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 DXTA2026061508444Battery Pack · dischargedWHEN DOING THE EMERGENCY LIGHT TEST WE FOUND THAT THE EXIT SIGN OVER THE MAIN ENTRANCE DOOR WILL NOT TURN ON. STARTED APU AND PLACED EMERGENCY LIGHT SWITCH IN ARM POSITION. ALLOWED 15 MINUTES FOR THE EMERGENCY LIGHTING BATTERY TO CHARGE. PERFORMED A SATISFACJun 14, 2026 · N211QS · Cndair CL6002B16 · Emergency LightingSDR CALA2026061517099Battery Pack · faultedCB POPPED L1 EMERGENCY LIGHTS M33424 EMERGENCY LIGHTS POWER SUPPLY SUSPECTED TO BE AT FAULT. POWER SUPPLY TO REPLACED IAW 33-51-06-960-803. EMERGENCY LIGHTS OPS TEST ACCOMPLISHED. ALL OPS NOW OK. IAW AMM 33-51-00-710-801.Jun 14, 2026 · N206UA · Boeing 777222 · Emergency LightingSDR CALA2026061517097Battery Pack · inoperativeEMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - LEFT MID M1670 EMERGENCY EXIT LIGHTING BATTERY INOP. REPLACED M1670 EMERGENCY EXIT LIGHTING CONTROLLER BATTERY PACK REF AMM 33-51-06-960-805. OPS CHECK GOOD.Jun 14, 2026 · N61886 · Boeing 737924ER · Emergency LightingSDR CALA2026061517081Fluid · leakingPOSSIBLE LIQUID SEEPING INTO E AND E BAY DEBRIEFED FLIGHT CREW, SMALL CAN EXPLODED/OPENED AND SEEPED INTO FLT DECK THRU DOOR.INPECTED E/E BAYS FWD AND MID, NO LIQUIDS FOUND AT THIS TIME . OK TO CONT.Jun 14, 2026 · N61887 · Boeing 737924ER · Standard Practices/StructuresSDR CALA2026061517080Unknown · odorSMOKE ODOR CONDITIONAL INSP REQUIRED PER AMM 05-51-XX DUE TO AN INCIDENT REPORTED BY THE CREW. CONDITIONAL INSPECTION PERFORMED IAW AMM: 05-51-58-800-801-C3 REV 106 WITHOUT FINDING ANY UNUSUAL SMELL. ALL AREAS SATIS.Jun 14, 2026 · N78017 · Boeing 777224 · Air Distribution SystemSDR SCNA20260615248Power Supply · inoperativeGALLEY EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR AND L1 DOOR INOP. REMOVED & REPLACED GALLEY EMERGENCY EXIT SIGN POWER PACK IAW AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.Jun 14, 2026 · N5179A · Boeing 737800* · Emergency LightingSDR DALA2026061503569Unknown · odorSULFUR ODOR IN COCKPIT AND CABIN ON TAXI OUT. PERFORMED LEVEL A DECONTAMINATION PER AMM 21-00-00. NO FURTHER SMELLS NOTED. OK FOR SERVICE. (LP: 9073650, AIRCRAFT WAS GROUNDED)Jun 14, 2026 · N314NB · Airbus A319114 · Air Distribution SystemSDR AALA202606152185Isolator · damagedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FORWARD OVER WING EXIT, FORWARD AND AFT ISOLATORS DAMAGED. RELACED ISOLATORS PER SRM 51-40-01.Jun 14, 2026 · N808NN · Boeing 737823 · Emergency ExitsSDR JR2R20260614860Panel · chafedRIGHT WING, FIXED LEADING EDGE OVER PYLON, PREVIOUS REPAIR HAS CHAFE MARKS OUT OF LIMITS. REPAIRED.Jun 14, 2026 · N85323 · Emb ERJ170200LL · Wing, Plate/SkinSDR JR2R20260614861Panel · chafedLEFT WING, FIXED LEADING EDGE OVER PYLON, PREVIOUS REPAIR HAS CHAFE MARKS OUT OF LIMITS. REPAIRED.Jun 14, 2026 · N85323 · Emb ERJ170200LL · Wing, Plate/SkinSDR F3LA202606140428Battery · no testDURING SCHEDULED HEAVY CHECK EPSU TEST FOUND 10WL FAILED TEST. AIRCRAFT WAS NOT GROUNDED. REMOVED AND REPLACED 10WL EPSU BATTERY IAW AMM 33-51-38-400-002-A OPS TEST GOOD. A/C OK FOR SERVICE. AIRCRAFT WAS RETUNED TO SERVICE.Jun 14, 2026 · N343FR · Airbus A320251N · Emergency LightingSDR 2026FA0000516Lens · missingLENS COVER BY L1 DOOR MISSINGJun 14, 2026 · N247BZ · Airbus BD5001A11 · Emergency LightingSDR SWIA2026061377702Stringer · corrodedSTGR23R HAS GALVANIC CORROSION FS36400 - 37900 C-CHECK RO 10132026REMOVED AND REPLACED STGR23R BETWEEN FS333 TO FS379 PER CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-31350 REV A AND COMPLIED WITH ALL STEPS OF 51-900-1002-SKYJun 13, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2026061377701Frame · corrodedFRAME FS34900 HAS CORROSION ON THE LOWER FLANGE STGR26L - 26R MARKED IN RED C-CHECK RO 10132026INSTALLED NEW LOWER FRAME SECTOR FS34900 BETWEEN STGR 23LH AND STGR 24REF IAW CRJ900 SRM 51-42-06-001-001-A01 REV 38 DATED JUL 252020 AND DWG SH690-31350 REV M AND Jun 13, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2026061377700Stringer · corrodedSTGR25R HAS AREAS OF GALVANIC CORROSION FS29500 - 31000 MARKED IN RED C-CHECK RO 10132026REPLACED STGR25R FS28000-FS33000 REF CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND DWG SH670-31360 REV K COMPLIED WITH TASK CARD 51-900-1002-SKY NO LEAKS DJun 13, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2026061377699Skin · corrodedSKIN INNER SURFACE IS CORRODED FS33300 - 31900 STGR25L -26L CIRCLED IN RED C-CHECK RO 10132026REMOVED CORROSION FROM SKIN INNER SURFACE AT FS33300, STGR25L - STGR26L PER REF CRJ 900 SRM 51-21-06-001-001-A01 REWORKED AREA IS WITHIN LIMITS PER REO 690-53-21-215Jun 13, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2026061377657Frame · corrodedFRAME FS36400 FORWARD LOSER FLANGE HAS A PIT OF CORROSION JUST OUTBOARD OF THE INTERCOSTAL BETWEEN STGR27 AND 26L MARKED IN RED C-CHECK RO 10132026REPAIRED FRAME FS36400 FORWARD LOWER FLANGE JUST OUTBOARD OF THE INTERCOSTAL BETWEEN STGR27 AND 26L REF CRJ900 Jun 13, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2026061377656Stringer · corrodedSTGR27 HAS AREAS OF GALVANIC CORROSION FS31900 -29500 MARKED IN RED C-CHECK RO 10132026REMOVED AND REPLACED STGR27, FS310 - FS333 PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K COMPLIED WITH ALL STEPS OF 51-900Jun 13, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2026061377614Stringer · corrodedSTRINGER 26L HAD AREAS OF GALVANIC CORROSION, BTWN BS 282 - 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-A01, 51-42-21-001-001-A01, AND DWG SH670-31360, REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY, NO LEAKS DETECTED.Jun 13, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2026061377309Rib · mislocatedMISLOCATED LT WING BOX RIB ANGLE AT WS 4830. REMOVED AND REPLACED LT WING BOX BATT-RIB ANGLE IAW DWG 600-10204 REV M AND SRM 51-42-06.Jun 13, 2026 · N936SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2026061377050Door · crackedRIGHT TRU DOOR AFT LATCH CUT-OUT WAS CRACKED. REMOVED THE RT TRU DOOR LANDING AND INSTALLED NEW, IAW REO 670-53-11-2328, REV -.Jun 13, 2026 · N792SK · Cndair CL6002C11 · Electrical/Electronic Compartment DoorsSDR REXA2026082601736Skin · crackedINITIAL INSPECTION: CRACK MULTI-FUNCTION SPOILER PANEL UPPER SKIN (2EAS OUTB) AT LH/RH WING MULTI-FUNCTION SPOILER PANEL UPPER SKIN RH WING WAS REPAIRED PER REO 690-57-73-027 REV -- AND MULTI-FUNCTION SPOILER PANEL UPPER SKIN LH WAS INSPECTED AND NOT DAMAGE WJun 13, 2026 · N926XJ · Cndair CL6002D24 · SpoilersSDR REXA2026082601734Fitting · wornWEAR ON LH/RH SIDE STAY FITTING IN MAIN WHEEL WELL AREA. LT - RT SIDE STAY FITTING IN MAIN WHEEL WELL AREA WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE REPAIRED PER EA CRJ953-22582 REV IR AND EA CRJ953-22583 REV IRJun 13, 2026 · N926XJ · Cndair CL6002D24 · Wing Main, Frame StructureSDR REXA2026082601685Skin · crackedCRACK ON SKIN AROUND HANDLE CUTOUT AT AFT BAGGAGE COMPARTMENT DOOR. HOUSING (P/N ON:H3415-31, S/N ON:2150 // P/N OFF:H3415-31, S/N OFF:2366) AT AFT BAGGAGE COMPARTMENT DOOR WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-01Jun 13, 2026 · N926XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026073001330Seat Track · corrodedCORROSION ON STGR 24R AND FS333.00/FS349.00. CORROSION ON STGR 24R AND FS333.00/FS349.00. WAS EVALUATED OUT LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-21-03-101-002-A04 AND SRM 53-00-03-201-001-A0Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026073001329Floorbeam · crackedCRACK ON FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS FOUND. NEW FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS VERIFIED PER CRJ900 SRM 53-11-43-001-001-A01 ///REPLACE WAS PERFORMED UNDER NRC 0057Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026073001328Stub Frame · corrodedCORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073001327Stub Frame · corrodedCORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073001326Floor Support · corrodedCORROSION ON FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-13-001-00Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001325Fitting · corrodedCORROSION ON FITTING APROX ON RBL12 FITTING ON RBL12 FS:290 APROX WAS REMPLACED PER. CRJ900 SRM 51-42-21-001-001-A01 6. C.Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026072801197Support Bracket · crackedCRACK ON SUPPORT BRACKET TO TIE BAR AT LEFT PYLON SUPPORT BRACKET TO TIE BAR AT LEFT PYLON WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01Jun 13, 2026 · N929XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR VNAA202607280004Support · corrodedCORROSION ON SILL RH BTW FS280.00 TO 286.00 AND STGR 17R. CORROSION ON SILL RH BTW FS280.00 TO 286.00 AND STGR 17RH WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND AREA IS OUT LIMITS PER CRJ-900 SRM 53-21-43-101-001-A01 AND AREA WAS REPAIRED PER CRJ-900 Jun 13, 2026 · N552NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202607280003Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB LH SIDE FS193 AT FWD EQUIPMENT COMPARTMENT. CRACK ON ELECTRICAL BAY FLOOR WEB LH SIDE FS193 AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER SRM 53-11-43-201-001-A01.Jun 13, 2026 · N552NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR IPXA2026072348181Web · corrodedCORROSION , WEB OF CENTER WING TANK REAR SPAR NEAR JETTSION PUMP AT STA 1240 RBBL 93. (REPAIR) 1.PERFORMED EO-98103-REQ1 REV.1 AND EGAT EI NO.F2026A57M-1365 REV.1. 2.JOB COMPLETED AND ATTACHMENT ARE UPLOADED.Jun 13, 2026 · N583UP · Boeing 7474R7F · Fuel StorageSDR SWAA2026061512179Radome · no discrepancyBIRDSTRIKE ON TAKEOFF ON L1 WINDOW, RETURNED BACK TO BZN. ALL ENGINES PARAMETERS NORMAL AND NO ABNORMAL ODORS, FOUND BIRDSTRIKE ON UPPER LT CORNER OF RADOME, CLEANED DEBRIS AND C/W BIRDSTRIKE INSP IAW AMM 05-51-18. NO DAMAGE FOUND AND INTERNAL INSP OF RADOMEJun 13, 2026 · N9003B · Boeing 7378 · Standard Practices/StructuresSDR SWAA2026071783960Flap · crackedCRACK INDICATION ON RT OTBD AFT FLAP INBD CARTRIDGE RADIUS ZONE. EVALUATED OTBD AFT FLAP INBD CARTRIDGE AND DID NOT FIND ALLOWABLE DAMAGE IAW SRM 57-53-02-1A-4 AND REPLACED OTBD AFT FLAP AT RT WING IAW AMM 27-51-26/401. INSTALLATION IS DOCUMENTED ON TTG8Q01Jun 13, 2026 · N930WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026071793471Access Panel · delaminatedDELAMINATED ACCESS PANEL 642EB AT RT WING. PERFORMED PERMANENT REPAIR ON ACCESS PANEL 642EB RT WING IAW EA 26-157-01758- WIP 1 AND STEP ARE DOCUMENTED ON FAULT TTG8Q01CZBT5.Jun 13, 2026 · N930WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026071788272Access Panel · damagedELONGATED HOLES ON PLATE ACCESS PANEL 644BB AT RT WING. REPLACED PLATE ON ACCESS PANEL 644BB AT RT WING IAW SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G-0.Jun 13, 2026 · N930WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026071704707Web · crackedCRACK ON WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING# 143A1222 SHEET 58 REV:-.Jun 13, 2026 · N930WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026071607247Rib · crackedCRACK INDICATION ON LT OTBD AFT FLAP INBD CARTRIDGE RADIUS ZONE.CRACK LENGHT 0.250 IN APPROX. LEFT WING. REPLACED OTBD AFT FLAP INBD CLOSURE RIB LT WING IAW SRM 51-10-02, ITEM 9; FOR CARTRIDGE ASSEMBLY INSTALLATION SEE TTG8Q01BR3XMJun 13, 2026 · N930WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026071600476Rib · crackedCRACK INDICATION ON RT OTBD AFT FLAP INBOARD CLOSURE RIB RADIUS ZONE.CRACK LENGHT 0.250 IN APPROX. RIGHT WING. EVALUATED OTBD AFT FLAP INBD CLOSURE RIB (CARTRIDGE) RT WING AND NOT FOUND ALLOWABLE DAMAGE IAW SRM 57-53-02-1A-4 AND REPLACED OTBD AFT FLAP AT RT WIJun 13, 2026 · N930WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026070711868Sign · inoperativeEMERGENCY EXIT SIGN HAS 1 BULB INOP AT THE R1 DOOR. REPLACED EMERGENCY EXIT SIGN ASSEMBLY IAW AMM 33-51-01-960-802; TEST PASSED. VERIFIED REPLACED EMERGENCY EXIT SIGN ASSEMBLY IAW AMM 33-51-01-960-802; TEST PASSED.Jun 13, 2026 · N8634A · Boeing 7378H4 · Emergency LightingSDR ASAA2026061366974Plate · corrodedFWD CARGO RT SIDEPLATE HAS CORROSIO FROM BS 500A - 500I. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO RT SIDEPLATE FROM BS 500A TO 500I IAW SRM 51-40-02-0G-0.Jun 13, 2026 · N548AS · Boeing 737890 · Fuselage Main, StructureSDR AALA202606266465Transmitter · inoperativeAIRCRAFT WAS GROUNDED: FLAPS WOULD NOT EXTEND PAST 1 WITH HANDLE IN 5,10,15 POSITION. DID ALTERNATE FLAP EXTENSION TO GET FLAPS TO 15 FOR NORMAL LANDING. EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LT FLAP POSITION TRANSMITTER IAW Jun 13, 2026 · N342PM · Boeing 737823 · Trailing Edge Flap Control SystemSDR ASAA2026061366858Window Frame · damagedRIGHT FUSE EXT, MAIN CABIN WINDOW BELT FWD UPPER EDGE HAS STATIC DISCHARGE DAMAGE, BS 500J- BS 500K, S11RH-S12R. GROUNDED - YES. REMOVED WINDOW FRAME BETWEEN BS 500J - BS 500K; BETWEEN S-11R-S-13R IAW B737-9MAX SRM 51-40-02, RECEIVED NEW P/N 143A4100-4 PO:1148Jun 13, 2026 · N723AL · Boeing 7379 · Fuselage Main, StructureSDR AALA202606244865Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER, CREW DOOR CUT OUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.Jun 13, 2026 · N9012 · Airbus A319115 · Fuselage Miscellaneous StructureSDR SWIA2026061376293Slat Track · chafedLEFT WING SLAT TRACK 3-1 IS CHAFED. REPAIRED LT WING SLAT TRACK 3-1 IAW REO 670-57-42-2474 REV -.Jun 13, 2026 · N703SK · Cndair CL6002C11 · Leading Edge DevicesSDR SWIA2026061376285Slat Track · chafedLEFT WING SLAT TRACK 1-3 IS CHAFED. COMPLIED WITH REPAIR OF LT WING SLAT TRACK 1-3 IAW REO 670-57-42-2473 REV -.Jun 13, 2026 · N703SK · Cndair CL6002C11 · Leading Edge DevicesSDR SWIA2026061376250Slat Track · chafedLEFT WING SLAT TRACK 2-1 IS CHAFED. COMPLIED WITH REPAIR OF LH WING SLAT TRACK 2-1 IAW REO REO 670-57-42-2485 REV--. COMPLIED WITH 51-900-1002-SKY.Jun 13, 2026 · N703SK · Cndair CL6002C11 · Leading Edge DevicesSDR IPXA2026061846827Bearing · wornWORN BEARING, NR 2 PYLON R/H AFT FAIRING DOOR NR 4 HINGE FITTING. (REPLACE). INSTALL LOCK FASTENERS ON NEW HINGE IAW SRM 51-40-02-0G REV. 95 AND DWG 313T3340 SH. 56 REV. -. REVIEWEDJun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon, Main Frame