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 AALA202604011337Fitting · wornAIRCRAFT IN BASE MAINTENANCE: WEAR TO RIGHT WING NUMBER 6 SLAT ACTUATOR FITTING AT WS 458.5. REPLACED FITTING PER AARD 51-00-05-1.SDR IPXA2026040163446Unknown · odorOILY SMELL START UP AND TAKEOFF REPLACED NR 2 ENG. ACCOMPLISHED HIGH POWER RUNS ON LT AND RT ENGINES WITH ALL BLEED SOURCES ISOLATED AND PACKS SELECTED ON. CONFIRMED ODOR IS COMING FROM R/H ENGINE AT HIGH POWER SETTING WITH L/H BLEED OFF. FOUND WITH LT ENGINSDR DALA2026040102132Windshield · arcedCENTER WINDSHIELD ANTIICE FAIL DUE TO ARCING HEATER CRACK IN WINDSHIELD. REPLACED CENTER WINDSHIELD PER B717 AMM 56-11-01 LEAK CK OK A/C OK FOR SERVICE (8424138)SDR WX0A2026040132773Epsu · no test(AIRCRAFT NOT GROUNDED) DURING WEEKLY CHECK FOUND EPSU BATT 12WL FAILED. REMOVED AND REPLACED 12WL EPSU BATTERY IAW AMM 33-51-38-400-001-A OPS CHECK GOOD.SDR CALA2026040115008Latch · brokenEVACUATION SLIDE RECORD INSTALLATION - 1L DOOR SLIDE LATCH BROKEN REMOVED AND REPLACED BROKEN SLIDE LATCH REF 25-66-01/401. OKAY TO CONTINUE PARTS USED: 29-2560-3-0060,QTY :1SDR CALA2026040115007Floor Support · corrodedPASSENGER CABIN AFT WET AREA FOUND CORROSION BETWEEN STA. 947.5 & 967 AND LBL-24. REMOVED AND REPLACED NEW FLOOR SUPPORT AT MAIN CABIN AFT WET AREA BETWEEN STA 947.5 AND STA 967 LBL-24 AS PER SRM 51-40-02-0G-0, DWG 147A5650.SDR CALA2026040115006Floor Support · corrodedPASSENGER CABIN AFT WET AREA FOUND CORROSION ON STRUCTURAL ELEMENT LOCATED BETWEEN STA. 967 AND 947.5 RBL-42 REMOVED AND REPLACED NEW FLOOR SUPPORT INTERCOSTAL BETWEEN STA 947 TO STA 967 RBL-50 REF SRM 51-40-02-0G-0 STEP 8.C FIGURE 12 AND DWG#147A5650 SHEETSSDR CALA2026040115005Floor Support · corroded(CORROSION) PASSENGER CABIN AFT WET AREA FOUND CORROSION AT DOOR R2 FLOOR STRUCTURE ENTRY ANGLE REF AAR N/R 100013086 REMOVED AND REPLACE NEW INNER CHORD R2(ENTRY ANGLE) AT STA 887+2 TO 1006 IAW B737 DWG. 147A8501 , SRM 51-40-02-0G-0. INSP HAS BEEN C/W. RESDR CALA2026040115004Access Door · missingLEFT WING LEADING EDGE SLAT MECHANISM ACCESS DOOR MISSING. PANEL 521WB. PANEL 521WB REPLACED I.A.W AMM TASK 57-41-01-400-801. LOOSE ARTICAL CHECK CARRIED OUT BEFORE PANEL FITTMENT. PARTS DEPARTING LOGPAGE CREATED.PARTS USED: 76-5741-3-0002,QTY :1SDR CALA2026040115003Light · inoperativeEMERGENCY LIGHT AT 12L FOUND INOPERATIVE. EMERGENCY LIGHT ASSY REPLACED IAW AMM TASK 33-51-00-432-006. OPS CHECK GOOD.SDR CALA2026040115002Hydraulic Line · leakingRH OUTBOARD LINE IN NOSE GEAR HAS ACTIVE LEAK STARTED DEPRESSURIZATION OF HYD SYSTEMS IAW AMM 29-11-00-862-053 UP TO AND INCLUDING STEP 6.E.5 REMOVED AND REPLACED NLG RH HYDRAULIC LINE REF AMM 32-32-01-404-025 STEP 3F.(1) LINE REQUIRES FINAL TORQUE WITH LEAK CSDR CALA2026040115001Bulb · no testEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCHES EMERGENCY LIGHT L/H FUSELAGE AFT OF WING TO BODY FAIRING U/S. FILAMENT FOUND NOT SEATED CORRECTLY IN CONNECTOR. FILAMENT ADJUSTED NOW FUNCTION SATIS. WORK CARRIED OUT IAW AMM 33-51-06SDR CALA2026040114988Battery · no testPROCEDURE - CABIN EMERG LIGHT TEST, EPSU TEST FAILED. MESSAGE "EPSU (10WL) FWD L". SEE PHOTO. REPLACED BATTERY OF THE EPSU PER AMM 33-51-38-000-002-A/400-002-A. EPSU BITE TEST PASS. PARTS USED: 18-3351-3-0001, QTY :1SDR CALA2026040114987Cart · odorVERBAL FROM CABIN CREW LEAD UPON DOOR OPENING. FOUL SMELL OF EXHAUST OR FUEL IN FWD AND AFT GALLEYS PERFORMED AMM 05-51-00 SMELL OR SMOKE IN CABIN INSPECTION. APU WAS OFF WHEN SMELL WAS ENCOUNTERED IN BOTH FWD AND AFT GALLEYS. FOUND DRY ICE IN GALLEY CARTS INSDR ABXA20260331141Gcu · defectiveL AC BUS OFF AT TOP OF CLIMB OUT FROM CVG BOUND FOR MHT. CREW RAN THROUGH THE QRH AND RESET EVERYTHNING. THEY DECLARED AN EMERGENCY (EDC) AND RETURNED TO CVG WITHOUT INCIDENT. (ATB). MAINTENANCE REMOVED AND REPLACED GCU IAW AMM 24-22-02. OPS CHECK GOOD AC SDR IXXA20260331027A/C Pack · odorBURNT SMELL DURING RIGHT PACK OPERATION JUST AFTER TURNING IT ON. OPERATIONAL CHECK IN ACCORDANCE WITH B767 AMM 21-51-00 NOTED NO FAULTS. NO BURNT SMELL WAS NOTED.SDR QXEA2026040100076Throttle · malfunctionedFLIGHT 2133. REVERSERS ARE DIFFICULT TO INITIATE. DIFFICULTY IS IN THE GATES, NO ABLE TO PULL UP ON THEM DURING THE ROLLOUT. REMOVED FROM SERVICE. REPLACED THROTTLE QUADRANT ASSY PER AMM 76-11-01-000-801-A/-400-801-A. OPS CHECK ALL GOOD. AIRCRAFT REMAINS CAT ISDR AALA202604018697Slide · dislodgedAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS FORWARD SERVICE DOOR SLIDE VISIBLE AND IS CONCERNED IT MAY CATCH WHEN DOOR IS OPENED AND DAMAGE SLIDE. RESECURED FORWARD SERVICE DOOR SLIDE COVER. PER AMM 25-66-01. CHECKS GOOD NO OTHER DEFECT NOTED.SDR AALA202604013720Sensor · faultedAIRCRAFT WAS GROUNDED: NOSE GEAR WARNING LIGHT ILLUMINATES INTERMITTENTLY AFTER TAKEOFF IN ALL PHASES OF FLIGHT WITH THE GEAR HANDLE IN THE OFF POSITION. REMOVED AND REPLACED NOSE LANDING GEAR DOWN POSITION SENSOR, S0845 AND OPS CHECKS NORMAL. PER AMM 32-61-51SDR AALA202604010972Heatshrink · missingAIRCRAFT WAS NOT GROUNDED: L1 DOOR SLIDE GIRT BAR MISSING RED HEAT SHRINK. REPLACED L1 DOOR GIRT BAR HEAT SHRINK. PER AARD 25-66-00-4.SDR AALA202604012996Lock · damagedAIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR LOCK DAMAGED PASSENGERS CAN NOT OPEN THE DOOR AND GET LOCKED INSIDE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).SDR AALA202604011429Pump · warning messageAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LOW PRESSURE LIGHTS ILLUMINATED ON BOTH THE SYSTEM A ENGINE DRIVEN PUMP AND ELECTRIC PUMP DURING GEAR RETRACTION ON TAKEOFF. HYDRAULIC INDICATION SHOWED AS LOW AS 1400 PSI BEFORE RECOVERING, LOW PRESSURESDR AALA202604019003Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L1 DOOR HAS INDICATION THAT SAYS TO CHECK DOOR PRESSURE. MAINTENANCE SERVICED L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14 AND THE INDICATION LIGHT CLEARED.SDR AALA202604019702Strap · unsecureAIRCRAFT WAS NOT GROUNDED: DOOR 4R HAS 4 INCH STRAP HANGING OUT. MAINTENANCE SECURED DOOR 4R SLIDE STRAP PER AMM 25-62-44.SDR AALA202604016200Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: WHILE CLOSING AND ARMING 1L. CHECK DOOR PRESSURE CAUTION MESSAGE ON FORWARD FLIGHT ATTENDANT PANEL. MAINTENANCE SERVICED THE L-1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 25-62-49.SDR SCNA20260401146Light · inoperativeREAR LEFT EMERGENCY SLIDE LIGHT INOPERATIVE. EPLACED REAR LEFT EMEGERNCY SLIDE LIGHT IAW B737 AMM 33-51-04 CHECK EMERGENCY SLIDE LIGHT . CHECK SATISFACTORY IAW B737 AMM 33-51-04.SDR CNMA2026030002Altimeter · inoperativeCA ALTIMETER INOP. FLAGGED OFF AT 25,000 FT.SDR 2026FA0000245Pump · failedHYDRAULIC PUMP WAS REPLACED DURING SCHEDULED MAINTENANCE. AFTER 1 FLIGHT, THE HYDRAULIC PUMP HAD FAILED. REPORTS FROM OTHER PHENOM 100 OPERATORS, REPORT THAT THEY HAVE HAD MULTIPLE FAILURES OF THE HYDRAULIC SYSTEM AS WELL.SDR 2026F00048Spar · corrodedFOUND #5 SPEED BRAKE HYDRAULIC RETRACT CARRY THRU HAS CORROSION AROUND IT ON LH WING AFT SPAR. MECHANICALLY REMOVED CORROSION LOCATED WHERE #5 SPEED BRAKE RETRACT LINE FITTING IS LOCATED ON LH WING, AFT SPAR, AFT FACE IN FLAP COVE IAW CESSNA 680 SRM 51-70-02. SDR 2026F00058Spar · corrodedFOUND #4 SPEED BRAKE BOTH HYDRAULIC PRESSURE AND RETURN CARRY THRU'S HAVE CORROSION AROUND THEM ON LH WING AFT SPAR. MECHANICALLY REMOVED CORROSION LOCATED WHERE #4 SPEED BRAKE HYD PRESSURE AND RETURN LINE CARRY THRU FITTINGS ARE LOCATED ON LH WING AFT SPAR, ASDR 2026F00057Spar · corrodedFOUND #2 SPOILER HYDRAULIC PRESSURE CARRY THRU HAS CORROSION AROUND IT ON LH WING AFT SPAR. MECHANICALLY REMOVED CORROSION LOCATED WHERE #2 SPOILER HYD PRESSURE LINE CARRY THRU FITTING IS LOCATED ON LH WING AFT SPAR, AFT FACE INSIDE FLAP COVE IAW CESSNA 680 SRSDR 2026F00056Access Panel · corrodedFOUND 39 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 523AB AND 2 AREAS ON PANEL LAND. MECHANICALLY REMOVED 39 AREAS AROUND NUTPLATES WHICH WERE REMOVED PLUS 2 AREAS OF CORROSION ON PANEL LAND OF CORROSION IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TSDR 2026F00055Nut Plate · corrodedFOUND 20 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 532GB. MECHANICALLY REMOVED 22 AREAS OF CORROSION WHERE 20 NUTPLATES WERE REMOVED LOCATED ON LH WING INSIDE ACCESS BAY 532GB IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSSDR 2026F00054Nut Plate · corrodedFOUND 21 AREAS OF CORROSION AROUND NUTPLATES FO. R PANEL 532FB. MECHANICALLY REMOVED 21 AREAS OF CORROSION WHERE 21 NUTPLATES WERE REMOVED LOCATED ON LH WING INSIDE ACCESS BAY 532FB IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESDR 2026F00053Nut Plate · corrodedFOUND 12 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 542GB. MECHANICALLY REMOVED 12 AREAS OF CORROSION WHERE 12 NUTPLATES WERE REMOVED LOCATED ON LH WING INSIDE ACCESS BAY 542GB IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSSDR 2026F00052Nut Plate · corrodedFOUND 13 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 542FB. MECHANICALLY REMOVED 13 AREAS OF CORROSION WHERE 13 NUTPLATES WERE REMOVED INSIDE WING LOWER ACCESS BAY 542FB IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SDR 2026FA0000244Nut Plate · corrodedFOUND 8 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 632GB. BLENDED 8 AREAS OF CORROSION AT CORRODED NUTPLATE AREAS IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOSDR 2026F00051Nut Plate · corrodedFOUND 20 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 642FB. MECHANICALLY REMOVED 20 AREAS OF CORROSION LOCATED WHERE 20 NUTPLATES WERE REMOVED INSIDE WING LOWER ACCESS BAY 642FB IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSSDR 2026F00047Nut Plate · corrodedFOUND 8 AREAS OF CORROSION AROUND NUTPLATES FOR PANEL 642EB. MECHANICALLY REMOVED 8 AREAS OF CORROSION LOCATED INSIDE WING LOWER ACCESS PANEL 642EB WHERE 8 NUTPLATES WERE LOCATED IAW SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCSDR 2026F00050Spar · corrodedFOUND #7 SPEED BRAKE HYDRAULIC RETURN CARRY THRU HAS CORROSION AROUND IT ON RH WING AFT SPAR. MECHANICALLY REMOVED CORROSION WHERE #7 SPEED BRAKE HYD RETURN LINE IS LOCATED ON RH WING, FLAP WELL, AFT SPAR, AFT FACE IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION SDR 2026F00049Spar · corrodedFOUND #9 SPOILER BOTH HYDRAULIC PRESSURE AND RETURN CARRY THRU'S HAVE CORROSION AROUND THEM ON RH WING AFT SPAR. MECHANICALLY REMOVED CORROSION WHERE #9 SPOILER HYD PRESSURE AND RETURN LINE CARRY THRU FITTINGS ARE LOCATED ON WING AFT SPAR, AFT FACE IAW CESSNA SDR KCSA202603311027Pressure Deck · crackedRIGHT WING GEAR WHEEL WELL CANTED PRESSURE DECK COMPOSITE PANEL HAS EVIDENCE OF A CRACKSDR KCSA202603311026Web · crackedL/H HORIZONTAL STAB OTBD CLOSURE RIB WEB CRACKEDSDR 2026F00045Frame · corrodedCORROSION FOUND UNDER NUTPLATES ON FAIRING FRAME AT FS 312.90. MECHANICALLY REMOVED 6 AREAS OF CORROSION LOCATED ON INNER AND OUTER SURFACES OF FAIRING FRAME FS 312.90 IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 5SDR KCSA202603311025Support Angle · crackedL/H HORIZONTAL STAB UPPER TIP FAIRING SUPPORT CRACKED APPROX 26 IN. FROM STAB T/ESDR KCSA202603311024Support Angle · crackedL/H HORIZONTAL STAB LWR TIP FAIRING SUPPORT CRACKED APPROX 38.5 IN. FROM STAB T/ESDR 2026F00046Mount · corrodedFOUND CORROSION ON MOUNTING FLANGES FOR PANEL 342AB. MECHANICALLY REMOVED CORROSION LOCATED WHERE 18 NUTPLATES WERE REMOVED ON INNER AND OUTER SIDE OF FLANGES ON PANEL 342AB ATTACHMENT BRACKETS (10 NUTPLATES ON LH SIDE AND 8 NUTPLATES ON RT SIDE) IAW SRM 51-70SDR DALA2026033102109Skin · gougedTWO EACH DENTS WITH GOUGE AND PUNCTURE BETWEEN FR7 AND FR 8 R/H SIDE FUSELAGE SKIN. PERFORMED REPAIR IAW PRI 633376-14 REV 0, 1 AND 2. ALL STEPS COMPLIED WITH. WAITING ON FINAL ERA, (448268). RECEIVED FINAL ER /A APPROVAL FROM ENGINEERING. O.K. FOR SERVICE. (LSDR 2026F00044Door Frame · corrodedFOUND 1 AREA OF CORROSION AROUND AIRCRAFT DATA PLATE. REPAIRED CORROSION ON AFT TAIL CONE UNDER DATA TAG IN REFERENCE TO AEROSPACE QUALITY RESEARCH AND DEVELOPMENT ENGINEERING REPAIR ORDER: ERO-988391 REV. IR; TITLED: N339QS AFT TAILCONE SKIN CORROSION; DATED:SDR KCSA202603311023Spar · corrodedCORROSION FOUND EXTERIOR AFT SPAR AT CENTER TANK R/H OVRD/ JETTISON PUMP