N514AS
Service difficulty reports · 370
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 = 'N514AS' 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 = 'N514AS' 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 ASAA2025123163493Door · bindingFA REPORTS L1 VERY DIFFICULT TO OPEN. GROUNDED - YES. PERFORMED L1 DOOR FWD ENTRY DOOR SYSTEM TEST. DOOR IS WITHIN OPEN / CLOSE TORQUE SPECS. NO HISTORY PAST 90 DAYS.SDR ASAA2025061658810Light · detachedFA REPORTS EMERGENCY LIGHTING COVER CAME OFF NEAR ROW 16F. GROUNDED - YES. INSTALLED NEW EMERG/EXIT LIGHTING COVER @ ROW 16F.SDR ASAA2025050757798Sign · detachedF/A S REPORT LOWER EXIT SIDEWALL SIGN WILL NOT STAY ATTACHED AT 16A. GROUNDED - YES. REMOVED AND REPLACED EXIT LIGHT ASSY AT ROW 16A I/A/W AMM 33-51-01. OPS CHECK GOOD.SDR ASAA2025012756002Skin · corrodedEXTERIOR SKIN BS.887 TO BS.1016 STR.23L UPPER LAP SHOWS SIGNS OF CORROSION 17 AREA. (MARKED IN RED). GROUNDED - YES. REMOVED CORROSION 17(EA) ON ZONE B. DAMAGE AREAS FROM STA 887-STA 1016 STR 23L UPPER LAP ORG MAT THICK 0.063, REMOVED 0.004 REMAINING 0.059 FOUSDR ASAA2025012155907Intercostal · corroded(LATE FIND) AFT PIT BILGE INTERCOSTAL AT STA 867 TO 887 LBL 10 IS CORRODED. GROUNDED - YES. UPON FURTHER EVALUATION THE AFT PIT INTERCOSTAL AT STA 867-887, LBL 10 IS FOUND TO HAVE 100% MAT LOSS NO ALLOWABLE DAMAGE LIMITS ARE GIVEN IN B737-800 SRM. REMOVED DAMASDR ASAA2025011455731Intercostal · corrodedAFT CARGO COMPARTMENT BS.847 TO BS.867 BETWEEN STR.25L - STR.26L INTERCOSTAL CORRODED. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT L/H INTERCOSTAL AT STA 847 TO 867, STR25L TO 26L IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .045" IAW B737-800SDR ASAA2025011355910Web · corrodedR/H AFT CABIN AT STA 992 FLOOR SUPPORT WEB UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS 0.040. REMOVED 0.007, REMAINING 0.033. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED WEB IAWSDR ASAA2025011355909Floor Support · corrodedR/N AFT CABIN AT STA 1016 FLOOR SUPPORT ANGLE UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02. 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02. LOCATED, SDR ASAA2025011355908Floor Support · corrodedL/H AFT CABIN AT STA 992 FLOOR SUPPORT ANGLE STRUCTURE UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION, 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02. DRILLED TO FIT NEW FLOOR SSDR ASAA2025011355905Floor Support · corrodedR/H AFT CABIN AT STA 992 FLOOR SUPPORT ANGLE UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-0.2. 100% MATERIAL LOSS-OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02. DRILLED TOSDR ASAA2025011355904Web · corrodedL/H AFT CABIN AT STA 992 FLOOR SUPPORT WEB UPPER SURFACE HAS CORROSION GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, 100% MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED WEB IAW B737-800 SRM 51-40-02 AND BOEING DWG 147A5700 REV BSDR ASAA2025011355903Support Angle · corrodedR2 GALLEY DOOR SILL PANEL SUPPORT ANGLE SURFASE CORRODED AT MULTIPLE SPOTS BETWEEN BS 951 AND 993. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02. AREA FOUND TO BE 100% MAT LOSS OUT OF LIMITS. REMOVED AND REPLACED MOP SEAL INNER CHORD IAW B737-800SDR ASAA2025011355802Floorbeam · corrodedR/H AFT CABIN AT STA 986 FLOOR BEAM UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, ORIG THICKNESS 0.150" , REMOVED 0.045" , REMAINING 0.105" OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1, REPAIRED DAMAGE IAW B737-800 SSDR ASAA2025011355801Floor Support · corrodedL/H AFT CABIN AT STA 992 FLOOR SUPPORT ANGLE STRUCTURE UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPPORT IAW B737-800 SRM 51-10-02. NO ALLOWABLE DAMAGE LIMITS STATED. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02 ANSDR ASAA2025011355649Floor Support · corrodedCORROSION FOUND IN HOLES (3 EACH) ON PANEL BREAK BETWEEN STATION 328 AND STATION 344 BUTT LINE 10. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 328 TO 344 BUTT LINE 10 IAW B737-800 SRM 51-40-02.SDR ASAA2025011355648Floor Support · corrodedL/H AFT CABIN BETWEEN STA 907 AND STA 927 FLOOR SUPPORT STRUCTURE UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION AREAS IAW B737-800 SRM 51-10-02. PART FOUND TO BE OUT OF LIMITS 100% MAT LOSS. REMOVED AND REPLACED NEW FLOOR SUPPORT STRUCTURE IAWSDR ASAA2025011355647Transition Panel · corrodedAFT CARGO COMPARTMENT LEFT TRANSITION PANELS HAVE CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT, L/H TRANSITION PANEL AT STA 727B+10 TO 797 IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040" IAW B737-800 SRM 53-60-53-01-2 TABLE 2 FOUND SDR ASAA2025011355646Floorbeam · corrodedAFT CABIN AT STA 951 FLOOR BEAM UPPER SURFACE HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE IAW B737-800 SRM 51-10-02, FOUND TO BE OUT OF LIMITS I.A.W. B737-800 SRM 53-70-51-1A-1 ORIGINAL THICKNESS .180, MAT REMAINING .142 IAW B737-800 SRM 53-70-51-01-1, FABRISDR ASAA2025011355643Transition Panel · corrodedAFT CARGO COMPARTMENT RIGHT TRANSITION PANELS HAVE CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANELS FROM STA 727 TO 767 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS .040" IAW B737-800 SRM 53-60-53-01-2. FOUND TO HAVE 100% MSDR ASAA2025011355642Intercostal · corrodedCORROSION FOUND IN HOLES (5 EACH) ON PANEL BREAK BETWEEN STATION 312 AND STATION 328 BUTT LINE 10. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 TO 328 BUTT LINE 10 IAW B737-800 SRM 51-40-02.SDR ASAA2025011255644Angle · corrodedFWD CARGO COMPARTMENT AFT MIX BAY ACCESS PANEL(A/C SIDE) NUT PLATE ANGLE L/H-R/H STA500I HAS SEVERAL AREAS OF CORROSION UPPER AND LOWER SURFACE. GROUNDED - YES. REMOVED AND REPLACED NEW RAIL P/N 143A9485Y35 P.O. 1111512.1, LOCATED AND DRILLED HOLES AT FWD CARGSDR ASAA2025011255565Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-136. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION 147A5810-136 IAW B737-800-SRM-53-00-50-2R-1 AND SRM-53-00-50-2R-0.SDR ASAA2025011255564Floor Panel · delaminatedFWD WET AREA FLOOR BOARD DELAME 141A5810-155. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF FORWARD WET AREA FLOOR BOARD DELAMINATION 141A5810-155 IAW B737-800-SRM-53-00-50-2R-1 AND SRM-53-00-50-2R-0.SDR ASAA2025011255563Floorboard · delaminatedFWD WET AREA FLOOR BOARD DELAME 141A5810-755. GROUNDED - YES. COMPLETED PERMANENT REPAIR TO FWD WET AREA FLOOR BOARD 141A5810-755 IAW B737-800 SRM 53-00-50-2R-0.SDR ASAA2025011255562Floorboard · delaminatedFWD WET AREA FLOOR BOARD DELAME 141A5810-728. GROUNDED - YES. COMPLETED PERMANENT REPAIR TO FWD WET AREA FLOOR BOARD 141A5810-728 IAW B737-800 SRM 53-00-50-2R-0.SDR ASAA2025011255561Floor Panel · damagedMAIN CABIN AFT WET AREA FLOORBOARD DELAMINATED 147A5810-137. GROUNDED - YES. PREFORMED PERMANT REPAIR TO MAIN CABIN AFT WET AREA FLOORBOARD 147A5810-137 IAW B737-800 SRM 53-00-50-2R-0.SDR ASAA2025011255560Floor Panel · damagedMAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-28. GROUNDED - YES. PERFORMED PERMANT REPAIR TO MAIN CABIN AFT WET AREA FLOORBOARD 147A5810-28 IAW B737-800 SRM 53-00-50.SDR ASAA2025011255559Floorboard · delaminatedFWD WET AREA FLOOR BOARD DELAME 141A5810-454. GROUNDED - YES. ACCOMPLISHED PERMANENT WET LAY UP REPAIR ON FWD WET AREA FLOOR PANEL 141A5810-454 IAW B737 SRM 53-00-50-2R-0.SDR ASAA2025011255558Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-90. GROUNDED - YES. ACCOMPLISHED PERMANENT WET LAY UP REPAIR ON MAIN CABIN AFT WET AREA FLOOR BOARD 147A5810-90 IAW B737 SRM 53-00-50-2R-0.SDR ASAA2025011255557Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME 147A5810-27. GROUNDED - YES. ACCOMPLISHED PERMANENT WET LAY UP REPAIR ON MAIN CABIN AFT WET AREA FLOOR BOARD 147A5810-27 IAW B737 SRM 55-00-50-2R-0.SDR ASAA2025011255503Transition Panel · corrodedFWD CARGO COMPARTMENT R/H TRANSITION PANEL HAS CORROSION AT SEVERAL AREAS STA500A-STA500I. GROUNDED - YES. REMOVED CORROSION FROM R/H TRANSITION PNL STA 500A-500I IAW B737-800 SRM 53-00-53-1A-2. ORIG. MATERIAL WAS .040" IAW B737-800 SRM 53-00-53-01-2. REMOVED SDR ASAA2025011255497Floorboard · delaminatedFWD WET AREA FLOOR BOARD DELAME 141A5810-765. GROUNDED - YES. REPAIRED FLOOR BOARD 141A5810-765 OF DELAM USING PERMANENT REPAIR IAW B737-800 SRM 53-00-50-1A-1, 53-00-50-2R-1, 53-00-50-2R-0.SDR ASAA2025011255496Floor Panel · delaminatedFWD WET AREA FLOOR BOARD DELAME 141A5810-763. GROUNDED - YES. REPAIRED FLOOR BOARD 141A5810-763 OF DELAM USING PERMANENT REPAIR IAW B737-800 SRM 53-00-50-1A-1, 53-00-50-2R-1, 53-00-50-2R-0.SDR ASAA2025011155906Web · corrodedAFT CARGO DOOR CUTOUT SILL WEB PLATE HAS CORROSION IN LARGE AREA. CIRCLED IN RED. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT DOOR SURROUND WEB IAW B737-800 SRM 53-60-15-1A-1. ORIG THICKNESS IS .050" IAW B737-800 SRM 53-60-15-01-1. FOUND TO BE 100% MATERIALSDR ASAA2025011155645Strap · corrodedAFT CARGO DOOR CUTOUT HAS CORROSION AROUND SCREW HOLES,AND OTHER SPOTS ON FLOOR STRUCTURE BEHIND THE SILL WEB PANEL. CIRCLED IN RED. GROUNDED - YES. AFTER FURTHER EVALUATION, CORROSION FOUND ON PREVIOUS REPAIR. NO ALLOWABLE DAMAGE LIMITS FOUND. REMOVED ADDITIOSDR ASAA2025010955701Pan · gougedR1 DOOR, EXTERIOR HANDLE PAN, INSIDE DIAMETER IS GOUGED. GROUNDED - YES. REMOVED GOUGED HANDLE PAN, RECIEVED & INSTALLED NEW HANDLE PAN IAW BAC DWG 141A6516 REV.B & B737-800 SRM 51-40-02-0G-0.SDR ASAA2024121354568Guide Arm · out of adjustAIRCRAFT WOULDN'T PRESSURIZED AFTER TAKEOFF. FA REPORTED L2 DOOR OPEN. NO DOOR INDICATION IN COCKPIT. RETURN TO JNU. GROUNDED - YES. AIR TURNBACK - ON ARRIVAL L2 DOOR FOUND SLIGHTLY OPEN. FWD ROLLERS FOUND TO BE OUT OF RECEIVERS. PERFORMED AFT ENTRY DOOR ADJUSSDR ASAA2024072651372Sign · detachedGALLEY 1 PLASTIC EXIT WALL SIGN FELL OFF. GROUNDED - YES. GALLEY 1 FWD OF R1 DOOR EXIT WALL LIGHT DAMAGED. REMOVED DAMAGED ASSEMBLY INSTALLED SERVICABLE ONE REF AMM 33-51-00 OPS CHECK GOOD.SDR ASAA2024072051184Sign · detachedR2 DOOR EXIT SIGN FELL OFF IN FLIGHT. GROUNDED - YES. (RESOLVED ON W/O: 2011019 TASKCARD: N/R-00001 ) R2 DOOR EXIT SIGN ASSY REPLACED REF AMM 33-51-01. OPS CHECK GOOD. THIS CLEARS THE PLT ON LP 61008281.SDR ASAA2024021847913Battery Pack · no testWHILE PERFORMING TC 78233001 FOUND 3 EMERGENCY LIGHT BATTERY PACKS FAILED. GROUNDED - YES. REPLACED BATTERY PACKS IAW AMM 33-51-06. OPS CHECKS GOOD.SDR ASAA2023101745740Packing · leakingFOLLOW-UP TO #2 IDG FREQUENT SERVICING. (#PRI2/ETOPS). GROUNDED - YES. (RESOLVED ON W/O: 1973837 TASKCARD: N/R-00001 ) C/W LEAK CHECK WITH A TEN MINUTE IDLE RUN. FOUND PISTON COVER PLATE LEAKING . PLATE IS BELOW IDG RECONNECT RING & ABOVE AFT FILTER. NO EXTERNSDR ASAA2023100645512Unknown · unknownMAP FLAG ILLUMINATED ON CAPTAIN MFD FO SIDE NORMAL. GROUNDED - YES. PERF FMC BITE TEST REF B737-800 FIM 34-61 TASK 801. SYS TEST NORMAL, NO FAULTS LOGGED.SDR ASAA2023092945384Unknown · unknown"AUTOFAIL" ILLUMINATED ON PRESSURIZATION PANEL "ALTN" ALSO ILLUMINATED. GROUNDED - YES. PERFORMED B737-800 FIM 21-31 TASK 827. PER INITIAL EVALUATION FAULT IS TRANSITORY POSITION OF SWITCH, LIGHT EXTINGUISHED. PERFORMED REPAIR CONFIRMATION AT END OF FIM. NO FASDR ASAA2023092245268Housing · brokenAFT EXIT SIGN BETWEEN L2 & R2 BROKEN & CROOKED. GROUNDED - YES. (ITEM RESOLVE UNDER MDDR: 60685168) (RESOLVED ON W/O: 1970745 TASKCARD: N/R-00001 ) REPLACED BROKEN EMERGENCY EXIT SIGN PER AMM 33-51-01. OP CHECKS NORMAL AT THIS TIME. THIS CLEARS MCT DEFERRAL ANSDR ASAA2023090144934Pressure Switch · faultyCENTER TANK RIGHT FUEL PUMP LOW PRESSURE LIGHT DOES NOT ILLUMINATE AFTER FUEL IS EXHAUSTED FROM THAT TANK. FUEL PUMP APPEARED TO OPERATE NORMALLY AND FUEL BURN WAS AS EXPECTED. GROUNDED - YES. PERFORMED INITIAL EVALUATION OF FIM 28-22 TASK 821, PUSH-TO-TEST LISDR ASAA2023073044328Unknown · unknownFAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL360. SUCCESSFUL CSS ACCOMPLISHED AFTER FAULT LIGHT EXTINGUISHED. GROUNDED - YES. RECIEVED ACARS MSSG AND PER SEAMC STEVE COLD SOACK APU PASSED. REMOVED MEL 49-99A. SEAMC STEVE NOTIFIED. A/C OK FOR SERVICE. SDR ASAA2023071744086Unknown · unknownDRASTIC REDUCTION OF SYSTEM A AT ROTATION. FLT CONTROL AND HYD CAUTION LIGHTS ILLUMINATED. AIR RETURN AS PER FODO/MX CONTROL. GROUNDED - YES. AIR TURNBACK - PERFORMED SYS A LEAK CHK REF AMM 29-00-00-790-810. NO LEAKS NOTED. PER CAPT BRIEFING REFERENCE, ON LANDSDR ASAA2023070543908Unknown · unknownAPU GEN OFF LIGHT NOT ILLUMINATING WHEN APU IS OPERATIONAL. GROUNDED - YES. STARTED APU. APU GEN OFF LIGHT WORKS NORMAL. CYCLED APU GEN OFF AND ON SEVERAL TIMES WITH NO FAULTS. APU GCU BITE GOOD. REF FIM 24-21 TASK 801.SDR ASAA2023060643478Plate · wornWHILE REPLACING OUTBOARD FWD STRIKER PLATE FOR ECS DOOR (192DR) FOUND DAMAGE UNDER STRIKER PLATE IN STRUCTURE MEASURING .093" DEEP, .281" LONG AND .156' WIDE. GROUNDED - YES. REF MIG-5 L/P 300010908 FOR PERMANENT REPAIR PER SRM 57-10-13-2R-3 REPAIR 3. ACC PERMSDR ASAA2023052143329Platform · damaged1 PLATFORM ON #1 ENGINE DAMAGED. GROUNDED - YES. PLATFORM REPLACED PER ASA T/C 78472010 TEST 7 VIBE SURVEY B737-800 AMM 71-00-00 PB SO1 ACCOMPLISHED.
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