N512AS
Service difficulty reports · 394
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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' WHERE n_number = 'N512AS' AND registry_match = 'registration' 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' WHERE n_number = 'N512AS' AND registry_match = 'registration' 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 ASAA2026100669116Guide Arm · out of adjustR1 DOOR DOES NOT CLOSE PROPERLY. GROUNDED - YES. ADJUSTED R1 GUIDE ARM IAW AMM 52-41-00-820-801, DOOR SHUTS SMOOTHLY WITH NO ADVERSE IMPACTS. OPS CHKD GOOD.SDR ASAA2026031764971Battery Pack · inoperativeR1 DOOR EMERGENCY LIGHT IS INOP. SRXR430X. GROUNDED - YES. REMOVED AND REPLACED R1 DOOR EMERGENCY BATTERY PACK AND PERFORMED R1 DOOR EMERGENCY LIGHT TEST IAW B737 AMM 33-51-06-960-805. TEST GOOD. SRXR430X.SDR ASAA2026022564886Web · crackedLEFT WHEEL WELL CENTER WING REAR SPAR VAPOR WEB HAS A CRACK ON THE LH AND RH SIDE OF THE HYDRAULIC RETURN FILTER. STICKER 001-76. SRXR430X. GROUNDED - YES. ACCOMPLISHED EA#800-57EA-30019, PI, P2, AND REV 00 MAJOR REPAIRON LEFT WHEEL WELL CENTER WING REAR SPAR SDR ASAA2026013064062Guide Arm · out of adjustTHE R-1 DOOR IS DIFFICULT TO CLOSE, WHILE CLOSING THE AFT SIDE OF THE DOOR IS NOT MOVING OUTBOARD ENOUGH. GROUNDED - YES. FOUND THE R-1 DOOR GUIDE ARM OUT OF ADJUSTMENT, ADJUSTED THE GUIDE ARM TO WITHIN LIMITS REF AMM 52-41-00-820-801 STEP 2I.THE R-1 DOOR OPERSDR ASAA2025121563103Hinge · dirtyR1 DOOR VERY DIFFICULT TO CLOSE, SHOWED UP TO A/C DOOR HANDLE WAS STOWED AND RIGHT SIDE OF DOOR WAS SHOWING APPROX. 1 INCH GAP. GROUNDED - YES. CLEANED AND INSPECTED R1 DOOR HINGES AND PERFORMED OPS CHECK IAW AMM 52-41-00. DOOR OPERATES NORMALLY. NO FURTHER DESDR ASAA2025073159823Faceplate · detachedFA REPORTS LEFT EXIT SIGN FACE PLATE DETACHED. GROUNDED - YES. REINSTALLED AFT L/H EXIT AMG SIGN FACE PLATE REF IPC 33-51-05-02A.SDR ASAA2025062358979Door · bindingFLIGHT ATTENDANT REPORTS R1 DOOR REQUIRES MORE EFFORT THAN NORMAL TO OPEN/CLOSE. GROUNDED - YES. PERFORMED SERVICE DOOR CHECK OF R1 DOOR. REF AMM 52-41-00. FOUND DOOR UNABLE TO CLOSE FULLY ON THE TOP RIGHT CORNER. FOUND TEAR IN DOOR SEAL AFT SIDE UPPER AND LOWSDR ASAA2025060858592Lens · missingEXIT SIGN NEXT TO DOOR L2 MISSING. GROUNDED - YES. INSTALLED L2 EXIT DOOR SIGN COVER PER AMM 33-51-01. NO DEFECTS NOTED. A/C OK.SDR ASAA2025012155495Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1676 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1676 S/N 130677 IAW B737-NG AMM 33-51-960-806. OPS CHECK GOOD.SDR ASAA2025012155494Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1670 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1670 S/N 33222 IAW B737-NG AMM 33-51-06-960-806. OPS CHECK GOOD.SDR ASAA2025011455445Stringer · corrodedLATE FIND:STRINGER 27L IS CORRODED AT STA. 727+14 ON I/B SIDE. GROUNDED - YES. REPAIRED CORRODED STRINGER 27L AT STA. 727+14 ON I/B SIDE IAW ASA EA#800-53EA-28156.SDR ASAA2024122755340Skin · crackedACCESS REQ AT STA 92.70 FOR 2EA CRACKS IN RIB, REPAIR 11 REQ. GROUNDED - YES. REPAIRED AREA WITH REPAIR 11 AT STA. 92.70 OF RH HORIZONTAL STABILIZER LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11, REPAIR 11. THIS IS A CATEGORY B REPAIR, INSPECTION THRESHOLD IS 56,SDR ASAA2024122155551Rib · crackedACCESS REQ AT STA 120.30 FOR 2EA CRACKS IN RIB, REPAIR 11 REQ. GROUNDED - YES. REMOVED EXISTING REPAIR AT STA 129.50, CUT NEW ACCESS HOLE AT STA 120.30 AND REPAIRED AREA IAW B737-800 SRM 55-10-01-2R-11. REPAIR IS CAT B INSPECTION THRESHOLD IS 56,000 FC METHOD SDR ASAA2024121355302Skin · crackedCRACK INDICATION FOUND: L/H HORZ. STAB. LOWER SKIN I/B STAB. STA. 147.90 FASTENER ROW, 16.25" FWD OF AFT SPAR, MARKED .370"L. GROUNDED - YES. REMOVED CRACK AT STA 147.90 IAW B737-800 SRM 55-10-01-2R-11 AND SRM 51-10-02 AND REPAIRED AREA IAW B737-800 SRM 51-10-SDR ASAA2024121055249Support · corrodedAFT PIT RH TRANSITION CORRODED FROM STA 727-767. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT RH TRANSITION STA 727-767. ORG MAT..040, REMOVED MAT .008, MAT REMAINING .032. FOUND TO BE OUT OF LIMITS IAW B737-NG SRM 53-00-53-1A-2. REPAIRED AFT PIT TRANSITION SDR ASAA2024121055139Web · corrodedAFT PIT THRESHOLD HAS NUMEROUS SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ORIG .050, REMAIN .039 LOSS OF .011. FOUND OUT OF LIMITS IAW B737 800 SRM 53-60-15. REMOVED AFT PIT THRESHOLD RECEIVED NEW THRESHOLD LOCATED AND DRILLED THRESHOLD AND INSTALLESDR ASAA2024121055138Transition Panel · corrodedAFT PIT LH TRANSITION CORRODED FROM STA 727-847. GROUNDED - YES. REMOVED CORROSION ORIG .040, REMAIN .034 LOSS OF .006. FOUND OUT OF LIMITS IAW B737 800 SRM 53-60-53. ACCOMPLISHED REPAIR OF TRANSITIONS PANEL IAW B737 800 SRM 53-00-53-2R-5 REP 5. ALODINED AND PSDR ASAA2024121055116Strap · corrodedAFT PIT UPPER SILL STRAP CORRODED. GROUNDED - YES. REMOVED CORROSION ORIG .100, REMAIN .088 LOSS OF .012. FOUND OUT OF LIMITS IAW B737 800 SRM 53-60-15. REMOVED SIL STRAP, LOCATED, DRILLED AND INSTALLED NEW STRAP IAW BAC DWG 146A3120 AND B737 800 SRM 51-40-02.SDR ASAA2024121055040Shield · corrodedAFT PIT RH FWD SHIELD HAS NUMEROUS SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON AFT PIT R/H FWD SHIELD. ORIGINAL MAT .050, REMOVED .010, REMAINING .040. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. REPLACED AFT PIT R/H FWD SHIELD IAW BSDR ASAA2024120955600Floorbeam · corrodedMAIN CABIN. TOP OF FLOOR BEAM CORRODED NEXT TO FITTING, STA 915, LBL 24 GROUNDED - YES. REMOVED AND REPLACED CORRODED P/N# 147A5690-10 INTERCOSTAL IAW B737-800 SRM 51-40-02 & BAC DWG# 147A5680 REV.F REMOVED HAECO DOT. ORIGINAL MAT'L THICKNESS .120, REMOVED .03SDR ASAA2024120955137Floor Support · corrodedMAIN CABIN. TOP OF FLOOR STRUCTURE STA 959 LBL 49, CORROSION AROUND FASTENER HOLE. GROUNDED - YES. REMOVED CORRODED INTERCOSTAL I.A.W B737-800 SRM 51-40-02, LOCATED & DRILLED AND INSTALLED NEW INTERCOSTALL P/N 147A5660Y21 PER BOEING DWG #147A5660 REV C AND I.ASDR ASAA2024120955136Floor Support · corrodedMAIN CABIN AFT WET AREA STA 947-967 LBL 27 INTERCOSTAL CORRODED. GROUNDED - YES. REMOVED CORRODED INTERCOSTAL BS 947-967 LBL27 AND 2 EACH FLOOR SUPPORTS IAW B737-800 SRM 51-40-02. LOCATED AND DRILLED NEW P/N#147A5660-3 INTERCOSTAL AND INSTALLED INTERCOSTAL ANDSDR ASAA2024120955117Floorbeam · corrodedMAIN CABIN. TOP OF FLOOR STRUCTURE STA 986 LBL27-RBL-34, CORROSION AROUND FASTENER HOLES. GROUNDED - YES. REMOVED CORROSION ORIG .150, REMAIN .125 LOSS OF .025. FOUND OUT OF LIMITS IAW B737 800 SRM 53-70-51. ACCOPLISHED REPAIR IAW B737 800 SRM 53-70-51 2R-4 RESDR ASAA2024120955041Support Angle · corrodedMAIN CABIN AFT WET AREA STA 990 RBL 40 SUPPORT ANGLE BARE METAL. GROUNDED - YES. CLEANED AREA IAW SOPM 20-30-03. FOUND CORROSION AND REMOVED IT. 100% LOSS IN A 1" X 1" AREA, FOUND OUT OF LIMITS IAW B737 800 SRM 53-70-51. REMOVED ANGLE LOCATED AND DRILLED IAW BSDR ASAA2024120955039Floorbeam · corrodedMAIN CABIN. TOP OF FLOOR BEAM CORRODED AFT OF FITTING, STA 915 ,LBL 25.5. GROUNDED - YES. FOUND INTERCOSTAL OUT-OF LIMITS IAW B737 SRM 53-70-58-1A-1 INSTALLED NEW INTERCOSTAL PART #147A5680U8 P.O. 1108949.3 IAW DWG #147A5680 AND B737-800 SRM 51-40-02. 80% LOSSSDR ASAA2024120954956Beam · gougedL2 DOOR, HANDLE BOX CUTOUT, UPPER STUB BEAM, LOWER SURFACE IS GOUGED. GROUNDED - YES. REMOVED AND REPLACED UPPER STAB BEAM IAW B737-800 SRM 51-40-02, BAC DWG 147A6149 REV A AND BAC DWG 147A6116 REV-SDR ASAA2024120954889Angle · corrodedMAIN CABIN AFT WET AREA STA 1006-1016 RBL 27 ANGLE HAS BARE METAL. GROUNDED - YES. REMOVED CORROSION AT FASTENER HOLE WITH 100% LOSS OF MATL FOUND OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED ANGLE IAW B737 800 SRM 51-40-02. LOCATED AND DRILLED NEW ANGLE ISDR ASAA2024120954888Angle · corrodedMAIN CABIN. TOP OF FLOOR STRUCTURE STA 991.5 - 994.5, LBL32, 2 AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION WITH 100% LOSS. FOUND OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED ANGLE IAW B737 800 SRM 51-40-02. LOCATED AND DRILLED NEW ANGLE IAW BAC DSDR ASAA2024120754882Pan · corrodedR1 DOOR HANDLE PAN INNER BORE DAMAGED (NICKED) GROUNDED - YES. REMOVED DAMAGE FROM AREA, MAX AMOUNT MATERIAL THAT CAN BE REMOVED IS .100", REMOVED .112" THICKNESS AREA OUT OF LIMITS. REMOVED DAMAGED HANDLE PAN. LOCATED, DRILLED AND INSTALLED (1EA) NEW HANDLESDR ASAA2024120655301Rib · crackedL/H HORIZONTAL STABILIZER HAS 2EA. CRACKS IN RIB STAB STA.120.30. GROUNDED - YES. REMOVED 2EA CRACKS IN RIB AT STA 120.30 ON LH HORIZONTAL STAB AND REPAIRED 2EA AREAS IAW B737-800 SRM 55-10-09-2R-4 CAT A REPAIR.SDR ASAA2024120655300Rib · crackedRH HORIZONTAL STABILIZER HAS 2EA. CRACKS IN RIB STAB STA.92.70. GROUNDED - YES. EXISTING REPAIR REMOVED IAW B737-800 SRM 51-40-02. PAINT STRIPPED IAW B737-800 AMM 51-21-11. 2EA CRACKS REMOVED AT STA 92.70 IAW B737-800 SRM 51-10-02. ACCOMPLISHED HFEC ON 2EA RIBSDR ASAA2024120655297Skin · damagedRIGHT HORIZONTAL STABILIZER BOTTOM SIDE HAS 3EA. DENTS AT STAB STA.157.10. GROUNDED - YES. EVALUATED DAMAGE ON RIGHT HAND HORIZONTAL STAB LOWER SKIN AT STA 157.1. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 55-10-01-1A-2 DUE TO DAMAGE ON FASTENER HOLE AND PROXISDR ASAA2024120655118Web · corrodedFWD PIT THRESHOLD HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICK .045", MATERIAL REMOVED .010" MAT REMAINING .035" FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED FWD PIT THRESHOLD WEB IAW B737-800 SRM 51-40SDR ASAA2024070350808Connector · not seatedR/H AFT SIDE/WING EMERGENCY LIGHT INOP. GROUNDED - YES. CONNECTOR FOR EMERGENCY LTS PSU NOT FULLY SEATED. RECONNECTED POWER SUPPLY CONNECTOR. EMER BATT LTS CHK GOOD. REF AMM 33-51-06.SDR ASAA2023111146141Bulb · inoperativeRIGHT SIDE SLIDE LIGHT FOUND INOP. GROUNDED - YES. RELAMPED RIGHT SIDE SLIDE LIGHT AND OPS CHECK NORMALREF B737-800 AMM 33-51-04-960-801.SDR ASAA2023103045945Unknown · unknownWINDOW OVERHEAT, LEFT SIDE L2 WINDOW. QRH WINDOW OVERHEAT CHECKLIST COMPLETED. WINDOW OVERHEAT, LEFT SIDE WINDOW (L2) ILLUMINATED AGAIN. GROUNDED - YES. INITAL EVAL, NO LT ON RECALL. L SIDE SW PLACED TO ON, STAYS IN ON, NO OVERHEAT. OPS CHECKS GOOD IAW AMM 30-SDR ASAA2023102045759Unknown · unknownLEFT LPACK LIGHT ILLUMINATED ON RECALL. GROUNDED - YES. ACCOMPLISHED PACK TEMP CONTROLLER BITE CK, FOUND TCV FAULT ON ZONE TEMPCONTROLLER 1, AFTER COMPLETING BITE CK HAD GREEN GO LIGHTS, RESET FAULTNO HISTORY LAST 30 DAYS, SEAMC JEREMY NTOFIED.SDR ASAA2023101745703Control Panel · faulty"B" - 2ND AUTO PILOT FAILED TO ENGAGE DURING ATTEMPTED AUTOLAND APPROACH. GROUNDED - YES. (RESOLVED ON W/O: 1973033 TASKCARD: N/R-00002 ) REMOVED AND REPLACED MCP PER AMM 22-11-34.ALL LLM TESTS C/W. NO FAULTS NOTED. REMOVED PLACARD. REMOVED MEL'S 22-1F AND 22-SDR ASAA2023101745699Controller · faultyAUTOFAIL LIGHT ILLUMINATED. GROUNDED - YES. (RESOLVED ON W/O: 1973033 TASKCARD: N/R-00004 ) REMOVED AND REPLACED #1 CPC PER AMM 21-31-01. NO FAULTS NOTED. REMOVED PLACARD. REMOVED MEL 21-14C. RESTORED CONFIGURATION CHANGE. SEAMC DAVE NOTIFIED.SDR ASAA2023100845522Controller · malfunctionedCLIMBING THROUGH APPROX FLIGHT LEVEL 340 SIGNIFICANT PRESSURE CHANGE, EARS POPPED, NO CAUTIOIN LIGHT, STOPPED CLIMB, STARTED DECENT, RAN UNCONTROLLED PRESSURE CHECLIST. REGAINED CONTROL WITH SELECTOR TO ALTN DIFF PRESSURE PEAKED AT 8.8. CONTINUED WITH NORMAL OSDR ASAA2023100545456Unknown · unknownELEC ANNUNCIATOR LT ILLUMINATED. GROUNDED - YES. PERFORMED B737-800 FIM 24-31 TASK 801. RESET INTERMITTENT FAULT. OK FOR SERVICE.SDR ASAA2023092545297Connector · damaged#2 ENGINE HYDRAULIC PUMP CONNECTOR DAMAGE FOUND DURING MX TASK CARD. GROUNDED - YES. REMOVED AND REPLACED #2 ENG EDP REF B737-800 AMM 29-11-11-400-801-001. OPS CHECK & LEAK CHECK SUCCESSFUL. OK FOR SERVICE.SDR ASAA2023090144930Transceiver · inoperativeHF 2 SHOWS FAIL FAIL MESSAGE. GROUNDED - YES. VERIFED FAIL FAIL ON FO'S RTP & HF TRANSCEIVER WILL NOT ENTER BITE. RESET #2 HF C/B = SAME RESULTS. REPLACED #2 HF TRANSCEIVER WITH SERVICABLE UNIT, INSTALLATION BITE TEST OK. REF AMM 23-11-21-400-801.SDR ASAA2023071744079Unknown · unknownWHILE ACCOMPLISHING T/C 78273000 FOUND ENG #2 ECONOMIC FAULT 75-10362 THE HPTACC POSITION SIGNALS IS OUT OF RANGE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023071744078Unknown · unknownWHILE ACCOMPLISHING T/C 78273000 FOUND ENG #2 ECONOMIC FAULT 75-30412. THE HPTACC POSITION SIGNALS DISAGREE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023072174077Unknown · unknownWHILE ACCOMPLISHING T/C 78273000 FOUND ENG #2 ECONOMIC FAULT 75-20462. THE HPTACC DEMAND AND POSITION SIGNALS DISAGREE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023071544032Unknown · unknownUNABLE TO TRANSMIT ON HF 1 OR 2. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023071544034Unknown · unknownMSG ECONOMIC FAULT CODE 77-90872 EGT SIGNAL OUT OF RANGE ENG #2. GROUNDED - YES. CLEANED S1 THRU S4 EGT PROBES REF B737-800 AMM 77-21-00 AND T/C N8420001 VERIFIED FAULT CODE NOT PRESENT AND EEC BITE CHECK PASS REF AMM 73-21-00.SDR ASAA2023070143852Unknown · unknown#2 ENGINE HAS ECONOMIC FAULT 73-31372 UPPER EGT LIMIT REACHED. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023032342499Unknown · unknownCATERING REPORTS R1 DOOR NOT CLOSE. GROUNDED - YES. FOUND R1 DOOR BINDING WHEN TRYING TO CLOSE. REQUIRES EXCESSIVE PRESSURE TO CLOSE. FOUND R-1 DOOR GUIDE ARM OUT OF RIG, ADJUSTED GUIDE ARM REF. B737-800 AMM 52-41-00-820-801 STEP 2. I., FOUND MISSING STOP PIN
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