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 IPXA2026091880437Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2598 S-5R. ACCOMPLISH THE REPAIR I.A.W EO-98604-REQ0036 REV.1 AND SRM 53-80-03-2R-2 REV.49 AND EGAT WORK SHEET NO.60709 AND EGAT EI NO.F2026A53M-1972 REV.0.SDR IPXA2026091880441Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2598 S-7R. ACCOMPLISHED REPAIR I.A.W EO-98604-REQ0038 REV.1 AND EGAT EI NO.F2026A53M-1974 REV.0 AND EGAT WORK SHEET NO.60707 AND SRM 53-80-03-2R-2 REV.49.SDR HNAA2026092300899Spar · crackedRELEVANT INDICATION NOTED DURING HFEC OF LT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE. REPAIRED LT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE TO 1ST OVERSIZE BUSHING IAW SB 145-54-0008 AND EO1-54-26-0423.SDR HNAA2026092300898Spar · crackedRELEVANT INDICATION NOTED DURING HFEC OF RT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE. REPAIRED RT PYLON SPAR 2 UPPER FLANGE AFT FASTENER HOLE TO 1ST OVERSIZE BUSHING IAW SB 145-54-0008 AND EO1-54-26-0423.SDR FDEA202609041263Jackscrew · leakingON APPROACH, PUT THE SLATS OUT, GOT SLATS 1 & 2 FAULTS. PER ECAM, CYCLED HANDLE. DID NOT EXTEND. FOLLOWED QRH. DECLARED EMERGENCY. UNEVENTFUL NO SLAT LANDING. PRI.0 DUE TO CAUSING DELAY, SFCC 1 SLAT FAIL INDS SHOW JAM. FLAP FAIL, INDS SHOW SUPPLY P. SW. SFCSDR IPXA2026091880427Stringer · crackedSTRINGER 8L CRACKED, FWD SIDE OF BS 2598. ACCOMPLISH THE REPAIR IAW EO-98604-REQ0035, REV 1, SRM 53-80-03-2R-2, REV 49, EGAT WORK SHEET 60710, AND EI F2026A53M-1970, REV 0.SDR AALA202609217771Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609216697Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609210605Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609183802Plate · crackedAIRCRAFT IN BASE MAINTENANCE: AFT LEFT PASSENGER CREW DOOR GIRT BAR FITTING PLATE ASSEMBLY CRACKED - REPLACED PLATE AS REQUIREDSDR AALA202609184740Hinge 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 AALA202609187577Hinge 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 IPXA2026091880448Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 2598 S-3R (LEVEL2). ACCOMPLISH THE REPAIR I.A.W EO-98604-REQ0040 REV.1 AND SRM 53-80-03-2R-2 REV.49 AND EGAT WORK SHEET 60715 AND EGAT EI F2026A53M-1992 REV.0.SDR IPXA2026091880446Stringer · crackedSTRINGER 5L CRACKED, AFT SIDE OF BS 2598 (LEVEL2). ACCOMPLISHED REPAIR IAW EO-98604-REQ0041, REV 1, EI F2026A53M-1993, REV 0, EGAT WORK SHEET 60714, AND SRM 53-80-03-2R-2, REV 49.SDR IPXA2026091884333Elevator · not reportedADD SDR FOR EO-85445-JIC2. ACCOMPLISHED EO-85445-JIC2. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR IPXA2026091784553Stringer · crackedSTRINGER 36R CRACKED, FWD SIDE OF BS 2180 (LEVEL 1. ACCOMPLISHED REPAIR IAW EO-98604-REQ0022, REV 1, EI F2026A53M-2031, REV 0, WORK SHEET 60716, & SRM 53-60-03-2R-3, REV 49.SDR SWAA2026091634109Assist Handle · looseL1 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED ASSIST HANDLE ON L1 DOOR IAW AMM 52-11-31-400-801 SUBTASK 52-11-31-420-004SDR IPXA2026091580268Bracket · corrodedALL ELECTRICAL WIRE BUNDLES, POWER FEED CABLES AND FLUID LINE SUPPORT BRACKETS ATTACHED TO APU COMPARTMENT FWD BULKHEAD STA 1885 HAVE CORROSION AND MISSING PROTECTIVE FINISH. RL035 QCI: VERIFIED STEP 5, C/W TOOL VERIFICATION ID # 22-840 DATE DUE 28-FEB- 2027 ISDR IPXA2026091580804Frame · corrodedFRAME STA 1992 FWD AND AFT SIDES HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH WITH HEAVY DEBRIS ON BACK SIDE PLUGGING DRAIN HOLE.SDR DALA2026091005077Warning Light · false activationON CLIMBOUT OF DTW 9000' FWD ENTRY LIGHT DOOR. CONFIRMED CLOSED & PRESSURIZED NORMALLY. LIGHT STAYED ON FOR DURATION OF THE FLIGHT. R & R DOOR SWITCH BRACKET PER BAC WG 114A6101. ADJUSTED SENSOR PER AMM 52-71. C/W ER/A 610188-14TR REV O SEC III PERM RESTORATSDR 2026FA0000724Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000721Stiffener · crackedR/H WING FWD LWR I/B SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR SWAA2026091451106Girt Bar · twistedFORWARD GALLEY DOOR, RIGHT EMERGENCY ESCAPE SLIDE GIRT BAR TWISTED AND BOUND UP AGAINST SLIDE COVER. UNBOUNDED AND REACCOMMODATED GIRT BAR. EXAMINED GIRT BAR FOR ANY DEFECTS OR DAMAGES THAT MAY CAUSE THE SLIDE TO OPERATE INCORRECTLY AS SPECIFIED IN THE ESCAPESDR IPXA2026091478857Frame · corrodedAFT FUSLAGE FRAME STA 1963 FWD AND AFT SIDES AND ALL ATTACHING STRUCTURE CIRCUMFERENTIALLY HAVE AREAS OF CORROSION AND LARGE AREAS OF MISSING PROTECTIVE FINISH AND TOPCOAT. VERIFIED STEP 20, C/W RII GMM 04-02.SDR CALA2026091419399Fitting · damagedREMOVED AND REPLACE NLG RETRACT ACTUATOR FITTING DAMAGED, P/N: 141A7650-2. REMOVED AND REPLACED NLG RETRACT ACTUATOR FITTING ALL WORK DONE IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, DWG 141A7001 REV A. REMOVED AND REPLACED NLG RETREACT ACTUATOR FITTING ALL WOSDR 2026FA0000690Strut · damagedDURING A 100-HOUR / CONDITIONAL INSPECTION OF ACFT, DAMAGE WAS FOUND IN THE NOSE LANDING GEAR STRUT ASSEMBLY. ITEM #25 (P/N 0942010-21 “WASHER – KEYED”) ROTATED AND CAUSED DAMAGE TO THE KEYWAY IN ITEM #11 (P/N 0942005-8 “ROD ASSEMBLY”) AND ALLOWED ITEM #26 (PSDR SWAA2026091199190Handle · deterioratedDETERIORATED HANDLE NUT, & YELLOW STRAP ON AFT ENTRY DOOR LINING AT AFT GALLEY AREA. REPLACED HANDLE NUT & YELLOW STRAP ON AFT ENTRY DOOR LINING AT AFT GALLEY AREA IAW AMM 25-21-25-420-801, STEP 3.B (5), AND DWG 411A2500, SH-5, REV C.SDR DALA2026091105096Door · soft latchAFTER DOOR CLOSED ALL OVERHEAD LIGHTS EXTINGUISHED. FA REPORTS WIGGLE ON FWD ENTRY INTERIOR DOOR HANDLE NOT CONFIDENT DOOR CLOSED PROPERLY. PERFORMED SOFT UNLATCHING ADJUSTMENT IAW AMM 52-11-00 -820-802. ADJUSTED LOWER LATCH TORQUE TUBE/ CONTROL ROD CRANK ANSDR IPXA2026090881106Skin · corrodedEXTERNAL FUSELAGE SKIN BS 1862 HAS AREAS OF CORROSION AREA JUST FWD OF ACCESS DOOR 313AL. RL050 ACCOMPLISHED VISUAL INSP WITH 10X MAGNIFYING GLASS AT CORROSION REMOVAL AREAS EXTERNAL SKIN BUTT JOINT LWR BILGE BETWEEN STA. 1862 TO STA 1863 FROM S-23L TO S-19R PSDR AALA202609117567Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND IN THE LH ECS BAY UPPER AFT CHORD ON THE I/B SIDE. FABRICATED NEW REPAIR ANGLE AND SPLICE, IAW B737-NG-SRM 57-10-10-2R-5 REPAIR 5.SDR AALA202609114176Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND IN THE RH ECS BAY UPPER AFT CHORD ON THE I/B SIDE. FABRICATED NEW R/H VAPOR BARRIER ANGLE IAW BOEING DOCUMENT NUMBER 111A1000 REV: F.SDR FDEA202609041305Repair · misinstalledEXISTING REPAIR ON FWD CARGO FLOOR BEAM AT FR30,Y140~Y805 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO FLOOR BEAM AT FR30,Y140~Y805 WAS EVALUATED AND FOUND NO APPLICABLE REPAIR IN A300-600 SRM FOR THE EXISTING REPAIR.NO RECORD FOSDR FDEA202609041304Repair · no discrepancyEXISTING REPAIR ON FWD CARGO ROLLER TRACK AT -Y140 BETWEEN FR35 AND FR36 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO ROLLER TRACK AT -Y140 BETWEEN FR35 AND FR36 WAS EVALUATED AND FOUND IN CONFORMITY WITH SRM53-10-15-201 FIG.203. NSDR CALA2026091119376Oven · dirtyOVEN SMOKING OR SPARKING 205, SPILLED FOOD IN OVEN CAUSES SMOKE WHEN ON NEEDS CLEANING OVEN HAS BEEN PLACARD AND DEACTIVATED IAW MEL ITEM # 2500BI. PERFORMED CONDITIONAL INSP OF OVEN IAW AMM 05-05-56, FOUND THE ODOR WAS COMING FROM THE OVEN WHICH HAS BEEN DESDR FXTA20260904001Skin · crackedINSPECTION PANEL ON TOP OF THE VERTICAL STABILIZER ATTACHMENT FLANGE CRACKED ALLOWING THE PANEL TO DEPART AIRCRAFT. THIS INSPECTION PANEL IN UNDER THE RUDDER HORN. TOP PANEL P/N: 7831102-23, ONCE ATTACHMENT FAILS HITS RUDDER AND PIECE FOUND IN ELEVATOR CONTROLSDR I5PA2026090468802Warning Message · illuminatedETOPS SIGNIFICANT EVENT AIR RETURN. LEFT PACK TEMP, FLIGHT DECK TEMP AND CABIN ALT WARNING EICAS MESSAGES. PERFORMED BITE TEST OF PACK TEMP AND CABIN PRESSURE CONTROLLERS, NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE.SDR CALA2026090919317Fitting · crackedFOUND CRACK WEB FITTING NR 2 PYLON AFT LOWER STRUT FAIRING AFT SUPPORT. R & R DISCREPANT TRAILING EDGE ASSY AT NR 2 PYLON AFT STRUT FAIRING IAW SRM 51-40-02-0G-0.SDR CALA2026090719298Computer · faultedSTATUS MESSAGE, TCAS & NO AUTOLAND. R & R THE TCAS COMPUTER DUE TO PREVIOUS HISTORY IAW AMM 34-45-01-400-801. OPS CHKD GOOD, TCAS MSG WENT AWAY AND AUTOLAND MSG DOES NOT APPEAR.SDR CALA2026090719281Light · damagedGENERAL VISUAL INSPECTION OF THE BE PINNACLE TOURIST SEAT PROCEDURE. EMERGENCY LIGHT SEAT 30F DAMAGED. R & R ESCAPE PATH LIGHT, SEAT-MOUNTED LIGHT ASSEMBLY REPLACEMENT.SEAT 30F. IAW AMM 33-51-10-962-104. GOOD FOR SERVICE.SDR CALA2026090719278Light · inoperativeRIGHT AFT SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED RT AFT SLIDE EMERGENCY LIGHT IAW AMM 33-51-04-960-801, OPS CHKD GOOD.SDR CALA2026090719274Skin · dentedON WALK AROUND FOUND DENT FWD OF EXT POWER DOOR.DENT IS IN SECTION 41, BS 276. DENT MEASURES 1.5INCH IN LENGTH, .5INCH WIDTH & .040 INCH DEEP. L/Y IS 33.33 ACP,D HFEC INSP NO CRACKS IAW NTM 51-00-00-23, PART 6. SKIN IS DENTED IN 0.105 IN. WITH .002 MATERIAL SDR CALA2026090719272Tire · overspeedDURING TAKEOFF IN DEN, UNSURE IF TIRE SPEED MAY HAVE EXCEEDED 204 IAW ENGINEERING REPORT ER3240R01126. REVIEW OF EFAR DATA CONFIRMED NLG TIRES ARE OK AT 201.6 KNOTS (MAX = 204.2 KNOTS) AND DO NOT REQUIRE REPLACEMENT. DATA SHOWED MLG TIRES DID OVERSPEED AT SDR CALA2026090719268Skin · crackedLT WING LOWER OTBD INTERSPAR SKIN AT PANEL 543BB IS CRACKED AT HOLE 27 AT THE 12 CLOCK, SEE ECRA 5720-03680 FOR WORK PERFORMED.SDR CALA2026090719266Unknown · odorNOTICED UNUSUAL BURNT PLASTIC/ELEC ODOR AS WE STARTED DESCENT. ALSO NOTICED IN AFT CABIN. PERFORMED ODOR MM 05-50-00.SDR CALA2026090719265Bracket · crackedLEFT MLG WW , BS 1040, LBL 64.9 ANGLE BRACKET WAS CRACKED AT INBD SIDE. REMOVED AND INSTALLED A NEW ANGLE BRACKET IAW SRM 51-40-02-0G-0, APPLIED SURFACE PROTECTION IAW AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.SDR CALA2026090719262Bracket · crackedLEFT MLG WW BS 1040, BY OTBD SIDE OF LBL 64.9, ANGLE BRACKET IS CRACKED. REMOVED AND INSTALLED NEW ANGLE BRACKET, IAW SRM 51-40-02-0G-0 DWG 149N7553, APPLIED SURFACE PROTECTION IAW AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.SDR CALA2026090719260Door Frame · crackedNLG WHEEL WELL. DOOR CUTOUT RT SIDE AT BS 275 HAS ONE GUSSET REINFORCEMENT PLATE IS BENT. REMOVED AND REPLACED FOR NEW GUSSET REINFORCEMENT PLATE IAW SRM 51-40-02-0G-0.SDR CALA2026090719258Gusset · crackedNLG WHEEL WELL. DOOR CUTOUT R.H SIDE AT BS 324 HAS 2EA GUS SET REINFORCEMENT PLATES CRACKED. REMOVED AND REPLACED 02EA GUSSETS REINFORCEMENT WITH NEW GUSSETS IAW SRM 51-40-02-0G.SDR ASAA2026090468556Door · out of adjustL1 DOOR IS HARD TO LATCH. GROUNDED - YES. MIG-2C INIT S/N:40-0080267,40-0080268,40-0080269, 40-0080270 ADJUSTED L1 DOOR INREF TO AMM 52-11-00-820-801 STEPS 2, CONTINUE ON ADJUSTING L1 DOOR IN REF TO AMM 52-11-00-8220-801 NO DEFECTS NOTED. MIG-2C SN 40-008267SDR SWAA2026090858400Battery · inoperativeFWD MEGAPHONE WILL NOT WORK. IAW AMM 25-64-00 R & R THE BATTERY. OK FOR SERVICE.