Service difficulty reports
1,770,704 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2026092813491Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT, BS 328+5 - 328+12, LBL 22, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5730, REV A. NUT PLATE DEBONDED AND TWO FASTENERS ARE NOT INSTALLED AT BS 344, LBL 22. AFTER INTERCOSTAL INSTALLED SDR SWAA2026092887408Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT AT BS 294+15, RBL 10, WL 208. REMOVED CORROSION ON FLOOR SUPPORT AND FOUND OF OUT LIMITS. THE FLOOR SUPPORT WAS R & R IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV -.SDR SWAA2026092882375Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM AT SEVERAL LOCATIONS AT BS 328, RBL 55 TO LBL 14, WL 208. REPAIRED THE FLOORBEAM IAW SRM 53-10-51-2R-7, REPAIR-7.SDR SWAA2026092826684Floor Support · corrodedFOUND CORROSION ON THE FLOOR SUPPORT AT BS 328+12, LBL 44, WL 208. REMOVED THE CORROSION, AND FOUND OUT OF LIMITS. THE FLOOR SUPPORT WAS REMOVED & REPLACED IAW SRM 51-40-02-0G-0, & DWG 141A5730, REV A.SDR SWAA2026092832078Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT AT BS 312+5, RBL 11, WL 208. REMOVED THE CORROSION AND FOUND OF OUT LIMITS, THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02-0G-0, & DWG 141A5400, REV -.SDR SWAA2026092894716Support Angle · corrodedL1 DOOR SURROUND CORROSION FOUND ON I/B THRESHOLD SUPPORT ANGLE AT STA 318 AND STA 337. MARKED. REMOVED CORROSION AND FOUND OUT OF LIMITS. THEREFORE REMOVED AND REPLACED FED I/B THRESHOLD SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND DWG: 141A8110 REV -.SDR SWAA2026092878437Floor Support · corrodedFOUND CORROSION ON FLOOR SUPPORT AT BS 328+3, LBL 11, WL 208. R & R THE FLOOR SUPPORT BTWN BS 328 - 344 IAW SRM 51-40-05-0G-0, & DWG 141A5410, REV -.SDR SWAA2026092837465Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 291.5, S5R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02, AND DWG 141A1251, REV J.SDR SWAA2026092817782Support Angle · corrodedFOUND CORROSION ON FED LOWER MAIN DOOR SILL AT SEVERAL LOCATIONS, LBL 60, WL 208. ACCOMPLISHED A REPLACEMENT OF THE CORRODED PART ON FAULT TTG8Q01DW6VZ.SDR SWAA2026092811189Floor Support · corrodedCORRODED FLOOR SUPPORT, BS 312+5, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT BTWN BS 312 - 328 IAW SRM 51-40-02, AND DWG 141A5400, REV -.SDR SWAA2026092813205Angle · crackedFCB, INTERCOSTAL ANGLE AT BS 500I+1 RBL7 IS CRACKED. THE INTERCOSTAL ANGLE WAS REMOVED & REPLACED IAW SRM 51-40-02 AND DWG 143A7902 REV A. TOP RIVETED FASTENER BUCK TAIL IS TO HIGH AND DOES NOT FILL HOLE. DRILLED, R & R RIVET IAW SRM 51-40-02 AND DWG 143A79SDR SWAA2026092852100Bracket · corrodedFOUND CORROSION ON FED FWD ESCAPE SLIDE LATCH BRACKET AT BS 312, LBL 55, WL 208. FWD ESCAPE SLIDE LATCH BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, & DWG 141A5220 REV -.SDR SWAA2026092851407Support Angle · corrodedFCB, SIDEWALL SUPPORT BS 500A TO 500I RBL 25 CORRODED. REMOVED AND REPLACED THE FLOOR TO SIDEWALL SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7500, REV -.SDR SWAA2026092803969Support Angle · corrodedR1 DOOR SURROUND CORRODED ON THRESHOLD SUPPORT ANGLE BS 305, BS 310, BS 316 & BS 323. REMOVED CORROSION, FOUND OUT OF LIMITS. THRESHOLD SUPPORT ANGLE REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 141A8310 REV -.SDR SWAA2026092884647Angle · crackedFCB, INTERCOSTAL ANGLE AT BS 500D RBL25 IS CRACK. REMOVED AND REPLACED THE INTERCOSTAL CLIP AT FWD SIDE OF BS500D RBL25 WL156 IAW SRM 51-40-02 AND DWG: 143A7505 ID:0052 REV: -SDR SWAA2026092801665Support · corrodedFCB, AFT LOWER RT BULKHEAD SUPPORT AT BS 500I RBL26 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED THE FCB AFT LOWER RH BULKHEAD SUPPORT AT BS 500I IAW SRM 51-40-02 AND DWG# 143A9481 REV: -.SDR SWAA2026092836615Support Angle · corrodedL1 DOOR SURROUND CORROSION FOUND ON O/B THRESHOLD SUPPORT ANGLE AT STA 316 AND STA 326. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED FED THRESHOLD SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND DWG:141A8110 ID:0011 REV: -SDR SWAA2026092431706Support Angle · crackedCRACKED SUPPORT ANGLE ON ACCESS PANELS 834DZ AT THE AFT ENTRY DOOR. REPLACED THE SUPPORT ANGLE ON ACCESS PANELS 834DZ IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DRILLED SUPPORT ANGLE IAW SRM 51-40-05, & APPLIED PROTECTIVE TREATMENT OPEN NEW HOLE IAW SRM 51-20-01SDR SWAA2026092490877Support Web · crackedCRACKED SUPPORT WEB INBD FAN COWL, LT ENGINE. REPLACED FASTENERS & SUPPORT WEB ON THE INBOARD FAN COWL IAW SRM 51-40-02, SRM 51-10-02, & 71-13-30, PAGE 10094.SDR SWAA2026092457388Plate · damagedELONGATED HOLE ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 282 AT LT WING. EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 282 LT WING AND DID NOT FIND ALLOWABLE DAMAGE IN SRM 57-51-02-1A-1, AND REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 28SDR SWAA2026092432884Plate · damagedELONGATED HOLE ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226 AT LT WING. EVALUATED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226 AT LT WING AND NOT FOUND ALLOWABLE DAMAGE IN SRM 57-51-02-1A-1 AND REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 226SDR SWAA2026092313467Web · crackedWEB CRACKED AROUND FASTENER HOLE, BS 251+ 6 INCHES, RBL 5. PERFORMED A PERMANENT REPAIR BTWN BS 251 - 255, RBL 3.60 - 15.32 IAW SRM 51-40-02, & EA 26-153-02349.SDR HNAA2026092300896Shear Tie · crackedCABIN SHEAR TIE CRACKED AT FR-61 BETWEEN STGRS 6L/7L. REMOVED AND REPLACED CRACKED CABIN SHEAR TIE IAW SRM 51-40-02.SDR HNAA2026092300895Door Sill · corrodedCARGO DOOR SILL CORRODED IN MULTIPLE AREAS. R & R CARGO DOOR SILL IAW SRM 51-40-02.SDR HNAA2026092300893Floor Support · corrodedLEFT FLOOR SUPPORT NR 4 HAD CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092300892Floor Support · corrodedLEFT FLOOR SUPPORT HAD CORROSION IN MULTIPLE AREAS. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092300891Floor Support · corrodedRIGHT CABIN FLOOR SUPPORT NR 2 CORRODED IN NUMEROUS AREAS. R & R RT CABIN FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092300890Floor Support · corrodedLEFT CABIN FLOOR SUPPORT NR 2 CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED LH CABIN FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092300889Seat Track · corrodedLEFT UPPER SEAT TRACK NR 3 CORRODED IN NUMEROUS AREAS. R & R LT UPPER SEAT TRACK IAW AMM 53-01-06SDR SWAA2026092237462Web · corrodedFCB, CORROSION AT THRESHOLD BS 440 - 480+12, RBL 25. REMOVED AND REPLACED SUB THRESHOLD WEB BS 440 - 492, WL156, RBL25 IAW SRM 51-40-02-0G-0, & DWG 143A8330, REV B.SDR IPXA2026092117554Stiffener · crackedRIGHT WING, KRUEGER FLAP MOVABLE VANE, CRACK UNDER TEFLON STOP BASE. INSPECTED AND VERIFIED INSTALLATION OF STIFFENER ON RT WING KRUEGER FLAP MOVABLE VANE IAW SRM 51-40-21.SDR AALA202609158678Web · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND EXFOLIATION CORROSION AT THE CENTER OF THE WEB AT THE AFT CARGO DOOR OPENING. REPAIRED LOWER SILL WEB IAW AARD 51-00-05-1A AND BOEING DWG 146A8340.SDR IPXA2026090711902Panel · debondedTHE LT FWD TORQUE BOX PANEL HAS 2EA DELAMINATED, DISBONDED AREAS NEAR FSS 245.653 AND FSS 171.39. REMOVED ALL FASTENERS FROM LT FWD TORQUE BOX PANEL, EXCEPT MOST BOTTOM ROW, & BOTTOM AFT ROW, IAW SRM 51-40-02. INSTALLED NEW TORQUE BOX PANEL ON LT FWD IAW SRSDR IPXA2026090916126Strap · corrodedMAJOR REPAIR, APU INLET DOOR AFT STRAP HAD CORROSION. REMOVED OUTER STRAP IAW SRM 51-40-02-0G-0. INSTALLED NEW REPAIR PARTS AT INLET DOOR AFT STRAP IAW SRM 53-80-15-2R-1,REPAIR 1, DETAIL II.SDR IPXA2026083017738Screen · crackedAFT CARGO PANEL 152CZ SCREEN IS CRACKED. REMOVED CRACK SCREEN AND INSTALLED NEW SCREEN IAW AMM 25-50-03-404-003.SDR SWIA2026082577136Cable · rupturedRUPTURED AFT SERVICE DOOR SLIDE CABLE. REPAIRED AFT SERVICE DOOR EMERGENCY EVAC SLIDE CABLE IAW RS-2022-3017, REV IR.SDR IPXA2026090407154Flap Track · erodedERODED SKIN, LT WING NR 1 FLAP TRACK FWD FAIRING EXTERNAL SKIN. REMOVED THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-53-70-2R-1, REFER TO SRM 51-70-17-0G-0 REV. 96SDR SWAA2026090961984Access Panel · damagedELOGANTED HOLES ACCESS PANEL 561AB AT LT WING. REPAIRED THE ACCESS PANEL 561AB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW. TASK COMPLETED.SDR IPXA2026090907726Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. IAW AMM 52-11-26-004-001, REV 149 AND AMM 52-11-26-404-003, REV 149. REPLACED THE PAWL.SDR AALA202609092028Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL ACCESS PANEL 550AB INNER SIDE AROUND FASTENER HOLES - REPLACED FUEL ACCESS PANEL 550AB PER JOB CARD 26C54057020SDR IPXA2026090305035Angle · brokenRIGHT WING #8 SLAT MAIN TRACK PANELS (2EA) ARE LOOSE. AFTER A MORE DETAILED INSPECTION, 02 LOOSE RIVETS AND 01 BROKEN ANGLE WERE FOUND ON THE PANELS. 02 RIVETS WERE REMOVED AND REPLACED, BROKEN ANGLE REMOVED. IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW BRSDR IPXA2026090305799Firewall · crackedNR 1 ENG OTBD T/R INTERNAL TOP METALLIC PLATE IS CRACKED. REMOVED INTERNAL TOP METALLIC PLATE DAMAGED AND REMOVED SEAL RETAINER (FOR ACCESS). #1 ENG O/B T/R. IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED INTERNAL TOP METALLIC PLATE AND SEAL RETAINER. IAW B757-2SDR IPXA2026090314351Support Plate · corrodedFLOOR PANEL JOINT SKIN SUPPORT PLATE CORRODED BELOW NUT PLATE BS 1450 BETWEEN STRG 29-28 (BELOW FLOOR). REMOVED SPLICE STRAP BY SEVERELY EXFOLIATED AT AFT CARGO STA 1450 IAW SRM 51-40-02. INSTALLED NEW PART IAW SRM 51-40-02-0G.SDR IPXA2026090314733Strap · corrodedAPU INLET DOOR FWD STRAP HAS CORROSION. REMOVED FWD STRAP CORRODED I.A.W. B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW STRAP ON APU INLET DOOR FWD IAW B757-200PF SRM 51-40-02.SDR IPXA2026090314768Angle · corrodedAPU INLET DOOR FWD UPPER CORNER ANGLE AT BS 1787.45, S3R HAS CORROSION. REMOVED UPPER CORNER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW UPPER CORNER ANGLE APU INLET DOOR FWD UPPER BS 1787.45, S3R IAW SRM 51-40-02.SDR IPXA2026090514834Angle · corrodedAPU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 S-6R HAS CORROSION. REMOVED LOWER CORNER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW LOWER CORNER ON APU INLET DOOR BS 1787.45 S-6R IAW SRM 51-40-02.SDR IPXA2026090516057Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM BS 1787.45 TO 1825.00 S-3R HAS A CORROSION. REMOVED UPPER ANGLE CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NEW ANGLE UPPER ON APU INLET DOOR BS 1787.45 TO 1825, S3R IAW SRM 51-40-02.SDR AALA202609070085Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609070713Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609073756Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42