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 IPXA2026081704713Strap · corrodedAFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1560 AND BS 1580, LBL 24.75, INSTALLED NEW AFT CARGO BAY CEILING STABILIZATION STRAP APPROX BTW BS 1560 AND BS 1580, LBL 24.75. NO REPETITIVE INSPECTIONS REQUIREDJul 22, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR HNAA2026082400773Support · crackedFWD FUSE II, FRAME 8, STRINGERS 11-12R HAD CRACKED SUPPORT. R & R SUPPORT IAW SRM 51-40-02Jul 22, 2026 · N925AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026082136859Engine · hot startDURING START OF NR 2 ENGINE HAD A HOT START AT 475 BOX FLASHING, AUTO SHUT DOWN_ CHECKED INLET AND EXHAUST FOR DEBRIS. RAN ENGINE TWICE IAW AMM 71-00-00. NO ABNORMAL INDICATIONS NOTED ACFT OK TO CONTINUEJul 22, 2026 · N8658A · Boeing 7378H4 · Engine (Turbine/Turboprop)SDR SWAA2026082100872Floor Panel · corrodedCORRODED FLOOR PANEL 140CF. REMOVED & INSTALLED THE FLOOR PANEL IAW AMM 25-52-10-000-801, & AMM 25-52-10-400-801.Jul 22, 2026 · N7878A · Boeing 7377K9 · Fuselage Floor PanelSDR SWAA2026082180021Access Panel · corrodedCORRODED ACCESS PANEL 140DF IN THE AFT CARGO BAY. REMOVED & INSTALLED THE ACCESS PANEL IAW AMM 25-52-10-400-801.Jul 22, 2026 · N7878A · Boeing 7377K9 · Fuselage Miscellaneous StructureSDR AALA202608209434Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERCOSTAL AT STA 847 TO STA 867, STR 22L. MAINTENANCE REPLACED NTERCOSTAL AT STA 847 TO STA 867, STR 22L IAW AARD 51-00-05-1.Jul 22, 2026 · N904AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR IPXA2026081706388Strap · corrodedAPU INLET DOOR AFT STRAP HAS CORROSION . ACCOMPLISHED THE REPAIR PER EO-98314-REQ1 AND VT-MAE EA 757-5380-27-A4592, REV. -, PRIOR TO FURTHER FLIGHT. REVIEWEDJul 22, 2026 · N424UP · Boeing 75724APF · APU Exhaust SystemSDR IPXA2026081492838Retainer · corrodedLOWER HALF OF FUSELAGE LAVATORY DRAIN VALVE ORANGE HEATED GASKET BROKEN AND RETAINER IS CORRODED. FABRICATED NEW RETAINER IAW DWG 69-71690-3.Jul 22, 2026 · N424UP · Boeing 75724APF · Fuselage Main, StructureSDR SWAA2026081760834Light · inoperativeINOPERATIVE EMERGENCY LIGHT ON LAVATORY B. REPLACED EMERGENCY LIGHT IAW AMM 33-51-01-960-802. TESTED OK.Jul 22, 2026 · N952WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026081757527Scuff Plate · crackedCRACKED SCUFF PLATE AT ENTRY DOOR, AFT GALLEY. REPAIRED THE CENTER SCUFF PLATE IAW SRM 53-70-15-2R-1, REPAIR 1.Jul 22, 2026 · N499WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026081771897Angle · crackedCRACKED ANGLE, BS 500D, STR 28L, FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7902, SHEET 126, REV A.Jul 22, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR ASAA2026072268072Floor Support · crackedFWD WET INTERCOSTAL STA 277 TO STA 294.5 BL-0 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL I.A.W. B737-800 S.R.M. 51-40-02-0G-0.Jul 22, 2026 · N566AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026072268071Floor Support · crackedFWD WET AREA INTERCOSTAL STA 328 TO STA 344 LBL 47 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL I.A.W. B737-800 S.R.M. 51-40-02-0G-0.Jul 22, 2026 · N566AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR IPXA2026081102426Strap · corrodedRIGHT AFT CARGO CEILING STABILIZER STRIP FROM BS 1360-1440 HAS CORROSION. INSTALLED NEW PART IAW SRM 51-40-02-0G.Jul 22, 2026 · N424UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026081506117Floor Support · corrodedMAJOR REPAIR, AREA BELOW LAVATORY AT FR 11A SHOWS EVIDENCE OF CORROSION. THE FLOOR SUPPORT WAS REMOVED AND REPLACED (STEPS 11 THRU 25) USING RAW MATERIAL IAW SRM 53-12-15-001, FIG 19, ITEM 10, SRM 51-40-44-001, & SRM 51-40-21-00-001.Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR 1Q2R2026081620178Skin · chafedEXTERIOR SKIN AT 2 INCHES FWD OF BS 985, STR 27L HAS CHAFE DAMAGE. PERFORMED PERMANENT REPAIR IAW RFTS-129909, REV 0, AND REO 670-53-51-401, REV-.Jul 22, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR IPXA2026081100691Strip · corrodedRIGHT AFT CARGO CEILING STABILIZER STRIP FROM BS 1360-1460 HAS CORROSION. 33-024. CLEANED AREA STR-200- R/H AFT CARGO CEILING STABILIZER STRIP FROM STA. 1360-1460- IAW SOPM 20-30-03. INSTALLED NEW PART IAW SRM 51-40-02-0G.Jul 22, 2026 · N424UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR ASAA2026072267941Floorbeam · corrodedAFT WET AREA FLOOR BEAM 986 HAS CORROSION AT OTBD MOST HOLES, LT AND SIDE. GROUNDED - YES. REPAIRED AFT WET AREA FLOORBEAM IAW SRM 53-70-51-2R-6. W= 1" O= .150 R= .106 L= 1 1/2" D= .044.Jul 22, 2026 · N531AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2026072267940Floorbeam · corrodedAFT WET AREA FLOORBEAM BS 986 HAD CORROSION AT OTBD MOST HOES, RT SIDE. GROUNDED - YES. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6. W= 1" O= .150 R= .140 L= 1" D= .010.Jul 22, 2026 · N531AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2026072267938Floor Support · corrodedAFT WET AREA FLOOR SUPPORT STRUCTURE IS CORRODED BETWEEN BS 947-967 LBL 20. GROUNDED - YES. REMOVED AND REPLACED AFT WET AREA FLOOR SUPPORT STRUCTURE BETWEEN BS 947-967 LBL 20 IAW B737-800 SRM 51-40-02-0G-0, STEP 7.B & C. W: 2" / O: .066" /R: .034" /L: 2" /Jul 22, 2026 · N531AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026072267936Floor Support · corrodedFWD WET AREA FLOOR SUPPORT HAS CORROSION BETWEEN BS 294-312, BL 0. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT LIMITS, REMOVED AND REPLACED FWD WET AREA FLOOR SUPPORT BETWEEN BS 294-312 BL 0 IAW B737-800 SRM 51-40-02-0G-0 STEP 4. B & 7. W= 2" O=.170" R= .1Jul 22, 2026 · N531AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR IPXA2026080806602Sidewall Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1410 AND BS 1530, LBL 16 THRU LBL 24. INSTALLED REPAIR PARTS (DOUBLER AND FILLER) AT AFT CARGO BAY FLOOR STRUCTURE SIDE PANEL BS 1490, IAW SRM 51-70-13-0G-0. STEP Jul 22, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026080806726Floor Support · corrodedAFT CARGO BAY FLOOR SUPPORT HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1440 - 1520, RBL 2.90. INSTALLED THE CHANNEL -7 AT AFT CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 53-00-53-2R-1, REPAIR 1, FIGURE 201, SHEET 7, PARAGRAPH 4. M, N, O.Jul 22, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026080806744Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1440 AND BS 1520, RBL 7.55. INSTALLED THE CHANNEL -7 IN AFT CARGO BAY FLOOR SUPPPORT BTW BS 1460 - 1480, RBL 7.55, IAW SRM 53-00-53-2R-1, REPAIR 1, FIGURE 201, SHEET 7, PARAGRAJul 22, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR AALA202608112009Beam · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING, DEFLECTION PANEL, JUST AFT OF REAR SPAR, FWD SUPPORTROD HAS EXCESSIVE PLAY I14-006. UPON FURTHER EVALUATION THE PLAY WAS DUE TO THE FIXED TRAILING EDGE BEAM BEING WORN. MAINTENANCE REMOVED AND REPLACED THE FIXED BEAM P/Jul 22, 2026 · N352PS · Boeing 737823 · Wing Main, Frame StructureSDR IPXA2026080806462Sidewall Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1310 AND BS 1410, LBL 20 THRU LBL 24. INSTALLED AND FILLET SEALED SIDEWALL PANEL ASSY AT AFT CARGO BS 1310 TO 1410, LBL 20 THRU LBL 24, IAW SRM 51-40-02-0G-0, REV 1Jul 22, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026080706754Angle · corrodedMAIN CABIN FLOOR DECK PLATE LOWER SURFACE NUTPLATE RETAINERS CORRODED THROUGHOUT LT & RT AND CENTER SECTION BS 1680 TO 1720. INSTALLED, RESTORED SURFACE FINISH AND APPLIED CIC ON NEW ANGLE IAW SRM 51-40-02-0G-0, PAR 4, REV 125, DWG 146N5221 REV B, AMM 51-21-1Jul 22, 2026 · N438UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026080806775Angle · corrodedMAIN CARGO AFT DECK PLATE LOWER SURFACE STIFFENER EXFOLIATED RH SIDE BS 1720. INSTALLED, RESTORED SURFACE FINISH AND APPLIED CIC ON NEW ANGLE IAW SRM 51-40-02-0G-0, PAR 4, REV 125 20, DWG 146N5221, REV B, AMM 51-21-15-370-801, PAR 2, & AMM 51-24-09-377-001, PJul 22, 2026 · N438UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026080805617Sidewall Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1530 AND BS 1640, RBL 16 AND RBL 22. FABRICATED AND INSTALLED, 3EA DOUBLERS AT AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL, BTW BS 1530 AND BS 1640 RBL 16 AND Jul 22, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026080805640Sidewall Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1440 & 1530, RBL 16 AND RBL 24. INSTALLED LT SIDE PANEL TO AFT CARGO FLOOR STRUCTURE BTW BS 1440 & 1530, IAW SRM 51-40-02-0G-0.Jul 22, 2026 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SCNA20260811349Skin · corrodedFUSELAGE SKIN, BS 727 TO 887, S4L - CORRODED REPAIR. PERFORMED EA 53-0313, FUSELAGE SKIN REPAIR BS 727 - 887 STR.4L REPAIRED.Jul 22, 2026 · N5479A · Boeing 73783N · Fuselage Main, Plate/SkinSDR ASAA2026072267848Transition Panel · corrodedFWD CARGO PIT R/H TRANSITION PANEL STARTING AROUND STA 500C AND CONTINUING AFT TO REAR BULKHEAD PANEL HAS NUMEROUS AREAS OF CORROSION, GROUNDED - YES. BLENDED AWAY CORROSION ORIGINAL THICKNESS .040, MAT. LOSS AT GREATEST .009, NEW THICKNESS AT LOWEST .031, ARJul 22, 2026 · N921AK · Boeing 7379 · Fuselage Miscellaneous StructureSDR ASAA2026072267846Transition Panel · corrodedAFT PIT LEFT TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS747 AND BS727J+13. GROUNDED - YES. BLENDED AWAY CORROSION, ORIGINAL THICKNESS .040, MAT LOSS AT LOWEST .007 NEW THICKNESS .033, AREAS OUT OF LIMITS PER B737-MAX9 SRM 5Jul 22, 2026 · N921AK · Boeing 7379 · Fuselage Miscellaneous StructureSDR ASAA2026072267845Transition Panel · corrodedAFT PIT LEFT TRANSITION PANEL UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS727J+13 AND BS727+4 AS MARKS. GROUNDED - YES. BLENDED AWAY CORROSION, ORIGINAL THICKNESS .040, MAT LOSS AT GREATEST .017, NEW THICKNESS AT LOWEST .023. AREAS OUT OF LIJul 22, 2026 · N921AK · Boeing 7379 · Fuselage Miscellaneous StructureSDR SWAA2026081077485Floorbeam · crackedFLOORBEAM CRACKED AT BS 540, BL 0, WL 208. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-40-05-0G-0, AND DWG 143A0060, REV A. R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0, AND DWG 143A0060, REV AJul 22, 2026 · N497WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2026081083067Plate · damagedRIGHT WING REAR SPAR WIGGLE PLATE HAS OVERSIZED ATTACHMENT HOLES AT ORSS 259. R & R RT WING REAR SPAR WIGGLE PLATE ORSS 259 AT SMRO IAW SRM 51-40-02-0G, AND DWG 115A2001, REV-.Jul 22, 2026 · N497WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026081099954Plate · damagedLEFT WING REAR SPAR WIGGLE PLATE HAS OVERSIZED ATTACHMENT HOLES AT ORSS 259 REF TO FAULT TTG8Q01DAC7Z, WHERE EA 26-157-02020 ADDED AS A SUBTASK. THE FAULT WILL BE REPAIRED ON TTG8Q01DAC7Z WHERE EA 26-157-02020 WAS ADDED AS A SUBTASK.Jul 22, 2026 · N497WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026081038759Shield · corrodedCORROSION ON AFT CARGO BAY FWD SHIELD, BS 767+10, RBL 20, WL 156. RECEIVED NEW SHIELD. LOCATED AND DRILLED IAW SRM 51-40-05-0G, & DWG 146A0081, REV A. R & R FWD SHIELD BS 767+10, RBL 20 IAW SRM 51-40-02, & DWG 146A0081, REV A.Jul 22, 2026 · N497WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026080905349Web · crackedMAJOR REPAIR, NDT SUSPECTED CRACKS ON FRAME 40 FUEL TANK SIDE VERTICAL STIFFENERS VERIFIED, SEALING WILL BE COMPLETED UNDER NON-ROUTINE T3F18E009BG1C.Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR AALA202608101203Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING, DEFLECTION PANEL, INTERCOSTAL HAS CRACK AROUND FASTENER HOLE, O/B SIDE I14-007. MAINTENANCE REPLACED LEFT WING, DEFLECTION PANEL, INTERCOSTAL IAW B737 SRM 51-40-02.Jul 22, 2026 · N352PS · Boeing 737823 · Wing Miscellaneous StructureSDR DALA2026080704567Strut · corrodedLEVEL 2 CORROSION, CORROSION ON INTERCONNECTING STRUT RH WING (REFERENCE RII AMDS CARD 2751-9202-DE). REMOVED INTERCONNECTING STRUT ON RH WING UNSERVICEABLE CONDITION PN: D5757032200200, SN: 04647 AS PER A320 FAM AMM 27-51-44-000- 001-A STEP 1 THRU 3.D(1) ANDJul 22, 2026 · N378NW · Airbus A320211 · Fuselage Main, StructureSDR J7SA2026080400507Fce · faultedP-TRIM NML FAIL DURING TRIM TESTS. REPLACED FCE 2 AND PERFORMED SUCCESSFUL RIGGING AND OPS CHECK. WORK COMPLETED IAW EMB 505 AMM 27-03-01 AND 27-60-00.Jul 22, 2026 · N368FX · Emb EMB505 · Flight Control SystemSDR U5QA202607220173Engine · vibrationDURING DESCENT REDUCED POWER AND IMMEDIATELY FELT ENGINE VIBRATION. ITT STARTED TO RISE AND R ENGINE VIBRATION CAS APPEARED. ITT CONTINUED TO RISE AND EVENTUALLY LED TO ENGINE SHUTDOWN IN FLIGHT. MX R & R RT ENGINE.Jul 22, 2026 · N334JE · Bombdr BD1001A10 · Engine (Turbine/Turboprop)SDR BAGA2026080400002Doubler · corrodedHEAVY CHECK, REAR BARREL WASTE DOUBLER FOUND CORRODED, WASTE DOUBLER REPAIRED.Jul 22, 2026 · N206BZ · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR ASAA2026072267680Rail · corrodedFWD CARGO PIT, AFT BULKHEAD LOWER RAIL HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO PIT, AFT BULKHEAD LOWER RAIL IAW SRM 51-40-02, SRM 51-40-05, AMM 50-10-04, AND DWG 143A9481 REV-.Jul 22, 2026 · N707AL · Boeing 7379 · Fuselage Main, StructureSDR SWAA2026080312289Lamp · inoperativeFWD LT OVERWING DOOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED FAULTY FORWARD LEFT SLIDE/OVERWING EMERGENCY LIGHT LAMP AND TESTED IAW AMM 33-51-04-960-801. TEST PASSED.Jul 22, 2026 · N8829Q · Boeing 7378 · Emergency LightingSDR SWAA2026080310149Web · crackedLEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP CRACKED. REMOVED AND REPLACED LT WING TRAILING EDGE TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP IAW SRM 51-40-02, AND AIPC 57-50-00-36A.Jul 22, 2026 · N8545V · Boeing 7378H4 · Wing Miscellaneous StructureSDR BAGA2026080300001Skin · corrodedHEAVY CHECK - FWD MID FUSELAGE SKIN BETWEEN FR 34/FR35, STGR 36L 36R, FOUND CORRODED. CORROSION REMOVED AND DAMAGE REPAIREDJul 22, 2026 · N206BZ · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR MASA20260731183Seat Track · corrodedCFIII, UH I/B CORRODED SEAT TRACK AT FR 85 WAS REMOVED BY BLENING IAW ERJ 175 SRM 51-10-03 AND WAS FOUND TO BE WITH IN LIMITS IAW ERJ 175 SRM 53-23-10, TABLE 101, AD 01. MAX MATRL REMOVED DEPTH .003'' AND WIDTH .005". NRG #4502666-1000-0041. REV #53 DATED AUG-Jul 22, 2026 · N85355 · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR MASA20260731182Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS OF CF I, WET AREA, CORRODED FLOOR SUPPORT SILL R/H STRUCTURE, FR 14 R/H TO FR 12 R/H. RBL 48. REMOVED AND REPLACED IAW ERJ 175 SRM 51-41-02 AND SRM 51-43-02. NRC#4502666-1000-0039, REV#45 DATED MAY-MAY-28-2021.Jul 22, 2026 · N85355 · Emb ERJ170200LR · Fuselage Miscellaneous Structure