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 SWAA2026081155594Support · corrodedCORRODED SUPPORT ZEE, BS 727D - 767, RBL 21, WL 156 IN AFT CARGO BAY. REPLACED THE SUPPORT ZEE BTWN BS 727 - 767 IAW SRM 51-40-02, AND DWG 146A7500, SHEET 85, REV A.SDR SWIA2026070676750Skin · crackedRIGHT WING FIXED LEADING EDGE IS CRACKED AT SLAT 2 INBD TRACK UPPER CUTOUT. PERFORMED DOUBLER REPAIR ON RT WING FIXED LEADING EDGE AT SLAT 2 INBD TRACK UPPER CUTOUT. IAW ETD2026-170-012023-B.SDR J7SA2026080400510Acm · faultedDURING CRUISE, CREW RECEIVED PACK TEMP HIGH CAS, HEARD A SQUEAL NOISE, AND NOTICED A BURNT SMELL. AIRCRAFT LANDED WITHOUT INCIDENT AT KDPA. FOUND AIR CYCLE MACHINE SEIZED. REPLACED ACM. OPS AND LEAK CHECKS SATISFACTORY. WORK COMPLETED IAW CL350 AMM 21-52-13.SDR IPXA2026072725783Adapter · corrodedCLS ADAPTER WITH WEAR DAMAGE AT FR65 Y0 RH SIDE. INSTALLED NEW CLS ADAPTER AT MDC FR65 Y0 RH SIDE IAW SRM 51-40-21.SDR IPXA2026073132503Bracket · crackedAFT CARGO COMPARTMENT, FWD BULKHEAD (FR54), Y0, UPPER SIDEWALL SUPPORT CRACK. INSTALLED UPPER SIDEWALL SUPPORT FR 54 Y0. AFT CARGO COMPARTMENT. IAW SRM 51-40-21.SDR IPXA2026073132508Support · crackedAFT CARGO COMPARTMENT, FWD BULKHEAD (FR54) Y953, 1EA UPPER SIDEWALL SUPPORT CRACK. INSTALLED UPPER SIDEWALL SUPPORT FR 54 Y953. AFT CARGO COMPARTMENT. IAW SRM 51-40-21.SDR AALA202608044687Shear Tie · corrodedAIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION ON SHEAR TIE AST STA 927, STR 27. MAINTENANCE REPLACED SHEAR TIE AST STA 927, STR 27 IAW AARD 51-00-05-1 AND BOEING DRAWIG 147A0040.SDR SWAA2026080328001Crossbeam · crackedPANEL BREAK BS540 CRACKED AT LBL 1; WL 208. REMOVED AND REPLACED PANEL BREAK ON BS540 LBL 1 TO LBL 24 IAW SRM 51-40-02 AND DWG 143A0060 ID: 0036 REV A.SDR IPXA2026073025756Adapter · corrodedCLS ADAPTER WITH CORROSION AT FR65 Y0 LH SIDE. INSTALLED NEW CLS ADAPTER P/N: A53275455200 AT MDC FR65 Y0 LT SIDE IAW A300-600 SRM 51-40-21.SDR IPXA2026073132491Bracket · crackedAFT CARGO COMPARTMENT, FWD BULKHEAD (FR54) Y953, 2EA UPPER SIDEWALL SUPPORT CRACK. INSTALLED (2 EA) UPPER SIDEWALL SUPPORT AT FR 54. Y953. AFT CARGO COMPARTMENT. IAW SRM 51-40-21.SDR IPXA2026073132481Bracket · crackedAFT CARGO COMPARTMENT, FWD BULKHEAD (FR54) Y1959, UPPER SIDEWALL SUPPORT CRACK. DOT 73-069 INSTALLED UPPER SIDEWALL SUPPORT FR 54 Y1959. AFT CARGO COMPARTMENT. IAW A300-600 SRM 51-40-21.SDR SWIA2026070676706Floorbeam · corrodedCORROSION ON LT FLOORBEAM AT FR 87, Y= -10". REMOVED AND REPLACED LH FLOORBEAM AT FR 87, Y= -10" PER SRM 51-40-08.SDR SWIA2026070676705Seat Track · corrodedFORWARD FUSELAGE PASSENGER CABIN FLOOR STRUCTURE WET AREA RH TRACK AT FRAMES 16-19 AT Y+10IN TO Y+14IN HAVE SIGNS OF CORROSION AND BUBBLING PAINT. REMOVED AND REPLACED FORWARD FUSELAGE PASSENGER CABIN FLOOR STRUCTURE WET AREA RT TRACK AT FRAMES 16-19 AT Y+10ISDR SWIA2026070676704Seat Track · wornLEFT FLOOR SEAT TRACK HAS WEAR BETWEEN FRAMES 78 AND 79, FRAMES 80 AND 81, AND FRAMES 82 AND 83. REMOVED AND REPLACED LEFT-HAND FLOOR SEAT TRACK FR 74-84 PER E175 SRM 51-40-08.SDR IPXA2026073031884Bracket · corrodedFWD CARGO COMPARTMENT CEILING, AT FR 26, Y0, CEILING SUPPORT WITH CORROSION. SURFACE PROTECTION RESTORED IAW SRM 51-21-10-001, PAINT APPLIED IAW SRM 51-75-10-201 & CIC APPLIED IAW EO-2780-REQ001 ( CIC TYPE AND LOCATION OF USAGE) T3F18E0098D4MSDR AALA202607280075Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO FLOOR STRUCTURE - RH TRANSITION PANEL HAS FILIFORM CORROSION STA 500A TO 500L RBL 26. MAINTENANCE REPLACED FORWARD CARGO TRANSITION PANEL STA 500A TO 500L RBL 26.SDR AALA202607285852Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: FRETTING CORROSION ON FASTNERS PULLING ON FUSELAGE SKIN AT STA 887, S26L. MAINTENANCE INSTALLED REPAIR DOUBLER IAW EA 376829SDR SWAA2026072714617Support Angle · crackedACB FWD LOWER BULKHEAD SUPPORT ANGLE ATTACH TO FLOOR PANEL (CAP STRIP) BS727+4 LBL21-RBL21; WL156 CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 AND DWG 453A2600 REV B.SDR SWAA2026072797693Slat · crackedPERFORMED OPEN HOLE INSP IAW B737 NDTM P6, 51-00-00 PROC 16. FOUND 1 EA FASTENER CRACKED IN FITTING ON NR 3 LE SLAT. REMOVED AND REPLACED NR 3 L/E SLAT ASSY IAW AMM27-81-21. ADJUSMENT & OPS TESTS GOOD,SDR SWAA2026072742218Slat · crackedPERFORMED OPEN HOLE INSP IAW NDTM P6, 51-00-00 PROC 16. FOUND 1EA FASTENER CRACKED IN FITTING ON NR 5 LE SLAT. REMOVED AND REPLACED NR 5 L/E SLAT ASSY IAW AMM 27-81-21. ADJUSMENT & OPS TESTS GOOD VERIFIED REMOVED AND REPLACED #5 L/E SLAT ASSY IAW AMM27-81-21.SDR IPXA2026071928626Stiffener · crackedBETWEEN FR38-FR38.1 LH SIDE STIFFENER (DOG BONE) CRACKED. INSTALLED FLOOR CHANNELS BETWEEN FR 38 TO FR 38.1 LT.IAW SRM 51-40-21-001.SDR ASAA2026070667514Stringer Clip · crackedSTRINGER CLIP IS CRACKED AT STA 500D STR 26R. GROUNDED - YES. REMOVED & REPLACED THE STRINGER CLIP STA 500D, STR 26R IAW SRM 51-40-02-0G-0.SDR IPXA2026071928866Stiffener · crackedBETWEEN FR38.1-FR38.2 RT SIDE STIFFENER (DOG BONE) CRACKED. REMOVED AND REPLACED (DOG BONE)BETWEEN FR38.1-FR38.2 RT, IAW SRM 51-40-21-001.SDR IPXA2026071928747Stiffener · crackedBETWEEN FR38-FR38.1 RT SIDE STIFFENER (DOG BONE) WITH CRACK. REMOVED AND REPLACED (DOG BONE) BETWEEN FR38-FR38.1 RH, IAW SRM 51-40-21-001.SDR IPXA2026071928788Stiffener · crackedBETWEEN FR37-FR38 RH SIDE STIFFENER (DOG BONE) CRACKED. REMOVED AND REPLACED (DOG BONE) BETWEEN FR 37 - FR 38 RT IAW SRM 51-40-21-001.SDR REXA2026072301088Lug · damagedRH AILERON HAS 1 #9 BEARING LUG MARKED E FOUND TO BE OVER SIZED UPON BEARING REMOVAL. COMPLIED WITH STEPS 1 THRU 3 OF MHIRJ REO 690-57-61-273 REV-- DATED 2022-10-13. HFEC PERFORMED IAW MHIRJ REO 690-57-61-273 REV - DATED 2022-10-13 STEP 4 NO INDICATIONS NOTED SDR REXA2026072301087Lug · damagedLH AILERON BEARING LUG MARKED E FOUND TO BE OVERSIZED UPON REMOVAL OF BEARING. RECEIVED MHIRJ REO 690-57-61-534 REV -- DATED 2026-07-11 COMPLIED WITH STEPS 1 REAM AND 2 CHAMFER IAW MHIRJ REO 690-57-61-534 REV -- DATED 2027-07-11 COMPLIED WITH STEP 1 REAM AND SSDR IPXA2026071928685Stiffener · crackedBETWEEN FR38.1-FR38.2 LT SIDE STIFFENER (DOG BONE) WITH CRACK. REMOVED AND REPLACED BETWEEN FR38.1-FR38.2 LT IAW SRM 51-40-21-001. INSTALLED FLOOR CHANNELS BETWEEN FR 38.1 TO FR 38.2 IAW SRM 51-40-21-001.SDR IPXA2026071732361Profile · corrodedAFT CARGO COMPARTMENT, FR 62, AT Y450, CEILING STRUCTURE WITH CORROSION. NEW PROFILE INSTALLED IAW SRM 51-40-21-001.SDR IPXA2026071832341Support · corrodedAFT CARGO COMPARTMENT, FR 62, AT Y0, CEILING STRUCTURE WITH CORROSION. INSTALLED FABBED/ NEW CEILING SUPPORT AT FR 62, Y0 IAW SRM 51-40-21. PART MARKED IAW GMM 09.08.01.03 REV 15.SDR AALA202607215879Stringer Clip · crackedAIRCRAFT IN BASE MAINTENANCE: GVI - FWD CARGO FLOOR STRUCTURE - RH STRINGER CLIP CRACKED STA 500I RBL 26. MSINTENANCE REMOVE AND REPLACE RH STRINGER CLIP STA 500I RBL 26 IAW SRM 51-40-02.SDR REXA2026072001078Bushing · damagedRH AILERON 4 EACH BUSHING LUGS MARKED B, C, F AND G FOUND TO BE OVER SIZED UPON BUSHING REMOVAL. REPAIRED RH AILERON BUSHING LUGS B, C, F, AND G IAW REO 670-57-61-237 REV -- DATED 2017-07-25.SDR REXA2026072001077Bushing · damagedLH AILERON FOUND 3 BUSHING LUGS MARKED C, F AND G TO BE OVER SIZED AFTER BUSHING REMOVAL REPAIRED LH AILERON BUSHING LUGS C, F, AND G IAW REO 670-57-61-237 REV -- DATED 2017-07-25.SDR SWAA2026071595022Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1671 INOPERATIVE. REPLACED BATTERY PACK M1671 AND PERFORMED A GOOD FUNCTIONAL TEST OF NEW BATTERY PACK IAW AMM 33-51-06-960-805.SDR CALA2026071217673Skin · dented(SUPPORT TASK) FOUND DENTS OUT OF LIMITS AT THE FWD CARGO DOOR EXTERNAL SKIN REQUIRE REPLACEMENT. REMOVED AND REPLACED THE FWD CARGO DOOR EXTERNAL SKIN IAW B737 SRM 52-30-01-2R-3. REMOVED AND REPLACED THE FWD CARGO DOOR EXTERNAL SKIN IAW SRM 52-30-01-2R-3.SDR SWAA2026071318820Sign · inoperativeAFT MIDDLE EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED AFT LT POWER SUPPLY AND BATTERY IAW AMM 33-51-06, R & R LAV D EXIT SIGN, OPS CHKD GOOD IAW AMM 33-51-01.SDR DALA2026071304090Oxygen Mask · unwanted deployO2 MASKS DROPPED AT 10A-C. RESET O2 MASK COVER PER AMM 35-12. ACFT OK. FOR SERVICE. (LP: 8441468, AIRCRAFT WAS GROUNDED)SDR WX0A2026070632873Engine · faulted(AIRCRAFT GROUNDED) (ENG SHUTDOWN EVENT) ENG 2 EGT OVER LIMIT / (FOLLOWUP - DI CLOSED) ENG 2 EGT OVER ALLOWED LIMIT. REMOVED #2 ENGINE PN CFM56-5B 4/3 SN 573435 IAW AMM 71-00-00-000-042-A. REPLACED WITH #2 ENG CFM56-5B 4/3 SN 779491 IAW AMM 71-00-00-400-042-A.SDR SWAA2026071018896Bulb · inoperativeEMERGENCY EXIT SIGN AT AFT LT DOORFRAME HAS INOP LIGHT BULBS. RELACED THE BULBS AND TESTED EMERGENCY EXIT SIGN AT AFT LT DOORFRAME PER AMM 33-51-01-960-801 TESTS GOOD.SDR SWAA2026071018897Bulb · inoperativeLEFT OVERWING EXIT OVERHEAD EMERGENCY LIGHT HAS INOPERATIVE LIGHT BULB. REPLACED THE BULBS AND PERFORMED GOOD TEST OF LT OVERWING EXIT OVERHEAD EMERGENCY LIGHT IAW AMM 33-51-01-960-801.SDR SWAA2026071018811Light · fluctuatesROW 11 DEF SIDEWALL LIGHT FLICKERING. REMOVED AND REPLACED 11 DEF SIDEWALL ASSY IAW AMM 33-21-00. OPS CHECK NORMAL.SDR SWAA2026071018895Bulb · inoperativeEMERGENCY EXIT SIGN AT FWD RT DOOR FRAME HAS INOPERATIVE LIGHT BULBS. REPLACED THE BULBS AND PERFORMED GOOD TEST OF FWD SERVICE DOOR EXIT INDICATOR LIGHT PER AMM 33-51-01-960-801.;[02] VERIFIED ITEM 1SDR IPXA2026071023113Angle · crackedCLOSE OUT ANGLE INBD ELEVATOR INBD SIDE 4 IN? CRACK INSTALLED NEW CLOSE OUT ANGLE ON INBOARD ELEVATOR INBD SIDE IAW SRM 51-40-02.INSTALLED NEW CLOSE OUT ANGLE ON IBD ELEVATOR INBD SIDE IAW SRM 51-40-02.SDR IPXA2026071022930Rib · crackedCRACK FOUND ON RIB I/B SIDE OF I/B ELEVATOR INSTALLED NEW CLOSEOUT RIB P/N 65B05845-1 IAW B747-8F SRM 51-40-02. INSTALLED NEW CLOSEOUT RIB P/N 65B05845-1 IAW B747-8F SRM 51-40-02SDR DALA2026070904027Power Supply · inoperativeEMERGENCY EXIT PATH AISLE LIGHTS INOP ROWS 21-31. REPLACED POWER SUPPLY M9009 IAW AMM 33-51. CHECKS OK. (LP 8875775 - AIRCRAFT WAS GROUNDED)SDR AALA202607095660Altimeter · defectiveAIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INTO RSW DUE TO THE FLIGHT CREW REPORTING THAT AFTER TAKEOFF AND GEAR RETRACTION, RECEIVED MASTER WARNING L/G DOWN MULTIPLE TIMES. AFTER LANDING, NAV RA DEGRADED CAUTION MESSAGE. MAINTENANCE RESET RADIO ALT'SDR AALA202607097027Cooling Fan · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO MCO DUE TO THE FLIGHT CREW REPORTING A BRAKES HOT ECAM AFTER TAKEOFF. THE FLIGHT CREW ACCOMPLISHED ECAM ACTIONS AND COOLED THE BRAKE TEMPERATURE WITH THE GEAR DOWN THE AIRCRAFT LANDED SAFELY AT MCO.SDR AALA202607092428Clamp · misinstalledAIRCRAFT IN BASE MAINTENANCE: CAPTAINS SLIDING WINDOW GUST LOCK RELEASE LEVER DOESNT RESET CORRECTLY. MAINTENNACE DETERMINED THAT THE LOCK RELEASE LEVER WAS FUNCTIONING CORRECTLY BUT DID FIND CLAMP IN SIDEWALL PANEL 211GW ON CAPTAIN SLIDE WINDOW WAS NOT INSTALSDR AALA202607097052Fitting · stuckAIRCRAFT WAS NOT GROUNDED: R1 DOOR LEFT HAND GIRT BAR FITTING STUCK DOWN. MAINTENANCE CLEANED AND LUBRICATED THE GIRT BAR FITTING PER AMM 53-11-00.SDR AALA202607098731Brake Assy · overheatedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO MCO DUE TO THE FLIGHT CREW REPORTING A BRAKES HOT ECAM AFTER TAKEOFF. THE FLIGHT CREW ACCOMPLISHED ECAM ACTIONS AND COOLED THE BRAKE TEMPERATURE WITH THE GEAR DOWN THE AIRCRAFT LANDED SAFELY AT MCO.