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.

SDR IPXA2026101980804Doubler · corrodedFRAME STA 1992 FWD AND AFT SIDES HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH WITH HEAVY DEBRIS ON BACK SIDE PLUGGING DRAIN HOLE. INSTALLED RING AND SPLICE AT FRAME STA 1992 IAW SRM 51-40-02-0G-0 AND DWG 148N1606.Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102080892Skin Panel · delaminatedAPU COMPARTMENT LT SIDE COMPOSITE SKIN PANEL SECTION BETWEEN BS 1918 AND 1941 DELAMINATED. PERFORMED REPAIR PER B757-200PF SRM 51-70-10-2R-4 REPAIR 4 (REPAIRS TO LARGE DAMAGE) FIG. 201 DETAIL A REV 126 USING B757-200PF SRM 51-70-10-2R-0 REV 126 REPAIRED GUIDESep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2026102080598Skin Panel · delaminatedAPU COMPARTMENT RT SIDE COMPOSITE SKIN PANEL SECTION BETWEEN BS 1918 & 1941 DELAMINATED. REPAIR FILLER AND DOUBLER MADE FROM 0.012-INCH-THICK 2024-T3 BARE AL SHT AND REPLACEMENT HONEYCOMB CORE MADE FROM BMS4-4 3-10N OR EQUIVALENT.B. REPAIRED PER SRM 53-80-01Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2026102993231Skin · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES, FOUND 2 CRACKS ON RIB 26 NOTED AND MARKED IN RED. CONFIRMED ACCOMPLISHED STEP 80 OF E.A.#: 300-5753-27-A4625 REV- PRELIMINARY 4 "REINSTALL HOISTING BRACKET WITH FASTENERS PER DRAWING REQUIREMENTS. IF FASTENER HOSep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102978857Frame · corrodedMAJOR REPAIR, AFT FUSLAGE FRAME STA 1963 FWD AND AFT SIDES AND ALL ATTACHING STRUCTURE CIRCUMFERENTIALLY HAVE AREAS OF CORROSION AND LARGE AREAS OF MISSING PROTECTIVE FINISH AND TOPCOAT. REMOVED 1EA ANGLE TO FACILITATE REMOVAL CORROSION ON FRAME AT STA 1963 Sep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, FrameSDR HNAA2026102901057Floor Support · corrodedLH FLOOR SILL AT FR 61 HAS CORROSION. REMOVED AND REPLACED LH FLOOR SILL AT FR 61 IAW EMB 145 SRM 51-40-02-PR.Sep 4, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026102901056Floor Support · corrodedRIGHT FLOOR SILL AT FR 66 HAS CORROSION. REMOVED BAD SILL AND INSTALLED NEW FROM STOCK RH FLOOR SILL AT FR 66 IAW SRM 51-40-02-PR, FAY SEALED MATING SURFACES. IAW SRM 51-20-01-PRSep 4, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR VNAA202610230076Aileron · corrodedAFTER REMOVAL BEARING AND BUCHINS THE RH AILERON CORROSION WAS FOUND INSIDE OF LUG BORE HINGE # 1 AND CENTER FITTTING BORES LUGS R 1, R 2, R 5 AND R 6 HINGE # 4 BORES LUGS UPPER AND LOWER ALSO NICKS ON HINGE LUGS R 1 AND R 2 IN EXTERIOR AT RH AILERON. HINGE #Sep 4, 2026 · N555NN · Cndair CL6002D24 · AileronsSDR VNAA202610230075Seat Track · corrodedCORROSION ON SEAT RAIL IN STGR 15L AND 797-847, 847-897, 897-969 AT CPAX. SEAT RAIL IN STGR 15L AND 797-847, 847-897, 897-969 WERE EVALUATED AND FOUND TO EXCESSIVE CORROSION PER CRJ-900 SRM 53-51-49-101-001-A01 AND WERE REPLACED PER AMM 53-00-49.Sep 4, 2026 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610230074Seat Track · corrodedCORROSION ON SEAT RAIL IN STGR 15R AND STA 744-761, 785-847, 847+32-942 AT CPAX. SEAT RAIL IN STGR 15R AND STA 744.15 TO 942 WERE EVALUATED AND FOUND TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ900 AMM 53-00-49Sep 4, 2026 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610230073Seat Track · corrodedCORROSION ON SEAT RAIL IN STGR 15R AND STA 485-533, 581-716, 661+90- 720 AT CPAX. SEAT RAIL STGR 15R BTW STA 485 TO STA 720 WERE EVALUATED AND FOUND TO EXCESSIVE CORROSION PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49Sep 4, 2026 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610230071Seat Track · corrodedCORROSION ON SEAT RAIL IN LBL 9 AND STA 379-485, 565-597, 661+32-677 AT CPAX. SEAT RAIL IN LBL 9 AND STA 379-485, 565-597, 661+32-677 AT CPAX WAS EVALUATED FOUND TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41Sep 4, 2026 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202610230070Seat Track · corrodedCORROSION ON SEAT RAIL IN LBL28 AND STA 421 TO 553 AT CPAX. SEAT RAIL IN LBL27 AND STA 421 TO 553 WERE EVALUATED AND FOUND TO EXCESSIVE CORROSION PER CRJ-900 SRM 53-21-49-101-001-A01 AND WERE REPLACED PER CRJ-900 AMM 53-00-49Sep 4, 2026 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102080618Skin Panel · delaminatedAPU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1941 AND 1963 DELAMINATED. REPAIR FILLER AND DOUBLER MADE FROM 0.012-INCH-THICK 2024-T3 BARE AL SHT AND REPLACEMENT HONEYCOMB CORE MADE FROM BMS4-4 3-10N OR EQUIVALENT. B. REPAIRED PER SRM 53-80Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026102380237Support Bracket · damagedALL APU COMPARTMENT R/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FINISH. RL037. REMOVED 03 EA SUPPORT BRACKETS AT APU COMPARTMENT STA 1885 BETWEEN BL 0 - RBL 30 WL 250.00 IAW B757-200PF SRM 51-40-02-0G-0. INSTSep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026101780235Bracket · corrodedALL APU COMPARTMENT L/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FINISH. INSTALLED 4EA NEW SUPPORT BRACKETS AT APU COMPARTMENT STA 1885 BETWEEN LBL 0 - LBL 30 WL 250.00 IAW B757-200PF SRM 51-40-02-0G-0.Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/ContainmentSDR SWAA2026101967807Plate · crackedWIGGLE PLATE COMMON TO ACCESS PANEL 651EB FOUND CRACKED. REMOVED AND REPLACED THE WIGGLE PLATE IAW SRM 51-40-02-0G-0, AND DWG 115A2001, REV A.Sep 4, 2026 · N8657B · Boeing 7378H4 · Wing Main, Frame StructureSDR I5PA2026090468801Sensor · faultyETOPS SIGNIFICANT REPORT AND EVENT. FLIGHT DECK TEMP REACHED 75 DEGREES FOR OVER AN HOUR. THE MIX MANIFOLD SENSOR WAS REPLACED. THE SUSPECTED UNSERVICEABLE MIX MANIFOLD SENSOR WAS CONFIRMED FAULTY DURING A BENCH CHECKSep 4, 2026 · N688SL · Boeing 757230 · Cabin Temperature Control SystemSDR IPXA2026101680268Support Bracket · damagedALL ELECTRICAL WIRE BUNDLES, POWER FEED CABLES AND FLUID LINE SUPPORT BRACKETS ATTACHED TO APU COMPARTMENT FWD BULKHEAD STA 1885 HAVE CORROSION AND MISSING PROTECTIVE FINISH. RL035. INSTALLED 3 EA SUPPORT BRACKETS P/N 287N4802-75 AT APU COMPARTMENT FWD BULKHESep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR HNAA2026101500983Skin · crackedSKIN CRACK AT RIVET LOCATED AT FR77 BTW STR2-3LSep 4, 2026 · N650AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR HNAA2026101500982Skin · crackedSKIN HAS CRACK AT RIVET LOCADED AT FR72 BTW STR2-3L. REPAIRED SKIN IAW SRM 53-32-01RESep 4, 2026 · N650AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SWAA2026101461993Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL, WING TO BODY FAIRING. REPAIRED THE W-B FAIRING ACCESS PANEL 193CL IAW SRM 51-70-05-2R-10, REPAIR 10.Sep 4, 2026 · N8656B · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2026101403330Floor Panel · corrodedCORRODED FLOOR PANEL 140DF. REPLACED THE FLOOR PANEL IAW SRM 51-10-02, AND DWG 453A2610, SHEET 13, REV B.Sep 4, 2026 · N8656B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026101409901Access Panel · delaminatedDELAMINATED ACCESS PANEL 444BR ON RT PYLON. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.Sep 4, 2026 · N8656B · Boeing 7378H4 · Nacelle/Pylon, Plate/SkinSDR SWAA2026101413738Floor Panel · corrodedCORRODED FLOOR PANEL 140CF. REPLACED THE FLOOR PANEL IAW SRM 51-10-02, ITEM 9, & DWG 453A2610, SHEET 12, REV C.Sep 4, 2026 · N8656B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026100917915Floorbeam · corrodedCORRODED FLOORBEAM, BS 947.5, RBL 50, WL 208.1. PERFORMED A PERMANENT REPAIR CATEGORY A ON THE FLOORBEAM BS 947.5 BTWN RBL 30 - 58.60 IAW SRM 53-70-51-2R-5, REPAIR 5, ALTERNATIVE 2.Sep 4, 2026 · N8715Q · Boeing 7378 · Fuselage Main, Floor BeamSDR SWAA2026100996673Floorbeam · corrodedCORRODED FLOORBEAM, BS 947, LBL 23, WL 208.1. REPAIRED UPPER TEE OF THE FLOORBEAM BS 947.5 BTWN LBL 2 - 58.60, WL 208.1. REPAIR WILL BE INSTALLED ON FAULT TTG8Q01E4RVD IAW EA 26-153-02558-WIP1, REV B, & SRM 53-70-51-2R-5, REPAIR 5.Sep 4, 2026 · N8715Q · Boeing 7378 · Fuselage Main, Floor BeamSDR SWAA2026100936251Floorbeam · corrodedCORRODED FLOORBEAM, BS 947, LBL 50, WL 208.1. PERFORMED PERMANENT REPAIR ON FLOORBEAM IAW EA 26-153-02558-WIP1, REV B, & SRM 53-70-51-2R-5, REPAIR 5.Sep 4, 2026 · N8715Q · Boeing 7378 · Fuselage Main, Floor BeamSDR SWAA2026100809422Plate · crackedWIGGLE PLATE INBD OF NR 7 FLAP TRACK, COMMON TO ACCESS PANEL 661AB WAS CRACKED. THE WIGGLE PLATE WAS REMOVED AND REPLACED WIGGLE PLATE AT INBD OF NR 7 FLAP TRACK IAW SRM 51-40-02-0G-0, AND DWG. 115A2001, REV A.Sep 4, 2026 · N8657B · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026100856519Drip Tray · crackedHORIZONTAL STAB, FWD CABLE DRUM DRIP SHIELD CRACKED.Sep 4, 2026 · N8657B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026100643752Floor Panel · crackedCRACKED FLOOR PANEL 241AEF. REPLACED THE FLOOR PANEL 241AEF IAW AMM 53-21-00-401, STEP 3.F.(5), AND FLOOR PANEL 241AEF WILL BE INSTALLED ON TTG8Q01DPZED.Sep 4, 2026 · N8715Q · Boeing 7378 · Fuselage Floor PanelSDR SWAA2026100680505Floor Support · corrodedCORROSION FLOOR SUPPORT LOCATED BS 947.4 PLUS 1 INCH, RBL 50, WL 208.1 IN THE AFT GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, ITEM 8, SRM 51-40-02 AND DWG 147A5650 SHEET 105 REV-.Sep 4, 2026 · N8715Q · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026100689293Access Panel · delaminatedDELAMINATED ACCESS PANEL 511AB LEADING EDGE LT WING. REPAIRED ACCESS PANEL 511AB LEADING EDGE LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.Sep 4, 2026 · N8715Q · Boeing 7378 · Wing, Plate/SkinSDR IPXA2026092678940Skin · debondedMAJOR REPAIR, LOWER BILGE COMPOSITE SKIN PANEL BETWEEN STA 1963 TO 1992 FWD AND AFT EDGES DISBONDED WITH AREAS OF CORROSION INCLUDING FWD EDGE LEVELING COMPOUND DETERIORATED AND NOT SECURED. RL028 VERIFIED STEP 17 OKAY TO TREAT AND PRIME REWORKED AREA. REF UPSep 4, 2026 · N463UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2026100280598Skin · delaminatedMAJOR REPAIR, APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1918 AND 1941 DELAMINATED. RL038 QCI(RII) VERIFIED FABRICATION OF DOUBLER PER STEP 16 AND GMM RII 04-02Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026100280618Skin · delaminatedMAJOR REPAIR, APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1941 AND 1963 DELAMINATED. RL039 QCI(RII) VERIFIED STEP 13 IS C/W AND VERIFIED TOOLS PER DOCUMENTS AND GMM RII 04-02Sep 4, 2026 · N463UP · Boeing 75724APF · APU Cowling/ContainmentSDR I5PA2026090468814Controller · malfunctionedETOPS SIGNIFICANT REPORT AND EVENT - LEFT PACK TEMP AND CABIN ALTITUDE EICAS MESSAGE. EMERGENCY DESCENT AND DIVERSION TO ROR - PERFORMED BITE CHECK OF PACK TEMP CONTROLLER AND CABIN PRESSURE CONTROLLER PER AMM. NO FAULTS FOUND, ALL MESSAGES CLEARED.Sep 4, 2026 · N688SL · Boeing 757230 · Cabin Pressure ControllerSDR SWAA2026093007465Crossbeam · crackedCROSSBEAM ANGLE CRACKED AT WL 208, BS 540, LBL 2. REMOVED CROSSBEAM AND INSTALLED A NEW CROSSBEAM AT 540 BTWN BL 0 - LBL 24.5 IAW SRM 51-40-02-0G-0, & DWG 143A0060, REV -.Sep 4, 2026 · N8714Q · Boeing 7378 · Fuselage Main, StructureSDR SWAA2026093006955Crossbeam · crackedCROSSBEAM ANGLE CRACKED AT WL 208, FS 540, RBL 2. REMOVED THE CROSSBEAM AND INSTALLED A NEW CROSSBEAM BS 540 BTWN BL 0 TO RBL 24.5 IAW SRM 51-40-02-0G-0, & DWG 143A0060M REV -.Sep 4, 2026 · N8714Q · Boeing 7378 · Fuselage Main, StructureSDR FDEA202609041453Backboard · puncturedLH PAX DOOR SLIDE BACK-PLATE PUNCTURED. REPLACED THE LH PASSENGER/CREW DOOR SLIDE/RAFT PER AMM 25-61-22-04-01. MINOR REPAIR IAW FEDEX GMM 6-2-100.Sep 4, 2026 · N731FD · Airbus A300B4605R · Escape SlideSDR SWAA2026092933599Web · crackedCRACKED WEB, BS 1016, BTWN LBL 25 - 45. REPLACED THE WEB AND FASTENERS IAW SRM 51-10-02, STEP 8, SRM 51-40-02, & DWG 148A0922, SHEET 3, REV A.Sep 4, 2026 · N8712L · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026092957301Intercostal · crackedCRACKED INTERCOSTAL BTWN BS 400 - 420, STR 26L. REPLACED THE INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND FASTENERS IAW SRM 51-40-02, & DWG 143A7505, SHEET 151, REV A.Sep 4, 2026 · N8653A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026092512762Strap · crackedLEFT BS 616 STUB BEAM STRAP HAD A CRACK INDICATION. FOUND IN FWD-MIDDLE FASTENER HOLE. REMOVED AND REPLACED THE STUB BEAM STRAP IAW SRM 51-40-02-0G-0, AND DWG 144A1714 REV -.Sep 4, 2026 · N210WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026092562472Strap · crackedRIGHT BS 639 STUB BEAM STRAP HAD A CRACK INDICATION, FOUND IN AFT FASTENER HOLE. REMOVED AND REPLACED THE STUB BEAM STRAP IAW SRM AND DWG 144A1715 REV.Sep 4, 2026 · N210WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026092280443Stringer · crackedSTRINGER CRACKED, AFT SIDE OF BS 2598 S-25R. ACCOMPLISH THE REPAIR IAW EO-98604-REQ0042, REV 1, & EI F2026A53M-1904, REV 2.Sep 4, 2026 · N613UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2026091880421Stringer · crackedSTRINGER CRACK,FWD SIDE OF STA 2598 S-5L. ACCOMPLISHED REPAIR I.A.W EO-98604-REQ0032 REV.1 AND EGAT EI NO.F2026A53M-1942 REV.0 AND EGAT WORK SHEET NO.60713 AND SRM 53-80-03-2R-2 REV.49.Sep 4, 2026 · N613UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2026091880395Stringer · crackedSTRINGER CRACKED, FWD SIDE OF STA 2598 S-7L. ACCOMPLISHED REPAIR I.A.W EO-98604-REQ0034 REV.1 AND EGAT EI NO.F2026A53M-1969 REV.0 AND EGAT WORK SHEET NO.60711 AND SRM 53-80-03-2R-2 REV.49.Sep 4, 2026 · N613UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2026091880429Stringer · crackedSTRINGER 8R CRACKED, FWD SIDE OF BS 2598. ACCOMPLISH THE REPAIR IAW EO-98604-REQ0039, REV 1, SRM 53-80-03-2R-2, REV 49, WORK SHEET 60706, & EI F2026A53M-1975, REV 0.Sep 4, 2026 · N613UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2026091880423Stringer · crackedSTRINGER CRACKED, FWD SIDE OF STA 2598 S-6L. ACCOMPLISHED REPAIR I.A.W EO-98604-REQ0033 REV.1 AND EGAT EI NO.F2026A53M-1943 REV.0 AND EGAT WORK SHEET NO.60712 AND SRM 53-80-03-2R-2 REV.49.Sep 4, 2026 · N613UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2026091880439Stringer · crackedSTRINGER 6R CRACKED, FWD SIDE OF BS 2598. ACCOMPLISHED REPAIR IAW EO-98604-REQ0037, REV 1, EI F2026A53M-1973, REV 0, WORK SHEET 60708, & SRM 53-80-03-2R-2, REV 49.Sep 4, 2026 · N613UP · Boeing 7478F · Fuselage Main, Longeron/Stringer