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 JR2R20260810811Ramp · nickedL1 DOOR BOTH FWD AND AFT DOOR COMMAND RAMPS HAVE MINOR NICKS. REPAIRSDR DALA2026081004599Seat Track · corrodedCORROSION SEAT TRACK -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA (SSI 5 34147). REPLACED SEAT TRACK -Y765 AND FASTENERS LOC. BTW FR64 TO FR66, AS PER SRM 51-72-11, A321 SRM 51-42-11, DWG D53472909, ISSUE: K, AND D53472903, ISSUE: Q. (LP 1748028 - AIRCRAFT WAS SDR ABXA20260810352Oxygen Bottle · low pressureDURING CREW PREDEPARTURE CHECK, EICAS PRESSURE INDICATION INOP READING 40 PSI. DEFERRED EICAS O2 PRESSOR INDICATION PER MEL 35-11-2-1 MX PROCEDURES COMPLY WITH PLACARD INSTALLED RE-INSPECT O2 PRESSURE BEFORE EA FLIGHT MUST BE COMPLY BY AUG 13, 2026. A/C RETURNSDR 2026FA0000633Mixer Box · failedSHORTLY AFTER REACHING CRUISE ALTITUDE OF FL410, AN AUDIBLE POP WITH ASSOCIATED RISE IN CABIN PRESSURE OCCURRED. CREW DESCENDED AND CABIN ALTITUDE AMBER CAS DISPLAYED AND QRH WAS ACCOMPLISHED. ACM O'HEAT AND HEAT EXCHG ONLY DISPLAYED UNTIL QRH PROCEDURE CLEARESDR FDEA202608101103Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BETWEEN BS 695 - 715, X = - 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK BS 695 - 715, X = - 47.5, EVALUATED AND FOUND EXCEEDED LIMT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1SDR FDEA202608101102Skin · dentedRIGHT WING OTBD FLAP LWR SURFACE 30 INCHES IB OF NR 7 FLAP SUPPORT FAIRING AND 5 INCHES FROM T/E FOUND DENTED. REPAIRED RHW OB FLAP LWR SURFACE 30 INCHES IB OF #7 FLAP SUPPORT FAIRING AND 5 INCHES FROM T/E DENT AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 ASDR JR2R20250810221Hinge Bracket · gougedRIGHT ELEVATOR HINGE #3 ON HORIZONTAL GOUGED AT O/B SIDE. OUT OF LIMITS. REPAIRED.SDR JR2R20250810220Hinge Bracket · gougedR/H ELEVATOR HINGE #2 ON HORIZONTAL GOUGED AT O/B SIDE. OUT OF LIMITS. REPAIRED.SDR CALA2026081018430Battery Pack · no testFOUND R4 FLASHLIGHT NOT TESTING. REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01, OPS CHECKED OKSDR IPXA2026102799400Angle · crackedLEFT WING, INSIDE FLAP KRUEGER COMPARTMENT, ANGLE BRACKET BESIDE LOWER PANEL SUPPORT HAS A CRACK. LOCATED AND DRILLED NEW ANGLE AT LT WING INSIDE FLAP KRUEGER COMPARTMENT IAW SRM 51-40-44-001.SDR IPXA2026110199453Web · gougedLEFT WING T/E BELOW SPOILER NR 4 OTBD HINGE, WEB IS GOUGED. INSTALLED NEW SKIN SUPPORT LT WING T/E BELOW SPOILER NR 4 OTBD HINGE IAW SRM 51-40-21-001.SDR IPXA2026110199370Hinge Fitting · crackedLEFT WING T/E BELOW SPOILER NR 5 I/B HINGE, WEB IS CRACKED. DOT 28-69. INSTALLED NEW SKIN SUPPORT AT ZONE 500: LH WING T/E BELOW SPOILER #5 I/B HINGE:I.A.W. A300-600 SRM 51-40-21-001: REVIEWED.SDR IPXA2026090798572Support · corrodedNR 2 PYLON, 482AR AFT PANEL SUPPORT HAS A GOUGE AND CORROSION AROUND. INSTALLED NEW GUSSET SUPPORT AT Z400- NR 2 PYLON, 482AR AFT PANEL SUPPORT IAW SRM 51-40-21-00-001.SDR IPXA2026102299324Bracket · crackedLH WING, FIXED LEADING EDGE INTERNAL STRUCTURE, ANGLE BRACKET INSIDE FLAP KRUEGER COMPARTMENT HAS A CRACK. LOCATED AND DRILLED NEW ANGLE BRACKET IAW SRM 51-40-44-001.SDR IPXA2026092998707Fitting · crackedRH FR40 CWB UPPER SKIN TENSION BOLT JUNCTION. MIDDLE FASTENER HOLE (SECOND FROM TOP) HAS MULTIPLE CRACK INDICATIONS THROUGHOUT HOLE. REAMED HOLE "B" (MIDDEL) AT FR 40 R/H 0.6140" IAW A300-600 SRM 57-10-24, FIG 206 SHEET#2, AND SRM 51-40-44. INSTALLED BOLT P/N:SDR IPXA2026100799313Stiffener · crackedLH WING, FIXED LEADING EDGE INTERNAL STRUCTURE, STIFFENER INSIDE FLAP KRUEGER COMPARTMENT HAS A CRACK .INSTALLED NEW STIFFENER AT INSIDE FLAP KRUEGER COMPARTMENT IAW SRM 51-40-21. REVIEWED.SDR IPXA2026100692769Plate · crackedNR 2 PYLON RH SIDE PANEL SUPPORT BETWEEN 422DR AND 424CR HAS CRACKED PLATE. NEW FISH PLATE INSTALLED IAW A300-600 SRM 51-40-21. REVIEWED.SDR SIMA20260809008Seat Track · corrodedSSI 53-10-027: FWD GALLEY LH SEAT TRACK DOUBLER CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION) RAR DOUBLER AND FILLER ON FWD GALLEY LH SEAT TRACK IAW ERJ 170 SRM 53-10-10/REPAIR 01P.SDR SIMA20260809006Floorbeam · corrodedFWD GALLEY CROSBEAM CORRODED BTWN RH FLOOR BEAM AND SERV DOOR CUTOUT AT FR 1. (MAJOR REPAIR). INSTALLED REPAIR PARTS (FILLER & INNER DOUBLER) ON FWD GALLEY CROSSBEAM FR 17 IAW ERJ-170 SRM 53-00-10 RE03.SDR SIMA20260809007Seat Track · corrodedSSI 53-10-027: RH LWR SEAT TRACK CORRODED BTWN FR 17-18. (LVL 2 CORROSION) (MAJOR REPAIR). RAR RH LOWER #1 SEAT TRACK BEAM IAW ERJ 170 SRM 51-40-08.SDR REXA2026092101857Latch · crackedFWD LAV SERVICING DOOR TOP HINGE AND BOTTOM LATCH BROKEN TOP HINGE AND BOTTOM LATCH AT FWD LAV SERVICING DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ9-00 SRM 51-41-02-001-001-A01.SDR REXA2026092101856Hinge · crackedFWD LAV SERVICING DOOR TOP HINGE AND BOTTOM LATCH BROKEN TOP HINGE AND BOTTOM LATCH AT FWD LAV SERVICING DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ9-00 SRM 51-41-02-001-001-A01.SDR REXA2026092101831Floorbeam · corrodedRT BS 280 BEAM HAS CORROSION UNDER UPPER SPLICE STRIP. BLENDED CORROSION ON RT BEAM UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. BEAM REQUIRES REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE RT CROSSBEAM IAW SRM 5SDR REXA2026092101830Floorbeam · corrodedLT FS280 BEAM HAS CORROSION ON FWD SIDE UNDER J-ANGLE. BLENDED CORROSION ON LH FS280 BEAM UNDER J-ANGLE & UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. LT 280 BEAM REQUIRES REPLACEMEMNT. INSTALLED UPPER SPLICE STRIP SDR SIMA20260809004Shear Panel · corrodedCENTER SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IS CORRODED. (LEVEL 2 CORROSION). R & R CENTER SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IAW SRM 51-40-08.SDR SIMA20260809005Shear Panel · corrodedRH SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IS CORRODED. (LEVEL 2 CORROSION) R & R RT SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IAW ERJ 170 SRM 51-40-08SDR AALA202609175155Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO RH TRANSITION PANEL 500C-500E MULTIPLE AREAS OF CORROSION AT FASTENER HOLES. INSTALLED NEW RH TRANSITION PANEL IAW IPC 53-42-11-11 AND AARD 51-00-05-1.SDR AALA202609154414Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO LEFT TRANSITION PANEL 500A-500C MULTIPLE AREAS OF GALVANIC CORROSION AT FASTENER HOLES. INSTALLED OF NEW LT TRANSITION PANEL AND SPLICE IAW IPC 53-42-11-11 AND AARD 51-00-05-1 AND SRM 53-00-53-2R-5.SDR AALA202609152914Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO- LT TRANSITION PANEL 500C-500I MULTIPLE AREAS OF EXFOLIATION CORROSION AT FASTENER HOLES. NEW L/H TRANSITION PANELSDR AALA202609152091Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO RH TRANSITION PANEL 500E-500I MULTIPLE AREAS OF CORROSION AT FASTENER HOLES. INSTALLED NEW RH TRANSITION PANEL IAW IPC 53-42-11-11 AND AARD 51-00-05-1.SDR REXA2026091101805Angle · crackedCRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001-SDR REXA2026091101804Angle · crackedCRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001-SDR IPXA2026082799311Bracket · crackedLEFT CENTER FLAP, OTBD FACE, AFT BRACKET BROKEN. REMOVED AND REPLACED ONE BRACKET AT LT CENTER FLAP, OTBD FACE IAW SRM 51-40-21-001.SDR IPXA2026083199328Structure · chafedLEFT WING, FIXED LEADING EDGE INTERNAL STRUCTURE, RIVETS AND STRUCTURE ABOVE THE PNEUMATIC DUCT HAVE CHAFE MARKS. REMOVED WEB AT LH WING LEADING EDGE INTERNAL STRUCTURE IAW SRM 51-40-21-001. INSTALLED NEW WEB AT LT WING LEADING EDGE INTERNAL STRUCTUR IAW SRM SDR REXA2026090401772Frame · corrodedSTRINGER 21L CORRODED FWD OF BS 319. REMOVED CORROSION FROM FS319 BETWEEN STR 21L AND STR 20L IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS MEASUREMENTS OF REWORKED AREAS IAW NDTM PART 1, 51-20-004-270-A01, REV-37. FOUND LOWEST REMAINING THICKNESS TO SDR SWAA2026090143085Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500, STR 26L IN THE FWD CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 TEM 9 AND DWG 143A7505 SHEET:119 REV:-.SDR SWAA2026090182195Shield · crackedCRACKED SHIELD WEB LOCATED BTW BS 492.5 TO BS 500A, STR 26R IN FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 492.5 TO BS 500A AT LVEL STR 26R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A0080 SDR SWAA2026090184084Scuff Plate · crackedCRACK ON SCUFF PLATE LOCATED FWD POSITION CUT OUT DOOR AT AFT CARGO COMPARTMENT. REPAIRED SCUFF PLATE LOCATED FWD POSITION CUT OUT DOOR AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SDR SWAA2026090160750Support Angle · crackedCRACKED SUPPORT ANGLE BS 500C FWD POSITION AT LEVEL STR 26L ON FWD CARGO COMPARTMENT. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 500C FWD POSITION AT LEVEL STR 26L ON FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET: 117 AND SHEET: 118SDR IPXA2026082792230Channel · crackedCRACKED SPLICE CHANNEL, LT BODY GEAR WHEEL WELL, OTBD STRUT INTERCOSTAL UPPER ATTACHMENT AT BS 1372. REMOVED THE DAMAGE CHANNEL IAW SRM 51-40-02-0G, REV 49. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 49, & DWG 65B15001, SH 6, REV B.SDR IPXA2026082792256Channel · crackedCRACKED SPLICE CHANNEL, RT BODY GEAR WHEEL WELL OTBD STRUT INTERCOSTAL UPPER ATTACHMENT AT BS 1372. REMOVED THE DAMAGED CHANNEL IAW SRM 51-40-02-0G, REV 49. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 49, & DWG 65B15001, SH 6, REV B.SDR MASA20260824215Gusset · corrodedDURING HEAVY CHECK, INSPECTIONS OF CF ILL, CORROSION ON GUSSET PLATE AT FR 90, RIH, RBL 23 REPLACED WITH NEW GUSSET PLATE IAW ERJ 175 SRM 51-41-02. NRC# 4502709-1000-0105, REV 45 DATED MAY-28-2021.SDR AALA202608249832Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202608244630Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202608246879Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202608241316Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202608242001Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER ELEVATOR POSITION 4 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202608247965Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202608246227Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202608242899Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42