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.
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 HNAA2026072400614Floor Support · not reportedLEFT OTBD FLOOR SILL FROM FR 47 TO FR 51 HAS CORROSION. REMOVED AND REPLACED LT OTBD FLOOR SILL FROM FR 47 TO FR 51 IAW SRM 51-40-02-PR.SDR HNAA2026072400613Floor Support · corrodedLEFT OTBD FLOOR SILL FROM FR 53 TO FR 57 HAS CORROSION. REMOVED AND REPLACED WITH NEW LT OTBD FLOOR SILL FROM FR 53 TO FR 57 IAW SRM 51-40-02-PR.SDR HNAA2026072400612Floor Support · corrodedRIGHT OTBD FLOOR SILL FROM FR 53 TO FR 57 HAS CORROSION. REMOVED AND REPLACED WITH NEW RT OTBD FLOOR SILL FROM FR 53 TO FR 57 IAW EMB 145 SRM 51-40-02-PR.SDR SWAA2026072176920Shield · corrodedIN THE AFT CARGO BAY RIGHT SIDE, THE SHIELD ASSEMBLY JUST FWD OF THE ENTRY THRESHOLD IS CORRODED. BLENDED AREAS OF CORROSION AT AFT CARGO BAY RIGHT SIDE; THE SHIELD ASSEMBLY JUST FWD OF THE ENTRY THRESHOLD; BLENDS FOUND TO BE OUT OF LIMITS ALL IAW SRM 53-0SDR SWAA2026072167251Angle · corrodedAFT CARGO BAY RT TRANSITION ANGLE, RBL 21, BS 727J+14 WAS CORRODED AT NUTPLATE HOLE. BLENDED AREAS OF CORROSION IN THE AFT CARGO BAY. RT TRANSITION ANGLE, RBL 21, BS 727J+14; BLENDS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. CUT AND REMOVED DAMAGED ASDR IPXA2026062250751Skin · gougedMAJOR REPAIR, GOUGE ON UNDERSIDE OF TAIL SECTION LOCATED NEAR FR 83, STR 44R. ACCOMPLISHED UT PER NTM 51-10-04 LOWEST MIN IS 0.056, ACCOMPLISHED HFEC SURFACE SCAN OF REPAIRED AREA IAW NTM 51-10-08. NO CRACKS DETECTED AT THIS TIME.SDR U2R2026F00000Frame · crackedDURING OPEN HOLE INSPECTION, DETECTED DEFECT SIGNAL AT FRAME WEB BS 1265. PERFORMED REPAIR IAW NAL FCD 744-53-0014 AND DWG 624U0060.SDR CALA2026071617804Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STAB LOWER SKIN AT STAB STA 157.10 , INBD ROW , 8 1/2" FROM REAR SPAR. CRACK LENGTH 1. ACCOMPLISHED REPAIR AT LT HORIZONTAL STAB, LOWER SKIN AT STA 157.10, INBD ROW 8 1/2 FROM REAR SPAR IAW SRM 55-10-01-2R-11.SDR 2026FA0000581Control Cable · bindingLH ENGINE THROTTLE CONTROL STIFF / BINDING.SDR U2RA2026071100033Skin · damaged.LIGHTNING-STRIKE DAMAGE FOUND ON THE FUSELAGE SKIN AT STA 225, STRINGER S-23R. PERFORMED REPAIR IAW BOEING BCS CASE MUA-MUA-26-0085. DATA APPROVED BY FAA FORM 8100-9 DATED 06/28/2026.SDR 2026FA0000574Strut · brokenDURING TAXI, FAILURE OF THE LEFT MAIN LANDING GEAR OCCURRED AROUND THE OLEO STRUT PISTON TUBE BOLT HOLE. PIPER AIRCRAFT SERVICE LETTER 1263 RECOMMENDS ROUTINE INSPECTION OF THIS FAILURE POINT EVERY 700 HOURS TIS ON AIRCRAFT WITH OVER 6,500 TOTAL HOURS IN SERVSDR IPXA2026070240523Support Bracket · crackedCRACKED ANGLE, RT BLG W/W HYD TUBE SUPPORT BRACKET AT BS 1480 UNDER BLG HYD TRUCK POSITIONER SHUTOFF FUSE. REVIEWED TASK IAW GMM-MTX 09.05.01.09. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G REV.107, AND DWG 272U4448, SH 6, REV B.SDR DALA2026070703949Relay · faultedATB- DUE TO THE AIRCRAFT NOT PRESSURIZING WITH AN ASSOCIATED -ALL PACKS OFF- MESSAGE. REPLACED R2-5104 PACK SHUTDOWN/AUTO OFF RELAY AND PERFORMED VERIFICATION FLIGHT. OPS CHECK GOOD.(8318756)(AIRCRAFT GROUNDED)SDR HNAA2026070600578Bushing · misinstalledUNRECORDED BUSHING REPAIR ON RHFUSE II SKIN, AT FR77 BTW STR8-9R. REPAIRED IAW SRM 53-32-01 ITEM:9 FIG-213SDR SWAA2026070614164Access Panel · crackedUPON ACCESS TO LT HORIZONTAL STAB ACCESS PANEL 333AB; NOTED THAT THE SHARK-FIN PLATE DAMAGED & CRACKED UPON ACCESS TO LT HORIZONTAL STAB ACCESS PANEL 333AB NOTED THAT THE SHARK-FIN PLATE DAMAGED. REMOVED DAMAGED SHARK FIN IAW SRM 51-40-02-0G-0. RECEIVED NEW SSDR SWAA2026070213650Intercostal · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AND STR 26R FWD CARGO COMPARTMENT. REPLACED INTERCOSTAL AND NEW FASTENERS LOCATED BTW BS 500A - 500B, STR 26R FWD CARGO BAY IAW SRM 51-10-02 STEP 9 & SRM 51-40-02 AND DWG 143A7505; SHEET 137; REV -.SDR AALA202607017104Plunger · missingAIRCRAFT IN BASE MAINTENANCE: RH AFT EMERGENCY EXIT DOOR HANDLE MISSING CENTER BUSHING PLUNGERS AND SPRINGS INSTALLED EMERGENCY EXIT DOOR HANDLE CENTER BUSHING PLUNGERS AND SPRINGS IAW B737-NG AIPC 52-22-51 AND AMM 52-22-51.SDR AALA202607014982Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202607019658Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202607012111Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202607011257Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202607012215Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202607017581Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR IPXA2026070154082Isolation Mount · crackedCOCKPIT CEILING ABOVE OVERHEAD PANEL ISOLATOR BRACKET CRACKED. REMOVED DAMAGED BRACKET AT COCKPIT CEILING ABOVE OVERHEAD PANEL BS 297 IAW SRM 51-40-02-0G-0 PAR 4. INSTALLED PANEL 232N1642-4 AT COCKPIT CEILING ABOVE OVERHEAD IAW SRM 51-40-02-0G-0.SDR R61A2026070100180Skin · gougedDURING HEAVY CHECK FWD FUSELAGE AFT PANEL OF LOWER SKIN, GOUGE FOUND BETWEEN FR17-18 AND STGR 26R-27R. FWD FUSELAGE AFT PANEL OF LOWER SKIN, GOUGE FOUND BETWEEN FR17-18 AND STGR 26R-27RREPAIRED IAW ETD2026-170-011110. HFEC PERFORMED WITH NO CRACKS FOUND.SDR YENA2026063000505Bulb · inoperativeDURING HEAVY MAINTENANCE, DOES NOT PASS TEST OF EMERGENCY LIGHT EPSU LH AT PASSENGER CABIN ; REF AEROMAN WO# 2026-267/1 NR 2026-305064 REMOVED AND REPLACED BULB IAW AMM 33-51-15-000-001-A. AND AMM 33-51-15-400-001-A. AND PERFOMED OPERATIONAL TEST EMERGENCY LSDR YENA2026063000504Slide Raft · failedDURING HEAVY MAINTENANCE, DOOR SLIDE "R2" INDICATION SHOWS ARMED ON THE GROUND, BUT AS SOON AS CAB PRESS REACHES 6.0, IT SHOWS DISARMED (6.0 PSI); REMOVED & REPLACED R2 ESCAPE SLIDE RAFT PACK ASSY IN REF. AMM 25-62-44, OPS CHK GOOD. AS PRECAUTIONARY, PRESSURIZSDR IPXA2026062754538Pad · corrodedNR 1 ENGINE O/B CORE COWL T/E RUB PAD, 3RD FROM BOTTOM, HAS AREA OF CORROSION. INSTALEED SERVICEABLE PART AT NR 1 ENGINE OTBD CORE COWL T/E STOP PAD, 3RD FROM BOTTOM IAW SRM 51-40-02-0G-0.SDR MASA20260626166Structure · corrodedDURING HEAVY CHECK INSPECTIONS OF INTERNAL CFIII FLOOR STRUCTURE, CORROSION FOUND ON UPPER SHEET AT RBL 11, BETWEEN FR 85 RT TO FR 86 RT HAS BEEN REMOVED AND REPLACED IAW SRM 51-43-01. REV 46,SDR MASA20260626165Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS OF INTERNAL CFIII FLOOR STRUCTURE, CORROSION FOUND ON BEAM AT RBL 11, BETWEEN FR 86 RT TO FR 89 RT HAS BEEN REMOVED AND REPLACED IAW SRM 51-43-01 AND SRM 51-42-01. REV 46, NRC 4502654-1000-0041.SDR DALA2026062603806Stringer · damagedVIASAT, S1R AND FUSELAGE SKIN, FWD OF FRAME 60, TOOLING DAMAGE. COMPLIED WITH ERA 627536-14 REV C. (1655809) AIRCRAFT WAS GROUNDED.SDR CALA2026062617353Floorbeam · corrodedCORROSION FOUND AFT CABIN WET AREA AT STA 947.5 RBL 52 HAS SPOT OF CORROSION ON AFT WET AREA FLOORBEAM AT BS 947.5, RBL 52. ACCOMPLISHED REPAIR AT FLOORBEAM AT BS 947.5, RBL 52 IAW SRM SRM-53-70-51-2R-5, & SRM 51-40-02-0G-0. ACCOMPLISHED REPAIR AT FLOORBEAM ASDR R61A2026061900168Unknown · odorFA AND PASSENGER REPORTED SMELLING TAR BURNING IN CABIN SHORTLY AFTER PASSING THROUGH 23000 FEET. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CYCLED PACKS 1 AND 2.SDR FDEA202606190784Floor Panel · crackedCRACK L=2.500" ON UPPER SURFACE OF FLOOR PANEL 242SFF AT MDC. FLOOR PANEL 242SFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025SDR AALA202606257597Elec Connector · not seatedAIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHT ON ROW 18ABC IS INOPERATIVE. MAINTENANCE FOUND SIDEWALL CONNECTOR 7260VC7 NOT FULLY SEATED. SECURED CONNECTOR AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST PER AMM 33-51-00 WITH NO ISSUES NOTED.SDR FDEA202606190795Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,-Y1959 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,Y1959 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH EA 6-5313-69642.SDR FDEA202606190794Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK SEAT TRACK FR36-FR38.1,Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR36-FR38.1,Y450 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH SRM 53-10-16, FIG 203.SDR FDEA202606190793Crossbeam · no discrepancyEXISTING REPAIR ON MAIN DECK CROSSBEAM FR38,Y0~Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM FR38, Y0~Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5314-69630SDR FDEA202606190787Skin · delaminatedDELAMINATION ON LWR SURFACE OF THE SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE, LH WING SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE LH WING WAS REPAIRED IAW B767 SRM 57-70-01-2R FIG 201 REP 1 SHEET 2 AND SRM 51-70-17-0G PAR SDR AALA202606245871Line · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAS DUE THE FLIGHT CREW REPORTING THAT WHILE IN FLIGHT OIL QUANTITY IN NUMBER 1 ENGINE FELL TO 0. PRESSURE STAYED. THE AIRCRAFT LANDED SAFELY AT LAS WITHOUT FURTHER INCIDENT. MAINTENSDR AALA202606247198Elec Connector · looseAIRCRAFT WAS NOT GROUNDED: FUEL RIGHT TANK PUMP 1 LOW PRESSURE ECAM AT CRUISE WITH ASSOCIATED FAULT LIGHT ON RIGHT TANK PUMP 1 SWITCH, THE FLIGHT CREW TURNED RIGHT TANK PUMP 1 SWITCH OFF AS PER ECAM SUPPLEMENTAL INSTRUCTIONS. MAINTENANCE FOUND LOOSE AND CONTASDR DALA2026062403760Wire · cut48AB SEAT NON PHOTOLUMINESCENT BULB IN ON ESCAPE PATH. FOUND WIRE FOR 48AB EMERGENCY ESCAPE LIGHT SHEARED. SPLICED EMERGENCY ESCAPE LIGHT WIRE TOGETHER. OPS NORMAL. (9078664) (AIRCRAFT GROUNDED)SDR DALA2026062403759Lens · out of positionEMERGENCY EXIT SIGNS INOPERATIVE. REINSTALLED EMERG LIGHT COVER IN CORRECT POSITION IAW AMM 33-51. (1654728) (AIRCRAFT GROUNDED)SDR CALA2026062417313Hmu · faultedRIGHT ENGINE COMPRESSOR STALLED ON ROTATION NO EXCEEDENCES. PERFORMED FAULT ISOLATION NR 2 ENG IAW FIM 71-05, TASK 807, STEPS A - E, NO DEFECTS NOTED. NR 2 ENGINE BORESCOPE PLUGS REMOVAL & INSTALL CONTINUED FAULT ISOLATION PROCEDURE ON FIM 71-05, TASK 807, SSDR CALA2026062417301Seat Track · corrodedCORROSION FOUND IN CABIN AT BS 500I, LBL 45.50. ACCOMPLISHED SEAT TRACK REPAIR, BS 500I - 520, LBL 45.5 IAW SRM 53-00-52-2R-4.SDR CALA2026062317287Light · broken24C FLOOR EMERGENCY LIGHTING DAMAGED PICTURE ADDED SECURED LIGHT HOUSING AND TESTED LIGHT. BOTH THE HOUSING AND THE LIGHT ARE GOOD. TRIM AT SEAT 24C BROKEN, SECURED IN PLACE. EPL WORKS. RESECURED WITH ZIP TIES. APPROVED TRIM AT SEAT 24C PLACED. A PASSENGERSDR CALA2026062217273Governor · faultedENGINE PARAMETER MISMATCH. ENG 2 N1 MUCH HIGHER WHILE EPR WAS L ESS. ENG 2 FF HIGHER. DUE TO PREVIOUS AIR RETURN REQUIRES FURTHER TESTING AND POSSIBLE ENG RUN. PERFORMED TEST 9 ON NR 1 AND NR 2 ENGINE IAW AMM 71-00-00-715-170-R03. BOTH ENGINES N1 N2 N3 & FUELSDR CALA2026062217261Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1676 FAILS CAPACITY CHECK, REMOVED AND REPLACED M1676 BATTERY PACK IAW AMM TASK 33-51-06-960-805. OPS CHECK NOT GOOD FROM TEST SWITCH AT POWER SUPPLY ONLY. POWER SUPPLY NIS CLE AND PLACED ON AOG. REMOVED AND REPLACED EMERGENCY LSDR SWAA2026062313906Door · inoperativeAIRCRAFT LEFT FA SEAT RETRACTABLE FLASHLIGHT DOOR INOPERATIVE. OKAY TO CONTINUE PER MEL 25-28-01B. DOOR LEFT IN COCKPIT. MDDR 325156 SP1B. R & R AFT GALLEY LEFT F/A SEAT HINGE ON FLASHLIGHT OTBD DOOR IAW AMM 25-25-12. OPS CHKD GOOD.SDR SWAA2026062314189Flashlight · inoperativeF/A FLASHLIGHT IN FWD GALLEY INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-64-00-SWA-807-MAX-01.