Service difficulty reports
1,771,708 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 SWIA2026031875949Skin · damagedUPON REMOVING FASTENERS ON RT SLAT NR 2 TRAILING EDGE, FOUND 1EA HOLE ELONGATED. REPAIRED 1 EA FASTENER IAW REO 670-57-42-2441 REV-.SDR SWAA2026042881169Web · crackedCRACKED WEB, BS 312 - 328, LBL 47, WL 208.1. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 141A5400, SHEET 26, REV -.SDR SWAA2026042881175Web · crackedCRACKED WEB, BTW BS 312 TO BS 328, RBL 32, WL 208.1. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 141A5400, SHEET 39, REV -.SDR SWAA2026042881167Support Angle · crackedCRACKED SUPPORT ANGLE, BTW BS 291.5 TO BS 294.5, STR 17R IN FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOC. BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9 AND DWG 141A8310 SHEET 33 REV -.SDR SWAA2026042881171Intercostal · crackedCRACKED INTERCOSTAL WEB, LOCATED BTW BS 344 TO BS 360 RBL 12 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL WEB IAW SRM 51-40-02 AND DWG 141A5400 SHEET 13 REV -.SDR SWAA2026042481166Web · crackedCRACKED WEB LOCATED BTW 277 TO BS 294.5 RBL 2 WL 208.1 AT FWD GALLEY AND LAV. REPLACED WEB LOCATED BTW 277 TO BS 294.5 RBL 2 WL 208.1 AT FWD GALLEY AND LAV IAW B737-800 SRM 51-40-02 AND DWG 141A5400 SHEET:20 REV:-.SDR SWAA2026042281154Floor Support · crackedCRACKED FLOOR SUPPORT BTWN BS 328 - 344, LBL 46. REPLACED FLOOR SUPPORT AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 141A5400, SHEET, 44, REV -.SDR SWAA2026042281155Floor Support · crackedCRACKED FLOOR SUPPORT BTWN BS 277 - 294.5, BL 0. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5400, SHEET 20, REV-.SDR SWAA2026042281146Tie Clip · crackedCRACK TIE CLIP LOCATED BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0; DWG 141A1110, SHEET 39 REV -, AND DWG 141A8380, SHEET 21, AND REV -.SDR SWAA2026042281160Stringer · crackedCRACKED STRINGER 16L AND BTW BS 294.5 - 303.9. PERFORMED PERMANENT REPAIR ON THE STRINGER 16L AND BTW BS 294.5 - 303.9 IAW SRM 53-00-03-2R-1 REPAIR 1, STEP 4. K. AND DWG 141A3120 SHEET 1 REV B.SDR SWAA2026042281148Stub Frame · crackedCRACK ON STUB FRAME STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BTW S-12R TO S-17R AT FWD GALLEY DOOR AREA AT PASSENGER CABIN IAW SRM 51-10-02-0G-0 ITEM 9 AND DWG 141A8370 SHEET 9 REV D.SDR SWAA2026042281145Angle · crackedCRACK ANGLE LOCATED BTW STA 291.5 TO STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED ANGLE CLIP LOCATED BTW STA 291.5 TO STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02-0G-0 AND DWG 141A8310 SHEET: 25 REV: SDR AALA202604226086Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON ANGLE AT FR 71 AND S29R AT THE THS COMPARTMENT ACCESS DOOR CUTOUT. REPLACED ANGLE PER SRM 51-42-11.SDR AALA202604226288Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING LOC. BTW FR67 +5 IN. AT LEVEL STR23 R AT AFT GALLEY AREA (CPCP 534136-01). MEASURES ARE L=0.992 IN, W= 0.297 IN, D= 0.091 IN. MAINTENANCE REPLACED CENTER FITTING LOC AT STRG 23R AND BTW FR66 AND FR68. IASDR HNAA2026042100334Skin · damagedCENTER FUSELAGE 1 EXTERNAL SKIN HAS DAMAGE AREA FROM PREVIOUS BLEND OUT BETWEEN FR22 AND FR23 AND BETWEEN STGR 19R AND STGR 20R. INSTALLED FABRICATED DOUBLER AND FILLER FOR REPAIR ON CENTER FUSELAGE 1 EXTERNAL SKIN FROM PREVIOUS BLEND OUT BETWEEN FR22 AND FR2SDR IXX2026F00005Stiffener · elongatedENGINE NO 2. SHIP FAIRING FWD SECTION VERTICAL ANGLE BRACKETS, I/B AND O/B BRACKETS FOUND ELONGATED HOLES. REF XTREME AVIATION NON ROUTINE 883SDR DALA2026041502389Doubler · corrodedER/A 632674-14 SECTION I REPAIR WAS ISSUED TO ADDRESS WASTE BOX COMPARTMENT CORROSION TO INTERNAL DOUBLER AND SKIN. FOLLOW ON ACTIONS ARE REQUIRED.ACCOMPLISH SECT. II WITHIN EVERY 1000 FH FROM SECT. I ACCOMPLISHMENT. ACCOMPLISH SECT. III WITHIN 10,000 FH FROM SDR SWAA2026040980898Strap · crackedFOUND CRACK AND CORROSION ON LEFT HAND WING LEADING EDGE TO WING LWR ATTACHMENT AT 452.75 WING STATION.<[01] REPAIRED LEFT HAND WING LEADING EDGE TO WING LWR ATTACH STRAP AT WSTA 452.75 (OSS 227.95) PER EA 26-157-00825 TTG8Q01BKAXB;[02] VERIFIED: REPAIRED LEFTSDR ASAA2026031865257Support · corrodedFWD CARGO BULKHEAD LOWER SUPPORT AT BS 520 CORRODED. GROUNDED - YES. REMOVED AND REPLACED THE FWD CARGO AFT BULKHEAD LWR SUPPORT AT BS 520 IAW SRM 51-40-02-0G-0.SDR IPXA2026033032521Actuator · faultedFOUND ROTARY ACTUATOR NOISE AT FWD CARGO DOOR. IAW AMM 52-33-04-004-027 REV.147 AND AMM 52-33-04-404-028 REV.147 REPLACED FWD CARGO DOOR ROTARY ACTUATOR.SDR 2026F00059Warning System · activatedON 3/18/26, DEPARTING FROM KDVT, CREW RETURNED TO KDVT DUE TO CLIMBING THRU 2000FT, WE GOT AURAL AND VISUAL WARNING, NO TAKEOFF”. AURAL WARNING WAS CONTINUOUS AND VISUAL WAS INTERMITTENT. CLIMBING THRU 10,000 NOTICED THE PRESSURIZATION WAS CLIMBING RAPIDLY, ESDR AALA202604011754Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 400 AND LBL 26. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR AALA202603315117Warning Message · false activationAIRCRAFT WAS NOT GROUNDED: OVERWING EMERGENCY DOOR SHOW OPEN R3 DOOR ERRONEOUS INDICATION. MAINTENANCE ACCOMPLISHED AN EMERGENCY OPERATIONAL CHECK OF THE 3R EMERGENCY EXIT DOOR INCATION PER AMM 52-73-00 AND FOUND NO ISSUES WITH THE DOOR INDICATION. MAINTENANCSDR SWAA2026033080973Battery Pack · inoperativeEMERGENCY BATTERY PACK M2816 DOES NOT HOLD CHARGE<[01] REMOVED; REPLACED AND PERFORMED A GOOD CHECK OF M2816 BATTERY PACK IAW SWA B737 MAX 8 AMM 33-51-06;[02] REMOVED; REPLACED AND PERFORMED A GOOD CHECK OF M2816 BATTERY PACK IAW AMM 33-51-06SDR SWAA2026033080974Battery Pack · inoperativeEMERGENCY BATTERY PACK M1670 DOES NOT HOLD CHARGE. REMOVED; REPLACED AND PERFORMED A GOOD CHECK OF BATTERY PACK AT M1670 IAW SWA B737 MAX 8 AMM 33-51-06;[02] REMOVED; REPLACED AND PERFORMED A GOOD CHECK OF BATTERY PACK AT M1670 IAW SWA AMM 33-51-06SDR IPXA2026032831078Angle · damagedDAMAGED ANGLE, NR 2 NACELLE AFT SKIRT FAIRING INNER RT, 4TH HINGE FITTING.. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3310, SHEET 1, REV L.SDR AALA202603304036Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR56 + 406.4MM, Y1292. MAINTENANCE REPLACED SEAT TRACK T FR56, Y1292 IAW SRM 51-42-11-801 AND DWG D53476980.SDR AALA202603270135Oven · odorAIRCRAFT WAS NOT GROUNDED: FORWARD OVEN NUMBER 2 HAS A STRONG BURNING SMELL, EVEN WHEN NOT IN USE. REMOVED AND REPLACED FORWARD GALLEY OVEN 2. PER AMM 25-32-03. OPS CHECK GOOD.SDR IPXA2026032731616Snubber · faultedFOUND NR 1 ENTRY DOOR ROTARY SNUBBER PIN EXTENSION OUT OF LIMIT. IAW AMM 52-11-10-000-801 REV.50 AND AMM 52-11-10-400-801 REV 50, REPLACED THE SNUBBER AND OPERATIONAL TEST NORMAL.SDR UATA202603275304Channel · wornWEAR MARK ON C CHANNEL SECTION BETWEEN L/H FRAMES 17-20. R&R WITH P/N: 212-23201-03-1 IRW CASA 212 SRM SECTION IV FIGURE 4.28 PAGES 0A-02 & INSTALLED WITH FASTENERS AN470E5, AN470E6, AN426E4, AN426E5, HL18-5, HL18-6, HL70-5, & HL70-6. IRW AC-43.13-1 B SECTION SDR UATA1740327265303Doubler · crackedREPAIR DOUBLER AT LOWER END OF FRAME 19 CRACKED (LH SIDE). REPLACED DOUBLER SEE 337 DATED 3/18/2026. CRACK FOUND AT DOUBLER FOR L/H FRAME 19. R&R WITH 2 DOUBLERS (ONE FWD AND ONE AFT OF FRAME) WITH .032IN 2024 T-3 ALUMINUM IRW CASA 212 SRM SECTION IV FIG 4.28 SDR U5QA202603180168Apu · faultedAPU FAILED TO START ON PAST 2 APPROACHES. CYAN APU SHUTDOWN CAS POSTED. ON SUBSEQUENT ATTEMPT AFTER LANDING THERE WAS A VERY STRONG SMELL OF FUEL IN THE CABIN. MX C/A: INSPECTED APU INLET AND APU IGNITER, APU INLET WAS CLEAR AND APU IGNITER WAS WITHIN LIMITS SDR SWAA2026032681084Elec Connector · damagedEMERGENCY AISLE LIGHT WIRE CLOSE TO CONNETOR D14714 IS DAMAGE (STA 727D+8) MID CEILING PANEL<[01] RETERMINATED WIRES FOR EMERGENCY LIGHT CONNECTOR D14714 APOX (STA 727D+8) MID CEILING PANEL RIGHT SIDE; PER SWPM 20-63-02; WDM 33-51-14.<BR>FUNCTIONAL TEST WILL BSDR IPXA2026032628471Bracket · damagedFOUND FWD CARGO DOOR LIFT ARM BRACKET DAMAGE. IAW AMM 52-34-01-010-801, REV 50, AND AMM 52-34-01-404-014, REV 50 TO REPLACE THE BRACKET. CONDITION CHECKED NORMAL.SDR IPXA2026032628875Bracket · damagedFOUND FWD CARGO DOOR FWD LIFT FITTING BRACKET DAMAGED. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.48 AND AIPC 52-34-01-12 REV.54.SDR IPXA2026032629120Bracket · brokenBROKEN BRACKET, LT WING NR 5 SLAT OTBD SIDE SEAL DOOR AREA. IAW AMM 57-41-50-004-001, REV 147, REPLACED THE BRACKET.SDR E07A202603260227Support Bracket · crackedFOUND CRACK ON LH AND RH NOSE OMEGA BEAM FORWARD SUPPORT BRACKETSDR 2026FA0000219Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH
NEWSDR AALA202603257925Overheat Loop · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. **SUPPLEMENTAL REPORT FOR (AALA202603197925) SUBMITTED 03/19/2026 BY DFW: REMOVED AND REPLACSDR AALA202603254160Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: FLOORBOARD SUPPORT UNDER CABIN FLOOR AT BS 540 AND RBL2 IS CRACKED. INSTALLED CABIN FLOORBOARD PANEL 231XF. PER AMM 53-21-00.SDR AALA202603256168Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: FLOORBOARD SUPPORT UNDER CABIN FLOOR AT BS 540 AND LBL 2 IS CRACKED. INSTALLED CABIN FLOORBOARD PANEL 231UF. PER IAW AMM 53-21-00.SDR U2RA2026032500002Lamp · inoperativeU/D EMEGENCY LIGHT NO ON QTY 3 EA. REPLACED THE LAMP AND OPERATION CHECK PER AMM 33-51-07 FOUND NORMALSDR IPXA2026032331814Clamp · brokenBROKEN CLAMP , NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, & DWG 313T3349, SH 2, REV B.SDR IPXA2026032332844Beam · crackedCRACKED BEAM , NR 2 NACELLE AFT LOWER FAIRING RT UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV 94 AND DWG 313T2380, SH. 10, REV K, 313T2380, SH 9, REV G, 313T2380, SH 22, REV F, & SERVICE BULLENTIN 767-54-010SDR DALA2026032401969Tire · failedATB/TIRE- RETURNED TO ATL DUE TO #1 MLG TIRE FAILURE, RT SYS HYDRAULIC LOSS AND SUBSEQUENT LT ENGINE DAMAGE ON TAKEOFF. CORRECTIVE ACTION: REPLACED #1 ENGINE.SDR DALA2026032401965Flap System · faultedWHILE SETTING FLAPS AFTER ENGINE START: F/CTL FLAPS LOCKED - WING TIP BRAKE ON ECAM RECEIVED. T/S PER A320 TSM 27-51-00-810-840-A. NO FAULTS OR ISSUES FOUND AT THIS TIME. A/C OKAY FOR SERICE. (PFR FAUTED RH 1,2 FLAPS). OPS CHECK GOOD. (LP: 8484302)SDR CALA2026032414801Channel · puncturedAFT CARGO COMPT. R/H 'Z' CHANNEL BETWEEN STAS 727F & 727G PUNCTURED. REF AAR N/R 100003328 REMOVED AND REPLACED NEW AFT CARGO COMPT. R/H 'Z' CHANNEL BETWEEN STAS 727F & 727G PER SRM 51-40-02-0G-0, DWG# 146A7500. ESFR ENTRY REMOVED AND REPLACED AFT CARGO COMPTSDR ASAA2026031865019Seat Track · damagedRH INBD CAPTAIN SEAT TRACK DAMAGED AJ004. GROUNDED - YES. REMOVED AND INSTALLED RH INBD CAPTAIN SEAT TRACK IAW IPECO CMM 53-01-02, B737 AMM 25-11-01-00, 25-11-01-400-801, 25-50-11-910-801 SDR TO BE SUBMITTED.SDR ASAA2026031865018Seat Track · damagedLH INBD FIRST OFFICER SEAT TRACK DEMAGED AJ005. GROUNDED - YES. REMOVED AND REPLACED LH INBD CAPTAIN SEAT TRACK IAW IPECO CMM 53-01-02, B737 AMM 25-11-01-00, 25-11-01-400-801, 25-50-11-910-801, SDR TO BE SUBMITTED.SDR SWAA2026032381353Retainer · out of adjustL1 GIRT BAR CLAMP IS LOOSE, GIRT BAR FALLS OUT. ADJUSTED TENSION ON GIRT BAR RETAINER IAW AMM 25-66-00.