Service difficulty reports

1,771,154 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AALA202606167724Battery Pack · no testAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHTS NOT CHARGING AND MISSING SECURITY STRAPS AT FA STATIONS 1L. MAINTENANCE REPLACED FA FLASHLIGHT BATTERY PACKS AND INSTALLED TAMPER SEALS FOR JUMP SEATS 1L PER AMM 25-64-01.Jun 15, 2026 · N789AN · Boeing 777223 · Emergency LightingSDR AALA202606167157Battery Pack · no testAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHTS NOT CHARGING AND MISSING SECURITY STRAPS AT FA STATIONS 2R. MAINTENANCE REPLACED FA FLASHLIGHT BATTERY PACKS AND INSTALLED TAMPER SEALS FOR JUMP SEATS 2R PER AMM 25-64-01.Jun 15, 2026 · N789AN · Boeing 777223 · Emergency EquipmentSDR DXTA2026061608458Brake Assy · faultedAFTER TAXIING IN TO A STOP ON THE RAMP POST LANDING THE MAIN BRAKES WILL EXTENSIVELY VIBRATE FROM A SLOW SPEED UNTIL COMING TO A COMPLETE STOP. CHECKED ALL BRAKE PINS AND EVERYTHING LOOKED GOOD. CHECKED THE BRAKES THEMSELVES AND DIDN'T SEE ANY UNUSUAL WEAR. Jun 15, 2026 · N586QS · Cessna 680A · Landing Gear Brake SystemSDR DXTA2026061608457Power Supply · no testWHEN DOING EMERGENCY LIGHTS TEST WE FOUND THAT THE EXIT SIGN OVER THE MAIN CABIN DOOR WILL NOT TURN ON. REPEAT WRITE UP. REMOVED EMERGENCY BATTERY AND INSTALLED CUSTOMER SUPPLIED OVERHAULED EMERGENCY BATTERY PERFORMED OPS CHECK OF EMERGENCY BATTERIES WITH NO Jun 15, 2026 · N211QS · Cndair CL6002B16 · Emergency LightingSDR UIEA2026061500501Amu · faultedFO OXYGEN MASK MIC INOPERATIVE. R & R AMU & OPS CHK NORMAL IAW AMM 23-51-04/401 & IPC 23-51-04-01.Jun 15, 2026 · N712GT · Boeing 777F · Communications SystemSDR MASA2026061520028Battery · no testFWD FA FLASHLIGHT NOT FLASHING/ REMOVED AND REPLACED BATTERY ON FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHTJun 15, 2026 · N89342 · Emb ERJ170200LR · Emergency EquipmentSDR WX0A2026061532848Web · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 9000-0012: (S//M)(34240-02) PASSENGER CABIN FWD WET AREA, WEB BTW FR12 - FR16 AND AT Y1584 CORRODED, PASSENGER CABIN FWD WET AREA, WEB BTW FR12 - FR16 AND AT Y1584 WAS REPLACED IAW SRJun 15, 2026 · N335NV · Airbus A319111 · Fuselage Miscellaneous StructureSDR WX0A2026061532847Pin · installed(AIRCRAFT NOT GROUNDED) (EMERGENCY DECLARED) LDG GEAR AND DOORS NOT CLOSED ON TAKEOFF. PREFORMED GVI OF NLG IAW AMM 32-21-00-200-002A. FOUND SAFTEY LOCK STILL INSTALLED IN NLG LOCK STAY. REMOVED SAFTY LOCK FROM NLG LOCK STAY IAW AMM 32-00-00-081-002A. NO OTJun 15, 2026 · N271NV · Airbus A320214 · Landing Gear Retraction/Extension SystemSDR 2026FA0000519Cylinder · crackedPILOT REPORTED LOUD NOISE FROM ENGINE, SIGNIFICANT POWER LOSS, AND LOUD VIBRATIONS. PILOT LANDED AT A NEARBY AIRPORT WHERE MANTIENCE DISCOVERED A LARGE CRACK IN CYLINDER #2(HEAD SEPERATING FROM THE BARREL).Jun 15, 2026 · N5251Z · Cessna 172S · Reciprocating Engine Cylinder SectionSDR 2026F00124Elec Connector · faultedNONE OF THE THREE GEARS WOULD COME DOWN. CYCLED REPEATEDLY BUT NOTHING WORKED. EMERGENCY GEAR DOWN WAS USED. R & R RT MLG UPLOCK ROLLER BEARING, R & R GEAR VALVE CANNON PLUG, SERVICED HYDRAULIC POWER PACK ACCUMULATOR. GEAR SEEING OPS CHECK GOOD. IAW MM 20-0Jun 15, 2026 · N889DC · Frchld SA227DC · Landing Gear System WiringSDR FDEA202606150745Seat Track · wornMAIN DECK CARGO SEAT TRACK AT STATION 1541, X= -47.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 1571 TO EXISTING SPLIJun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150744Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1541, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150743Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-10, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGJun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150742Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-Jun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150741Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = 47.5 WAS EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPJun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150740Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -27.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK BS 1279, X = - 27.5 WORN CROWN EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRAJun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150739Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 5-10, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRJun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150738Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 5-63 TO EXISJun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606150737Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= -8.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = - 8.5 WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONALJun 15, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 2A6R2026061575601Floor Skin · dentedDENTS AND LOCALIZED DELAMINATION WERE FOUND ON THE UNDERSIDE SKIN OF THE CABIN FLOOR, MEASURING UP TO 89 MM × 914 MM (3.5 IN × 36 IN) AND 50 MM × 610 MM (2 IN × 24 IN). REPAIRED IN ACCORDANCE WITH AIRBUS HELICOPTERS RDAS RDAS EC135 53 2026 2040A, ISSUE DATE 11Jun 15, 2026 · N831ME · Urocop EC135T2 · Fuselage Main, StructureSDR QR9R2026061500001Control Lever · out of limitsRECEIVED CONTROL LEVER ASSY FROM AIRBUS UNSERVICEABLE. MEASURED .060 AROUND SLIP BUSHING; MAX ALLOWED IS .019.Jun 15, 2026 · Bolkms BK117C2 · Main Rotor HeadSDR DALA2026061503574Web · crackedWEB (BETWEEN C20 AND C21) AT STR-44L OF THE FWD CARGO COMP'T FOUND CRACK. REPAIRED PER A330 SRM 53-21-14-300-005. (1647798) AIRCRAFT WAS GROUNDED.Jun 15, 2026 · N801NW · Airbus A330323 · Fuselage Miscellaneous StructureSDR AALA202606157071Battery · inoperativeAIRCRAFT WAS NOT GROUNDED: FA 2 FLASHLIGHT INOP. MAINTENANCE REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00.Jun 15, 2026 · N341SV · Boeing 7378 · Emergency EquipmentSDR JR2R20260615969Floor Support · corrodedFLOOR SUPPORT AT RBL11 BETWEEN FR 12 TO FR 18 IS CORRODED OUT OF LIMITS IN MULTIPLE SPOTS. REPLACEDJun 15, 2026 · N85323 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR ABXA20260615258Warning Message · illuminatedON FINAL APPROACH, AFT CARGO DOOR EICAS MSG. DEFERRED IAW MEL 52-71-1-1, PLACARDS INSTALLED, MBCB 6/25/26. REINSPECT EVERY CYCLE. A/C RETURNED TO SERVICE.Jun 15, 2026 · N774AX · Boeing 767281 · Door Warning SystemSDR SIMA20260615001Control Lever · failedLANDING GEAR WOULD NOT EXTEND WITH LEVER. RAN QRH LANDING GEAR LEVER DISAGREE/ALTERNATE GEAR EXTENSION CHECK. GEAR DEPLOYED. (EMERG DECLARED) FOUND LANDING GEAR LEVER DISAGREE RAR LANDING GEAR CONTROL LEVER IAW AMM 32-33-01. OPS CHECK GOOD.Jun 15, 2026 · N749BM · Emb ERJ170100SE · Landing Gear SelectorSDR DXTA2026061508451Pin · lack of lubeBOTH THE INTERIOR DOOR LATCHING HANDLE AND THE EXTERIOR DOOR HANDLE REQUIRE MORE THAN NORMAL FORCE TO OPERATE (LATCHING CLOSED). THE PROBLEM IS INTERMITTENT. CORRECTIVE ACTION: PERFORMED DOOR PIN LUBRICATION IAW AMM 12-20-25. OPS CHECK GOOD, NO DEFECTS AT THIJun 15, 2026 · N885QS · Textrn TEXTRON700 · Passenger/Crew DoorsSDR COEA2026102210807Skin Panel · damagedWO 275316 NR 800004 HEAVY CHECK COE/MAJOR REPAIR: FWD CARGO DOOR INNER SKIN FWD OF THE MIDDLE LATCH DAMAGED. CORRECTIVE ACTION: REPAIRED PER SRAS-00054114-01 ISSUE A, DATED 8/31/2026.Jun 14, 2026 · N807FX · Aerosp ATR72212 · Cargo/Baggage DoorsSDR SWIA2026061477707Stub Frame · corrodedUNDER FLOOR STUB FRAME CORRODED BETWEEN FLOOR SILL AND ABOVE CARGO DOOR OPENING BS 533. INSTALLED REPAIRED FRAME SECTOR, FRAME SPLICE, ANGLE SPLICE, REINFORCEMENT ANGLE ON FRAME AT BS 533 BTWN STRINGERS 13L AND 16L, IAW REO 690-53-31-1178 REV -. LEAK CHKD GOJun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2026061477706Stub Frame · corrodedUNDER FLOOR STUB FRAME CORRODED BETWEEN FLOOR SILL AND ABOVE CARGO DOOR OPENING BS 549. REMOVED AND INSTALLED NEW STUB FRAME AT BS 549 IAW REO 690-53-31-1143, REV -A. COMPLIED WITH TASK CARD 51-900-1002-SKY PRESSURE CHECK GOOD.Jun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2026061477705Floor Support · corrodedLEFT OTBD FLOOR SUPPORT LBL 27 WAS CORRODED BTWN BS 1000 - 1035. REPAIRED FLOOR SUPPORT IAW SRM 53-00-41-201-001-A03, AND DWG MM690-35041, REV AB. COMPLIED WITH ALL STEPS OF 51-900-1002-SKY.Jun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2026061477704Floorbeam · corrodedFS280 CROSSBEAM CORROSION AT LBL900 C-CHECK RO 10132026EVALUATED LH CROSSBEAM FS 28000 AND FOUND OUT OF LIMITS REPLACED WITH 1 EA OF NEW LH FS28000 CROSSBEAM REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-22-001-001-A01Jun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA2026061477703Floorbeam · crackedFS280 CROSSBEAM RBL9 OUTBOARD ANGLE CRACKED C-CHECK RO 10132026REMOVED AND REPLACED WITH 1 EA OF NEW FS280 CROSSBEAM RBL9 OUTBOARD ANGLE REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV K COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY SEE COJun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA2026061477658Stub Frame · corrodedUNDER FLOOR STUB FRAME CORRODED BETWEEN FLOOR SILL AND ABOVE CARGO DOOR OPENING FS 64500 C-CHECK RO 10132026FRAME FOUND TO BE OUT OF LIMITS DUE TO CORROSION ON MULTIPLE ELEMENTS IAW CRJ900SRM 53-31-06-101-002-A02 REPAIRED FRAME IAW CRJ900 REO 690-53-31-1150 Jun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2026061477635Stub Frame · corrodedUNDER FLOOR, STUB FRAME CORRODED BETWEEN FLOOR SILL AND ABOVE CARGO DOOR OPENING BS 661. REMOVED AND INSTALLED LT SECTION FRAME AT BS 661. BTWN STR 16L - 18L IAW SRM 53-00-06-201-001-A03, & REO 690-53-31-1150, REV- . COMPLIED WITH TASK CARD 51-900-1002-SKY. Jun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2026061477634Bulkhead Web · corrodedFS 280 BULKHEAD LEFT UPPER WEB CORRODED INBD SIDE AT WL 79.50. EVALUATED THE BS 280 BULKHEAD LEFT UPPER WEB AND FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE BULKHEAD WEB IAW SRM 53-11-10-201-003-A01, REPAIR B, REV 38. COMPLIED WITH ALL STEPS OF TASK CJun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, BulkheadSDR SWIA2026061477633Floorbeam · crackedBS 280 FLOORBEAM, LBL9 OTBD ANGLE CRACKED. REMOVED AND REPLACED THE FLOORBEAM OTBD ANGLE IAW SRM 51-42-21-001-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Jun 14, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA2026061477549Handle · chafedTHERE IS CHAFING ON THE HANDLE OF THE GALLEY SERVICE DOOR AT THE INNER AREA OF THE HANDLE EXTERIOR HANDLE. INSTALLED A NEW SERVICEABLE SERVICE DOOR HANDLE HOUSING ASSY IAW SRM 51-42-06-001-001-A01.Jun 14, 2026 · N713SK · Cndair CL6002C10 · Service DoorsSDR IPXA2026061568089Longeron · crackedNR 1 AFT LWR PYLON FAIRING LONGERONS CRACKED UNDER GUSSET PLATE. INSTALLED LONGERON SPLICE DOUBLERS, 2EA IAW SRM 51-40-21-001.Jun 14, 2026 · N144UP · Airbus A300F4622R · Nacelle/Pylon, Longeron/StringerSDR REXA2026082601671Rib · crackedCRACK ON LEADING EDGE RIB SS57.16 AT RH WING LEADING EDGE RIB SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV --Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026082601670Angle · crackedCRACK ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT. ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 & SRM 51-42-13-001-001-A01Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601669Angle · crackedCRACK ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT. ANGLE (2EA) ON FS1148.00 STGR 10RH AND FS1155.00 STGR 8RH AT AFT ACCESORIES COMPARMENT WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 & SRM 51-42-13-001-001-A01Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601668Panel · crackedCRACK ON TOP PANEL AT MAIN PASSENGER DOOR. TOP PANEL AT MAIN PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-006-A01.Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026082601657Bracket · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19), SUPPORT PLATE LBL 40'' & RBL 40'' & SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL LH/RH AREA, RBL 45 AND LBL45. CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) & SUPPORT PLATJun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601656Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19), SUPPORT PLATE LBL 40'' & RBL 40'' & SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL LH/RH AREA, RBL 45 AND LBL45. CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) & SUPPORT PLATJun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601655Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19), SUPPORT PLATE LBL 40'' & RBL 40'' & SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL LH/RH AREA, RBL 45 AND LBL45. CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) & SUPPORT PLATJun 14, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601647Rib · crackedCRACKED BAT RIB AT WS 14.50 OUTER WING, LH MLG WHEEL WELL TRUNNION AREA. BAT RIB AT WS 14.50 OUTER WING, LH MLG WHEEL WELL TRUNNION AREA WAS REPLACE PER CRJ900 SRM 51-42-21-001-001-A01,SRM 51-42-22-001-001-A01 AND SRM 51-41-02-001-001-A01.Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2026082601645Handle · crackedCRACK ON OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM. OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.Jun 14, 2026 · N926XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2026061476791Door Sill · corrodedMAIN A-BAY BACKUP SILL, STR 21L, BETWEEN BS 333 TO 349, CORRODED. REMOVED AND INSTALLED A NEW MAIN A-BAY BACKUP SILL IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31810, REV AE. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE FOR WORK PERFORMED. LEAK CHECJun 14, 2026 · N719SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026061476786Angle · corrodedMAIN A-BAY ANGLE REINFORCEMENT, STR 18L TO 22L, BS 333 CORRODED. REMOVED AND INSTALLED NEW MAIN A-BAY ANGLE REINFORCEMENT, STR 18L TO 22L, BS 333 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG SH670-31810, REV AE. COMPLIED WITH TASK CARD 51-900Jun 14, 2026 · N719SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure