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 AALA202608316505Actuator · fault messageAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT HAD AN INTERMITTENT CONDITION RESULTING IN ALL 5K LBS OF CENTER TANK FUEL POTENTIALLY BEING TRAPPED FUEL - THE FLIGHT CREW CONFIRMED ALL MEL 28-05H PROCEDURES HAD BEEN COMPLIED WITH BUT ON CLIMB OUT HAD AN ECAM SDR IPXA2026082983908Evas Unit · damagedCAPTAIN`S EVAS UNABLE TO DO BATTERY & BLOWER CHECK DUE TO TEST BUTTON SEEMS TO BE LOOSE INSIDE BOX. THE EVAS WAS REPLACED IAW AMM 25-69-00 PB. 401, REV 05-03-21. REF AIPC 25-69-00-01-001 REV. 05-03-21.SDR IPXA2026082983557Slide · no testCREW ENTRY DOOR SLIDE ARMED WARNING LIGHT DOES NOT TEST. R & R ESCAPE SLIDE LIGHT INDICATION PER AMM 52-73-11. NO HELP. SHOT WIRES 1 & 2 ON FIN 7WN LIGHT ASSY FOR VOLTAGE WITH TEST BUTTON PUSHED & RECEIVED LESS THAN 1 VOLT DC. CK GRD TO GRD & GOT 00.3 OHMS FRSDR IPXA2026083188098Tire Tread · separatedNUMBER 6 TIRE LOST TREAD FROM ENTIRE CIRCUMFERENCE. CASING PLIES SHOWING. EMERGENCY DECLARED. REPLACED NR 6 MAIN WHEEL ASSY IAW MM 32-45-01-4.SDR 6CBA2026083126001Warning Light · illuminatedDURING FLIGHT FROM KLAL TO KLZU, THE CREW RECEIVED A LH FUEL QTY FAIL CAS, AND AN ASSOCIATED FUEL IMBALANCE CAS APPEARED. THE CREW FOLLOWED THE QRH AND NOTED THE RECOMMENDATION WAS TO LAND AS SOON AS POSSIBLE. AN EMERGENCY WAS DECLARED AND THEY PERFORMED A SSDR DALA2026083104909Bottle · low pressureDOORS 1L, 2L, 3L, 4L, 4R, & 3R ASSIST BOTTLES LOW. CORRECTIVE ACTION: SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. (9317309) AIRCRAFT WAS GROUNDED.SDR SIMA20260829001Sign · crackedEXIT SIGN ABOVE 1R DOOR MISSING. INSTALLED EXIT-MARKING-SIGN LENS ON R1 DOOR IAW AMM33-50-17 OPS CHECK GOODSDR WX0A2026083132939Epsu · inoperative(AIRCRAFT NOT GROUNDED) EPSU TEST RESULT BAT/EPSU (11WL) EMER LT. R & R EPSU BATTERY AT FIN 11WL IAW AMM REF 33-51-38-000-002-A AND 33-51-38-000-002-A. OPS CHECK PERFORMED, OPS CHECKED GOOD.SDR IXXA20260829076Sign · inoperativeCOCKPIT EMERGENCY EXIT SIGN INOPERATIVE. WILL NOT TEST OR TURN ON. SUPERNUMERARY EMERGENCY LIGHTS WORK WHEN TESTED. R & R FLIGHT DECK DOOR EMERGENCY LIGHT ASSEMBLY IAW WDM 33-51-11, & IAI SUPPLEMENTAL MANUAL 33-51-01. OPS CHECKED GOOD.SDR ABXA20260829376Pump · defectiveNR 1 CENTER HYDRAULIC PRIMARY PUMP FAILED (PRESS LIGHT ON) AFTER PUSH AND START. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED ACFT. MTX REMOVED AND REPLACED #1 CNT HYD PUMP IAW B767 AMM 29-11-02 OPS CHECK GOOD AND RETURNED A/C TO SERVICE.SDR SCNA20260831375Light · no testL2 EMERGENCY LIGHT ASSY DID NOT TEST. REPLACED ATTENDANTS L2 EMERGENCY LLIGHT ASSY IAW AMM 25-64-00SDR CALA2026083119096Lamp · inoperativeR2 DOOR EXTERIOR EMERGENCY LIGHT INOP REPLACED LAMP REF AMM 33-51-00 NO HELP, FUTHER TROUBLE SHOOTING REQUIRED. RELAMPED R2 DOOR EXT EMERG LIGHT IAW 33-51-00. OPS CHECK NORMALSDR CALA2026083119076Skin · puncturedPUNCTURE BETWEEN AFT CARGO DOOR AND R3 ENTRY DOOR ON THE RIGHT SIDE OF ACFT. DAMAGE LOCATED BTWN BS 1439 & 1461 IAW SRM 53-00-00-0G-0. FOUND DAMAGE TO BE 5.4 INCH LONG BY 2.6 INCH WIDE, ON BS 1439 - 1461, STR 21-22R. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-SDR CALA2026083119071Pump · leakingSUSPECTED POTABLE WATER LEAK AFTER DEPARTURE, RATE 1GAL/10 SECS. FOUND WATER LEAKAGE FROM AFT WATER PUMP. REPLACED AFT WATER PUMP, OPS CHKD OK. IAW AMM DMC-B787-A-38-15-07-00A-720A-A.SDR CALA2026083119070Door · openHIGH FREQUENCY VIBRATION HEARD & FELT ON FLIGHT DECK & FWD LAV. FOUND EXTERNAL POWER DOOR OPEN UPON ARRIVAL. INSPECTED EXTERNAL POWER DOOR AND SURROUNDING AREA. NO DEFECTS NOTED. VERIFIED EXTERNAL POWER DOOR CLOSES AND SECURES PROPERLY IAW AMM 52-49-02-40SDR CALA2026083119039Unknown · odorAFTER 2ND ENG START, BURNING PLASTIC ODOR IN BACK WITH VISIBLE SMOKE IN AFT GALLEY. PILOT STATED THE PLASTIC ODOR RETURNED AFTER ENG 2 WAS STARTED & APU DESELECTED, ENG 1 ON. ACCOMPLISHED ENGINE RUN. ATTEMPTED TO REPLICATE FLT CREW ENGINE START PROCEEDURE ASDR CALA2026083119029Power Unit · faultedBURNING ODOR FROM OUTLET AT SEAT 22F PAX AT 22F HAD A CHARGER PLUGGED INTO OUTLET. THE DEVICE GOT VERY HOT AND CABLE BURNED. SEVERAL PAX SMELLED BURNING & REPORTED TO FA. SMOKE & ODOR DISSIPATED AFTER BEING UNPLUGGED. DEVICE & CABLE STORED IN THERMAL CONTAINSDR CALA2026083119025Relief Valve · faultedTHUMPING NOISE AT DOOR 1R INFLIGHT. DURING A DETAILED VISUAL INSPECTION OF R1 DOOR, FOUND LOWER DOOR BUSTLE DETACHED & LOOSE ON FWD SIDE. BUSTLE RESECURED IAW AMM 25-66-01-416-010. WHILE CARRING OUT THE EXCESSIVE CABIN PRESSURE LEAKAGE TEST IAW AMM 05-51-2SDR CALA2026083119023Outflow Valve · faultedCABIN ALT AUTO 1 EICAS M THE AUTOMATIC PRESSURIZATION CONTROLLER 1 BITE FOUND A FAILURE. CABIN ALT UP TO APPROX 13000 FEETAS PER TOMC REQUEST REPLACED CABIN AUTO 1 PRESSURE CONTROLLER IAW AMM 21-31-02-004-00 & AMM 21-31-02-404-005 UP TO SECTION 3(D)1. REPLACESDR CALA2026083119021Battery Pack · faultedTHE EMERGENCY LIGHT BATTERY PACK, DEEP CYCLE CHECK FOUND BATTERY LOW ON R2 DOOR POWER SUPPLY M33098. REPLACED M33098 BATTERY PACK, INSTALLATION INSPECTION AND INSTALLATION TEST FOUND NORMAL IAW AMM 33-51-06-960-801, REV 107, GMM 09-10-05 REV 202.SDR CALA2026083119019Battery · no testLLAR BACK UP LIGHT BATTERY LOW. REPLACED LLAR BACK UP LIGHT BATTERY PACK. . INSTALLATION TEST FOUND NORMAL IAW AMM 33-29-01-960-809, REV 107, GMM 09-10-05, REV 202.SDR CALA2026083119017Battery Pack · no testTHE EMERGENCY LIGHT BATTERY PACK, DEEP CYCLE CHECK FOUND BATTERY LOW ON THE DOOR 2R POWER SUPPLY M33097. REPLACED M33097 BATTERY PACK AND INSTALLED INSPECTION INSTALLATION TEST FOUND NORMAL. IAW AMM 33-51-06-960-802, REV 107, GMM 09-10-05 REV.202.SDR AALA202608305033Battery Pack · inoperativeAIRCRAFT WAS NOT GROUNDED: DURING PS CHECK OF CABIN EMERGENCY LIGHT AT R4 DOOR WERE INOP. MAINTENANCE REPLACED POWER SUPPLY - BATTERY PACK M1672 AT AFT GALLEY CEILING PANEL IAW AMM 33-51-06 OPS TEST NORMAL.SDR AALA202608307720Tire · deflatedAIRCRAFT WAS NOT GROUNDED: IN CRUISE-LEFT MAIN TIES MESSAGE: TIRE 01 153LBS TIRE 02 224 LBS. TIRE 01 PRESSURE STEADILY DECREASED REF MIC 8137457. EMERGENCY DECLARED AS A PRECATION AND AIRCRAFT LANDED WIHTOUT ISSUE. MAINTENANCE REPLACED #2 MLG TIRE IAW AMM 32-4SDR AALA202608309828Oven · odorAIRCRAFT WAS GROUNDED: THE FLIGHT ATTENDANTS REPORT THAT WHEN STARTING TO USE THE LEFT OVEN A STRONG BURNING PLASTIC SMELL STARTED. THEY TURNED OFF THE OVEN AND THE SMELL DISSIPATED. MAINTENANCE REPLACED GALLEY OVEN IAW AMM 25-32-03 .SDR AALA202608303210Start Valve · stuckAIRCRAFT WAS GROUNDED: START VALVE OPEN LIGHT IN FLIGHT. DECESION MADE TO RETURN TO PHX, EMERGENCY DECLARED AND AIRCRAT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED ENG 1 START VALVE IAW AMM 80-11-03. .SDR DALA2026083004891Unknown · odorON DESCENT THROUGH 15000 FA FRONT AND BACK OF THE PLANE SMELLED A STRONG DIRTY SOCK SMELL THAT PERSISTED UNTIL LANDING AND SLOWLY DISSIPATED AFTER, THEY SMELLED A CHEMICAL SMELL AS WELL AFTER OPENING CABIN. PER P TRAK RESULT, DEEMED APU CHANGE REGUIRED. REPLSDR DALA2026083004889Skin · ground damagePUSH BACK TUG STRUCK NOSE OF A/C NEAR GROUND POWER DOOR. COMPLIED WITH ER/A 636558-14 REV. ORIG. PRI REV. 0, 1, 2, & 3 REPAIR INSTRUCTIONAL STEPS. ENSURED ALL ER/A 636588-14 REV. ORIG. PRI REV. 0, 1, 2, & 3 REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH SDR R61A20260829485Skin · crackedFOUND IN HEAVY CHECK-CRACK DAMAGE AFFECTING THE LH WING MAIN BOX LOWER SKIN, LOCATED IN THE END POINT OF STGR 19, BETWEEN RIBS 16-17.SDR VNAA202610300022Drag Angle · crackedCRACK ON PREVIOUSLY REPAIR DOUBLER OF RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE. PREVIOUSLY REPAIR DOUBLER OF RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE ON 67.5% REAR SPAR DATUM AT SDR VNAA202610300021Frame · corrodedCORROSION ON FRAME STRG 26L AND 26R STA 1051 AT AFT CARGO COMPARTMENT. CORROSION FRAME STRG 26L AND 26R STA 1051 AT AFT CARGO COMPARTMENT WAS REMOVED PER SRM 51-21-06-001-001-A01, WAS EVALUATED, THEREFORE THERE ARE OUT LIMITS PER CRJ-700 SRM 53-61-06-101-003SDR HNAA2026100900966Floor Support · crackedLH OMEGA BEAM FLANGE CRACKED AT FR 26. REPAIRE DFLANGE IAW ETD 2026-145-015161 AND EO 1-53-26-0439SDR HNAA2026100600965Floor Support · crackedCTR OMEGA BEAM CRACKED AT FR 27. REPAIRED IAW ETD2026-145-015174SDR AALA202610063512Link · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FLAP TRACK 2 INBOARD LINK - MAINTENANCE REPLACED LINK PER SRM 51-42-11SDR SWAA2026100547731Support Angle · crackedCRACKED SUPPORT ANGLE, BS 663, RBL 8. REPLACED THE SUPPORT ANGLE AND FASTENERS, BS 663 BTWN RBL 5 - 65 IAW SRM 51-10-02, ITEM 8, SRM 51-40-02-0G-0, DWG 111A1000, SHEET 329, REV A & DWG 111A1000, SHEET 389, REV-.SDR SWAA2026100549788Support Angle · crackedCRACKED SUPPORT ANGLE, BS 663, LBL 8 IN THE AIR CONDITIONING BAY. PERFORMED CLEANING OF FASTENERS HEADS IAW SOPM 20-30-03. REPLACED THE SUPPORT ANGLE AND FASTENERS, BS 663, BTWN LBL 5 - 71 IAW SRM 51-10-02, ITEM 8, SRM 51-40-02-0G-0, DWG 111A1000, SHEET 32SDR HNAA2026100500946Yoke · damagedPYLON YOKE 2 UPPER FLANGE, LT & RT FWD RIVET HOLES ELONGATED. UPSIZED HOLES, INSTALLED BUSHINGS AND RIVETS IAW SB 145-54-0008SDR HNAA2026100200939Floor Support · crackedCTR OMEGA BEAM CRACKED AT FR 28. REPAIRED IAW ETD 2026-145-015174 AND EO 1-53-26-0441SDR HNAA2026100200938Support · corrodedLEFT SILL NR 2 CORRODED. R & R SILL IAW SRM 51-40-02.SDR HNAA2026093000929Floor Support · cracked53-2074 LH OMEGA BEAM IB FLANGE CRACKED AT FR28. REPAIRED IAW ETD 2026-145-015161 AND EO 1-53-26-0439SDR HNAA2026093000927Floor Support · crackedLEFT OMEGA BEAM IB FLANGE CRACKED AT FR26. REPAIRED IAW ETD 2026-145-015161 AND EO 1-53-26-0439SDR HNAA2026093000926Floor Support · crackedLH OMEGA BEAM IB FLANGE CRACKED AT FR 24. REPAIRED IAW ETD 2026-145-015161 AND EO1-53-26-0439SDR HNAA2026093000924Floor Support · crackedLH OMEGA BEAM CRACKED AT FR36. REPAIRED IAW ETD 2026-145-015226 AND EO 1-53-26-0439SDR HNAA2026093000920Plate · corrodedFWD CTR DIGITAL PLATE CORRODED. R & R DIGITAL PLATE IAW SRM 53-21-10SDR HNAA2026093000919Floor Support · crackedLH OMEGA BEAM IB FLANGE CRACKED AT FR31. REPAIRED IAW ETD 2026-145-015218 AND EO 1-53-26-0440SDR HNAA2026093000918Floor Support · crackedLEFT INBD OMEGA BEAM FLANGE CRACKED AT FR30. REPAIRED IAW ETD 2026-145-015218 AND EO 1-53-26-0440SDR HNAA2026092900917Floor Support · crackedCTR OMEGHA BEAM CRACKED AT FR27. REPAIRED IAW ETD 2026-145-015074 AND EO 1-53-26-0441SDR AALA202609270763Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 35 AND Y765 RIGHT - REPLACED SEAT TRACK PER SRM 51-72-11SDR AALA202609272690Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 35 AND Y1292 RIGHT - REPLACED SEAT TRACK PER SRM 51-72-11SDR U2RA2026092700064Battery · no testDURING A SYSTEM TEST ON EPSU 16WL FOUND "BATTERY FUALT" LED ILLUMINATING. REMOVED AND REPLACED BATTERY ON EPSU 13WL IAW A330 33-51-38-420-050-A REV25, TEST GOOD