Service difficulty reports
1,770,281 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 UIEA2026100800970Power Supply · inoperativeR/H #5 SLIDE LIGHT INOP(<P>REMOVED AND REPLACED POWER SUPPLY ASSY IAW AMM 33-51-07. OPS CHECK GOOD AT THIS TIME, REF AIPC 33-51-07.</P>)SDR UIEA2026100800971Power Supply · inoperativeRH #6 SLIDE LIGHT INOP AND #7 SLIDE LIGHT INOP(<P>REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51-07 & IPC 33-51-07. OPS CHECK GOOD AT THIS TIME.</P>)SDR VNAA2026100826402Washer · disconnectedOVERHEAD BIN INTERFERES WITH L/H AFT OVERWING EMERGENCY EXIT DOOR OPENING / FOUND OVERHEAD BIN EYELET TO BE DISCONNECTED AT L/H AFT EMERGENCY DOOR. RECONNECTED EYELET IAW AMM 25-23-01-400-801-A50-PSA. OPS CHECKS GOOD AT THIS TIME.SDR DALA2026100805567Battery · faultedDURING SVC CK FOUND OVERWING DOOR RT EPSU BATTERY (16WL1) FAULTED ON CIDS TEST. REPLACED OWD R EPSU BATTERY (16WL1) IAW AMM 33-51. OPS TEST GOOD. (LP 8965314 - AIRCRAFT WAS GROUNDED)SDR DALA2026100805563Light · damaged42H AND 42B EMERGENCY LIGHTS DAMAGED. REPLACED LIGHT ASSY IAW AMM 33-51. OK FOR SERVICE. (9141287) AIRCRAFT WAS GROUNDED.SDR ABXA20261008462Warning Message · false activationRIGHT ENGINE FIRE LOOP 2 STATIC MSG. MTC PERFORMED OPS TEST OF RIGHT ENGINE FIRE LOOP IAW AMM 26-11-00, OPS TEST GOOD. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.SDR DALA2026100805562Light · missingEXIT LIGHTING STRIP AND TRIM MISSING IN FRONT FWD SIDE, INSTALLED EMERGENCY LIGHTING STRIP IAW AMM 23-50. (8981540) (AIRCRAFT GROUNDED).SDR ABXA20261008461Sensor · brokenNOSE A/G DISAGREE THAT RESULTED IN TAKEOFF CONFIG ON CLIMB OUT. CREW AIR TURNED BACK TO CVG (ATB) AND LANDED WITHOUT FURTHER INCIDENT. MTC FOUND NLG SENSOR S266 TARGET & SENSOR BUSTED. REMOVED & REPLACED S266 IAW B767 AMM 32-09-08. REPAIRED SENSOR TARGET IAW SDR FDEA202610081495Doubler · crackedRIGHT WING, FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 667 REMOVED AND INSTALLED WITH FABRICATED RIB DOUBLER AS PER MD-11 SRM 51-31-01-0G.RIB DOUBLER FABRICATESDR FDEA202610081494Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.3". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR ISDR FDEA202610081493Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 682 FOUND CRACK ABOUT 0.2". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 682 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJSDR FDEA202610081492Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS SDR FDEA202610081491Lamp · failedPRE-FLT MX INSP, (1EA) DIRECT GALLEY OVERHEAD EMERGENCY LIGHT INOP. REPLACED THE LAMPS, IAW AMM 33-51-04-2. LIGHTS TESTED SATIS, ITEM OK FOR SVC.SDR IPXA2026102946563Angle · corrodedUNDER AFT DECK PLATE AT STA 1716, LBL 45 HAS ANGLE CORRODED. INSTALLED NEW ANGLE. AT STA 1716, LBL 45 UNDER AFT DECK PLATE. IAW SRM 51-40-02-0G-0.SDR IPXA2026102846376Support Angle · corrodedTAIL COMPARTMENT STRUCTURE THAT ATTACH APU INTEL DOOR WITH CORROSION IN THE FWD FRAME AND AFT FRAME. INSTALLED NEW UPPER ANGLE 1 EA IAW SRM 51-40-02-0G-0.SDR IPXA2026102946374Angle · corrodedUNDER THE AFT DECK PLATE AT STA 1716 AT RBL 30, HAS A CORRODED ANGLE. INSTALLED NEW ANGLE. AT STA.1716 AT RBL 30 UNDER AFT DECK PLATE. IAW SRM 51-40-02-0G-0.SDR IPXA2026102946643Angle · crackedFWD CARGO COMPARTMENT STA 560, PANEL 122AZ SUPPORT ANGLE BROKEN. INSTALLED NEW ANGLE SUPPORT IAW B757-200PF SRM 51-40-02-0G. REVIEWEDSDR SWAA2026110240734Support Bracket · crackedCRACK SUPPORT BRACKET ACCESS PANEL 834DZ AT PASSENGER CABIN. REPLACED SUPPORT BRACKET ACCESS PANEL 834DZ IN THE CABIN IAW SRM-51-10-02, SRM-51-40-02, & DWG 411A2119, SHEET 72 REV-.SDR J7SA2026110200531Fce · unserviceableBACKUP PITCH TRIM FAIL ON PREFLIGHT CHECKS. REPLACED FCE #1 IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD.SDR SWAA2026103071801Support Angle · corrodedAFT CARGO BAY FOUND CORROSION ON SUPPORT SUPPORT OF FWD SHIELD, BS 767 - 787, RBL 21, WL 165. REMOVED THE CORROSION FROM THE SUPPORT ANGLE IAW SRM 53-60-15-1A-1, STEP 4.G.(4), FIG 103 DETAIL D, & APPLIED PRIMER & PAINT IAW AMM 51-21-41-370-802, & AMM 51-21-99SDR R61A2026102800333Skin · crackedDURING C-CHECK CRACK FOUND ON LT WING FIXED LEADING EDGE SLAT TRACK NR 4 CUTOUT BETWEEN, RIB 14-15. CRACK REPAIRED IAW ETD 2026-170-017565.SDR R61A2026102800332Doubler · crackedDURING C-CHECK CRACK FOUND ON LEFT WING FIXED LEADING EDGE TRACK NR 6 CUTOUT DOUBLER. REMOVED AND REPLACED DOUBLER IAW SRM 51-41-02 AND 51-43-04.SDR R61A2026102800331Floorbeam · corrodedDURING C-CHECK FWD FUSELAGE FLOOR SUPPORT BRACKET AT FR 16, LBL 45 FOUND CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BRACKET IAW SRM 51-43-03SDR SWIA2026100777801Skin · ground damageDURING DOWN JACKING OF THE ACFT, THE TAIL JACK PAD FAILED MAKING CONTACT WITH THE FUSELAGE AND CAUSING DAMAGE. COMPLIED WITH REPAIR TO DAMAGED AREA TO REAR FUSELAGE LOWER SKIN BETWEEN FR 92 - 93, STRINGERS 29L & 29R AT THE TAIL JACKING POINT IAW ETD 2026-170-SDR IPXA2026102444654Screen · crackedAFT CARGO COMPT. FWD BULKHEAD PANEL 152CZ HAS A CRACKED PLASTIC INLET ENCLOSURE. REMOVED CRACK PLASTIC INLET ENCLOSURE AND INSTALLED NEW PLASTIC INLET ENCLOSURE IAW B757-200PF AMM 25-50-03-404-002. INSPECTED AND VERIFIED REMOVED CRACKED PLASTIC INLET ENCLOSURESDR AALA202610276707Panel · crackedAIRCRAFT IN BASE MAINTENANCE: R-4 DOOR CUTOUT AFT SIDE PANEL CRACKED AROUND FASTENER HOLES.RG-013. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR ON R-4 DOOR CUTOUT AFT SIDE PANEL IAW REF B787-9 CMM 25-00-66. REPAIR 3-1.SDR IPXA2026102644073Floor Support · corrodedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT ANGLE HAS CORROSION APPROX BTW BS 1180 AND BS 1200, RBL 63.SDR SWAA2026102646569Plate · crackedRIGHT INBD MAIN FLAP PLATE CRACKED. R & R FLAP PLATE IAW SRM 51-40-02-0G-0, & AMM 20-50-11-910-801.SDR 2026FA0000903Pushrod · bentNR 2 EGT SLOW TO RISE, UPON RUN UP, FOUND DIFFICULT TO START, ENGINE RUNNING VERY ROUGH WITH POOR ACCELERATION. FOUND NR 2 PUSH ROD AND SHROUD BENT. REAMED ALL EXHAUST VALVE GUIDES IAW LYC SI1485B, MSB 388C, SI1425A, AND THE LYC IO390-CMM. REINSTALLED THE VSDR IPXA2026102245017Strap · corrodedMAIN DECK CABIN BTW STA 1400 TO 1420 AND RBL 45.50 STABILIZATION STRAP HAS EXFOLIATION, C/W SRM 51-10-02-0G-0.SDR MASA20261022242Seat Track · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE AT FWD WET AREA, CORRODED R/H SEAT TRACK FROM FR 12 R/H TO FR 23 R/H, RBL 11. REMOVED AND REPLACED WITH NEW IAW ERJ 175 SRM 51-41-01, SRM 51-41-02, AND SRM 51-43-03. NRG# 4502703-2000-023SDR MASA20261022243Seat Track · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE AT FWD WET AREA, CORRODED UH SEAT TRACK FROM FR 12 UH TO FR 20 UH, LBL 11, REMOVED AND REPLACED WITH NEW IAW ERJ 175 SRM 51-41-01, SRM 51-41-02 AND SRM 51-43-03. NRC 4502703-2000-0279. RESDR AALA202610228777Rib · crackedAIRCRAFT IN BASE MAINTENANCE: NOTICED 2EA CRACKS ON INTERNAL STRUCTURE MAIN RIB STIFFENERS 1ST AND 2ND FROM FWD TO AFT LOWER END INBD SIDE STAB STA 92.70. REMOVED AND REPLACED RIB ASSY ON RH HORIZONTAL STABILIZER INTERNAL STRUCTURE STA 92.70 IAW SRM 51-40-02 SDR AALA202610206378Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FLOORBOARD SUPPORT HOLE. REMOVED AND REPLACED IAW AARD 51-00-05-1 AND BOEING DRAWING 147A5676.SDR IPXA2026101746122Floorbeam · corrodedUNDER DECK PLATE AT STA 1716 FROM RBL 5 AND LBL 5 HAS NUTPLATES WITH RUST. INSTALLED ANGLE IN UNDER DECK PLATE AT STA 1716 FROM RBL 5 AND LBL 5. I.A.W. SRM 51-40-02-0G.SDR SWAA2026101999456Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE AT OVERWING AREA. REMOVED AND REPLACED THE BATTERY PACKS M1668, M1669, AND M1672 IAW AMM 33-51-06-960-805. PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06-960-805.SDR IPXA2026101646046Plate · corrodedFLOORBEAM AT BS 1680 HAS A CORRODED PLATES FROM RBL 5 TO RBL 35. INSTALLED PLATES (4 EA) ON BS 1680, RBL 5 TO RBL 35 IAW SRM 51-40-02.SDR IPXA2026101946534Fitting · crackedFRAME 12A LT FITTING. 2 EA CRACK NOTED IN ZONE "A" (0.100") & (0.205") AND 1 EA CRACK NOTED IN ZONE "B" (0.130"). REPLACE THE DISCREPANT FITTING PRIOR TO FURTHER FLIGHT IAW EO-23539-REQ003. VERIFIED REMOVAL OF AIR CONDITION DUCTS TWO FR 12A LT. IAW SRM 51-40-SDR QREA202610140007Alternator · overheatedRIGHT AC GENERATOR FAILED IN FLIGHT WHICH CAUSED RH WINDSHEILD HEAT FAIL. AIRCRAFT WAS ENROUTE TO TXKF OCEANING FLIGHT FROM KHPN. EXITED ICING CONDITIONS AND RETURNED TO BASE AT KDXRSDR CALA2026101320354Light · inoperativeSIDEWALL EMERGENCY LIGHT INOP AT SEAT 20A. DOES NOT BLINK OR FLICKER. LIGHTING IS SUFFICIENT FOR CREW TO PERFORM DUTIES. C/W MEL 3302B. REMOVING THE OVERWING EXIT SIGN LIGHT ASSY. TASK 33-51-01-960-802 AND ALSO GET ACCESS TO THE LIGHT ASSY. INSTALLED ON THSDR DALA2026101305612Skin · damagedDAMAGE FROM LIGHTNINIG STRIKE ON RUDDER TRAILING EDGE. C/W ERA 637395-14. (9548558)(AIRCRAFT GROUNDED)SDR DALA2026101305608Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BS 328, 348, 360, AND 391. REPAIRED IAW SRM 53-00-01-2R, PROCEDURE 6. (1853249)(AIRCRAFT GROUNDED)SDR DALA2026101305607Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BS 328 - 348, 360, & 391, REPAIRED IAW SRM 53-00-01-2R, PROCEDURE 6. (1853238)(AIRCRAFT GROUNDED)SDR DALA2026101305606Seat Track · corrodedCORROSION ON INBD RT SEAT TRACK BS 365.25 - 440. REPAIRED IAW SRM 51-40-02. (1852590)(AIRCRAFT GROUNDED)SDR DALA2026101305605Seat Track · corrodedCORROSION ON OTBD RT SEAT TRACK FROM BS 365.25 - 440 IN PASSENGER CABIN. REPAIRED IAW SRM 51-40-02. (1852583)(AIRCRAFT GROUNDED).SDR COEA2026101213738Armature · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE LT FWD INERTIAL SEPERATOR ARMATURE. REPLACED INERTIAL SEPERATOR FWD TORQUE TUBE IAW C408 MM 30-20-16. OPS CHECK GOOD.SDR COEA2026101212767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK ON THE RT UPPER WING SKIN BETWEEN WS 224.32 AND WS 241.68. OPENSDR COEA2026101211767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK IN THE LT UPPER WING SKIN BETWEEN WS 157.95 AND WS 142.30. OPENSDR DALA2026101205597Nut Plate · damagedWHILE WORKING JIC CARD 2560-2653, FOUND R1 DOOR FWD SLIDE PACK BOLT NUTPLATE DAMAGED. INSTALLED NEW NUTPLATE AND REINSTALLED R1 DOOR SLIDE PACK IAW AMM 25-66. OPS CHECK NORMAL. (9519243) AIRCRAFT WAS GROUNDEDSDR DALA2026101205590Light · missingEMERGENCY LIGHT AT ROW 11F MISSING. REPLACED THE EMERGENCY LIGHT AT SEAT 11F PER AMM 33-51. LIGHTS CHKD NORMAL. (9110854) AIRCRAFT WAS GROUNDED