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 DALA2026053103288None · noneDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D AT FR68RH AND S-22 PER ER/A 634286-14AD. C/A: SECTION I IS LIMITED TO 71500FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE ASSOCIATED ER/A 14-634286 ADDESDR DALA2026053103287None · noneDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR AT FR68R H & S-22 PER ER/A 634286-14AD. ER/A TO BE REVISED PRIOR 32328FC FROM SECTION I (40K FC FROM SB 53-1290 EMBODIMENT) ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-634286 ADDED FOR AC 3251. (LP:SDR DALA2026053103286None · noneER/A 634286-14AD ISSUED FOR REPAIR AT FR68RH AT S-22. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II EVERY 16200FC AFTER SECTION I. ASSOCIATED ER/A 14-634286 ADDED FOR AC 3251. (LP: 1605169, AIRCRAFT WAS GROUNDED)SDR IPXA2026052990543Actuator · corrodedFOUND RT WING NR 17 OUTBD, INBD AND NR 24 INBD SIDE ROTARY ACTUATOR CORROSION. I.A.W AMM 27-81-07-404-008 REV.50 STEP 3A TO 3F(2)(N) INSTALLED NO.17 OUTBD'S INBD AND NO.24 INBD SIDE ROTARY ACTUATOR.SDR IPXA2026052990524Actuator · crackedFOUND LT WING NR 5 INBD , NR 3 INBD , NR 10 OUTBD'S INBD V.C FLAP ROTARY ACTUATOR CORROSION AND NO.8 OUTBD'S OUTBD V.C FLAP ROTARY ACTUATOR COVER CRACK. I.A.W AMM 27-81-07-404-008 REV.50 STEP 3.A TO 3.F.(2)(N) INSTALLED THE LH WING NO.3 INBD SIDE, NO.5 INBD SDR DALA2026052903261Skin · crackedCRACK AND WEAR EXTERNAL SKIN ON AFT CARGO DOOR CUTOUT AFT EDGE BTW LONG 24RH TO LONG 26RH AT LOWER FUSELAGE SECTION. REPAIRED PER B717-200 SRM 53-20-15 (1605105) (AIRCRAFT GROUNDED)SDR CALA2026052916644Skin · damagedFOUND POSSIBLE LIGHTNING STRIKE BTWN BS 500A - 500B, STR 3L. REMOVED DAMAGE, HFEC AREA, NO DEFECTS NOTED. FABRICATED REPAIR PARTS, LOCATED, DRILLED AND INSTALLED, RESTORED COATINGS IAW SRM 53-00-01-2R-1, REPAIR 1, AND UAL ECRA 5310-08866, REV A. THIS IS A CSDR CALA2026052816589Transition Panel · corrodedFWD PIT TRANSITION PANEL UPPER SURFACE HAS CORROSION FROM APPROX STA 500+15 - 500D, LH SIDE. REMOVED CORROSION IAW B737-900ER SRM 51-10-02. ORIGINAL THICKNESS 0.040, MATERIAL LOSS 0.005, REMAINING THICKNESS 0.035 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMSDR AALA202605283318Slide · wornAIRCRAFT IN BASE MAINTENANCE: L2 DOOR SLIDE CURTAIN IS WORN. REPLACED L2 DOOR SLIDE PER WORK CARD 08L22125001.SDR DALA2026052803220Cusp Web · crackedCRACK ON LH SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60. CRACK ON LT SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60 WAS REPAIRED PER B717-200 SRM 53- 00-55 (1606007) (AIRCRAFT GROUNDED)SDR DALA2026052803219Longeron · crackedCRACKED LONGERON END 2LH , STA Y=1133 AT AFT ACCESSORIES COMPARMENT. REPAIRED PER B717-200 SRM 53-00- 05 (1605407) (AIRCRAFT GROUNDED)SDR WX0A2026052732825Toilet · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 2000-0003: AFT LAVATORY TOILET CORRODED. AFT LAVATORY TOILET REPLACED IAW AMM 38-31-41-400-001. SEE AWS FOR DETAIL.SDR DALA2026052703214Window Frame · damagedSHIP 3241 DISC: DTE ERA 633400-14AD REV. ORIGINAL. REPAIR AT FR4 LATERAL WINDOW FRAME REQUIRES DTE FOLLOW UP PRIOR TO 64,502 TFC. C/A: REVISE AND UPDATE ERA 633400-14AD WITH DTE RESULTS PRIOR TO 64,502 TFC. REFERENCE AIRBUS DOSSIER 81769612. ASSOCIATED AA 5311SDR 2026FA0000443Structure · degradedPROBLEM: A ZIP DRONE RETURNED TO DOCK AT PEA RIDGE WITH A BROKEN PROPELLER AND BOOM ARM AFTER A LOUD POPPING NOISE WAS HEARD ON APPROACH. IMPACT: ONE ZIP AT PEA RIDGE SUFFERED A BROKEN PROPELLER AND BOOM ARM (AFT LEFT). THERE HAVE BEEN NO INJURIES, AND ALL PESDR DALA2026052703193Unknown · odorAT APPROX 15000 AFT FA REPORTED A SMELL IN AFT GALLEY. WE DECIDED TO CONTINUE AND LAND IN CVG. R/R AFT DOOR HEATER REF B737 AMM CH 21-45. LEAK AND OPS CHECK GOOD. (LOG 888822 - AIRCRAFT WAS GROUNDED).SDR FDEA202605210634Door Frame · crackedRH PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPLACED THE CRACKED SEGMENT ON RH PAX DOOR FRAME AT FR14C PER A300-600F SRM51- 40-21 AND DWG: F52181299(ISSUE: G). RSC TRACKING EA: 6-5210-T0387549 RAISED AND ACCOMPLISHED. TITLE: DOORS - PASSENGER/CREWSDR AALA202605277444Light · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ABOVE OVERHEAD BIN AT SEAT 24F IS OUT. (OPEN).SDR ASAA2026052164861Anti-Ice System · faultedDMI 548009 FAP MESSAGE SLIDES ICE PROTECTION DOOR 3L AND 3R DOOR INOP.DMI 548011 FAP MESSAGE SLIDES ICE PROTECTION DOOR 4L AND 4R DOOR INOP ( ESC SLIDE LOCK MECH ICE PROT DOOR 1,2,4 ). GROUNDED - YES. REMOVED & REPLACED IPCU (16DS) PER AMM 25-27-35, OPS CHECSDR AALA202605267933Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 101.90, 9.5 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202605268311Elec Connector · unsecureAIRCRAFT IN BASE MAINTENANCE: RIGHT AFT EMERGENCY EXIT DOOR AFT OF WING WHITE DOOR ARMED INDICATION INOPERATIVE. MAINTENANCE RESECURED ELECTRICAL CONNECTOR TO SLIDE ARMED INDICATOR LIGHTAND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-73-21,SDR IPXA2026052693472Door · noiseEXTREMELY LOUD SQUEAL EMANATING FROM MAIN DOOR ON AIRCRAFT. SOUND IS COMING FROM AREA OF LOWER DOOR HINGE OR FLOOR. INSTALLED NEW ENTRY DOOR SEAL PER AMM 52-10-18. AWAITING SEALANT CURE TIME AND PRESSURIZATION LEAK CHECK. PERFORMED PRESSURIZATION OF ACFT PER SDR DXTA2026052608187Latch · contaminatedAFTER COMPLETING THE FINAL WALK AROUND AND WALKING UP THE MAIN ENTRY DOOR STAIRS, LOCKING HANDLE POPPED OUT OF THE OPEN POSITION CAUSING THE DOOR TO MOVE DOWNWARD FORCING THE BOTTOM OF THE DOOR INTO FUSELAGE SKIN CAUSING 3 SCUFF MARKS. RETURNED HANDLE TO OPENSDR DXTA2026052608191Indication Sys · malfunctionedLEFT WING FUEL QUANTITY WILL RAPIDLY INCREASE IN INDICATED AMOUNT. THIS LARGE INCREASE CREATES A FUEL IMBALANCE AMBER CAS MESSAGE, AND THE AUTO TRANSFER SYSTEM WILL ATTEMPT TO TRANSFER FUEL FROM THE PERCEIVED HEAVY LEFT WING TO THE RIGHT WING, CREATING AN ACTUSDR DXTA2026052608183Brake · faultedAFTER TOUCHDOWN WHEN APPLYING BRAKES GRADUALLY BETWEEN 70 AND 80KTS THE LEFT MAIN BRAKE STARTS GRABBING AND SHIMMERING NOTICEABLY. WHEN BELOW ANTI SKID SPEED NO GRABBING NOR SHIMMERING IS OCCURRING. INSPECTED LT INBD AND OTBD BRAKE, WHEEL ASSEMBLIES AND SURSDR DALA2026052603162Skin · puncturedSKIN DAMAGE (PUNCTURE) JUST ABOVE STR 22R AT FRAME 500G. COMPLIED WITH ER/A 634486-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS, ENSURE ALL ER/A 634486-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FSDR DALA2026052603161Skin · damagedSKIN DAMAGE AT STR 21R (2 SPOTS) JUST FWD OF FRAME 500F. COMPLIED WITH ER/A 634484-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS, ENSURE ALL ER/A 634484-14 REV ORIGINAL PRI REV "0", "1","2" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FSDR DALA2026052603157Wire · arcedAPU STARTER GENERATOR T4 WIRE IS ARCHING AND MELTED THROUGH THE LEAD COVER. REMOVED AND REPLACED APU STARTER GENERATOR IAW B737 AMM 49-41-21. OPS TEST GOOD. (LOG 1606182 - AIRCRAFT WAS GROUNDED).SDR JJBA20260526028Terminal · arcedVISIBLE SMOKE FROM THE FO SIDE WINDOW AREA UNDER THE PTT BUTTON PANEL. REMOVED, INSPECTED AND REINSTALLED RH SIDE CONSOLE. NO DEFECTS NOTED. REMOVED GLARESHIELD AND FOUND FOS WS HEATING SENSORS TERMINAL G LOOSE AND BURNT. PERFORMED FIM. FOUND FO WINDSHIELD HEASDR SWAA2026052605321Girt Bar · looseFWD SERVICE DOOR GIRT BAR RETENTION CLIP LOOSE. ACCOMPLISHED EAM 23-125-01839SDR SWAA2026052605323Sign · detachedCENTER AISLE EMERGENCY EXIT SIGN FELL OFF. SECURED EMERGENCY EXIT SIGN AT CENTER AISLE IAW AMM 33-51-01.SDR DALA2026052603155Drive Unit · failedDIV- TO SAV DUE TO WEATHER RADAR FAULT. REPLACED WX RADAR DRIVE UNIT/ANTENNA. OPS CHECK NORMAL. (8894956) (AIRCRAFT GROUNDED)SDR DALA2026052603151Pawl · faultedR1 DOOR WOULD NOT ARM FOR DEPARTURE. ARMING LEVER WOULD NOT MOVE . CHECKED DOOR TRACK & RECYCLED DOOR. STILL WOULD NOT ARM. REPLACED DOOR HANDLE PAWL REF AMM 52-11. VERIFIED DOOR ARMS /DISARMS NORMALLY. OK FOR SERVICE. (8661364) (AIRCRAFT GROUNDED).SDR YENA2026052600481A/C Pack · leakingFLT#773, BOS-AUA. DURING DESCENT FA REPORTED DIRTY SOCK SMELL DESCENDING THRU 6000FT ROW 12-21 LASTED ( PACKS ); CORRECTED 2 AIR LEAKS AT PACK #1 CONNECTIONS TO ACM. OPS CHK OF #1 PACK OPS CHK OK. REF MM 21-52-41. #2 PACK AT NORMAL OPERATING TEMPS OPS CHK SDR REXA2026052600609Seat Track · corrodedPAX FLOOR SEAT TRACK AT RBL9 CORRODED AT FS349. REPAIRED IAW MHI RJ REO 670-53-00-589 REV -D 2025-08-20.SDR REXA2026052600608Seat Track · corrodedPAX FLOOR SEAT TRACK AT LBL9 CORRODED AT FS379. REPAIRED IAW MHI RJ REO 670-53-00-589 REV -D 2025-08-20.SDR AALA202605259091Pressure Switch · faultedAIRCRAFT WAS NOT GROUNDED: WHILE ATTEMPTING TO BALANCE FUEL THE CROSSFEED VALVE OPEN LEFT AFT AND FORWARD FUEL PUMPS TURNED OFF. ALSO, THE AFT LOW PRESSURE LIGHT DID NOT ILLUMINATE WHEN FUEL PUMP TURNED OFF. REMOVE AND REPLACED LEFT HAND AFT FUEL BOOST PUMP PRSDR AALA202605255975Sign · detachedAIRCRAFT WAS NOT GROUNDED: CEILING EXIT SIGN ROW 16 IS DETACHED. RESECURED OVERHEAD EXIT SIGN AT ROW 16.SDR AALA202605258498Megaphone · no testAIRCRAFT WAS NOT GROUNDED: MEGAPHONE BATTERIES REQUIRES REPLACEMENT. REPLACED BATTERIES. PER AMM 25-64-00.SDR AALA202605252097Hinge · lack of lubeAIRCRAFT WAS NOT GROUNDED: DOOR 1L DIFFICULT TO OPEN FROM OUTSIDE THE AIRCRAFT ON JETBRIDGE. LUBRICATED L1 DOOR HINGES. PER GPM 02.01.2B2. OPS CHECKED DOOR GOOD.SDR AALA202605251856Battery Pack · inoperativeAIRCRAFT WAS NOT GROUNDED: EXIT RIGHT HAND AFT OVERWING EMERGENCY LIGHT AND EXIT RIGHT HAND SLIDE EMERGENCY LIGHT INOPERATIVE. REMOVE AND REPLACED BATTERY PACK AT ROW 23 RIGHT HAND SIDEWALL, OPS CHECK GOOD. PER AMM 33-51-06.SDR AALA202605257304Battery Pack · inoperativeAIRCRAFT WAS NOT GROUNDED: AISLE EMERGENCY LIGHTS AT 19FED AND 23FED INOPERATIVE. REMOVE AND REPLACED BATTERY PACK AT ROW 23 RIGHT HAND SIDEWALL, OPS CHECK GOOD. PER AMM33-51-06.SDR AALA202605251812Light · missingAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT ADVISES SEAT 10C EMERGENCY LIGHT MISSING. RESECURED EMERGENCY LIGHT FIXTURE. OPS CHECK GOOD.SDR AALA202605250573Battery Pack · inoperativeAIRCRAFT WAS GROUNDED: CABIN SEAT MOUNTED EMERGENCY LIGHT ROWS 17 THROUGH 25 INOPERATIVE. REMOVE AND REPLACED EMERGENCY POWER SUPPLY M01670. PER AMM 33-51-06. OPS CHECK OF ROW 17 THROUGH 25 SEAT EMERGENCY LIGHTS GOOD.SDR CALA2026052516522Shutoff Valve · faultedDUCT PRESSURE SPLIT OF 30 PSI. HIGHER ON LEFT SIDE. STARTED PRSOV REMOVAL REF AMM 36-11-04-000-801 UP TO AND INCLUDING STEP E.(4) REMOVED AND REPLACED NR 1 ENG PRSOV AS REQUIRED REF AMM 36-11-04, OPS. CHECK GOOD. NO FAULTS FOUND AT THIS TIME. REEF AMM 36-00-0SDR CALA2026052516521Gps · faultedGPS-R INVALID BOTH GPS SYS CHECK NORMAL. REF AMM 34-58-00.SDR CALA2026052516490Panel · corrodedNLG WHEEL WELL PANEL 113BW HAS SURFACE CORROSION ADJACENT TO ATTACHMENT FASTENER. EVALUATED PANEL TO BE BEYOND REPAIRABLE LIMITS IAW SRM 53-10-14. RECEIVED REPLACEMENT PANEL IAW AIPC 32-22-11-02 ITEM 35 FOR EFFECTIVITY.SDR CALA2026052516488Panel · corrodedNLG WHEEL WELL PANEL 114AC HAS SURFACE CORROSION ADJACENT TO ATTACHMENT FASTENER. EVALUATED PANEL TO BE BEYOND REPAIRABLE LIMITS IAW SRM 53-10-14. RECEIVED REPLACEMENT PANEL IAW AIPC 32-22-11-02 ITEM 35 EFFECTIVITY. EVALUATED PANEL TO BE BEYOND REPAIRABLE LSDR DALA2026052403132Floor Support · corrodedLEVEL 2 CORROSION FLOOR SUPPORT -Y1292-1162.5 LOC. FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1292, -Y1162.5 AND LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 AND DWG D53472816, ISSUE F, AND DWG D53472780 ISDR DALA2026052403131Rib · corrodedLEVEL 2 CORROSION, LT WING, TRAILING EDGE REAR SPAR RIBLET WITH CORROSION AT RIB 19. PERFORMED REPLACEMENT REPAIR AT RIBLET M LOCATED AT LT WING TRAILING EDGE REAR SPAR AREA AT RIB 19 IAW SRM 57-51-12-300 -007 PARG 2.B REV 157. THIS TASK IS CATEGORY A WITH NSDR DALA2026052403130Seat Track · corrodedLEVEL 2 CORROSION SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA. : REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. BTW FR12 TO FR24 FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112812 ISSUE E00. DWG D53110920 ISSUE E00.RELEASE, DWG D53110