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 SWAA2026062912728Attach Angle · crackedCENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE HAS A 1.1 INCH VERTICAL CRACK THROUGH THE FASTENER AT BS 661.95, LBL 6.14+3.4. C/W M-26-157-01480 REPAIR OF LT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW TASK TTG8Q01CRT4G.Jun 16, 2026 · N8661A · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026062913127Attach Angle · crackedCENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE HAS A 0.5 INCH VERTICAL CRACK THROUGH THE FASTENER AT BS 661.95, RBL 34.80. C/W M-26-157-01481 REPAIR OF RH BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW TASK TTG8Q01CRTLX.Jun 16, 2026 · N8661A · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026062912729Attach Angle · crackedCENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE HAS A 1 INCH VERTICAL CRACK THROUGH THE FASTENER, BS 661.95, RBL 6.15+3.4. C/W M-26-157-01481 REPAIR OF RT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW TASK TTG8Q01CRT82.Jun 16, 2026 · N8661A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026062913126Attach Angle · crackedCENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE HAS A .6 INCH VERTICAL CRACK THROUGH THE FASTENER AT BS 661.95, LBL 34.79. C/W M-26-157-01480 REPAIR OF LT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW TASK TTG8Q01CRU7S.Jun 16, 2026 · N8661A · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR IPXA2026062787236Bonding Jumper · corrodedL/H HORZ STAB OTBD END TO ELEVATOR BONDING STRAP AND BOTH FWD AND AFT ATTACH BRACKETS HAVE CORROSION. INSTALLED ONE ANGLE BRACKET STRAP JUMPER & REINSTALLED ONE BRACKET ATTACH BY ACCESS IAW SRM 51-40-02-0G-0.Jun 16, 2026 · N429UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026062794337Support · corrodedAPU COMPARTMENT L/H LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION, ACCOMPLISHED REPAIR PER EO-98077-REQ1 AND STE-SAA EA 757-5330-01-B0762, REV IRJun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2026062794351Longeron · corrodedAPU COMPARTMENT RT LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION. ACCOMPLISHED REPAIR PER EO-98076-REQ1 AND STE-SAA EA 757-5330-01-B0763, REV IRJun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026062792720Frame · corrodedRIGHT FWD LOWER FUSELAGE WASTE DISPOSAL ACCESS PANEL 118AR HAS CORROSION ON INNER AND LOWER FRAME. INSTALLED PANEL 118AR IN FWD FUSELAGE LAVATORY DISPOSAL IAW SRM 51-40-02-0G-0.Jun 16, 2026 · N418UP · Boeing 75724APF · Fuselage Main, StructureSDR SIMA20260616002Seat Track · corrodedSSI 53-10-027-0392 LEVEL 2 CORROSION CORROSION AT FWD PASSENGER FLOOR STRUCTURE WET AREAS RH SEAT TRACK FROM FR 16 TO FR 18 Y = +273. (LVL 2 CORROSION) (MAJOR REPAIR) BLENDED CORROSION AT FWD PASSENGER FLOOR STRUCTURE WET AREAS RH TRACK FROM FR 16 TO FR 18 Y =Jun 16, 2026 · N298FR · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260616001Crossbeam · corrodedLEVEL 2 CORROSION FRAME 87 CROSS BEAM HAS CORROSION AROUND 1EA FASTENER HOLE. (LVL 2 CORROSION) (MAJOR REPAIR) BLENDED CORROSION ON FRAME 87 CROSS BEAM IAW E-175 SRM 51-10-03. ORIGINAL THICKNESS .098" IAW EMBRAER DRAWING #170-86056-003. MATERIAL REMOVED .055" Jun 16, 2026 · N298FR · Emb ERJ170200LR · Fuselage Main, StructureSDR REXA2026062900985Door · crackedR/H FWD OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED IAW MHIRJ REO 670-52-21-103, REV --, DATE 2024-11-06Jun 16, 2026 · N147PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2026062600981Bracket · crackedRIGHT AFT OVERWING EMERGENCY EXIT DOOR HAS POSSIBLE CRACKS ON THE UPPER BRACKETS. REPAIRED RT AFT OVERWING EMERGENCY EXIT DOOR UPPER BRACKETS IAW REO 670-52-21-103, REV --.Jun 16, 2026 · N147PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2026062600978Floorbeam · crackedLEFT COCKPIT FLOORBEAM LBL12 AT BS 280 CRACKED. REINSTALLED BS 280 LT COCKPIT DOOR POST IAW SRM 51-42-06-001-001-A01, & SRM 51-42-13-001-001-A01. REMOVED SHORING FROM BS 250 BTWN S23L AND S23R IAW SRM 53-11-43-201-003-A01. INSTALLED NEW SERVICEABLE SEGMENT OFJun 16, 2026 · N147PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR 2026F00132Warning Light · illuminatedELEC LIGHT TURNS ON DURING GROUND HANDLING. PERFORMED ELEC LIGHT MSG BITE PROCEDURE IAW AMM 24-31-00-740-801. NO FURTHER DEFECTS NOTEDJun 16, 2026 · N109JS · Boeing 7378 · Central WarningSDR RU3A202606250249Cooling Fan · arcedDURING FLIGHT INSPECTION AT KSAV IN N77 ALL CREW MEMBERS ACKNOWLEDGED SIGNIFICANT EYE IRRITANT PRESENT. MYSELF AND MS HAD WATERING PRESENT IN EYES, SIC ACKNOWLEDGE EYES BURNING. I DECLARED AN EMERGENCY WITH SAV APPROACH AND WAS GIVEN AN IMMEDIATE CLEARANCE Jun 16, 2026 · N77 · Beech 300BEECH · Air Distribution FanSDR IPXA2026062585393Torque Box · dentedMANY DENTS & DISBOND - L/H V.S.T LOWER FWD TORQUE BOX UPPER PANEL. INSTALL NEW TORQUE BOX PANEL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 175T0000 SH 1 REV: B, SH 2 REV: A, 114T2800 SH 5 REV: G AND SREO-62436-REQ001 REV2Jun 16, 2026 · N334UP · Boeing 76734AF · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026062495344Skin Panel · gougedMAJOR REPAIR, LT WING, SLAT NR 1 OUTER EDGE INNER SURFACE CLOSE TO PYLON HAS A SCRATCH BY A FASTERNER UNLOCK OF THE PANEL 512AT. ACCOMPLISHED REPAIR IAW EO-97805-REQ1 AND VT-MAE EA 300-5742-27-A4521, REV. -.Jun 16, 2026 · N166UP · Airbus A300F4622R · Wing, Plate/SkinSDR FDEA202606160758Floor Panel · puncturedPUNCTURED FLOOR PANEL 232EFF.SEC 43 OF MDC. FLOOR PANEL 232EFF SEC 43 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15,2025.Jun 16, 2026 · N166FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202606160756Floor Panel · puncturedPUNCTURED FLOOR PANEL 242AFF. SEC 45 OF MDC. FLOOR PANEL 242AFF. SEC 45 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2. REV. 94 DEC 15,2025.Jun 16, 2026 · N166FE · Boeing 7673S2F · Fuselage Structure (General)SDR FDEA202606160754Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X= -27.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 755, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROJun 16, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026062485353Longeron Fitting · crackedLEFT UNDERWING LONGERON FITTING HAS CRACK DURING PERFORMED J/C: EO-48156-JIC001. ACCOMPLISHED JOB I.A.W UPS EO-48156-JIC003 REV2 AND UPS EO-97843-REQ1 REV1 (EGAT EI NO.F2026A57M-1306 REV.0) AND BOEING DWG NO. 111T4022 SH 1 REV: CJun 16, 2026 · N334UP · Boeing 76734AF · Wing, Longeron/StringerSDR IPXA2026062294955Support Bracket · crackedLEFT SIDE UPPER HORIZONTAL APRON SUPPORT BRACKET IS CRACKED. INSTALLED SUPPORT FITTING AT LT SIDE HORIZONTAL APRON IAW SRM 51-40-21-001.Jun 16, 2026 · N161UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR CALA2026062317279Skin · crackedCRACK FOUND ATRIGHT HORIZONTAL STAB LOWER SKIN AT STAB STA 120.30 , 18.5" FROM REAR SPAR, I/B ROW. REPAIRED CRACK ON RIGHT HORIZONTAL STAB LOWER INSPAR SKIN AT STA 120.3", 18.5" FWD OF REAR SPAR INBD ROW IAW SRM 55-10-01-2R-11, REPAIR 11, AND 51-40-02-0G-0. Jun 16, 2026 · N37413 · Boeing 737924ER · Horizontal Stabilizer, Plate/SkinSDR SWAA2026062312885Skin · delaminatedDELAMINATION ON INBOARD CORNER ON AFT FLAP OUTBOARD LT WING. EVALUATED DAMAGE ON INBOARD CORNER OF OUTBOARD AFT FLAP AT LT WING IAW SRM 57-53-01-2R-16. FOR REMOVE AND INSTALL AFT FLAP OUTBOARD LT WING PROCEDURE SEE TTG8Q01CRW1PJun 16, 2026 · N476WN · Boeing 7377H4 · Trailing Edge FlapsSDR FDEA202606160753Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK BETWEEN STATION 1801-1821 LONGERON 46 RIGHT. CRACKED LONGERON SPLICE FITTING AT LOWER CENTER CARGO COMPARTMENT BILGE AREA BETWEEN STATION 1801-1821, LONGERON - 46 RIGHT REMOVED AJun 16, 2026 · N620FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202606160752Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 979, X= -27.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 979, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWAJun 16, 2026 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026062201Skin · nickedNICK FOUND ON LOWER FUSELAGE SKIN FWD OF FS 977.00 AT STGR 27. REPAIR ON BS 977 AND S27 AT FUSELAGE SKIN WAS COMPLETED IAW EO C550-53MR-108, REV O.Jun 16, 2026 · N587GJ · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWAA2026062213163Slide · out of positionCREW REPORTS AFT LT SLIDE NEEDS REPOSITIONED. RE-PACKED SLIDE AS REQUIRED AFT LT IAW MT 725-66-01Jun 16, 2026 · N212WN · Boeing 7377H4 · Escape SlideSDR SWAA2026062212850Strap · stuckFORWARD GALLEY SERVICE DOOR ESCAPE SLIDE MANUAL INFLATION STRAP/HANDLE STUCK. SECURED THE R1 DOOR ESCAPE SLIDE MANUAL STRAP COVER AND HOOK AND LOOP IAW SIP.Jun 16, 2026 · N8626B · Boeing 7378H4 · Escape SlideSDR SWAA2026062213145Flashlight Assy · inoperativeAFT FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED CRADLE AND FLASHLIGHT IAW AMM 25-64-00.Jun 16, 2026 · N8845L · Boeing 7378 · Emergency EquipmentSDR SWAA2026062212552Battery Pack · inoperativeINOPERATIVE EMERGENCY LIGHT ON STOWAGE BIN 2 AND 3 RT. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.Jun 16, 2026 · N951WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026062212550Battery Pack · inoperativeINOPERATIVE EMERGENCY LIGHT IN FWD GALLEY 1. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.Jun 16, 2026 · N951WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026062212780Cover · looseEMERGENCY EXIT SIGN COVER AT ROW 15 DEF FELL OFF. INSTALLED EMERGENCY EXIT SIGN COVER AT ROW 15 DEF IAW S.I.P.Jun 16, 2026 · N8653A · Boeing 7378H4 · Emergency LightingSDR SWAA2026062212758Light · brokenRIGHT AFT EXIT ROW LIGHT BROKEN. REPLACED LIGHT ASSY IAW AMM 33-51-01.Jun 16, 2026 · N8691A · Boeing 7378H4 · Emergency LightingSDR SWAA2026062212782Cover · missingMID CABIN EMERGENCY EXIT CEILING LIGHT COVER MISSING. REPLACED LENS IAW AMM 33-51-03 ON BOTH MID CABIN LIGHTS.Jun 16, 2026 · N8751R · Boeing 7378 · Emergency LightingSDR SWAA2026062212613Seal · crackedHORIZONTAL STAB-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED ON THE LEFT SIDE. REMOVED AND REPLACED HORIZONTAL STAB-TO-BODY UPPER FRONT SPAR SLIDING SEAL ON LT SIDE IAW AMM 53-31-31.Jun 16, 2026 · N8739L · Boeing 7378 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026062212611Seal · crackedHORIZONTAL STAB-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED ON THE RIGHT SIDE. R & R HORIZONTAL STAB-TO-BODY UPPER FRONT SPAR SLIDING SEAL ON THE RIGHT SIDE IAW AMM 53-31-31.Jun 16, 2026 · N8739L · Boeing 7378 · Horizontal Stabilizer Miscellaneous StructureSDR ASAA2026061666860Lamp · inoperativeOVERWING EXIT AFT EMERGENCY LIGHT INOPERATIVE, GROUNDED - YES. REPLACED OVERWING (LH) EXIT EMERGENCY LAMP LIGHT IAW AMM 33-51-04-960-801. TEST GOOD.Jun 16, 2026 · N943AK · Boeing 7379 · Emergency LightingSDR IPXA2026062298593Support Bracket · brokenSUPPORT BRACKET ON UPPER L1 CREW DOOR IS BROKEN. INSTALLED BRACKET ON L1 CREW DOOR IAW SRM 51-40-21.Jun 16, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061989107Adapter · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061989218Seal · crackedCRACKED SEAL, NR 2 ENG RT CORE COWL FLIPPER DOOR. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV.95. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV.95, & CMM IPL 71-13-24 REV. 50.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026061990900Adapter · chafedCHAFED BRACKET, NR 1 ENG LT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061989175Adapter · chafedCHAFED BRACKET, NR 2 ENG LT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026061988855Adapter · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24 REV. 50.Jun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026062287436Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 3:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE AND 25.5" FROM LOWER EDGE, AT 3 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). FILL THE CUT OUT WITH AJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062287408Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 8:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 7.5" FROM AFT EDGE AND 16.5" FROM OUTBD EDGE, AT 8 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). FILL THE CUT OUT WITH ADJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062287404Nose Cowl · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 5:30 POSITION. (REPAIR). CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.75" FROM AFT EDGE AND 50" FROM INBD EDGE, AT 5:30 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). BOND THE SPAJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026062286352Skin · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 6:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.25" FROM FWD EDGE AND 38.5" FROM INBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). BOND THE SPACER WITH FIJun 16, 2026 · N334UP · Boeing 76734AF · Nacelle/Pylon, Plate/SkinSDR IPXA2026061989062Bracket · chafedCHAFED BRACKET, NR 1 ENG RT T/R FWD LWR CLOSURE DOOR T/E AREA. (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96. C/W REVIEWJun 16, 2026 · N334UP · Boeing 76734AF · Engine Thrust ReverserSDR QXEA2026062200137Shear Web · corrodedAFT WET AREA RIGHT HAND SHEAR WEB IS CORRODED AT FS 87. REPLACED WEB.Jun 16, 2026 · N636QX · Emb ERJ170200LR · Fuselage Miscellaneous Structure