED THE EMERGENCY AND CONTINUED TO PHL WITHOUT FURTHER ISSUE. FERRY TO CKB FOR PRESSURIZATION CHECK AND DISPLAY COOL PERM REPAIR.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 34,993 hrs · 34,843 cycles

DURING CLIMB AND INTO CRUISE PHASE OF FLIGHT A CRACK BEGAN TO SPREAD ON THE CAPTAIN'S SIDE WINDSHIELD. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL. THE FLIGHT HELD FOR APPROXIMATELY 45 MINUTES TO BURN OFF FUEL TO GET UNDER LANDING WEIGHT. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER ISSUE. R&R WINDSHIELD. LEAK CHECKS GOOD

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,085 hrs · 33,955 cycles

CREW REPORTED A BURNING SMELL IN THE COCKPIT AND RETURNED TO THE GATE. FOUND THE SMELL COMING FROM THE RIGHT HAND AIR-CONDITIONING PACK. THE LEFT HAND AIR CONDITIONING PACK WAS CURRENTLY ON DEFERRAL. MAINTENANCE DEFERRED THE RIGHT HAND AIR CONDITIONING PACK. NOW THE AIRCRAFT HAS BOTH AIR CONDITIONING PACKS ON DEFERRAL.

Part: RESERVOIR — FAULTY (HYDRAULIC SYS) · airframe 33,639 hrs · 33,538 cycles

CREW HAD A GEAR DISAGREE MESSAGE AND A HYDRO SYSTEM 3 HIGH TEMP MESSAGE GOING INTO CLT. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REPLACED NR 3 RESERVOIR. OPS AND LEAK CHECKS GOOD, GEARS SWINGS GOOD.

Part: PUMP — FAILED (OIL SCAVANGE) · airframe 32,628 hrs · 32,627 cycles

CREW REPORTED RECEIVING A LT ENGINE OIL PRESSURE MESSAGE, FOLLOWED BY AN OIL PRESSURE DROPPING AND ITT RISING TO 908C, DURING DESCENT. RAN THE QRH WHICH DIRECTED THEM TO SHUTDOWN THE ENGINE. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LUBE AND SCAVENGE PUMP. OPS AND LEAK CHECKED GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 31,965 hrs · 32,034 cycles

CREW DECLARED EMERGENCY DUE TO GEAR DISAGREE MESSAGE AND LOSS OF HYDRAULIC SYSTEM 3 FLUID WHEN GEAR WAS SELECTED DOWN. THE CREW HAD TO USE GEAR MANUAL DEPLOY. MAINTENANCE REPLACED HOSE ON THE NUMBER 3 HYDRAULIC PUMP.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 31,474 hrs · 31,510 cycles

RIGHT ELEVATOR UPPER SKIN CRACKED AT FORWARD EDGE. PERFORMED A MAJOR REPAIR.

Part: STRINGER — CRACKED (BS 310) · airframe 31,474 hrs · 31,510 cycles

STRINGER 9R CRACKED FORWARD OF BS 310. PERFORMED A MAJOR REPAIR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,404 hrs · 30,508 cycles

EXIT PATH FLOOR LIGHTING AND RT SIDE OVERWING EXIT LIGHT INOPERABLE. MAINTENANCE INSPECTED, R & R FORWARD EMERGENCY LIGHTING BATTERY PACK AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: REGULATOR VALVE — FAILED (AIR CONDITIONING) · airframe 28,561 hrs · 28,644 cycles

CREW REPORTED RT PACK SHUTOFF WHEN BLEEDS TRANSFERRED FROM APU TO ENGINE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT AIR CONDITIONING PRESSURE REGULATING AND SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 26,763 hrs · 26,838 cycles

CREW REPORTED FLAPS FAIL MESSAGE AT ZERO DEGREES ON APPROACH. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FAULT ISOLATION MANUAL, R & R NR 1 LT INBD FLAP ACTUATOR AND PERFORMED CHECKS IAW AMM. AFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED · airframe 25,025 hrs · 25,117 cycles

CREW REPORTED LIGHTNING STRIKE TO NOSE DURING CLIMB THROUGH 14,000 FT WITH GEAR AND FLAPS RETRACTED. LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R THE LT HORIZONTAL STABILIZER TIP FAIRING, STATIC WICK AND BASE MISSING AND BURNED, 3 SCREWS FROM LT HORIZONTAL STABILIZER TIP FAIRING, BURNED ON UPPER SURFACE, LOWER VHF ANTENNA, LIGHTNING STRIKE DAMAGE AND STATIC WICK ON RT HORIZONTAL STABILIZER, NO CONTINUITY. RESECURED VERTICAL STABILIZER TOP STATIC WICK, LOOSE. MAINTENANCE PERFORMED CHECKS AND ACFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM.

Part: RESERVOIR — WARNING LIGHT (HYD SYS) · airframe 24,862 hrs · 24,962 cycles

CREW REPORTED HYD QTY INDICATED 25 PERCENT AT 26 DEGREES ON HYD SYS NR 1. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R HYD SYS NR 1 RESERVOIR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: IDG — FAILED (NR 2 GENERATOR) · airframe 24,022 hrs · 24,181 cycles

CREW REPORTED NR 2 GENERATOR OFF MESSAGE WITH ACCOMPANYING INTEGRATED DRIVE, NR 2 GENERATOR DISCONNECT MESSAGE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED & R & R RT IDG AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: TURBINE — DAMAGED (RT ENGINE) · airframe 22,751 hrs · 23,025 cycles

THE CREW REPORTED A VIBRATION IN THE RIGHT ENGINE. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LOW PRESSURE TURBINE USING THE AIRCRAFT MANUALS. CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 22,618 hrs · 22,899 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE CLIMBED TO 116 AND TURNED AMBER ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED, SERVICED ENGINE OILS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS NOTED AND OIL PRESSURE FOUND TO BE WITHIN SERVICEABLE LIMITS. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,434 hrs · 22,742 cycles

CREW REPORTED CABIN WOULD NOT PRESSURIZE ON CLIMBOUT. DELTA-P WAS 0.1 TO 0.2. ATTEMPTED MANUAL PRESSURIZATION PROCEDURE WITHOUT SUCCESS. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. NO EXCESSIVE NOISE OR SQUEALING FROM ANY DOORS WAS REPORTED BY CREW. MAINTENANCE CHECKED MDC (MAINTENANCE DIAGNOSTIC COMPUTER). NO FAULTS LOGGED. MAINTENANCE PERFORMED FUNCTIONAL TEST OF CPC (CABIN PRESSURE CONTROLLER) AND PERFORMED MANUAL PRESSURIZATION TO DELTA-P 4.0 PSI USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECKS GOOD AND NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: TIRE — FLAT (RT MLG) · airframe 22,109 hrs · 22,460 cycles

CREW REPORTED EXCESSIVE VIBRATION ON TAKEOFF. CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHT INBOARD MAIN LANDING GEAR TIRE FLAT AND DAMAGE ON LOWER SKIN OF RIGHT INBOARD FLAP. MAINTENANCE REMOVED AND REPLACED RIGHT INBOARD AND OUTBOARD MAIN LANDING GEAR TIRE ASSEMBLIES, REMOVED AND REPLACED RIGHT INBOARD FLAP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (LT HORIZ STAB) · airframe 21,852 hrs · 22,236 cycles

CREW REPORTED LIGHTNING STRIKE WHILE IN DESCENT AT 11,000 FEET. CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO LEFT HORIZONTAL STABILIZER. COMPLIED WITH VISUAL ENROUTE VISUAL INSPECTION, LIGHTING STRIKE IAW AMM 05.51.25.210.801.

Part: WATER SEPARATOR — CONTAMINATED (AC BAY) · airframe 21,290 hrs · 21,741 cycles

CREW REPORTED STRONG SMELL OF FUEL ON DESCENT AFTER SWITCHING PACK BLEED AIR TO APU. MAINTENANCE INSPECTED AND FOUND WATER SEPARATOR COALESCER CONTAMINATED. MAINTENANCE CLEANED COALESCER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PDU — FAILED (THRUST REVERSER) · airframe 20,872 hrs · 21,377 cycles

CREW REPORTED LEFT REVERSER UNLOCK MESSAGE AT ALTITUDE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED LEFT THRUST REVERSER PER MEL. AIRCRAFT RELEASED FOR SERVICE. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED LEFT THRUST REVERSER POWER DRIVE UNIT (PDU), PERFORMED CHECKS AND CLEARED DEFERRAL. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 20,201 hrs · 20,773 cycles

DURING INITIAL CLIMB AT 600 FEET, CREW REPORTED COMPRESSOR STALL AND POWER SURGE IN LEFT ENGINE. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND DETERMINED LEFT ENGINE NEEDED TO BE REMOVED AND REPLACED. PERFORMED VISUAL INSPECTION OF LT ENGINE FOR OBVIOUS DEFECTS. NONE FOUND. ENGINE RAN NORMALLY ON GROUND TESTS.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 18,987 hrs · 19,576 cycles

CREW REPORTED SMOKE CARGO WARNING MESSAGE IN FLIGHT. DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH VISUAL INSPECTION OF CARGO COMPARTMENT AND FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND BOTH CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLES AND PERFORMED CHECKS IAW MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: THERMOCOUPLE — FAULTY (APU) · airframe 18,552 hrs · 19,149 cycles

CREW REPORTED APU OVERTEMP WHILE ON APPROACH TO TYS. CREW LANDED IN TYS WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT APU, REMOVED AND REPLACED APU THERMOCOUPLE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 18,509 hrs · 19,108 cycles

CREW REPORTED F/O’S ATTITUDE INDICATION FAILED AND EFIS COMMON CAUTION MESSAGE UPON TAKEOFF FROM MOB. CREW RETURNED TO MOB AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, SWAPPED AHC’S (ATTITUDE AND HEADING COMPUTER) FROM SIDE TO SIDE, RESET SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RIVET — BURNED (FUSELAGE) · airframe 18,202 hrs · 18,819 cycles

CREW REPORTED LIGHTNING STRIKE IN CRUISE FLIGHT EN ROUTE FROM PGV TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED SEVERAL MINOR RIVET BURNS ON RIGHT FUSELAGE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,920 hrs · 18,529 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE BOTTLE — LOW PRESSURE (FIRE PROTECTION) · airframe 16,903 hrs · 17,542 cycles

CREW REPORTED APU FIRE MESSAGE, APU BOTTLE LOW AND APU AUTOMATICALLY SHUT DOWN ON TAXI OUT AT DCA. NO VISIBLE SMOKE OR FIRE. MESSAGE EXTINGUISHED. CREW FOLLOWED QRH AND RETURNED TO THE GATE. MAINTENANCE INSPECTED APU COMPARTMENT AND FOUND NO VISUAL SIGNS OF FIRE OR LEAKS. MAINTENANCE REMOVED AND REPLACED APU FIRE BOTTLE, APU FIRE BOTTLE DISCHARGE CARTRIDGE AND FIDEX CONTROL UNIT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: AMPLIFIER — FAILED (COCKPIT) · airframe 16,765 hrs · 17,406 cycles

AT AGS, CREW REPORTED THE PASSENGER ADDRESS SYSTEM INOPERATIVE, CIRCUIT BREAKER OUT AND AN ELECTRICAL SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE PASSENGER ADDRESS AMPLIFIER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (RT MLG) · airframe 16,239 hrs · 16,895 cycles

CREW REPORTED A PARTIAL DE-CAP OF THE RIGHT INBOARD MAIN LANDING GEAR TIRE ON LANDING IN LIT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT INBOARD AND OUTBOARD MAIN LANDING GEAR WHEEL / TIRE ASSEMBLIES AND THE RIGHT HAND INBOARD FLAP ASSEMBLY. MAINTENANCE ALSO REMOVED AND INSTALLED THE FLAP STUB FAIRING AND PERFORMED CHECKS. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 14,240 hrs · 14,874 cycles

CREW REPORTED A LIGHTNING STRIKE ON APPROACH TO MYR. AIRCRAFT LANDED IN MYR WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RADOME AND REPAIRED DAMAGE TO THE LT HORIZONTAL STABILIZER TIP, LT NOSE LANDING GEAR DOOR, LT AFT FUSELAGE AND TAIL CONE. ALSO, A BURNT STATIC WICK WAS REMOVED AND REPLACED AND THE WINDSHIELD WIPER ARMS WERE DEMAGNETIZED. CHECKS WERE PERFORMED. WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUAL, AIRCRAFT STRUCTURAL REPAIR MANUAL AND VENDOR DOCUMENTATION. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 14,124 hrs · 14,737 cycles

CREW REPORTED THE NOSE GEAR MADE AN UNUSUAL NOISE AT GEAR RETRACTION ON TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL AND FOUND THE NOSE LANDING GEAR (NLG) DOORS VIBRATING OPEN AND CLOSED WHEN THE NLG WAS RETRACTED. MAINTENANCE REMOVED AND REPLACED THE NOSE NLG SOLENOID SELECTOR VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — FAULTY (WARNING SYS) · airframe 14,081 hrs · 14,691 cycles

CREW REPORTED AN ANTI-ICE DUCT WARNING MESSAGE DURING ROTATION ON TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED HEAT SENSING ELEMENT A15WK AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOE SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 11,657 hrs · 12,155 cycles

CREW REPORTED A BURNING SMELL IN COCKPIT AND BACK TO ROW NR 2 IN FLIGHT. F/O’S RA FLAG WAS FLASHING AT TIME OF SMELL. AN EMERGENCY LANDING / DIVERSION WAS MADE TO ATL. LANDING IN ATL WAS MADE WITHOUT INCIDENT. MAINTENANCE CHECKED THE AVIONICS COMPARTMENT, AIR CONDITIONING SYSTEM, PASSENGER CABIN LIGHTS, FLIGHT DECK LIGHTS, GALLEY AREA, AND RA SYSTEM PER AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — BROKEN (PITCH TRIM) · airframe 11,657 hrs · 12,155 cycles

WHILE IN CRUISE THE CREW RECEIVED A STAB TRIM DISCONNECT AMBER CASS MESSAGE. THE FLIGHT LANDED WITHOUT INCIDENT AT PHL. MAINTENANCE REPAIRED A BROKEN WIRE ON THE CAPTAINS PITCH TRIM SWITCH. CHECKS WERE DONE PER THE AIRCRAFT MAINTENANCE MANUAL. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,569 hrs · 12,062 cycles

CREW REPORTED A FLAP FAIL AMBER MESSAGE ON APPROACH INTO PHL. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET SKEW DETECTOR AND RESET FLAPS IAW SL 00-001 AND ACFT MM. ACFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,566 hrs · 12,059 cycles

CREW REPORTED A FLAP FAIL CAS MESSAGE ON APPROACH INTO CVG LEFT FLAP 40 DEG RT FLAP 41 DEG. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET FLAPS IAW AIRCRAFT MAINTENANCE MANUAL, MSG CLEARED. AIRCRAFT RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,432 hrs · 11,919 cycles

ON APPROACH INTO AVP THE CREW REPORTED FLAPS FAIL CAS MSG, FLAPS FAILED AT 37 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED FAULT CODES AND RESET SYSTEM AND CYCLED SYSTEM CB'S IAW SERVICE LETTER 00-001. NO DEFECTS WERE NOTED AND AIRCRAFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 10,193 hrs · 10,537 cycles

CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE LT AND RT WINGTIPS. MAINTENANCE REPAIRED THE DAMAGE UNDER REO 601R-57-30-001 AND THE STRUCTURAL REPAIR MANUAL. NO OTHER DEFECTS NOTED AT THIS TIME. ACFT WAS RELEASED FOR SERVICE. (S)

Part: CONTROLLER — MALFUNCTIONED (T/E FLAP) · airframe 9,401 hrs · 9,672 cycles

CREW REPORTED A FLAPS FAIL MESSAGE ON APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET FLAP CONTROLLER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 8,137 hrs · 8,336 cycles

CREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT OF CLT. CREW CONTINUED ON TO PHF WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH A VISUAL AND EN ROUTE LIGHTNING STRIKE INSPECTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-210-801 AND GENERAL MAINTENANCE MANUAL 2-5-18-C. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-220-802. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — ODOR (LAVATORY) · airframe 7,426 hrs · 7,543 cycles

CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM THE LAVATORY AREA. MAINTENANCE INSPECTED THE LAV AND SURROUNDING AREA INCLUDING OPS TESTING THE LAV LIGHT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS TEST GOOD, NO DEFECTS NOTED AT THIS TIME. MAINTENANCE INSPECTED AND FOUND INSULATION NEAR THE LAV LIGHT BALLAST. MAINTENANCE RE-POSITIONED THE INSULATION NEAR BALLAST. IN ADDITION, MAINTENANCE FOUND THE LAV STUFFED WITH HAND TOWELS. MAINTENANCE REMOVED TOWELS, SERVICED LAVATORY AND PERFORMED OPS TEST OF LAV WASTE DISPOSAL SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — BROKEN (TEMP BULB) · airframe 6,686 hrs · 6,801 cycles

CREW REPORTED A NR 2 GENERATOR CAS MESSAGE ON TAKEOFF. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 GENERATOR. MAINTENANCE PROPERLY SERVICED OIL LEVEL AND REPAIRED A BROKEN WIRE ON NR 2 IDG TEMP BULB. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 5,787 hrs · 5,866 cycles

ON DESCENT THE CREW REPORTED AUTO PILOT UNCOMMANDED DOWN 15 DEGREES. MAINTENANCE DEFERRED THE AUTO PILOT PER MEL 22-10-01 CODE B. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 5,362 hrs · 5,399 cycles

CREW REPORTED -FLAPS FAIL- MESSAGE FROM 20 DEGREES - 30 DEGREES. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (TAIL CONE) · airframe 5,044 hrs · 5,061 cycles

THE CREW REPORTED TAKING A LIGHTNING STRIKE IN FLIGHT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR DAMAGE WAS FOUND ON THE TOP VHF ANTENNA, LOWER TAIL STATIC DISCHARGER, AND THE TAIL CONE. THE ANTENNA AND STATIC DISCHARGER WERE REPLACED WITH SERVICEABLE UNITS. THE TAIL CONE DAMAGE WAS INSPECTED AND FOUND WITHIN ALLOWABLE LIMITS AT THIS TIME. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — BIRD STRIKE (FUSLEAGE) · airframe 3,383 hrs · 3,402 cycles

AFTER LANDING INSPECTION REVEALED DAMAGE TO THE RADOME FROM A BIRD STRIKE. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REPLACED THE RADOME WITH A SERVICEABLE UNIT IAW CRJ200 AMM 53-81-01-000(400)-801. NO FURTHER DAMAGE WAS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: COWLING — DAMAGED (RT LOWER) · airframe 3,187 hrs · 3,198 cycles

AFTER POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT ENGINE LOWER NOSE ACCESS COWL WAS MISSING. THE COWL WAS FOUND ON THE RUNWAY. MAINTENANCE INSTALLED A SERVICEABLE NOSE ACCESS COWL IAW CRJ200 AMM 71-14-01-400-802. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 3,037 hrs · 3,044 cycles

THE NOSE DOOR OPEN WARNING ILLUMINATED AND SOUNDED AFTER GEAR RETRACTION. THE FLIGHT RETURNED TO SDF. THE AIRCRAFT WAS FERRIED TO PHL WHERE MAINTENANCE REMOVED & REPLACED THE NLG DOOR SELECTOR VALVE IAW CRJ200 AMM 32-22-20-000-801 AND 32-22-20-400-801. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (NLG DOOR) · airframe 3,031 hrs · 3,039 cycles

THE NOSE DOOR OPEN WARNING ILLUMINATED AND SOUNDED ON SHORT FINAL. MAINTENANCE INSPECTED THE NLG DOORS IAW CRJ200 AMM 32-20-00-210-801. OPERATIONAL CHECKS WERE NORMAL. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 2,073 hrs · 2,060 cycles

AFTER LANDING AT CAK THE CREW OF FLIGHT 2286 REPORTED A FLAPS HALFSPEED STATUS MESSAGE. PSA MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ 200 AMM 27-51-05-400-801. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 1,971 hrs · 1,959 cycles

FLAPS SELECTED TO 8 DEG ON APPROACH, FLAPS FAIL CAUTION MESSAGE ILLUM. RIGHT FLAPS INDICATED 0 DEG & LEFT 2 DEG. C/W QRH, DECLARED AN EMERGENCY, MADE AN UNEVENTFUL LANDING WITH ZERO FLAPS. MX DEPLOYED FLAPS TO 20 DEG, AIRCRAFT FERRIED TO DAY. MX INSPECTED & FOUND SKEW DETECTION UNIT CONNECTORS CONTAMINATED WITH GLYCOL. CANNON PLUGS CLEANED IAW STANDARD MAINTENANCE PROCEDURES. AS PRECAUTION FLAP ELECTRONIC CONTROL UNIT WAS REPLACED IAW CRJ 200 AMM 27-51-05-000-801/400-801. THE REMOVED UNIT WAS PUT INTO QUARANTINE. THE FLAP RIGGING WAS CHECKED IAW CRJ 200 AMM 27-54-00-710-801 AND THE FLAP SYSTEM WAS OPERATIONALLY CHECK GOOD IAW CRJ 200 AMM 27-54-00-710-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 47 hrs · 45 cycles

IN FLIGHT, THE CREW RECEIVED A RIGHT HAND EMERGENCY DOOR CAS MESSAGE. AIRCRAFT PRESSURE STAYED NORMAL. MAINTENANCE CONTROL, WITH THE CREW, THEN DEFERRED THE DOOR WITH 52-70-03 CAT C.

Part: SENSOR — DIRTY (RT EMER DOOR) · airframe 41 hrs · 40 cycles

DURING FLIGHT, THE CREW RECEIVED A RIGHT EMERGENCY DOOR ILLUMINATION AND YELLOW CAS MESSAGE. UPON ARRIVAL AT PHL, OUTSTATION MAINTENANCE FOUND CODE S42 IN THE PSEU. MAINTENANCE THEN CLEANED AND INSPECTED THE PROXY SENSOR AND TARGET IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 52-00-00 AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.