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 HNAA2026100100933Support · corrodedCORROSION ON RH TOILET WASTE VALVE SUPPORT. RAR SUPPORT IAW SRM 51-40-02SDR F3LA202608310445Engine · leakingFA'S REPORTED STRONG DIRTY SOCK SMELL IN CABIN BELOW FL180 ON ARRIVAL. AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NR 2 ENGINE IAW TASKCARDS: MP71042-05/ MP71042-06. LEAK CHECK OK. OPS CHECK OK. ORIGINAL SUBMISSION DATE: 8-31-2026SDR SWAA2026092999840Angle · corrodedCORROSION ON LOWER ANGLE, BS 767 - 787, RBL 21, WL 155.3. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV-.SDR SWAA2026092890492Wire · brokenBROKEN WIRE FOUND AT BS 500C, S11L. REPAIRED THE WIRE W3142-0503 22 IAW SWPM 20-10 20-30, AND WDM 33-51-11. PERFORMED GOOD CONTINUITY CHECK FROM CONNECTOR D13018 TO CONNECTOR D40096P W1342-0503-22 IAW WDM33-51-11, PAGE 11, SHEET 1, AND PERFORMED GOOD OPS TESDR CALA2026092819863Skin · crackedEA 5510-01843, CRACK FOUND ON RT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 120.30, INBD OF INBD FASTENER ROW, 10.5" FWD OF T/E. REPAIRED RT HORIZONTAL STAB LOWER IN SPAR SKIN AT HSS 120.30 IAW SRM 55-10-01-2R-11. REPAIR 11.SDR R61A2026092600273Strap · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND AFT WTF FAIRING ATTACHMENT STRAP BETWEEN FR 73- 75, STR 23R - 29R CORRODED. THE ATTACHMENT STRAP WAS REMOVED AND REPLACED IAW SRM 51-43-04 AND 51-41-02.SDR R61A2026092600272Strap · corrodedDURING HEAVY CHECK MAINTENANCE FOUND AFT WTF FAIRING ATTACHMENT STRAP BETWEEN FR 73- 75, STR 23L - 29L CORRODED. WTBF FAIRING ATTACHMENT STRAP WAS REMOVED AND REPLACED IAW SRM 51-43-04 AND 51-41-02.SDR R61A2026092600271Support · corrodedDURING HEAVY CHECK MAINTENANCE FOUND WTB FAIRING RIB LT & RT SUPPORT CORRODED AT CFII FR54. THE WTB FAIRING RIB SUPPORT WAS REPLACED IAW SRM 51-41-02, AND 51-42-02.SDR R61A2026092600268Skin · dentedDURING HEAVY CHECK, MAINTENANCE FOUND REAR FUSELAGE SKIN FOUND TO HAVE 3 DENTS BETWEEN FRAMES 99 AND 100, STR 27R & 28R. PERFORMED SKIN CUT OUT, AND PERMANENT REPAIR DOUBLER IAW ETD2026-170-015273-A.SDR HNAA2026092500910Floor Support · corrodedRIGHT FLOOR SUPPORT HAD CORROSION AT MULTIPLE LOCATIONS FROM FR 52-59. R & R CENTER FUSELAGE IV RH FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092500909Floor Support · corrodedCENTER FUSELAGE IV, THE LH FLOOR SUPPORT HAD CORROSION AT FR 57. R & R CENTER FUSELAGE IV, THE LT FLOOR SUPPORT NR 7 IAW SRM 51-40-02.SDR HNAA2026092500906Floor Support · corrodedPAX ENTRYWAY FWD FLOOR SUPPORT HAD CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092500905Floor Support · corrodedLEFT NR 3 OTBD FLOOR SUPPORT CORRODED. R & R L3 OTBD FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092500904Floorbeam · corrodedLEFT NR 4 OTBD FLOOR SUPPORT CORRODED. R & R L4 OTBD FLOOR SUPPORT IAW SRM 51-40-02.SDR HNAA2026092500903Floorbeam · corrodedCENTER FUSELAGE IV, THE RH CROSS BEAM GUSSET HAD CORROSION AT FR57. REMOVED AND REPLACED RT CROSS BEAM AT FR57 IAW EMB 145 SRM 51-40-02.SDR SWAA2026092440445Plate · crackedCRACKED CORRUGATED PLATE, IRSS 216 RT WING T/R. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2781, SHEET 2, REV B.SDR SWAA2026092488382Plate · damagedELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 320 TRAILING EDGE, RT WING. REPLACED CORRUGATED PLATE, DID NOT FIND ALLOWABLE DAMAGE LIMITS IN SRM 57-51-02-1A-1, ALLOWABLE DAMAGE 1, SRM 51-10-02, ITEM 9, & DWG 115A3700, SHEET 96, REV - .SDR AALA202609242511Angle · crackedAIRCRAFT IN BASE MAINTENANCE: LH ECS BAY AFT BULKHEAD UPPER ANGLE INBOARD SIDE CRACKED. REMOVED AND INSTALLED NEW REPAIR ANGLE AND SPLICE, IAW SRM 57-10-10-2R PROCEDURE 5 REPAIR 5.SDR AALA202609232511Angle · crackedAIRCRAFT IN BASE MAINTENANCE: LH ECS BAY AFT BULKHEAD UPPER ANGLE INBOARD SIDE CRACKED. REMOVED AND INSTALLED NEW REPAIR ANGLE AND SPLICE, IAW SRM 57-10-10-2R PROCEDURE 5 REPAIR 5.SDR 2026FA0000767Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR HNAA2026092100869Shear Tie · crackedSHEAR TIE CRACKED AT FR 58 BTWN STR 15-16L. R & R SHEAR TIE IAW SRM 51-40-02.SDR HNAA2026092100868Shear Tie · crackedSHEAR TIE CRACKED AT FR 59 BTWN STR 15-16L. R & R SHEAR TIE IAW SRM 51-40-02.SDR HNAA2026092100867Angle · crackedRIGHT WING UPPER SKIN LATERAL FAIRING LOWER RETAINING ANGLE CRACKED. R & R ANGLE IAW SRM 51-40-02.SDR HNAA2026092100866Angle · crackedLEFT WING UPPER SKIN LATERAL FAIRING LOWER RETAINING ANGLE NR 2 CRACKED. R & R ANGLE IAW SRM 51-40-02.SDR HNAA2026092100865Angle · crackedRIGHT WING UPPER SKIN LATERAL FAIRING LWR RETAINING ANGLE CRACKED. R & R THE RETAINING ANGLE IAW SRM 51-40-02.SDR IXXA20260919NKJ01Cowling · crackedNUMBER 2 ENGINE OUTBOARD CORE COWL INTERNAL AREA #5 RIB/FRAME HAS CHAFING/WEAR MARKS (IS CRACKED)SDR IPXA2026091656998Skin · gougedAFTER REMOVAL OF RUB STRIP, FOUND DAMAGE UNDER RUB STRIP ON AFT AREA. PERFORMED CUT OUT THE SKIN AS REQUIRED REPAIR N43 NOTE A. IAW SRM 54-30-00. INSTALLED FILLER AND DOUBLER AT NR 1 ENG UNDER RUBSTRIP IAW SRM 51-40-21-001.SDR 2026FA0000720Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000709Skin · crackedRIGHT WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEW.SDR MASA202609142042Seat Track · corrodedDURING HEAVY CHECK OF AFT WET AREA FLOOR STRUCTURE, CFIII, CORRODED SEAT TRACK AT FR 74 L/H, LBL 11, TO FR 84 L/H REMOVED AND REPLACED IAW SRM 51-40-08. NRC # 4502706-2000-0281, REV 45.SDR SWAA2026091438273Bracket · crackedCRACK BRACKET TRAILING EDGE LOCATED IRSS 210 APROX AT RT WING. REPLACED BRACKET IAW SRM 51-40-02, SRM 51-10-02, AND DWG 115A2001, SHEET 24, REV A.SDR AALA202609119354Support Beam · wornAIRCRAFT IN BASE MAINTENANCE: RH WING INB FIXED TRAILING EDGE LOWER PANEL 651GB HAS PLAY. REMOVED AND REPLACED RH WING INBOARD FIXED TRAILING EDGE LOWER SUPPORT BEAM IAW SRM 51-40-02, SRM 51-40-05 AND AIPC 57-50-00-30A.SDR IPXA2026090447613Nose Cowl · dentedFAULT - DENT - SKIN , NO. 2 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.2", 16" FROM L/E AND AT 9 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR SDR IPXA2026090443491Nose Cowl · dentedDENT - SKIN , NO.1 ENG NOSE COWL INNER BARREL NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.3", 9" FROM AFT EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.SDR REXA2026090801781Door · lack of lubePASSENGER DOOR AND GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE LUBED DOORS IAW AMM 12-20-52 OPS TEST GOOD. IAW AMM 52-11-08.SDR IPXA2026090446102Strap · corrodedFOUND FORWARD CARGO CEILING STRUCTURE CORROSION AT STA 566 RIGHT SIDE. REMOVED DAMAGE STRAP I.A.W SRM 51-40-02-0G REV. 96. ACCOMPLISHED REPAIR I.A.W EO-98506-REQ1 REV. 1, BOEING DWG NO. 453T1001 SH. 1 REV. A AND BOEING DWG NO. 453T1183 SH. 6 REV. -.SDR DALA2026090805020Indicator · inoperativeR1 DOOR SLIDE LIGHT IS BURNED OUT. REPLACED THE LIGHT ASSEMBLY, OPS CHKD GOOD IAW AMM 52-73, MEL/PLACARD REMOVED NO M PROC (8399099)(AIRCRAFT GROUNDED)SDR SWAA2026090790305Wire · pulledSPLICE AT EXIT INDICATOR LIGHT LO1191 HAS PULLED WIRE. TERMINATED D10086. CONNECTOR OF EXIT IND LIGHT L01191. IAW SWPM 20-61-12. AND GOOD OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00. CARD COMPLETE.SDR IPXA2026090346191Angle · crackedFAULT - FOUND THE FIRE DETECTION LOOP FASTENER ANGLE CRACK AT STA 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G RE.96. INSTALLED FABRICATED ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO: 218T4100 SHEET 3 REV. B AND SDR IPXA2026090346129Former · crackedCRACKED FORMER , RT WING CAVITY FORMER OF THE CRACK AT OSS 648. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV. 96. INSTALLED NEW FORMER IAW SRM 51-40-02-0G, REV 96, & DWG 114T2513, SHT 1, REV D, AND SREO-50900-REQ001, REV 2.SDR AALA202609031178Lamp · burned outAIRCRAFT IN BASE MAINTENANCE: FAULT MESSAGE CROSS AISLE LT/EPSU(13WL) AFT L DISPLAYED DURING SYSTEM TEST - MAINTENANCE FOUND LAMP OUT IN SIDE WALL EXIT SIGN 90WL5 AT THE L2 DOOR AND REPLACED THE LAMP - A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO SDR DALA2026090304974Unknown · odorROTTEN EGG/DIRTY SOCK ODOR DURING CLIMBOUT. NEW ENGINE INSTALLED, REF LP 1781608. PERFORMED PACK BURNOUT AND CHANGED RECIRC FILTERS IAW AMM 21-25. ALL OOPS GOOD. (1779260)(AIRCRAFT GROUNDED)SDR SWAA2026090104673Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M1675 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1675 IAW B737 AMM 33-51-06. OPS CHECK GOOD.SDR SWIA2026082777026Skin · damagedSCRATCH AND DENT APPROXIMATELY 31 INCHES LONG ON THE RT SIDE BETWEEN FR 17 AND FR 14, BTWN STR 20R AND STR 21R.AT THE DEEPEST 0.125" OPENSDR DALA2026090104935Elec Connector · not seatedON A SERVICE CHK, FOUND SEATS 20 H/J AND 21 H/J EMERGENCY LIGHTS INOPERATIVE. DEFERRED TO MEL 33-50-07A, PLACARD INSTALLED. NO M PROCEDURES. OK FOR SERVICE. RE SEATED CONNECTOR AT 542WL43. NOW CHECKS OK PER A350 AMM 33-51. MEL AND PLACARD REMOVED. (LP 931717SDR AALA202609015215Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND CRACKED BAFFLE CLIP. REMOVED DAMAGED BAFFLE CLIP AND INSTALLED BAFFLE CLIP 143A7502-159 IAW BOEING DWG 143A7505 SRM 51-40-02, AARD 53-00-01 AND AARD 51-00-05-1.SDR AALA202609012496Oil System · fluid lossAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO SAL DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 OIL QUANTITY SHOWED 13.5 QTS BEFORE START. IN CRUISE AFTER 2 HOURS, SHOWS 7.0 QTS - THE AIRCRAFT LANDED SAFLEY AT SAL WITHOUT FURTHER INCIDENT. (OPEN)SDR UIEA2026082700810Flashlight · no testCAPTAINS FLASHLIGHT TEST LIGHT NOT BLINKING GREEN. TRANSFER TO DMI 258243 PER MEL 25-64-02C CAT C, LP 2190195 M8. CAPTAINS EMERGENCY FLASHLIGHT REPLACED, TESTED GOOD IAW AMM 25-64-01 AND AIPC 25-64-61-03. DMI 258243 CLOSED.SDR DALA2026090104922Vent · corrodedON WALKAROUND FOUND CORROSION AFT OF LAV VENT. APPEARS TO RUN VERTICALLY ALONG SKIN SPLICE AT BULKHEAD. ALL WORK PERFORMED ON LP 1779817. (LP: 8733336, AIRCRAFT WAS GROUNDED)SDR YENA2026083100714Contactor · faultedFLT 552, MCO-MCO. ELEC AC ESS FEED FAULT AT APPROX 60 KTS DURING TO. FLICKERED AND THEN LOST SCREENS 1, 2, 3 AT APPROX 70 KTS, EXECUTED AN RTO; R & R ACCESS BUSS SWITCHING CONTACTOR IAW AMM 24-25-55. OPS CHKD GOOD. OK FOR SVC. OPEN