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 SWIA2026031476146Intercostal · corrodedPAX DOOR MID INTERCOSTAL DD3 FOUND CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD3 IAW SRM TASK 51-42-06-001-001-A01AND SRM TASK 51-42-21-001-001-A01.SDR VNAA20260501005Hinge · scratchedWEAR ON LUG LAND AT PIANO HINGE PASSENGER DOOR. LUG LAND AT PIANO HINGE PASSENGER DOOR WAS REPAIRED WITH INSPECTION REQUIREMENTS FOR TYPE REPAIR IV: THRESHOLD 5,700 FLIGHT CYCLES AND REPEAT WITH 5,700 FLIGHT CYCLES PER REO 670-53-21-582 REV.-G.SDR VNAA20260501004Hinge · scratchedSCRATCHES ON SEVERAL POINTS AT PIANO HINGE LUGS PASSENGER DOOR. PIANO HINGE LUGS PASSENGER DOOR WAS REPAIRED WITH INSPECTION REQUIREMENTS FOR TYPE REPAIR I: THRESHOLD 5,700 FLIGHT CYCLES AND REPEAT WITH 5,700 FLIGHT CYCLES PER REO 670-53-21-582 REV.-G.SDR VNAA20260501003Door · crackedCRACK ON TOP EDGE MEMBER AT LH AFT EMERGENCY EXIT DOOR. TOP EDGE MEMBER AT LH AFT EMERGENCY EXIT DOOR WAS REPAIRED PER REO 670-52-21-103 REV-.SDR 3EJA202605010002Bracket · bentIMMEDIATELY FOLLOWING TAKEOFF FROM KSYR, THE LANDING GEAR HANDLE WAS SELECTED UP. THE LANDING GEAR FAILED TO RETRACT, AND THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. R&R NLG BRACKET ASSY WITH NEW BRACKET AND ADJUSTED AND SECURED LH MLG ACTUATOR LOCK NUSDR CALA2026042915831Skin · crackedNDT CRACK INDICATION IDENTIFIED AT FS500A +20, .35" OTBD OF S2L IN PROXIMITY TO EA 5330-04336 CHEM MILL STEP INSPECTION AND PREVENTATIVE MOD SERVICE BULLETIN AREA FWD LH DOUBLER AND FILLER. WORKING DEFECT ON LAUNCH NON ROUTINE 5310-08359/006.THIS WILL BE A MAJSDR SWAA2026042779882Rib · crackedCRACKED BEAM, DEFLECTION CONTROL RIB ON RT WING. PERFORMED PERMANENT REPAIR LOCATED ON DEFLECTION CONTROL RIB AT RT WING IAW SRM 57-51-02-2R-3 REPAIR 3.SDR SWAA2026042779881Lens · missingMISSING LENS EMERGENCY LIGHT ON SIDEWALL PANEL 231ZKW AT PASSENGER CABIN. INSTALLED LENS EMERGENCY LIGHT ON SIDEWALL PANEL 231ZKW AT PASSENGER CABIN IAW AMM 33-51-01-960-802.SDR AALA202604238829Support Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL STRUCTURE SUPPORT ANGLE AT FR 71 BETWEEN S27R AND S31R IN THE THS COMPARTMENT. REPLACED ANGLE PER SRM 51-72-11.SDR SWAA2026042279868Nut · looseDETERIORATED NUT ASSIST HANDLE ON DOOR LINING 831 FWD ENTRY DOOR AT FWD GALLEY AREA 4EA. REPLACED NUT ASSIST HANDLE ON DOOR LINING 831 FWD ENTRY DOOR AT FWD GALLEY AREA IAW AMM 52-11-31-400-802 STEP 3.G ITEM (2).SDR SWAA2026042279867Handle · deterioratedDETERIORATED NUT ASSIST HANDLE ON DOOR LINING 841 FWD SERVICE DOOR AT FWD GALLEY AREA 2EA. REPLACED NUT ASSIST HANDLE ON DOOR LINING 841 FWD SERVICE DOOR AT FWD GALLEY AREA 2EA IAW AMM 52-41-31-000-802 STEP 2. E. ITEM (4) AND AMM 52-41-31-400-802 STEP 3. F.SDR SWAA2026042091121Frame · crackedCRACK FRAME LOCATED BS 312 BTW STR5L TO STR6L AT PASSENGER CABIN 2026-181127<[01] PERFORMED TRIMMING OUT ON FRAME BS 312 BTW STRINGER 5L & 6L AT PASSENGER CABIN. IAW EA# M-22-153-01244 REV 3.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETED TASK CERTIFIEDSDR SWAA2026042079836Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, LBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 149A8102, SHEET 19, REV A. MEASUREMENT OF CRACK IS L= 0.602.SDR SWAA2026042079837Fitting · crackedCRACKED FITTING, BS 947.5 AND LBL10. REPLACED THE FITTING IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DWG 149A8103, SHEET 8, REV -.SDR SWAA2026042079742Frame · crackedCRACK FRAME LOCATED BS 312 BTW STR5L TO STR6L AT PASSENGER CABIN. PERFORMED TRIMMING OUT ON FRAME BS 312 BTW STRINGER 5L & 6L AT PASSENGER CABIN. IAW EA M-22-153-01244 REV 3.SDR SWAA2026042079743Tie Clip · crackedCRACK TIE CLIP LOCATED BS 277 STR10R AT PASSENGER CABIN . REPLACED TIE CLIP LOCATED BS277 STR10R AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A1110 SHEET 55 REV -.SDR SWAA2026041779834Hook And Loop · out of adjustVELCRO STRIP ON THE GIRT ARE NOT ATTACHED TO THE VELCRO STRIP ON THE BACKING PAN SHELF LOCATED AFT SERVICE DOOR AT PASSENGER CABIN. INSTALLED CORRECTLY GIRT VELCRO STRIP ON BACKING PAN SHELF AT ESCAPE SLIDE AFT SERVICE DOOR.SDR CALA2026041715458Pressure Web · crackedCRACK FOUND AT VERTICAL PRESSURE WEB BS 663 AT RBL 40 - RBL45.64. INSTALLED 100-% FASTENERS AT RT SIDE VERTICAL PRESSURE WEB REPAIR FROM RBL-25 TO RBL-50 BS 663 REF SRM 57-10-10-2R-3 STEP 5.L TABLE 202 FIGURE 204 CATEGORY B REPAIR INSPECTION REQUIREMENTS FOR SDR SWAA2026041679842Support Angle · corrodedCORROSION ON SUPPORT ANGLE BTW BS 767 - 787, WL 156 AND RBL 21 AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 146A8123, SHEET 16, REV -, & DWG 146A0081, SHEET 49, REV A.SDR SWAA2026041679835Web · corrodedCORROSION ON SHIELD WEB, BETWEEN BS 767 - 787, WL 156, & RBL 21 IN THE AFT CARGO BAY. REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS767 TO BS787 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG146A0081 SHEESDR SWAA2026041679838Intercostal · crackedCRACKED INTERCOSTAL BTW BS 927 - 947, RBL 21 IN THE AFT CARGO BAY. REPLACED THE INTERCOSTAL, NUTPLATE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A7500, SHEET 37, REV-.SDR SWAA2026041579824Frame · crackedCRACK FRAME ON BS 440 BTW STR 8R TO STR 9R AT PASSENGER CABIN. REPAIRED FRAME UPPER FUSELAGE AIR CONDITIONING BRACKETS AREA AT BSTA 440 AND BETWEEN S-8R AND S-9R IAW EA 26-153-00794-WIP1; EA 26-153-00794-WIP2 AND EA 26-153-00794.SDR SWAA2026041579825Frame · crackedCRACKED FRAME ON BS 440 BTW STR 8L TO STR 9L AT PASSENGER CABIN. REPAIRED FRAME UPPER FUSELAGE AIR CONDITIONING BRACKETS AREA AT BSTA 440 AND BETWEEN S-8L AND S-9L IAW EA 26-153-00793-WIP1; EA 26-153-00793-WIP2 AND EA 26-153-00793.SDR SWAA2026041379806Attach Angle · crackedLH SIDE 663 VAPOR BARRIER ATTACH ANGLE AT APPROXIMATELY LBL 34 HAS CRACK. SEE IMAGE.<[01] CUT AND REMOVED CRACKED ANGLE FROM APPROX LBL32 TO LBL65 IAW SRM 57-10-10-2R-5;[14] L/H VAPOR BARRIER ATTACH ANGLE REPAIRED IAW SRM 57-10-10-2R-5; EA M-24-157-02340 AND ESDR SWAA2026041379805Attach Angle · crackedRH SIDE 663 VAPOR BARRIER ATTACH ANGLE AT APPROXIMATELY RBL 34 HAS CRACK. SEE IMAGE.<[01] CUT AND REMOVED CRACKED ANGLE FROM APPROX RBL32 TO RBL65 IAW SRM 57-10-10-2R-5;[02] VERIFIED CA #1 <BR>CUT AND REMOVED CRACKED ANGLE FROM APPROX RBL32 TO RBL65 IAW SRM 57SDR IPXA2026033168029Tray · crackedAPU FIRE BOTTLE TRAY CRACKED AT 4EA MOUNTING BOLT HOLES. INSTALLED FIRE BOTTLE BRACKET AT THE AFT BULKHEAD APU. IAW SRM 51-40-02-OG.SDR IPXA2026040374899Doubler · corrodedMAJOR REPAIR, NR 2 PYLON INTERNAL AREA BETWEEN PANELS 443CR AND 443BR HAVE CORROSION. COMPLIED WITH EO-97012-REQ1 AND VT-MAE EA 757-5450-27-A4401, REV -SDR HNAA2026040600267Floor Support · corrodedFLOOR SILL RH AT FR 39 HAS CORROSION. REMOVED AND REPLACED WITH NEW FLOOR SILL RH AT FR 39 IAW EMB 145 SRM 51-40-02-PRSDR SIMA202604064001Seat Track · corrodedSEAT TRACK IS CORRODED BETWEEN FR 84 & 85, Y+276 (MAJOR REPAIR). BLENDED CORROSION IN MULTIPLE AREAS, AREAS OUT OF ALLOWABLE LIMITS IAW SRM 53-23-10 AD01. REMOVED DAMAGED SECTION OF RT AFT SEAT TRACK IAW ETD2022-170-022163 REV.:C. LOCATED, TRIMMED, DRILLESDR SIMA20260314003Floorbeam · corrodedRIGHT FLOORBEAM CORRODED, Y+276 AFT OF FRAME FR 90 (MAJOR REPAIR). BLENDED CORROSION ON RT FLOORBEAM IAW SRM 51-10-03. BLENDED AREA MEASURES (INTERCOSTAL - W =1.3", L = 2.0", H = 010".) ORIGINAL MATERIAL THICKNESS OF .040, (ANGLE - W = .8", L = 2.- 0", H = .0SDR IPXA2026040178991Angle · crackedFAULT - Z400 - STR #1 PYLON INBD SIDE THROUGH CIRCLE ACCESS PANEL, INTERNAL AFT UPPER SURFACE HAS A CRACKED STRUCTURAL CLIP. DOT 93-012. REMOVED CRACKED CLIP AT #1 PILON I/B SIDE INTERNAL AREA AFT UPPER SURFACE IAW B757-200 SRM 51-40-02. INSTALLED CLIP IAW B75SDR IPXA2026040278578Rib · crackedUPON FURTHER INSPECTION OF DAMAGED LEFT WING #5 SPOILER ACCESS DOOR, FOUND UNDERLYING STRUCTURAL DAMAGE TO SPOILER HINGE. INSTALLED NEW "RIB JACK ABX 148-625" AT LEFT WING #5 SPOILER IAW A300-600 SRM 51-40-21-001.SDR SWAA2026040179794Floorboard · frayedCENTER CABIN FLOORBOARD 231XF HAD FIBERS FRAYING. REMOVED AND INSTALLED THE FLOORBOARD 231XF IAW AMM 53-21-00.SDR SWAA2026040179795Floorboard · frayedCENTER CABIN FLOORBOARD 241AF, FIBERS FRAYING. REMOVED AND INSTALLED THE FLOORBOARD 241AF IAW AMM 53-21-00.SDR CALA2026033014890Skin · crackedCRACK IN RT LWR WING SKIN FOUND DURING EA 5720-03614 REV 'A' INSPECTION PERFORMED IN SFO BY UAL. AIRCRAFT FERRIED TO GSO FOR REPAIR. MAJOR REPAIR. REMOVED, LOCATED, DRILLED AND INSTALLED NEW RT WING LOWER OUTBD SKIN PANEL AND RESTORED COATINGS REF SRM 51-40SDR IPXA2026032668052Gusset · crackedLEFT AND RIGHT LATCH STOPS AT THE CUT-OUT, FOUR BRACKETS ARE CORRODED. INSTALLED THE FOUR BRACKETS, LT OTBD GUSSET LT INBD GUSSET, RT INBD GUSSET, RT OTBD GUSSET IAW SRM 51-40-02.SDR IPXA2026032579167Angle · crackedFWD CARGO THROUGH ACCESS PANEL 122AZ CUTOUT HAS A CRACK. INSTALLED NEW CORNER ANGLE ON INNER LOWER STRUCTURE AND REINSTALLED INNER LOWER STRUCTURE ON ACCESS PANEL 122AZ I.A.W SRM 51-40-02.SDR IPXA2026031475944Web · corrodedCORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN.SDR 4DPA2026031400001Fuel Unit · failedCREW REPORTED-DURING CLIMB OUT WE GOT FUEL IMBALANCE FOLLOWED BY LEFT TANK SHOWING ZERO AND ALSO ON MFD . ALL FUEL PUMPS WERE OUT . RIGHT TANK WAS SHOWING 2700 . ALL REQUIRED CHECKLIST WAS PERFORMED AND FLIGHT DIVERTED TO BURBANK . LANDED SAFELY IN BURBANK ANDSDR AALA202603259581Stop Pad · out of positionAIRCRAFT WAS NOT GROUNDED: RIGHT HAND AFT OVERWING EXIT DOOR UPPER AFT STOP PAD ROTATED. ROTATED THE RIGHT HAND AFT OVERWING EXIT DOOR UPPER AFT STOP PAD TO THE CORRECT POSITION AND ORIENTATION. PER B737NG SRM 51-40-02.SDR AALA202603242106Engine · vibrationAIRCRAFT WAS GROUNDED: AT CRUSE AT FL360 NR 1 ENGINE STARTED MAKING A THUDDING NOISE, AND THE N1 ROLLED BACK FALLOWED BY A ENG 1 STALL ECAM. N1 THEN RECOVERED, HOWEVER THERE WAS MORE THUDS THAT COULD BE FELT, AND N1 CONTINUED TO FLUCTUATE. WE OPTED FOR A PRECSDR AALA202603239507Escape Hatch · bindingAIRCRAFT IN BASE MAINTENANCE: 2EA MAIN CABIN OFAR AFT ESCAPE DOOR LATCHS HARD TO OPEN. REMOVED AND REPLACED ESCAPE DOOR LATCHS (AALA202603232475) (AALA202603239507) AT MAIN CABIN OFAR. PER BOEING AMM DMC-B787-A-20-11-00-00A-030A-A TORQUE 24-220. OPS CHECK GOODSDR AALA202603232475Escape Hatch · stuckAIRCRAFT IN BASE MAINTENANCE: 2EA MAIN CABIN OFAR AFT ESCAPE DOOR LATCHS HARD TO OPEN. REMOVED AND REPLACED ESCAPE DOOR LATCHS (AALA202603232475) (AALA202603239507) AT MAIN CABIN OFAR. PER BOEING AMM DMC-B787-A-20-11-00-00A-030A-A TORQUE 24-220. OPS CHECK GOODSDR IPXA2026032179037Bracket · crackedRIGHT MLG WHEEL WELL, FWD SEAL RETAINER, SECOND FROM MOST OUTBD BRACKET IS CRACKED. DOT 93-013 INSTALLED ANGLE AT RH MLG WHEEL WELL, FWD SEAL RETAINER, SECOND FROM MOST OUTBD IAW SRM 51-40-02-0G-0.SDR IPXA2026032069539Angle · crackedFOUND CRACKED ANGLE, BULK CARGO BAY CEILING AREA, BS 1577, LBL 74, INBD SIDE. REMOVED THE DAMAGE ANGLE IAW SRM 51-40-02-0G, REV.94. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, AND DWG 146T5650, SH 5, REV C.SDR IPXA2026032069514Angle · crackedFOUND A CRACKED ANGLE, BULK CARGO BAY CEILING AREA, BS 1577, LBL 74, OTBD SIDE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 146T5650, SH 5, REV C.SDR MASA202603200009Battery · no testFWD FA FLASHLIGHT IS INOPERATIVE. R & R BATTERY IN FLASHLIGHTSDR REXA2026032000242Lamp · inoperativeOVERHEAD EMERGENCY LIGHT INOP AT ROW 17. R & R BULB IAW AMM 33-51-09, OPC GOOD.SDR IPXA2026032070105Check Valve · faultedFUEL IMBALANCE IN FLIGHT OF 1900LBS WITH FUEL CONFIG MESSAGE. 7.2 LBS LEFT TANK, 9.1 LBS RIGHT TANK. ALL ENGINE INSTRUMENTS NORMAL INCLUDING FUEL FLOW. FMC CALCULATED AND TOTALIZER FUEL WITHIN 100 LBS NO FUEL IMBALANCE NOTED DURING ENGINE RUNS. REMOVED AND RESDR IPXA2026032076960Beam · crackedMAJOR REPAIR, FWD CARGO DOOR HAS CRACK IN BEAM 1 FWD OF FR22A ITEM HAS BEEN TEMPORARY REPAIRED IAW EO-96845. NEW FAULT T3F18E008H4ZS HAS BEEN GENERATED FOR TRACKING PURPOSES OF NEW DEFERRAL. THIS ACTION CLOSES ORIGINATING DEFERRAL.