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 CALA2026042715732Oven · failedFORWARD GALLEY OVEN 109 ODOR POSSIBLY ELECTRICAL. PRECAUTIONARY C-B PULLED OPEN GALLEY OVEN 109. GALLEY OVEN REPLACED IAW AMM 25-31-00SDR CALA2026042715731Battery · dischargedEMERGENCY FLASHLIGHT AT F/A SEAT AT DOOR 3R REQUIRES REPLACEMENT. PUSH TO TEST SHOWS RED LIGHT. REMOVED AND REPLACED EMERGENCY FLASHLIGHT AT F/A SEAT AT DOOR 3R REF AMM 25-64-01. PUSH TO TEST OK.SDR CALA2026042715730Light · brokenPASSENGER SEAT 9D AFTER CIRCULAR PROXIMITY LIGHT INOPERATIVE. R/R PASSENGER SEAT 9D AFTER CIRCULAR PROXIMITY LIGHT REF. AMM 33-51-06, OK.SDR CALA2026042715729Shroud · damaged21 ABC EXIT ROW PATH LIGHT BRACKET NOT ATTACHED PROPERLY. REMOVED AND REPLACED EPL SHROUD REF CMM 25-22-55..OPS CHECK NORMAL REF AMM 33-51-01.SDR CALA2026042715728Drain Line · displacedVERY LOUD SQUEEL CLIMBING THROUGH 9000 RETURNED TO IAD DURING INITIAL EVALUATION FOUND CAPTS P5 CONDENSATION DRAIN TUBE DISPLACED AND CAUSING RH #2 SLIDING WINDOW SEAL TO NOT MAKE CONTACT FOR A PROPER SEAL. RESECURED CAPTS DRAIN TUBE, AND ACP CABIN PRESSURIZASDR YENA2026042700431Compressor · contaminatedFLT# 1245, ISP-PBI. "IMMEDIATE OIL FUME SMELL W/ ASSOC. SYMPTOMS ON DECENT ONCE HPV'S KICKED IN. PACK ONE OFF HELPED BUT STILL NOTICEAABLE; ACCOMPLISHED INFO NOTICE 2017-TO15M STEPS 1 AND 2 IDENTIFIED ODOR TO BE A TYPE 1 APU LOAD COMPRESSOR,CLEANED OIL AND WISDR AALA202604271448Elec Connector · looseAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS OUT AT AISLE ROW 13,14,15. T/S AND FOUND EMERGENCY CONNECTOR NOT SECURED. MAINTENANCE SECURED CONNECTOR AT SEAT 17 AISLE. OPS CHECKED OK PER AMM 33-51-00.SDR AALA202604272906Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R1 MAIN CABIN DOOR DAMPER ASSIST PRESS LOW. MAINTENANCE CHARGED R1 MAIN CABIN DOOR DAMPER IAW AMM 52-10-00-614-001-A.SDR AALA202604279506Battery · inoperativeAIRCRAFT WAS NOT GROUNDED: FLASHLIGHT INOP AT FLIGHT ATTENDANT SEAT DOOR R4. MAINTENCE REPLACED BATTERY PACK OF FLASHLIGHT AT FLIGHT ATTENDANT SEAT DOOR R4 IAW AMM 25-64-00.SDR BAGA2026042700006Battery Pack · failedEMERGENCY LIGHTS FLICKERING ON AND OFF IN ARMED PPOSITION. EMERGENCY LIGHTS ALSO TURNED ON AFRTER AIRCRAFT WAS POWERED DOWN WITH SWITCH IN OFF POSITION. ERMER LT BATT FAULT EICAS INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT NR 4.SDR BAGA2026042700005Oil System · low pressureDURING FLIGHT ENGINE OIL 2 PRESSURE DECREASED WENT TO APPROX 20 RED INDICATION, RAN QRH AND SHUT ENGINE DOWN. NO FURTHER INCIDENT.SDR 2026FA0000301Indication Sys · false indicationRDAU DISPLAYS FAULTY FUEL INDICATIONS. AFTER START-UP #1 FUEL QUANTITY DROPS APPROX. 100 LBS. THEN RISES THE SAME AFTER SHUTDOWN.SDR DXTA2026042707766Battery Pack · defectiveWHILE TESTING THE EMERGENCY LIGHTS DURING PRE-FLIGHT, SEVERAL INTERIOR OVERHEAD LIGHTS AND 3 EXTERIOR LIGHTS FAILED TO ILLUMINATE WITH THE EMERGENCY SWITCH IN ARM. REPEAT WRITE-UP. GAINED ACCESS TO ALL 4 EMEGENCY BATTERIES REMOVED DEFECTIVED ONES AND INSTALLSDR DXTA2026042707769Pump · leakingAT FL430 WE RECEIVED HYD PRESS LOW R CAS MESSAGE. ON HYDRAULIC SYSTEMS PAGE WE COULD SEE THE VOLUME OF FLUID SLOWLY DECREASING. EVENTUALLY CAS MESSAGE HYD VOLUME LOW ILLUMINATED. FOLLOWED QRH & UNLOADED BOTH HYDRAULIC PUMPS. PULLED BLOWDOWN BOTTLE FOR GEAR & LSDR DXTA2026042707770Control Lever · faultyON APPROACH INTO DAL WE SELECTED GEAR DOWN AND THE NOSE WHEEL DID NOT COME DOWN. WE THEN RECEIVED A WARNING CAS MESSAGE OF LG LEVER DISAG. RAN QRH AND AFTER WE CYCLED THE LANDING GEAR, THE NOSE WHEEL CAME DOWN. CORRECTIVE ACTION: REMOVED LANDING GEAR CONTROL SDR DXTA2026042707771Door · lack of lubeMAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE DOOR HANDLE FROM INSIDE THE CABIN. UPON ARRIVAL AT AIRCRAFT, CONFIRMED CABIN DOOR IS SLIGHTLY HARDER TO OPEN THAN USUAL. WE NOTED SAND AND DEBRIS ON THE LOCKING PINS. WE REMOVED THE DOOR TRIM AND INSPSDR DXTA2026042707774Steering Unit · failedNOSE STEERING FAIL CAS IN CLIMB WOULD NOT RESET. REPLACED STEERING CONTROL UNIT WITH K-BALLED UNIT FROM IAW AMM 32-51-01-400-801.SDR DXTA2026042707778Latch · inoperativeMAIN PAX DOOR DOWN LOCK LATCH MECHANISM IS IN-OP. INSPECTED MAIN PAX DOOR AND CHECKED LENGTH OF HOIST ROD. ADJUSTED THE MAIN DOOR HOISTING ROD TO 8.5 INCHES PER AMM RECOMMENDATIONS. OPERATIONAL CHECKED GOOD. WORK DONE IAW PHENOM 300 AMM 52-10-00.SDR SCNA20260427170Light · inoperativeRIGHT EMERGENCY LIGHTS ROW 25 AND ROW 27 INOPERATIVE. OPENSDR SCNA20260427169Elec Connector · disconnectedEMERGENCY LIGHT R2 OUTSIDE INOPERATIVE. PERFORMED T/S AT R2 OUTSIDE IAW B737 WDM 33-51-13 FWD EMERGENCY LIGHT L733 DISCONNECTED AT THE REAR AND RE CONNECTED IT PERFORMED OPS CHECK IAW B737 AMM 33-51-00 OPS CHECK SATISFACTORY REV 89 15/FEB/2026SDR SCNA20260427168Lamp · inoperativeR/H AFT SLIDE EMERGENCY LIGHT INOP. R/H AFT SIDE EMERGENCY OVERWING LIGHT LAMP REPLACED IAW B737 AMM 33-51-04 OPS CHECK SATISFACTORY REV 89.SDR SCNA20260427167Carpet · unsecureFA REPORTS CARPET AT ROW 12 IS BUNCHING AND CAUSING TRIPPING HAZARD. SECURED CARPET AT ROW 12 . OK FOR SERVICE.SDR ABXA202604264173Start Valve · faultedDURING TAXI OUT WHILE STARTING NR 1 ENGINE NO ROTATION ON NR 1, START VALVE STAYED OPEN , A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C AND DEFERRED NR 1 START VALVE IAW MEL ABX-80-00-2-1 .A/C REMAINS ETOPS 180 . AND RETURNED ACFT TO SERVICE .SDR DALA2026042502629Engine · odorON TAXI IN TO BOS FA'S IN AFT OF THE AIRCRAFT NOTICED A MILDEW/DIRTY SOCK ODOR THAT BEGAN ON FINAL JUST BEFORE GEAR EXTENTION. NO PAX NOTICED IT AND THE SMELL DISIPATED AFTER BLOCK IN. APU BLEED WAS NOT USED. REPLACED NR 2 ENGINE. (LP 8537300 - AIRCRAFT WAS SDR DALA2026042502628Structure · damagedBURRED MATERIAL (OVALIZATION) ON LOWER LATERAL FITTING RH SIDE RACK 80 VU ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER F LIGHT REFER TO AA CARD 2515-01014-02B AD RELEATED. C/A: COMPLIED ER/A 633348-14AD REV ORIGINAL WAS VERIFIED AGAINST RESDR DALA2026042502627Floor Support · brokenBROKEN FLOOR SUPPORT +Y254 FR 33 TO FR 34 IN PASSENGER CABIN. REPLACED FLOOR SUPPORT Y254, LOC. BTW FR24 TO FR35 IN PAX CABIN IAW SRM 51-42-11, SRM 51-72 -11, & DWG: D53231346, ISSUE: D00, RELEASE DATE: 06/AUG/92. DWG: D52110920, ISSUE: E00, RELEASE DATE: 28SDR DALA2026042502626Structure · damagedBURRED MATERIAL (OVALIZATION) ON LOWER LATERAL FITTING RT SIDE RACK 80 VU ADDITIONAL ENGINEERING DOC IS REQUIRED PRIOR TO FURTHER FLT, REFER TO AA CARD 2515-01014-02B AD RELEATED. COMPLIED ER/A 633348-14AD, REV ORIGINAL WAS VERIFIED AGAINST REPAIR INST ER/A 6SDR DALA2026042502621Floor Support · corrodedTASK 5320-6010, CPCP 2021-2001. PAX CABIN AFT SECTION, FLOOR STRUCTURE AT FR68 Y512.5 LONGITUDINAL BEAM WITH CORROSION. REPLACED FLOOR STRUCTURE LONGITUDINAL BEAM P/N: 5347219420400 AT FR67 TO FR70, Y512.5 IAW A319 SRM 53-41-14-03A FIG 303, ITEM 180. REV 157.SDR AALA202604245642Pan · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND WING, MAIN INBOARD TRAILING EDGE FLAP, OUTBOARD EDGE PAN ASSEMBLY AT WS 442. REPAIRED PAN PER SRM 57-53-01-2R-REPAIR 1.SDR EE4Y2026042424376Skin · damagedDURING THE STRUCTURAL INSPECTION, EXISTING SKIN BLEND-OUTS AND LIGHTNING STRIKES DAMAGE WERE FOUND BETWEEN FR23-24, NEAR STRINGER 27R. THE BLEND-OUTS WERE REWORKED IN ACCORDANCE WITH SRM PART II 51-10-03 REQUIREMENTS. ADDITIONALLY, LIGHTNING STRIKES DAMAGE WERSDR EE4Y2026042424374Skin · canningDURING A STRUCTURAL INSPECT, AN EXISTING REPAIR DOUBLER BETWEEN FR08 AND FR09, AND BETWEEN STRINGER 20L AND 21L WAS IDENTIFIED. ACCORDING TO PREVIOUS OPERATOR RECORDS, THIS REPAIR WAS INSTALLED IN ACCORDANCE WITH ETD2017-190-105910 GUIDELINES. THE RECORDS DID SDR EE4Y2026042424373Skin · not reportedDURING THE REMOVAL OF THE LIVE TV KA BAND CONNECTIVITY SYSTEMS STRUCTURAL PROVISIONS IN ACCORDANCE WITH SB 190-53-0125 (UNDER ETD2026-190-001029 EFFECTIVITY), THE FOLLOWING DISCREPANCIES WERE IDENTIFIED. THE SB 190-53-0125 DOES NOT INCLUDE INSTRUCTIONS TO INSTSDR 2026FA0000296Panel · damagedLH WING OUTBOARD FLAP TRAILING EDGE PANEL (P/N 532BB) WAS DAMAGED DUE TO A MISMATCH BETWEEN THE FLAP POSITION AND THE FLAP LEVER POSITION. THE INCIDENT OCCURRED DURING A LANDING GEAR SWING AND ADJUSTMENT OF THE NOSE LANDING GEAR (NLG) DOORS. DURING THIS ACTIVSDR TSAA2026042400002Symbol Generator · failedCAPTAINS SIDE EFIS DISPLAYS WENT BLANK. NR 1 SG FAILED.SDR IPXA2026042460169Landing Gear · failedATB, WHEN RAISING GEAR ON TAKE OFF WITH GEAR DIDN`T RAISE. RECIEVED GEAR DISAGREE AND GEAR DOOR EICAS MESSAGES . RESULTED IN AIR TURN BACKSDR 2026FA0000295Skin Panel · corrodedFOUND SEVERAL SPOT OF CORROSION ON FWD FUSELAGE RH LOWER SECTION JUST FWD PANEL 153AC. BLENDED AND REMOVED CORROSION FROM FWD FUSELAGE RH LOWER SECTION JUST FWD PANEL 153AC. BLENDED AREA ON RH SIDE OF FUSELAGE WAS BEYOND LIMITS AND SUBMITTED TO AQRD. COMPLIED SDR DALA2026042402619Bolt · wornRIGHT WING NR 4 SLAT HOLD DOWN BOLT FOUND WORN. REPLACED RT WING NR 4 SLAT HOLD DOWN BOLT PER AMM 27-84-00. (1559954) AIRCRAFT WAS GROUNDED.SDR WX0A2026042432793Unknown · odor(AIRCRAFT NOT GROUNDED) DIRTY SOCK ODOR REPORTED BY ALL FA'S AND SEVERAL PAX. SMELL DETECTED IN FWD, MID, AND AFT CABIN. DURATION 5 MINUTES ALTITUDE 3500 MSL DURING APPROCH. APU OFF. / T/S PER TSM 05-50-00-810-831-A AND PERFORMED TC A32X-21-00-001 SMELL REPRODSDR 2026FA0000294Trim Motor · defectiveELEVATOR PITCH TRIM MOTOR HOUSE ATTACH SCREWS ARE WORKING LOOSE AND CAUSING EXCESSIVE MOVEMENT OF THE ELEVATOR SYSTEM. THIS HAS BEEN AN ONGOING ISSUE WITH ALL 24 OF OUR AIRCRAFT. CIRRUS HAS BEEN NOTIFIED OF THE DEFECT BUT HAS TAKEN NO ACTION AS OF THIS DATE. TSDR EE4Y2026042424372Pinion · corrodedDURING THE ACCOMPLISHMENT OF INSPECTION TASK CARD 57-40-006-0547, WE FOUND SLAT PINION #9 (LH AND RH, SLAT PINION #9 P/N: 190-03175-403) PRESENTING PITTING CORROSION. THE CONDITION IS LIMITED TO THE PINION TEETH, WITH NO MATERIAL LOSS OBSERVED. WE SEARCHED FORSDR EE4Y2026042424371Inlet · dentedAZORRA AVIATION HOLDINGS, LLC REPORTS THAT DENTS WERE FOUND ON THE ENGINE #2 AIR INLET MODULE INNER BARREL LOWER SKIN, LOCATED BETWEEN THE 5.0 AND 7.0 O’CLOCK POSITIONS. THE DENTS WERE EVALUATED IN ACCORDANCE WITH SRM 71-61-01 AD53 AND DETERMINED TO BE OUT OF SDR EE4Y2026042424370Inlet · dentedAZORRA AVIATION HOLDINGS, LLC REPORTS THAT DENTS WERE FOUND ON THE ENGINE #1 AIR INLET MODULE INNER BARREL LOWER SKIN, LOCATED BETWEEN THE 5.0 AND 7.0 O’CLOCK POSITIONS. THE DENTS WERE EVALUATED IN ACCORDANCE WITH SRM 71-61-01 AD53 AND DETERMINED TO BE OUT OF SDR 2026FA0000292Vertical Beam · corrodedDURING EMPENNAGE COVE INSP, FOUND VERTICAL AFT SPAR HAS CORROSION ON RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AND REMOVED ALL VISIBLE SIGNS OF CORROSION ON AFT SPAR RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AREA WAS BEYOND ALLOWABLE LIMITS AND WAS SUBMITTED TO SDR ABXA20260424172Eec · faultedDURING TAXI, ON ENGINE START BOTH EEC TO ALT W/ L & R ENG EEC MODE EICAS MESSAGES. CREW RETURNED TO THE GATES (BTB). MTC DEFERRED IAW MEL 73-21-1-3 NO MX ACTIONS REQUIRED. PLACARD INSTALLED. MBCB 05-04-2026. ALSO: ANOTHER ISSUE CAUSING THE (BTB), ON ENGISDR CALA2026042415724Light · damagedEMERGENCY EXIT SEAT LIGHHT BROKEN AT 26C. REMOVED AND REPLACED BROKEN EPL LIGHT AT SEAT. 26C. REF CMM 25-23-59-3784.SDR CALA2026042415722Light · damagedEMERGENCY EXIT SEAT LIGHHT BROKEN AT 27C. REMOVED AND REPLACED BROKEN EPL LIGHT AT SEAT. 27C. REF CMM COLLINS AEROSPACE 25-23-59-3784.SDR CALA2026042415707Wire Harness · damagedSEAT 34C ESCAPE PATH LIGHT HOUSING FELL OUT. INOP STICKERS INSTALLED AND LIGHT HOUSING TAPE SECURED TO SEAT. TOMC APPROVED MEL 3351A INTERIOR EMERGENCY AISLE LIGHTING ASSEMBLY(IES) INOPERATIVE. APPLIED MEL 3351A, SEAT 34C ESCAPE PATH HOUSING SECURED TO SEASDR CALA2026042415702Release Mech · brokenFWD DOOR SLIDE GIRT BAR STOP RELEASE BROKEN. L1 DOOR. PART AOG. REMOVED AND REPLACED GIRT BAR STOP IAW IPC 25-66-00-13.SDR FDEA202604240495Skin · dentedNR 5 SLAT APPEARS TO HAVE A DENT REPAIRED LH WING #5 SLAT DENT DAMAGE AT WS.118 TOP SKIN SURFACE IN REF. TO 757 SRM:57- 43-02-2R AND 757 SRM 51-70-10-2R . THIS IS A MAJOR REPAIR, SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.SDR FDEA202604240494Lamp · no testON SERVICE CHECK FOUND LH EMERGENCY SLIDE LIGHT INOP. AMM 33-51-06-2-1 RELAMPED LH EMERGENCY SLIDE LIGHT AS PER 757 AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. FACT 24APR26 03:02 GSO AMM 33-51-06-2-1 RELAMPED LH EMERGENCY SLIDE LIGHT