Service difficulty reports

1,771,708 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 SWIA2026051277174Skin · corrodedEXTERNAL SKIN FROM BS 559.80 - 559.112, STR 21R - 24R HAD EVIDENCE OF CORROSION. REPAIRED EXTERNAL SKIN FROM BS 559.80 TO 559.112, STR 21R -24R IAW REO 601R-53-51-745 REV --, AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE.May 12, 2026 · N455SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR 4VAA202605120017Spar · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT ELEVATOR FORWARD SPAR AND RIBS, AND THE EMER PITCH TRIM ACTUATOR BRACKET. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060708.May 12, 2026 · N749SA · Saab 2000SAAB · Elevator, Spar/RibSDR 4VAA202605130015Mount · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RUDDER FRONT SPAR LEFT HAND AND RIGHT HAND LEADING EDGE PANEL MOUNT SCREW HOLES. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060677.May 12, 2026 · N749SA · Saab 2000SAAB · Rudder Miscellaneous StructureSDR 4VAA202605120013Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT AIR CYCLE MACHINE BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060669.May 12, 2026 · N749SA · Saab 2000SAAB · Fuselage Miscellaneous StructureSDR 4VAA202605120012`Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT HAND AIR CYCLE MACHINE BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060669.May 12, 2026 · N749SA · Saab 2000SAAB · Fuselage Miscellaneous StructureSDR 4VAA202605120009Frame · crackedDURING INSPECTION, A CRACK WAS FOUND AT LEFT LOWER FRAME FORWARD WING BOX. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060707.May 12, 2026 · N749SA · Saab 2000SAAB · Fuselage Main, FrameSDR SWAA2026061597632Rib · crackedRT HORZ STAB L/E 341B 4TH RIB FROM I/B CRACKED AT LE STA 105.26. CRACKED RIB FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN SRM. .REMOVED AND REPLACED RT HORZ STAB L/E 4TH RIB FROM I/B AT L/E STA 105.26 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWGMay 12, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026061597865Skin · crackedCRACK ON RT LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90. CRACKED WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGE AND REPAIRED AS PER SRM 55-10-01-2R-11 REP 11.May 12, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR IPXA2026070254508Seal Depressor · brokenLOWER FORWARD CRG DOOR SEAL DEPRESSOR WITH MINOR DAMAGE. REVIEWED TASK PER GMM-MTX 09.05.01.09. INSTALLED NEW SEAL I.A.W SRM 51-40-02-0G REV.107 AND BOEING DWG NO: 65B04220 SH 2 REV.F.May 12, 2026 · N583UP · Boeing 7474R7F · Cargo/Baggage DoorsSDR AALA202607013475Light · brokenAIRCRAFT IN BASE MAINTENANCE: BROKEN EMERGENCY LIGHT PREMIUM ECONOMY SEATS ROW 15 DEGH RH SIDE IN PASSENGER CABIN. MAINTENANCE REPLACED EMERGENCY LIGHT PREMIUM ECONOMY SEATS ROW 15 DEGH RH SIDE IN PASSENGER CABIN IAW B777 AMM 33-51-05-960-802 STEP C.(1) AND B7May 12, 2026 · N777AN · Boeing 777223 · Emergency LightingSDR VNAA202607010014Lug · corrodedCORROSION AND WEAR ON LH AILERON BORE LUGS OF HINGES 2 AND 3 (6EA) L1=[AIL STA=336.4015], L2=[AIL STA=337.657], L3=[AIL STA=338.424], L4=[AIL STA=342.123], L5=[AIL STA=342.911], L6=[AIL STA=344.1665]. L4=[AIL STA=342.123] WAS CLEANED PER SRM 51-26-00-001-001-AMay 12, 2026 · N530EA · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNA2026F00008Striker · wornWEAR ON FORWARD BAGGAGE BAY DOOR SURROUND AT FS=533.00 AND SGTR=23L TO SGTR=22LER, SRM 53-11-43-201-001-A01. FORWARD BAGGAGE BAY DOOR SURROUND (STRIKER SEAL) AT FS=533.00 AND SGTR=23L TO SGTR=22L WAS BLENDED OUT AND WAS EVALUATED, DAMAGE IS 80% OF ORIGINAL THMay 12, 2026 · N530EA · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA202606300012Web · crackedCRACK ON LH ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT. CRACK ON LH ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ 700 SRM 53-1May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202606300011Access Panel · corrodedCORROSION AT SETTLEMENT AREA OF ACCESS PANEL 542BZ ,542AZ AND 642AZ. CORROSION AT SETTLEMENT AREA OF ACCESS PANEL 542AZ WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER SRM 53-00-00-101-001-A01. ACCESS PANELS 542BZ AND 642AZMay 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202606300010Skin · corrodedCORROSION ON SETTLEMENT AREA OF E/E COMPARTMENT DOOR AT EXTERNAL SURROUND. SETTLEMENT AREA OF E/E COMPARTMENT DOOR AT EXTERNAL SURROUND WAS REPAIRED PER REO 670-53-21-242 REV. -CMay 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202606300009Diaphragm · crackedCRACK ON RH DIAPHRAGM OF MAIN WHEEL WELL BIN SUPPORT FS 797.00 AND RBL34 AT RH MAIN WHEEL WELL AREA. CRACK ON RH DIAPHRAGM OF MAIN WHEEL WELL BIN SUPPORT FS 797.00 AND RBL34 AT RH MAIN WHEEL WELL AREA WAS REPLACED PER SRM 51-41-02-001-001-A01.May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202606300008Support · crackedCRACK ON ATTACHMENT ANGLE OF DIAPHRAGM AT SUPPORT OF AFT WING TO FUSELAGE FAIRING LT SIDE, FS909. THE ATTACH ANGLE OF DIAPHRAGM AT SUPPORT OF AFT WING TO FUSELAGE FAIRING LT SIDE, WAS REPAIRED IAW REO 670-53-82-478, REV -A.May 12, 2026 · N530EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202606300007Attach Angle · crackedCRACK ON ATTACHMENT ANGLE INNER SKIN-TO-AFT SIDE PANEL NEAR TO PULLEY SUPPORT AT PASSENGER DOOR EXTERNAL STRUCTURE. ATTACHMENT ANGLE INNER SKIN-TO-AFT SIDE PANEL NEAR TO PULLEY SUPPORT AT PASSENGER DOOR EXTERNAL STRUCTURE WAS REPAIRED PER CRJ-700 SRM 52-11-04May 12, 2026 · N530EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWAA2026062998042Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE CRACKED AT AFT EDGE. ACCOMPLISHED REPAIR OF CRACKED FSD SCUFF PLATE PER SRM 53-10-15-2R-2. SCUFF PLATE WILL BE INSTALLED BY TASK TTG8Q002E2N5. ] RII N/A DUE TO SRM 53-10-15-2R-2 4.B. NOTE, THIS ITEM IS NOT A STRUCTURAL PART.May 12, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR DALA2026062903821Smoke Detector · false activationATB- AIR RETURN DUE TO AFT LAV SMOKE DETECTOR ALARMING. PLACED ON MEL FOR DISPATCH AND LATER REPLACED THE SMOKE DETECTOR. (LOG PAGE 8900488 - AIRCRAFT WAS GROUNDED).May 12, 2026 · N391DA · Boeing 737832 · Smoke DetectionSDR SIMA2026062500001Battery · inoperativeFWD SERVICE DOOR LOWER EMERGENCY LIGHT INOP COMPLETE:REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT PER EMB 175 AMM 33-50-01. BONDING CHECK GOOD AND OPS CHECK GOOD. MILLIOHM METER MCN-10685 DUE 10-24-26. SEE WIPS AND TASKS FOR WORK PERFORMEDMay 12, 2026 · N299JJ · Emb ERJ170200LR · Emergency LightingSDR SWAA2026061897994Floorbeam · corrodedCORRODED FLOORBEAM BS 947.5, LBL 25, WL 208.1 AT AFT GALLEY AREA. THIS REPAIR HAS BEEN ACCOMPLISHED IAW SRM 53-70-51-2R-5 ALTERNATIVE 2 WITH A MINOR DEVIATION CONSIDERED ACCEPTABLE AS PER EA 26-153-01390.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026061897652Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061897653Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT I.A.W. B737-800 S.R.M 53-30-15-2R-1 REPAIR 1 AND BAC 5975 SEE INDIVIDUAL SIGN OFF BELOW. RII COMPLETED.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061897996Intercostal · corrodedCORROSION INTERCOSTAL LOCATED BTW BS947.5 TO BS967 LBL53 AND WL208.1 AT AFT GALLEY AREA. REPLACED INTERCOSTAL LOCATED BTW BS947.5 TO BS967 LBL53 AND WL 208.1 AT AFT GALLEY IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. AND DWG 147A5650 SHEET 54 REV A.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061897995Intercostal · corrodedCORROSION INTERCOSTAL BTW BS 947.5 - BS 967, RBL 52, WL 208.1 IN THE AFT GALLEY AREA. REPLACED INTERCOSTAL IAW SRM 51-10-02 ITEM 9 AND DWG 147A5650 SHEET 71 REV A:May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061897997Web · corrodedCORRODED WEB, BS 986.5 + 4 INCHES, LBL 43, WL 208.1 IN THE AFT GALLEY AREA. FAULT RESOLVED ON OTHER FAULT TTG8Q01C650B.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061897990Floorbeam · corrodedCORRODED FLOORBEAM, BS 947.5, LBL 53, WL 208.1 IN THE AFT GALLEY AREA. REPAIRED THE UPPER TEE FLOORBEAM WILL BE INSTALLED ON FAULT TTG8Q01C5CAC IAW SRM 53-70-51-2R-5, REPAIR 5.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026061897869Floorbeam · corrodedCORRODED FLOORBEAM, BS 986.5, LBL 43, WL 208.1 IN THE AFT GALLEY AREA. PERFORMED REPAIR ON FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026061897870Floorbeam · corrodedCORROSION FLOORBEAM, BS 986.5, RBL43, WL 208.1 IN THE AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.May 12, 2026 · N500WR · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026061897998Access Panel · delaminatedDELAMINATED WING TO BODY FAIRING ACCESS PANEL 191CR INTERNAL AREA AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191CR INTERNAL AREA AT LOWER FUSELAGE IAW SRM 51-70-04-2R-6, REPAIR 6.May 12, 2026 · N500WR · Boeing 7378H4 · Aerodynamic FairingsSDR ASAA2026051266694Sidewall Support · crackedAFT CARGO LT UPPER SIDEWALL SUPPORT CARCKED AT BS 727D. GROUNDED - YES. REPAIRED AFT CARGO LT UPPER SIDEWALL SUPPORT AT BS 727D, 727C, 727B, 727F, 727G, & 727E IAW EA 800-53EA-30312.May 12, 2026 · N584AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026051266693Transition Panel · corrodedFWD CARGO RT TRANSITION CORRODED STA 500A TO STA 500I. GROUNDED - YES. REMOVED DAMAGE ON FWD CARGO R/H TRANSITION FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2. REMOVED AND REPLACED TRANSITION PANEL IAW B737-800 SRM 51-40-05-0G-0 AND 51-40-02-G-0.W:May 12, 2026 · N584AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 2026FA0000518Fire Detector · faultedRIGHT ENGINE FIRE ANNUNCIATION ILLUMINATED ON DESCENT INTO CMH. ANNUNCIATION ILLUMINATED AND DISAPPEARED CONTINUOUSLY. SEEMED TO SUBSIDE SOMEWHAT AT STRAIGHT AND LEVEL. TEMPS WERE NORMAL. AIRCRAFT TOOK OFF OUT OF SDF AND LANDED IN CMH.May 12, 2026 · N392L · Diamon DA42NG · Fire DetectionSDR WX0A2026051332813Cover · missing(AIRCRAFT NOT GROUNDED) EPSU BATTERY COVER MISSING AT ROW 17DEF. INSTALLED NEW LOWER SIDEWALL PANEL AT ROW 17DEF IAW AMM 33-51-38-400-001-A. THIS CLEARS MDDR 231401. NEF LOG UPDATED.May 12, 2026 · N305NV · Airbus A319112 · Emergency LightingSDR IPXA2026061144531Floorbeam · corrodedWHILE WORKING FAULT T3F18E008T21R FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT STA. 1200 LBL 45.5 TO 62.2. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97555-REQ1 AND VT-SAA EA 757-5360-01-B0745, REV IRMay 12, 2026 · N417UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR SWAA2026061197596Support Angle · crackedFORWARD CARGO RT TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA 500D TO STA 500E IS CRACKED. REMOVED AND REPLACED FORWARD CARGO RH TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA 500D TO STA 500E PER SRM 51-40-02.May 12, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061197971Support Angle · crackedFWD CARGO RT TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA.500C TO 500D IS CRACKED. REMOVED AND REPLACED FORWARD CARGO RH TRANSITION ANGLE SUPPORT BAFFLE BETWEEN BS 500C TO 500D IAW SRM 51-40-02.May 12, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026060253330Bulkhead · gougedMAJOR REPAIR, NR 2 PYLON AFT BULKHEAD LT SIDE REINFORCMENT FITTING IS GOUGED COMPLIED WITH EO-97567-REQ1 AND VT-MAE EA 757-5453-27-A4500, REV.-May 12, 2026 · N423UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/FirewallSDR ASAA2026051266654Transition Panel · corrodedAFT CARGO L/H TRANSITION STA 847 TO STA 727 CORRODED. GROUNDED - YES. REMOVED CORROSION TRANSITION PANEL FOUND TO BE OUT OF LIMITS, REPAIRED TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5W: 1" O: .040 R: .027 L: 1.5" D: .013.May 12, 2026 · N584AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026051266653Web · corrodedAFT CARGO SILL WEB CORRODED STA 847 TO STA 787. GROUNDED - YES. REMOVED DAMAGE ON SILL WEB AFT CARGO STA 847 TO STA 787 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW B737-800 SRM 51-40-02-0G-0 AND 51-40-05-0G-0W: 2" O: .050" R: .041" L: 2" D: .009".May 12, 2026 · N584AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR AALA202606116237Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD AFT FLAP OUTBOARD BOTTOM CORNER SKIN DELAMINATED. REPLACED SKIN PER TI575309-601R1.May 12, 2026 · N901AN · Boeing 737823 · Trailing Edge FlapsSDR SWAA2026061098179Lens · brokenBROKEN EMERGENCY EXIT LENS (WITHOUT ARROW) LAVATORY A AT FWD GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS (WITHOUT ARROW) LAVATORY A AT FWD GALLEY AREA (1 EA) IAW AMM 33-51-01-960-802, STEP 3.C,.(5)(D) AND 3.C.(10).May 12, 2026 · N7749B · Boeing 7377BD · Emergency LightingSDR SWAA2026061098180Lens · brokenBROKEN EMERGENCY EXIT LENS (WITHOUT ARROW) GALLEY 1 AT FWD GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS (WITHOUT ARROW) GALLEY 1 AT FWD GALLEY AREA (1 EA) IAW AMM 33-51-01-960-802 STEP 3.C.(5)(D) AND 3.C.(10).May 12, 2026 · N7749B · Boeing 7377BD · Emergency LightingSDR SWAA2026061098183Lens · brokenBROKEN EMERGENCY EXIT LENS (WITHOUT ARROW) LAVATORY B AT AFT GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS IAW AMM 33-51-01-960-802, STEP 3.C.(5)(D), & 3.C.(10).May 12, 2026 · N7749B · Boeing 7377BD · Emergency LightingSDR SWAA2026061097755Scuff Plate · crackedCRACK AFT POSITION CORNER SCUFF PLATE CUT OUT DOOR AT FWD CARGO COMPARTMENT. REPAIRED AFT POSITION CORNER SCUFF PLATE CUT OUT DOOR OF FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1 REPAIR 1, AND BAC 5975.May 12, 2026 · N7749B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2026061097915Access Panel · crackedCRACK ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-2 REPAIR 2.May 12, 2026 · N7749B · Boeing 7377BD · Aerodynamic FairingsSDR SWAA2026061097913Access Panel · crackedCRACKED SEAL BLADE ACCESS PANEL 431AL AT LT PYLON. REPLACED SEAL BLADE ACCESS PANEL 431AL AT LT PYLON IAW SRM 51-10-02-0G-0, ITEM 9, & SRM 51-40-02-0G-0.May 12, 2026 · N7749B · Boeing 7377BD · Nacelle/Pylon, Plate/SkinSDR SWAA2026061097912Angle · crackedCRACKED ANGLE LOCATED INBD SIDE OF RT WING INBD AUXILIARY TRACK SLAT 6. REPLACED ANGLE LOCATED INBD SIDE OF INBD AUXILIARY TRACK SLAT 6 AT RT WING SRM 51-40-02, AND DWG 114A5030, SHEET 2 REV:C. MEASUREMENT OF CRACK: L: 2.400'.May 12, 2026 · N7749B · Boeing 7377BD · Wing Miscellaneous StructureSDR ASAA2026051266525Transition Panel · corrodedAFT CARGO RT TRANSITION CORRODED BS 727 TO 767. GROUNDED - YES. REMOVED CORROSION TRANSITION PANEL FOUND TO BE OUT OF LIMITS, REPAIRED TRANSITION PANEL IAW SRM 53-00-53-2R-5.May 12, 2026 · N584AS · Boeing 737890 · Fuselage Miscellaneous Structure