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 AALA202609211556Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: WING CENTER SECTION,REAR SPAR FORWARD SIDE UPPER VAPOR BARRIER ATTACH ANGLE IS CRACK,AT LBL 15, BS.663. ACCOMPLISHED PERMANENT REPAIR TO VAPOR BARRIER ATTACH ANGLE AT BS 663, LBL 15 IAW EA 378964.SDR IPXA2026092146237Lamp · inoperativeMAIN CARGO COMPARTMENT ENTRY, EMERGENCY LIGHTS INOP. RELAMPED AND OPS CHKD IAW AMM 33-51-00.SDR WX0A2026092132957Epsu · inoperative(AIRCRAFT NOT GROUNDED) BAT/EPSU(12WL) EMER R MESSAGE / REMOVED AND REPLACED EPSU BATTERY 12WL MESSAGE GONE, IAW AMM 33-51-38-00-002 AND 33-51-38-400-002"SDR DALA2026092105262Annunciator · inoperativeR1 DOOR WARNING ANNUNCIATION INOP. T/S PER B717 FRMFIM 52-70-00-810-809, PERFORMED PSEU BITE TEST, TEST PASSED, NO DEFECTS NOTED. PSEU SENSOR READOUT OK. (1823746) AIRCRAFT WAS GROUNDED.SDR ABXA20260921415Idg · faultedDURING ENGINE START AND TAXI, L ENG GEN DRIVE & DISC. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED LT ENGINE IDG IAW MEL 24-00-1-1. MBCB 09/24/26. REF ITEM 2, GEN DRIVE LIGHT INOP. MBCB 09/24/26. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.SDR JR2R20260921477Block · debondedRT APU IGNITOR CABLE BLOCK DISBONDED. REPAIREDSDR FDEA202609211390Stringer Splice · crackedMDCC FR 47, S-18L STRINGER SPLICE CRACKED. REPLACED THE STRINGER SPLICE AT MDCC FR47, S-18L PER A300-600F SRM51-40-21 & DWG.A53833157(ISSUE:F00). THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA202609211389Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -27.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICSDR FDEA202609211388Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -47.5 FOUND THE CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING SPLICES SDR FDEA202609211387Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -8.5 FOUND THE CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING SPLICES BSSDR FDEA202609211386Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 8.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BTWN EXISTING SSDR FDEA202609211385Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= 27.5 FOUND THE 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 BTWN BS 6-60 - SDR FDEA202609211384Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= 47.5 FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICES BSSDR FDEA202609211383Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= 47.5 FOUND THE 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, BS 969 - 1029,SDR FDEA202609211382Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= 8.5 FOUND THE 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, BS 989 - 1029, X=SDR FDEA202609211381Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= -8.5 FOUND THE CROWN WORN. SEAT TRACK BS 1010 X= -8.5", EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 989SDR FDEA202609211380Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1010 X= -47.5 FOUND THE CROWN WORN. SEAT TRACK EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 989 - 1029 X= -47.5" IAWSDR FDEA202609211379Floor Panel · puncturedONE PUNCTURE ON FLOOR ACCESS PANEL 252DFF OF MDC FLOOR ACCESS PANEL 252DFF OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAGRAPH 4.B FIGURE 201 REVISION NO.96 AUG 15/2026SDR FDEA202609211378Floor Panel · puncturedONE PUNTURE ON FLOOR ACCESS PANEL 231FFF OF MDC FLOOR ACCESS PANEL 231FFF OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAGRAPH 4.B FIGURE 201. REVISION NO.96 AUG 15/2026SDR FDEA202609211377Floor Panel · puncturedTWO PUNCTURES ON FLOOR PANEL 241AFF MDC FLOOR PANEL 241AFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAGRAPH 4.B FIGURE 201 REVISION NO.96 AUG 15/2026SDR FDEA202609211376Floor Panel · puncturedPUNCTURED FLOOR PANEL 232GFF IN THE MAIN DECK CARGO COMPARTMENT (ONE LOCATION) FLOOR PANEL 232GFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAGRAPH 4.B FIGURE 201 REVISION 96.SDR FDEA202609211375Floor Panel · puncturedPUNCTURED FLOOR PANEL 231GFF IN THE MAIN DECK CARGO COMPARTMENT (ONE LOCATION) FLOOR PANEL 231GFF IN THE MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767SRM 53-00-50-2R PARAGRAPH 4.B FIGURE 201 REVISION NR 96SDR JR2R20260921420Stop Fitting · scratchedR2 DOOR CUT-OUT STRUCTURES 2ND UPPER DOOR STOP SCRATCHED ON UPPER SURFACE. REPAIRSDR REXA2026110402025Rib · crackedCRACK ON MACHINED RIB, LEADING EDGE SS58.41 RT WING. THE RIB WAS REPLACED IAW SRM 51-42-13-001-001-A01, SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.SDR AALA202611032597Fitting · burredAIRCRAFT IN BASE MAINTENANCE: BURRED RACK 80VU MATERIAL ON LOWER LATERAL FITTING LH IN AFT AVIONIC COMPARTMENT. ACCOMPLISHED PERMANENT REPAIR OF RACK 80 VU LOWER LATERAL FITTING LH SIDE IN AFT AVIONIC COMPARTMENT (1 E/A) IAW AARD 53-20-00-1.SDR AALA202611032385Fitting · burredAIRCRAFT IN BASE MAINTENANCE: BURRED RACK 80VU MATERIAL ON LOWER LATERAL FITTING RH IN AFT AVIONIC COMPARTMENT. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR OF RACK 80 VU LOWER LATERAL FITTING RH SIDE IN AFT AVIONIC COMPARTMENT (1 E/A) IAW AARD 53-20-00-1.SDR VNAA202610300029Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 211 ON GALLEY 2. FLOOR FITTING IN FWD ACCESS 211 ON GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-78 REV 16 DATE OCT 20/25SDR VNAA202610300028Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 1-11 ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 1-11 ON GALLEY 1 WAS REPLACED PER C&D ZODIAC CMM 25-33-66.SDR SWAA2026102798315Floor Panel · crackedCRACKED FLOOR PANEL 140BF IN THE AFT CARGO BAY. FABRICATED A FLOOR PANEL IN AFT CARGO BAY IAW AMM 25-52-01-201-801, AND DWG 453A2610, SHEET 3, REV C.SDR IPXA2026102242761Landing · crackedNR 2 INBD THRUST REVERSER UPPER PANEL LANDING HAS A CRACK. INSTALLED NEW SERVICABLE PANEL LANDING ANGLE PN LJ76226 AT NR 2 I/B TR IAW SRM 51-40-02-0G-0.SDR SWAA2026102158537Support · no discrepancyCORROSION ON THE LT WING OTBD T/E ON RAIL SUPPORT. PERFORMED A DETAILED VISUAL INSPECTION ON THE LT WING OTBD T/E RAIL SUPPORT IAW SRM 51-10-04, & NO FOUND CORROSION ONLY MISSING PROTECTIVE TREATMENT. THE APPLICATION SEE TTG8Q01ERA8A.SDR AALA202610202967Crease Beam · corrodedAIRCRAFT IN BASE MAINTENANCE: R1 DOOR - CREASE ANGLE IS CORRODED AT THE FWD END OF THE DOOR THRESHOLD STA 296. REMOVED AND INSTALLED CREASE ANGLE IAW BOEING DRAWING 141A8316 AND AARD 51-00-05-1.SDR SIMA20260920002Seat Track · corroded1 EA IB RH SEAT TRACK AT FR 17 HAS CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION) PERFORMED CUTOUT AND FILLER AND DOUBLER REPAIR OF IB RH SEAT TRACK AT FR 17 IAW EMB 175 SRM 53-10-10/REPAIR 01P RESTORED SURFACE PROTECTION IAW EMB SRM 51-23-04,51-23-05,51-23-06SDR AALA202610191644Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: LH TRANSITION PANEL HAS MULTIPLE AREAS OF CORROSION FROM STA.500D+12 TO STA.500I. REMOVED AND REPLACED IAW AARD 51-00-05-1 AND BOEING DWG 143A7500.SDR AALA202610193202Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: LH TRANSITION PANEL HAS MULTIPLE AREAS OF CORROSION FROM STA.500-500D+12. REMOVED AND REPLACED LH TRANSITION PANEL IAW SRM 51-40-02.SDR AALA202610197357Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION IN AFT CARGO ON TRANSITION PANEL AT STA 747 TO STA 767 RBL25. REMOVED AND REPLACED TRANSITION PNL IAW BOEING DRAWING 146A7500, AARD 51-00-05-01.SDR AALA202610199696Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: L1 DOOR - FWD GIRT BAR FITTING SUPPORT BRACKET IS CORRODED STA 312. REMOVED AND REPLACED GIRT BAR FITTING IAW AARD 51-00-05-01 AND BOEING DWG 141A5220.SDR AALA202610190525Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: L1 DOOR - AFT GIRT BAR FITTING SUPPORT BRACKET IS CORRODED STA 344 . REMOVED AND REPLACED GIRT BAR FITTING IAW AARD 51-00-05-01 & BOEING DWG 141A5220.SDR AALA202610190888Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: SEVERAL SPOTS OF CORROSION ON TRANSITION PANEL. REMOVED AND REPLACED TRANSITION PANEL IAW BOEING DRAWING # 146A7500, AARD 51-00-05-01, AND SRM 51-40-05.SDR IPXA2026101639999Skin · corrodedLEFT WING UPPER SURFACE OUTBD FIXED TRAILING EDGE INBD AFT SIDE IS BULGING AROUND A FASTNER, POSSIBLE INTERNAL CORROSION. INSTALLED LANDING P/N UPA57246385200 AT LH WING IAW A300-600 SRM 51-40-21-001.SDR SWAA2026101229388Access Panel · crackedCRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW SRM-51-40-02-0G-0 AND SRM-51-10-02-0G-0 ITEM 9.SDR SWAA2026101279104Fitting · deterioratedDETERIORATED PASSENGER SEAT TRACK FITTING AT SEAT ROWS 9 LEFT. REPLACED PASSENGER SEAT TRACK FITTING IAW CMM 25-21-42-3859, REV 07.SDR AALA202610084568Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: IN THE FORWARD CARGO, ON THE LH SIDE, THE BAFFLE FROM 500B TO 500C IS CRACKED. REMOVED AND INSTALLED L/H BAFFLE FROM 500B TO 500C IAW BOEING DRAWING 143A7505 SHEET 151 AND AARD 51-00-05-01.SDR AALA202610053334Intercostal · damagedAIRCRAFT IN BASE MAINTENANCE: DUE TO 947 T-CAP REPAIR, INTERCOSTAL AT STA. 947-967 RBL 52 REQUIRES REPLACEMENT. NEW INTERCOSTAL INSTALLED PER AARD 51-00-05-1 & DWG 147A5650.SDR AALA202610027632Baffle Angle · crackedAIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP CRACKED UNDER R/H TRANSITION PANEL, STA.500H, RBL25. REMOVED AND REPLACED THE CRACKED AFT BAFFLE CLIP AT STA 500H RBL25 IAW AARD 53-00-01-6.SDR AALA202610026644Shear Tie · crackedAIRCRAFT IN BASE MAINTENANCE: SHEAR TIE CRACKED UNDER L/H TRANSITION PANEL, STA 500I, LBL24. REMOVED AND REPLACED THE CRACKED SHEAR TIE AT STA 500I LBL24 IAW AARD 53-00-01-6.SDR AALA202610020914Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP CRACKED UNDER R/H TRANSITION PANEL, STA 500G, RBL25. REMOVED AND REPLACED THE CRACKED FWD BAFFLE CLIP AT STA 500G RBL25 IAW AARD 53-00-01-6.SDR AALA202610025329Shear Tie · crackedAIRCRAFT IN BASE MAINTENANCE: SHEAR TIE CRACKED UNDER R/H TRANSITION PANEL, BS 500I, RBL24. REMOVED AND REPLACED THE CRACKED SHEAR TIE AT STA 500I LBL24 IAW AARD 53-00-01-6.SDR AALA202610022982Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP CRACKED UNDER R/H TRANSITION PANEL, STA 500H, RBL25. REMOVED AND REPLACED THE CRACKED FWD BAFFLE CLIP AT STA 500H RBL25 IAW AARD 53-00-01-6.SDR AALA202609303067Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY UE TO WEAR - REPLACED HINGE FITTING PER CMM 52-81-18