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 JJBA20260819015Battery Pack · inoperativeRH OVERWING EXIT IDENTIFIER AND AFT GALLEY WALL EXIT LOCATOR INOPERATIVE. REMOVED AND REPLACED INVERTER 3. OPS CHECK FAIL. REMOVED AND REPLACED BATTERY SUPPLY. OPS CHECK SAT.SDR SIMA20260818001Door · no discrepancyCATERING TRIED TO OPEN L2 DOOR AND THEY COULDN'T OPEN IT FROM OUTSIDE. OPERATED L2 DOOR IAW AMM 52-12-00 AND FOUND NO DEFECTSSDR CALA2026081918727Light · brokenESCAPE PATH LIGHT ASSEMBLY ON SEAT 33D, 40F AND 50F ARE BROKEN. REMOVED AND REPLACED ESCAPE PATH LIGHT ASSEMBLY ON SEATS 40F AND 50F REF AMM 33-51-10-962-104. ESCAPE PATH LIGHT SYSTEM IS GOOD FOR SERVICE.SDR CALA2026081918725Skin · damagedAFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN BTW STA 269 AND 1.5" ABOVE OF S-19R. APPLIED PRIMER ON NEW RIVET ON FUSELAGE EXTERNAL SKIN AND SPOTFACE ON INTERNAL SKIN IAW B737-900ER IAW SRM 53-00-01-2R-38 STEP 4 E (6) SOPM 20-44-04. PERFOSDR TSAA2026081700001Cabin Press Sys · faultedAT 1000 FT ON CLIMB OUT AUTO FAIL LIGHT ILLUMINATE AND STANDBY LIGHT ILLUMINATE CLIMB RATE PASS 3000FT/MIN DRIVE CABIN PRESS BELOW SEA LEVELSDR 2026FA0000652Skin · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON RT SIDE OF STINGER SKIN, UPPER VORTEX GENERATOR ATTACHMENT AREA IAW SRM 51-70-03. FOUND CORROSION BLENDS TO BE BEYOND SRM 51-70-03 LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. PERFORMED AN EDSDR 2026FA0000651Fuel Cap · failedAIRCRAFT EXPERIENCED A LOSS OF ENGINE POWER WHILE IN FLIGHT NEAR AMALGA, UTAH. THE PILOT ELECTED TO MAKE A PRECAUTIONARY LANDING IN A FIELD. THE CAUSE OF THE ENGINE POWER ISSUE WAS DETERMINED TO BE A VENTED FUEL CAP THAT WAS NOT VENTING PROPERLY. THE IMPROPER SDR IPXA2026081835595Crash Axe · corrodedMAIN CARGO DECK CRASH AX IS CORRODED AND DAMAGED REMOVED AND REPLACED THE MAIN CARGO DECK CRASH AX IAW AMM 25-63-04-400-801.SDR IPXA2026081830212Actuator · faultedATB, GEAR DISAGREE EICAS AND GEAR LIGHT. RAN CHECKLIST RETURN TO CAE & CAUTION LIGHT TOO. REVERSED DMP 32-30-1. REPLACED PROX SWITCH 065 REF FIM 32-09 FAULT TREE 821. ADJUSTED PROX SWITCHES 065 AND 078 AS REQUIRED TO 5.5 MILIHENRI NEAR BOTH LOCKED AND UNLOCKEDSDR IPXA2026081830886Life Vest · missingFO'S LIFEVEST MISSING. INSTALLED LIFEVEST PER MM 25-62-05.SDR FDEA202608181142Processor · faultedTAKEOFF AT IND, MLG WOULD NOT RETRACT. C-W QRH. RETURNED. EMERG DECLARED. AMM 32-31-00-05, NLG RETRACT FULLY, GREEN ON BOTH MLG INDS, BOTH LT & RT MLG STAYED GREEN DOWN ON INDS. PERFORMED MLG EXTEND & RETRACT AT GATE & VERIFIED ALL MLG DOORS EXTEND & RESDR FDEA202608181141Skin Panel · dentedDENT ON RH LWR HORIZONTAL IB FWD SKIN APPLIED PERMANENT REPAIR AT RH LWR HORIZONTAL I/B FWD SKIN IAW B757 SRM 51-70-10-2R REP 4SDR JR2R20260818112Panel · chafed429NR HAS BARE METAL SPOTS AND CHFING ON INNER SURFACE. REPAIRSDR 2026FA0000650Control Valve · faultedAIRCRAFT EXPERIENCED AN AIR DUCT OVERHEAT.SDR DALA2026081804712Carriage · crackedLEFT WING FLAP TRACK 3 OTBD CARRIAGE-BRIDGE CRACKED. REPLACED IAW AMM 27-54-78. OK FOR SERVICE. (1762944) AIRCRAFT WAS GROUNDED.SDR DALA2026081804710Skin · damagedELONGATED HOLES ON CUT OUT LOC BTW RIB14 AND RIB15 FUEL TANK ON RH WING, REPAIRED CUT OUT HOLES PER SRM 57 -21-11-300-002 AND REPLACED GANG CHANNEL AS PER A320 SRM 51-72- 11. (1762554) (AIRCRAFT GROUNDED).SDR DALA2026081804707Holder · looseSLIDE INDICATOR LIGHT INOPERATIVE OR DAMAGED. FOUND LAMP BASE LOOSE AT DOOR. BASE REINSTALLED & TESTED. (1762599)(AIRCRAFT GROUNDED)SDR QR9R2026081800001Sensor · erraticROTOR RPM INDICATOR GAVE ERRATIC INDICATIONS FROM 101% TO 80% DURING FLIGHT. THE ROTOR LOW WARNING LIGHT INDICATION FLUCTUATED INTERMITTENTLY, NEVER STAYING ON. THE LOW ROTOR AUDIO NEVER SOUNDED OFF. REMOVED AND REPLACED THE SPEED PICKUP SENSOR IAW AMM 62-41-0SDR CALA2026081818706Controller · faultyAT 30000 FT BOTH PACK TEMP AND PACK OFF LIGHTS ILLUMINATED, EICAS AUTO EVENT RECORDED. PERF. PACK TEMP. CONTROLLER BITE REF. FIM 21-51 FAULT TREE 803. NO FAULTS. OPERATED BOTH PACKS WITH APU BLEED AIR FOR 1 HOUR REF. AMM 21-00-00. UNABLE TO DUPLICATE FAULTS. PSDR SWIA2026081777830Web · crackedCRACK NOTED ON THE AFT LOWER REFUEL MOUNT, ON THE WEB LOCATED FWD OF BS 677 BELOW STRINGER 21R. REPAIR WAS PERFORMED ON AFT LOWER REFUEL MOUNT ON THE WEB LOCATED FWD OF BS 677 BELOW STGR 21R, IAW SRM 51-42-06, SRM 51-42-21, & REO 690-28-25-052, REV -.SDR VNAA202610280006Skin Panel · damagedLIGHTNING STRIKE DAMAGE TO WING RH UPPER FWD PLANK BETWEEN WS29.76-WS68.00 AND BETWEEN STR19R-STR21R. LIGHTNING STRIKE DAMAGE TO WING RH UPPER FWD PLANK BETWEEN WS29.76-WS68.00 AND BETWEEN STR19R-STR21R WAS REPAIRED PER 690-57-21-576 REV. - -SDR VNAA202610280005Skin Panel · dentedSKIN LWR BELLY PANEL FS 270.5 BETWEEN R/H STG 26 & 25 1. WITHIN 7248.62 FLIGHT HOURS FROM REV A, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. SKIN LWR BELLY PANEL FS 270.5 BETWEEN R/H STG 26 & 25 WSDR VNAA202610280004Rib · damagedTEMP REPAIR FOR DAMAGE TO LH PYLON UPPER CANTED RIB BETWEEN FS1069.75 - FS1088.20 THIS TEMPORARY REPAIR IS STRUCTURALLY ACCEPTABLE FOR 8000 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV "-" PERFORM A PERMANENT REPAIR IAW APPROVED PROCEDURES. // ENSDR IPXA2026100228085Stiffener · crackedL/H WING, KRUEGER FLAP MOVABLE VANE, CRACK UNDER TEFLON STOP BASE. DOT 73-176. INSTALLED STIFFENER AND REINSTALLED COVER SEAL + FITTING IAW A300 SRM 51-40-21. REVIEWEDSDR SWIA2026081777535Pressure Deck · corrodedEVIDENCE OF CORROSION UNDER THE RH OVERWING EMERGENCY EXIT DOOR ON THE PRESSURE DECK AREA IN TWO SPOTS BETWEEN FS 76185 AND FS 78515 MARKED WITH RED GREASE PENCIL C-CHECK RO 10062026REPAIRED CORROSION DAMAGE TO RH PRESSURE FLOOR SILL ANGLE BETWEEN FS75652- FSDR SIMA20260817003Spar · bentSSI # 55-10-017 RH HORIZONTAL STAB LOWER LEADING EDGE ATTACHMENT FLANGE BENT BETWEEN RIB 10 AND RIB11. (MAJOR REPAIR). PERFORMED A PERMANENT REPAIR ON RH HORIZONTAL STAB LOWER LEADING EDGE ATTACHMENT FLANGE BENT BETWEEN RIB 10 AND RIB 11 IAW ERS-EJ-55MR-1161SDR SWAA2026092971274Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727F, LBL 51. REPAIRED THE SUPPORT ANGLE BTWN BS 727D+15 - 727F+8 IAW SRM 51-70-11-2R-0, REPAIR GENERAL.SDR SWAA2026092953464Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE BS 727D, LBL 51. REPAIRED SUPPORT ANGLE BTWN BS 727A - 727D + 16 IAW SRM 51-70-11-2R-0, REPAIR GENERAL.SDR SWAA2026092953453Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727B, LBL 51. REPAIRED THE SUPPORT ANGLE BS 727A - 727D + 16, LBL 51 IAW SRM 51-70-11-2R-0, REPAIR GENERAL.SDR SWAA2026092956036Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727H, LBL 51. REPAIRED THE CARGO LINER SUPPORT ANGLE BTWN BS 727H - 727J +14, RBL 51 IAW SRM 51-70-11-2R-0, REPAIR GENERAL.SDR AALA202609272215Hinge 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 55-16-42SDR SWAA2026092490291Support Angle · crackedCRACK ON CARGO LINER SUPPORT ANGLE, BS 887, RBL 52 IN THE AFT CARGO. REPAIRED CARGO LINER SUPPORT ANGLE LOCATED IAW SRM 51-70-11-2R-0, REPAIR GENERAL.SDR SWAA2026092313059Nut Plate · crackedCRACKED NUT PLATE, OFSS 604, INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATE BTWN OSS 362.51 - 384.24. IAW SRM 51-40-02, & DWG 112A4402, SHEET 14, REV-.SDR SWAA2026092332053Doubler · damagedELONGATE HOLE ON DOUBLER ON REAR SPAR, RT VAPOR BARRIER BS 663 BTWN RBL12 - 27. FABRICATED A DOUBLER, & LOCATED IAW DWG 111A1512, SHT 3, REV-.SDR SIMA20260817002Rib · chafedVERTICAL STABILIZER RIB 14 HAS 2 CHAFED SPOTS. (MAJOR REPAIR) REMOVED AND REPLACED VERTICAL STABILIZER RIB 14 IAW SRM 51-40-08.SDR SWAA2026092106314Nut Plate · crackedCRACKED NUT PLATE, OFSS 404, INTERNAL CAVITY L/E OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092101997Support Frame · damagedELONGATE HOLE ON FRAME ON RT VAPOR BARRIER BTWN BS 655 - BS 693, RBL 12. EVALUATED & FABRICATED THE FRAME IAW SRM 51-40-05-0G-0, & DWG 149A7214, SHEET 7, REV -. DOUBLER INSTALLATION WILL BE ACCOMPLISHED TTG8Q01DQJAS.SDR SWAA2026092127237Nut Plate · crackedCRACKED RAIL NUT PLATE LOC OFSS 570, INTERNAL CAVITY LEADING EDGE OF RT WING. REMOVED THE NUT PLATE IAW SRM 51-40-01 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREAS AND DID NOT FIND OTHER DAMAGE. REPLACED THE NUT PLATE IAW SRM 51-40-01, SRM 51-40-02, SRM SDR SWAA2026092139892Strap · crackedCRACK INDICATION ON STA 639 AT LBL 45.57 STUB BEAM STRAPS AREA (IN AFT FASTENER HOLE) AT PASSENGER CABIN. REPLACED STRAPS (2EA) LOCATED AT STUB BEAM BTW STA 639 AT LBL 45.57 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 DWG 144A1705 SHEET:8 REV:- AND DWSDR SWAA2026092130117Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE IN THE RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092188030Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 385 INTERNAL CAVITY LEADING EDGE OF THE LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092147620Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 337 INTERNAL CAVITY LEADING EDGE OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092127663Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 588 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-.SDR SWAA2026092109501Nut Plate · crackedCRACK RAIL NUT PLATE LOC OFSS 449 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG:112A4402, SHEET 40, REV A.SDR SWAA2026092186645Nut Plate · crackedCRACKED RAIL NUT PLATE LOC OFSS 491 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A.SDR SWAA2026091814040Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727B, LBL 51 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE BTWN BS 727A - 727E+10 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 149A9490, SHEET 21, REV -.SDR SWAA2026091837580Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE LOC STA 727C LBL 51 AT AFT CARGO BAY. REPLACED CARGO LINER SUPPORT ANGLE LOCATED BTW BS727A TO BS727E+10 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 149A9490, SHEET 21, REV -.SDR SWAA2026091883552Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727E, LBL 51 IN THE CARGO BAY. REPLACED THE SUPPORT ANGLE BS 727A - 727E+10 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 149A9490, SHEET 21, REV -.SDR SWAA2026091802628Crossbeam · crackedCRACKED BRAKE PANEL LOCATED BS 540 BTW RBL 24.75 TO RBL 45.5 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW RBL 24.75 TO RBL 45.5 WL 208.1 AT PASSENGER CABIN IAWSRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG: 143A0060 SHEET: 46 REV: -SDR SWAA2026091864779Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW LBL 24.75 TO LBL 45.5 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL IAW SRM 51-10-02 ITEM 9 AND DWG 143A0060, SHEET 46, REV -.