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 AALA202609148477Handle · looseAIRCRAFT WAS GROUNDED: CABIN ENTRY DOOR 1R CONTROL HANDLE LOOSE. RESECURED 1R INTERIOR DOOR HANDLE AS PER AMM 52-11-11.Sep 12, 2026 · N967AN · Boeing 737823 · Service DoorsSDR AALA202609147528Power Supply · inoperativeAIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY M33093 FAILS TO ILLUMINATE ASSOCIATED LIGHTS FOR 15 MINUTES. REPLACED AND REPLACED EMERGENCY POWER SUPPLY M33093 IAW AMM 33-51-06-960-802.Sep 12, 2026 · N760AN · Boeing 777223 · Emergency LightingSDR SWIA2026091277137Spring · brokenFOUND FWD SERVICE DOOR FWD ESCAPE SLIDE FITTING ASSEMBLY FLAP SPRING BROKEN. REMOVED AND REPLACED WITH SERVICEABLE ASSY FDW SERVICE DOOR FWD ESCAPE SLIDE FITTING ASSEMBLY IAW AMM 53-10-25Sep 12, 2026 · N511SY · Emb ERJ170200LR · Escape SlideSDR YENA2026091400801Pump · faultedFLT 1075, MCO-PVD-DIVERSION-JFK. THE AIRCRAFT IS REPORTING AN HYD B ELEC PUMP LO PR. THE FLIGHT CREW HAS COMPLIED WITH QRH 10-27.THE AIRCRAFT IS UNABLE TO LAND IN PVD DUE TO THE REDUCED LANDING DISTANCE ASSOCIATED WITH THE CURRENT CONDITION. THE AIRCRAFT IS DISep 12, 2026 · N662JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR IPXA2026091219560Warning Buzzer · inoperativeEVACUATION SLIDE WARNING SYSTEM BUZZER INOPERATIVE. REPLACED WARNING HORN (BUZZER) AND CARRIED OUT OPS CHECK GOOD IAW AMM 52-73-12/401.Sep 12, 2026 · N135UP · Airbus A300F4622R · Escape SlideSDR WX0A2026091432953Slide · expired(AIRCRAFT GROUNDED) BOTH REAR INSPECTION STICKER EXPIRED OM EMERGENCY SLIDES. INSPECTED BOTH REAR MID CABIN EMERGENCY EXIT DOORS. FOUND RT DOOR TO STILL BE WITHIN LIMITS. REMOVED AND REPLACED LT MID EXIT DOOR ESCAPE SLIDE. IAW AMM 25-67-01-000-801/400-801. Sep 12, 2026 · N812NV · Boeing 7378200 · Standard Practices/StructuresSDR DALA2026091405121Housing · detachedEMERGENCY PATH LIGHT HOUSING FOR SEAT 44HJ WAS FOUND DETACHED FROM SEAT. REPLACED HOUSING PER AMM 33-51. OK FOR SERVICE. (9320796) AIRCRAFT WAS GROUNDED.Sep 12, 2026 · N858NW · Airbus A330223 · Emergency LightingSDR ABXA20260912402Overheat Sys · false activationFIRE/OVHT SYS ON FINAL APPROACH. AC LANDED AND MTX GROUNDED A/C. PERFORMED OPERATIONAL CHECK I.A.W A.M.M B767 26-11-00. ALL FOUND NORMAL. UNABLE TO DUPLICATE FAULT, NO STATUS MESSAGE. AIRCRAFT REMAINS NO ETOPS AND RETURNED A/C TO SERVICE.Sep 12, 2026 · N317CM · Boeing 767338 · Overheat DetectionSDR FDEA202609121330Unknown · odorACRID FUMES IN COCKPIT DURING CLIMB OUT AND DESCENDING THROUGH 14,000 . PERFORMED AIR CONDITIONING SYSTEM OIL SMOKE/FUME CONTAMINATION REMOVAL PER AMM 21-00-21-2. NO ABNORMAL NOTED. PERFORMED OIL INSPECTION CHKD IAW AMM 79-00-00-6. FOUND NORMAL. PERFORMESep 12, 2026 · N132FE · Boeing 7673S2F · Air Distribution SystemSDR CALA2026091419418Battery Pack · no testEMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1672 IAW AMM 33-51-06-960-805 OPS CHECK GOODSep 12, 2026 · N35271 · Boeing 737824 · Emergency LightingSDR CALA2026091419395Battery Pack · faultedFOUND OFAR & FA SEAT WITH AFT OF DR 1 RT & FWD OF DR 1 L/H & AFT OF DR 1 L/H & FWD OF DR 2 L/H & AFT OF DR 2 L/H & AFT OF DR 2 R/H & FWD OF DR 3 R/H & AFT OF DR 5 L/H & AFT OF DR 5 R/H & FWD OF DR 5 - CL R/H TOTAL 11EA EMERGENCY FLASHLIGHT BATTERIES WERE OVER Sep 12, 2026 · N2142U · Boeing 777300ER · Emergency EquipmentSDR CALA2026091419394Light · inoperativeFWD AND AFT EMERGENCY LIGHT PATH AT SEAT 20F ON THE RIGHT SIDE IS OUT. ALREADY ORDERED THE NEW LIGHT ASSEMBLYS R & R FWD EMERGENCY PATH LIGHT. FWD AND AFT OPS CHECK GOOD REF AMM 33-51-10Sep 12, 2026 · N649UA · Boeing 767322 · Emergency LightingSDR CALA2026091419393Light · dimEMERGENCY PATHWAY LIGHTS AT SEAT 41D & 45D VERY DIM. REMOVED AND REPLACED EMERGENCY PATHWAY LIGHTS AT SEATS 41D & 45D. REF. AMM 33-51-06. OPS CHECK GOOD.Sep 12, 2026 · N29907 · Boeing 7878 · Emergency LightingSDR CALA2026091419388Unknown · odorHIGH HEAT ODOR ON CLIMB FO SIDE HAD ELECTRICAL BURNING ODOR SEVERAL TIMES IN CLIMB & CREW REPORTED FLIGHT DECK WAS COOL BEFORE TAKEOFF. DURING CLIMB NOTICED FWD INSTRUMENT PANEL WAS VERY HOT BUT PACK ON FULL COLD & WAS BLOWING COLD AIR. HOTTER ON FO SIDE THANSep 12, 2026 · N677UA · Boeing 767322 · Air Distribution SystemSDR CALA2026091419387Lavatory · odorACFT CABIN HAS RANCID ODOR. FULL LAV SERVICE COMPLETED. WALKAROUND FOUND VERY STRONG ODOR COMING OUT OF OUTFLOW VALVE. GAINED ACCESS TO BACK OF OUTFLOW VALVE & LAV SERVICE PANEL. IDENTIFIED STRONG FOUL ODOR. LIKELY COMING FROM THIS AREA. IDENTIFIED SMALL ASep 12, 2026 · N13110 · Boeing 757224 · Waste Disposal SystemSDR SIMA20260912001Skin · dentedDURING RE-CONTOURING OF 2 DENTS FOR TDMI786T5322 (NON-ROUTINE #F144316) DAMAGE OCCURRED TO FUSELAGE SKIN BETWEEN FR5-6, STRG'S 10R & 12R (PROTRUSION SKIN DENT). (MAJOR REPAIR) NOT AN SSI ITEM. REPAIRED IAW ERS-EJ-53MR-5532.Sep 12, 2026 · N786SM · Emb ERJ170100SE · Fuselage Main, Plate/SkinSDR DALA2026091305113Microphone · inoperativeF/O OS MASK MICROPHONE NOT WORKING. C/A: SWAPPED THIRD OBSERVER SEAT OT MASK WITH F/O AND FWD THIRD OBSERVER SAET TO MEL 25-11-07. R/R THIRD OBESERVER O2 MASK PER A320 AMM 35-12. LEAK AND OPS TESTS OK. RFID INDUCTION C/W. F/O MASK RFID REPLACEMENT C/W TO REFLESep 12, 2026 · N351NW · Airbus A320212 · Crew Oxygen SystemSDR DALA2026091305112Skin · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE AFT CARGO COMPARTMENT FROM FR56 TO FR 57 BETWEEN STRG-42L AND STRG-43L AFT ATG4 ANTENNA INTERNAL DOUBLER WITH CORROSION. PERFORMED REPAIR AT LOWER FUSELAGE AFT CARGO COMPARTMENT SKIN PANEL SECTION FROM FR 56 TO FR 57, BETWEENSep 12, 2026 · N353NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026091305111Shear Plate · corrodedLEVEL 2 CORROSION, PAX CABIN, LATERAL SHEAR PLATE WITH CORROSION LOC.BTW FR 69 TO FR 70 STR 23L. REPLACED SHEAR PLATE AT PAX CABIN BETWEEN FR 69 TO FR 70 STG 23L AS PER A320 SRM 51-72-11-911-001 PARAG 2, REV 158.00 DATED 01-JUN-26 AND REFERENCE DRAWING D5347Sep 12, 2026 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026091305110Panel · detachedOXYGEN PANEL IN AFT GALLEY FELL OFF. FOUND RUBBER SEAL TUBE MISSING FROM BOTH SIDES, NO DMG TO MODULE . INSTALLED NEW SEALS AS REQ'D, MODULE SECURED. MEL & PLACARDS REMOVED, OK FOR SVC. (LP: 9118950, AIRCRAFT WAS GROUNDED)Sep 12, 2026 · N337NB · Airbus A319114 · Passenger Oxygen SystemSDR DALA2026091305104Cover · looseEMERGENCY EXIT SIGN COVER LOOSE, LOCATIONS:605, CABIN. EXIT COVER IN CENTER AISLE ON AFT SIDE OF AIRCRAFT FELL OFF. ATTACHED EXIT SIGN. LIGHT OPS NML. (LP 1809628 - AIRCRAFT WAS GROUNDED)Sep 12, 2026 · N3766 · Boeing 737832 · Emergency LightingSDR IPXA2026110406772Adapter · corrodedMAIN DECK FLOOR STRUCTURE, FR 65 Y0 RH CLS HAS CORROSION. VERIFIED LOCATED AND DRILLED CLS IAW SRM 51-40-44. VERIFIED SURFACE PROTECTION APPLIED IAW A300 SRM 51-21-10.Sep 11, 2026 · N146UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102106812Web · crackedMAIN DECK FLOOR STRUCTURE HAS A CRACK BETWEEN FRAME 73 & 74 AND Y2127 & FUSELAGE (UNDERNEATH). NEW FLOOR STRUCTURE BETWEEN FRAME 73 & 74 AND Y2127 WAS INSTALLED IAW SRM 51-40-21.Sep 11, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR VNAA202610310001Tail Cone · dentedDENT ON TIP OF TAILCONE BTWN 2 & 3 O'CLOCK POSITION. THE TAILCONE WAS REPAIRED IAW REO 690-53-85-123, REV -.Sep 11, 2026 · N616NN · Cndair CL6002D24 · Aerodynamic FairingsSDR VNAA202610300020Floor Support · corrodedCORROSION ON SUPPORTS, BTW FS280 TO FS310 AND RBL35 TO LBL35 WL72.5 BELOW FLOOR PANELS. SUPPORTS, BTW FS280 TO FS310 AND RBL35 TO LBL35 WL72.5 BELOW FLOOR PANELS WERE REPLACED PER CRJ700 SRM 51-42-21-001-001-A01.Sep 11, 2026 · N725PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR IPXA2026102203705Splice · corrodedMAJOR REPAIR, AFT CARGO FLOOR SPLICE EXFOLIATED IN 2 PLACES STR 30L BS 1460. REMOVED CORROSION ON OTBD WEB AT AFT CARGO, IAW SRM 51-10-02-0G-0. MEASUREMENTS ARE AS FOLLOWS: L=2.50" X W=1" X D=.050" R/T=.040" O/T=.090" ALLOWED DAMAGE 20%, MAT LOSS .050", FOUSep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102803755Web · corrodedAFT CARGO COMP ABOVE DOOR CUTOUT CEILING SUPPORT WEB CORRODED STA 1440. PERFORMED UT. THICKNESS INSP. OF AFT CARGO CEILING SUPPORT WEB REWORKED AREA AT STA. 1440 PER NTM PT. 4, MINIMUM REMAINING THK VALUE IS .048". INSP. ITEM ONLY.MATERIAL LOSS OF .002" MAXISep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102703845Retainer · corrodedBULK CARGO MAIN CABIN FLOOR RH SIDE STA 1680 NUT PLATE RETAINER CORRODED. LOCATED, DRILLED AND INSTALLED NUTPLATE RETAINER STRAP (PLATE) AT BS 1680.985 AND RBL 39.720 REF. BOEING SRM 51-40-05-0G-0 AND REF. BOEING SRM 51-40-02-0G-0 AND APPLIED CIC REF BOEING Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102403849Nut Plate · corrodedBULK CARGO MAIN CABIN FLOOR LH AND RH SIDE STA 1680 TO 1720 MULTIPLE NUT PLATE RETAINERS CORRODED STR ATA 51-00 GM015. INSTALLED NUT PLATE RETAINER AND APPLIED CIC AT BULK CARGO MAIN CABIN FLOOR LH SIDE BS 1680 LBL 36. IAW SRM 51-40-02-0G-0. AND AMM 51-24-03Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102400357Seat Track · crackedINT-COCKPIT CAPTAIN SEAT I/B FWD SEAT TRACK IS CRACKED ATA 53-10. REMOVED AND REPLACED COCKPIT CAPTAIN SEAT I/B FWD SEAT TRACK FLOOR TRACK ALIGNMENT IAW B757 AMM 25-11-01-822-078.Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102491077Skin Panel · delaminatedSTR, ATA 55: R/H HORZ STAB UPPER HONEYCOMB SKIN PANEL BETWEEN AUX AND FRONT SPAR AT STAB STA 93 (MOST INBD AREA AT EXISTING REPAIR) DISBONDED. RL037. INSTALLED I/B AND O/B LOGO LIGHT ASSY'S, R/H HORZ STAB UPPER IAW AMM 33-45-00-402-030. LOGO LIGHT-DEACTIVATIONSep 11, 2026 · N402UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR IPXA2026102798760Skin Panel · damagedAPU COMPARTMENT SKIN PANEL HAS EVIDENCE OF DELAMINATION APPROX BTW BS 1885 AND BS 1896, STGR 17R AREA, PERFORMED REPAIR PER. SRM 51-70-10-2R-4 REPAIR 4 (REPAIRS LARGE DAMAGE) FIG. 201 DETAIL A REV 126 USING SRM 51-70-10-2R-0 REV 126 REPAIRED GUIDLINES PER SRM Sep 11, 2026 · N402UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026102499320Support Angle · corrodedLEFT FUSELAGE SECTION 48 INTERIOR STRUCTURE RIB HAS EVIDENCE OF CORROSION ON LOWER AREA APPROX AT BS 1992.8, LOCATED, DRILLED AND INSTALLED SUPPORT ANGLE (DOUBLER LHS) AT SECTION 48 IN AFT FUSELAGE FRAME LOWER AREA APPROX AT BS 1992.8, IAW B757-200 SRM 51-40-Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102400353Seat Track · crackedCOCKPIT CAPTAIN SEAT O/B FWD SEAT TRACK IS CRACKED. REMOVED AND REPLACED COCKPIT SEAT TRACK IAW AMM 25-11-01-822-078.Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102206792Adapter · corrodedMAIN DECK FLOOR STRUCTURE, FR 61 Y0 RH CLS HAS CORROSION. INSTALLED OF CLS ADAPTER ON MDC FR61 Y0. R/H IAW SRM 51-41-21-001.Sep 11, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026102206731Adapter · corrodedMAIN DECK FLOOR STRUCTURE, FR 65 RH BETWEEN -Y1456 AND -Y1959, CLS HAS CORROSION. VERIFIED INSTALLATION OF CLS ADAPTER ON MDC FR65 R/H -Y1456 AND -Y1959 IAW SRM 51-41-21-001.Sep 11, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR SWAA2026102160553Support Angle · crackedCRACKED SUPPORT ANGLE, BS 663.75, LBL 36, WL 168, BLENDING PERFORMED WITH THE GRAIN DIRECTION INSTEAD OF CROSS GRAIN ON NEW ANGLE, PERFORMED BEND TO FORM NEW ANGLE IAW SRM 51-30-01, & DWG 111A1322, SHEET 14, REV A. PERFORMED CLEANING & REMOVED PROTECTIVE Sep 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102117862Access Panel · damagedELONGATED HOLES ON THE RT WING ACCESS PANEL 661AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.Sep 11, 2026 · N8658A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2026102197527Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 193AR AT LOWER FUSELAGE. THE REPAIR REFERENCE OF PRE PREG SEND TO THE WET LAY UP REPAIR FOR THAT REASON WAS DOCUMENTED BOTH ON STEPS 3 AND 4. REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW SRM 51-70-05-2R-9 REPAIR 9.Sep 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2026102193853Angle · crackedCRACK SLAT 3 OTBD ANGLE OF INBOARD AUXILIARY TRACKAT LT WING. REPLACED OUTBOARD ANGLE OF INBD AUXILIARY TRACK AT LT WING IAW SRM 51-40-02-0G-0 AND SKIN PAD ADJUSTMENT IAW AMM 27-81-00-820-803. ADJUSTMENT IS OK.Sep 11, 2026 · N8658A · Boeing 7378H4 · Leading Edge DevicesSDR SWAA2026102150779Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 540, LBL 6 IN THE LT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 212A1110, SHT 11, REV-, & PERFORMED GENERAL VISUAL INSPECTION ON AREA WHEN SUPPORT BRACKET WAS REMOVED AND NO FOUND DSep 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026101803114Skin · crackedRT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1 EA CRACK NOTED AT RIB 25. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98679 AND EA 300-5753-27-A4632, REV-.Sep 11, 2026 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR SWAA2026101961698Door Frame · crackedFED UPPER DOOR SURROUND CUTOUT FRAME WAS CRACKED AT BS 312, STR 5L. THE DOOR FRAME WAS REPAIRED IAW EA M-22-153-01244 LBL 33 BETWEEN S5L & S6L.Sep 11, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2026101980796Angle · crackedCRACKED ANGLE ON LINING ACCESS PANEL 831AW. REPLACED THE ANGLE IAW SOPM 20-50-12, REV 58, AND DWG 411A2111, SHEET 35, REV B.Sep 11, 2026 · N8656B · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2026101961032Angle · crackedCRACKED ANGLE ON LINING ACCESS PANEL 841AW OF AFT SERVICE DOOR. REPLACED THE ANGLE IAW SOPM 20-50-12, REV 58, AND DWG 411A2112, SHEET 28, REV B.Sep 11, 2026 · N8656B · Boeing 7378H4 · Service DoorsSDR SWAA2026101953037Crossbeam · crackedPASSENGER CABIN FLOOR CROSSBEAM CRACKED, TOP PLATE ONLY, AT BS 540, RBL 27, WL 208. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 143A0060, REV B.Sep 11, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, StructureSDR IPXA2026101698760Skin · delaminatedMAJOR REPAIR, APU COMPARTMENT SKIN PANEL HAS EVIDENCE OF DELAMINATION APPROX BTW BS 1885 AND BS 1896, STGR 17R AREA,Sep 11, 2026 · N402UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026101599728Retainer · brokenRIGHT FUSELAGE SECTION 48 INTERIOR STRUCTURE RIB ASSY ANGLE SUPPORT HAS A SEAL RETAINER BROKEN APPROX AT BS 1963.80, BL 0 THRU RBL 10, LOCATED AND DRILLED SEAL RETAINER AT STA 1963 BL 0 THRU RBL 10 SIDE I.A.W B757-200 S.R.M 51-40-05-0G-0.Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026101203705Floor Support · corrodedAFT CARGO FLOOR STGR SPLICE EXFOLIATED IN 2 PLACES STR 30L, BS 1460 REMOVED THE INCOMING REPAIR INSTALLED BY SB 757-53A0053 R1. IAW E.A 757-5360-01-B0851, REVISON: P2, STEP 9Sep 11, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 2026FA0000839Bracket · out of positionRIGHT ENGINE (#2) REAR COWLING BRACE PIN CABLE CAUGHT AROUND THROTTLE LEVER AND WOULD NOT ALLOW THROTTLE MOVEMENT. CABLE AND BRACKET WERE ADJUSTED TO PREVENT FUTURE ISSUES. THIS OCCURRED AFTER ENGINE START ON THE GROUND.Sep 11, 2026 · N900BF · Raythn HAWKER900XP · Engine Controls