N529AS
Service difficulty reports · 344
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 = 'N529AS' 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 = 'N529AS' 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 ASAA2022111740867Rub Strip · debondedREF ASA T/C 78472010 #1 ENG. CFM56-7 FAN BLADE LUBRICATION. FOUND PLATFORM #8 HAS BOTH RUBSTRIPS DEBONDED HALF WAY DOWN. #8 IS PRE-SERVICE (816) REQ #20 TO BE REPLACED. GROUNDED - YES. REPLACED #8 AND #20 PLATFORM IAW T/C 78472010 STEP 1.C.(3) AND 1.A.(35). (8SDR ASAA2022111540788Warning Flag · false activationFLIGHT CREW REPORTS VTK ON F.O. DISPLAY. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 836. OPS CHECK GOOD.SDR ASAA2022111540782Fmc · failedSINGLE FMC OPERATION ON SCRATCH PAD AFTER BOTH ENGINES STARTED. F/O HAS VTK FLAG AND MAP FLAG ON NAV DISPLAY. GROUNDED - YES. REMOVED & REPLACED #2 FMC PULLED & RESET 2 ASSOCIATED C.B.'S B737-800 AMM 34-61-02 OPS TEST NORMAL.SDR ASAA2022111240747Fmc · faultedSINGLE FMC "VTK" ON FO'S SIDE. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 835. DUAL FMC RESTORED.SDR ASAA2022100540182Fmc · failedVNAV INOP. DURING CRUISE ATC GAVE US ALTITUDE CHANGE. UPON REACHING CRUISE ALTITUDE VNAV DROPPED OFF AND UNABLE TO SELECT. FMC CLIMB PAGE WAS BLANK AND UNABLE SELECT ALTITUDE IN REQUIRED BOX. FMC UNABLE TO COMPUTE ETA'S AND FUEL CONSUMPTION ESTIMATES. GROUNDEDSDR ASAA2022072039143Circuit Breaker · noneDURING AFTER T/O CHECKLIST, WHEN LANDING GEAR IN OFF POSITION, RED NOSE GEAR ANNUNCIATOR ON. NOSE GEAR DOWN AND LOCKED. GEAR CAME BACK UP W/2ND UP LEVER. GROUNDED - YES. 20 CBS PULLED AND NOSE OF AIRCRAFT JACKED UP REF B737-800 AMM 07-11-21-580-801. PERFORMED SDR ASAA2022061838690Autothrottle Sys · faultedON TAKE OFF ROLL AFTER PRESSING TOGA #1 THRUST LEVER ADVANCED AND #2 DID NOT. A/T DISENGAGED. RE-ENGAGED WITH SAME RESULT. GROUNDED - YES. COMPLETED BITE TEST OF AUTO THROTTLE AMM 21-31 TASK 801 RESET FCC-A AS PER TEST RESULTS, SECOND BITE TEST ATTEMPT PASSED.SDR ASAA2022052338432Fmc · faultedFMC DISAGREE ON GROUND, RESOLVED PER QRH PROCEDURE. GROUNDED - YES. RESOLVED PER QRH RESET PROCEDURE.SDR ASAA2022051538340Lamp · failedTHE FA REPORTS THE LIGHTS THAT ILLUMINATE THE EMERGENCY EXIT AT 17A ARE INOP. GROUNDED - YES. RELAMPED SIDEWALL LIGHT ON EMERGENCY EXIT @ 17A AS REQUIRED. OPS TEST NORMAL.SDR ASAA2022051138322Harness · faultyFLT CREW REPORTS #2 ENG FIRE DETECTION FAILS TEST - B LOOP INOP. GROUNDED - YES. ON DEFERRAL.
FLT CREW REPORTS #2 ENG FIRE DETECTION FAILS TEST - B LOOP INOP. GROUNDED - YES. CONFIRMED FAULT, #2 ENGINE B-LOOP INOP. REPAIRED R/H CORE DETECTOR HARNESS WIRING TESDR ASAA2022042738146Unknown · failedAFTER ENGINE START, NO VOLTS/FREQS ON #1 GENERATOR. GROUNDED - YES. REMOVED AND REPLACED # 1 IDG IAW B737-800 AMM 24-11-11 . OP CHECK/ LEAK CHECK GOOD .SDR ASAA2022040937967None · leakingON PUSHBACK WHILE STARTING #2 ENGINE RAMP REPORTED EXCESSIVE FUEL LEAKING FROM ENGINE SHUT DOWN WAS NORMAL. GROUNDED - YES. INSPECTED ENG DRAINS REFB737-800 AMM 71-71-00. NO LEAKS N0TED WITH ENGINE OFF. FUEL PUMP PAD DRAIN LEAKS 3 DROPS PER MINUTE ENG RUNNING.SDR ASAA2022022437579Unknown · unknownIFSD DISPLAYS OUT OF ORDER. GROUNDED - YES. AIR TURNBACK - DIVERSION TIME 83 MINUTES. T/S IAW B737-800 FIM 34-24 TASK 810. DETERMINED TO BE INTERMITTENT FAULT. PERFORMED ISFD OPS CHK IAW B737-800 AMM 34-24-02. OPS CHK OK.SDR ASAA2022012637270Unknown · unknownCONT CABIN ZONE TEMP ON RECALL CLEARS WHEN RESETTING MASTER CAUTION. GROUNDED - YES. FOUND PZTC 2 FLT DECK TRIM VALVE FAULT-CLEARED ON VERIFY REFB737-800 FIM 21-62 TASK 832.SDR ASAA2022011037120Flange · crackedFLANGE ASSEMBLY ON #2 ENGINE HAS CRACKS WERE THE BOLTS ATTACH. GROUNDED - YES. REMOVED AND REPLACED # 2 ENG AFT FLANGE ASSY REF B737-800 AMM 72-56-00-400-801-F00.SDR ASAA2022010837098Unknown · unknownLEFT FMC FAILURE DURING FLIGHT. DID NOT COME BACK ON. GROUNDED - YES. CONFIRMED. OPENED, RESET 1 EA C/B ON P18-2 L/H FMC. L/H FMC NOW OPS NML REF B737-800 FIM 34-61 TASK 810. ETOPS GROUND VERIFICATION SUCCESSFUL.SDR ASAA2021122537000Unknown · unknownSPEED TRIM FAIL LIGHT ILLUMINATED. (GROUND MAINT. WRITE-UP). GROUNDED - YES. ACCOMPLISHED DFCS BITE SPEED & STAB TRIM, FOUND ELEV POS SEN-2 FAULT. RESEATED POSN SEN-2 PLUG RAN BITE AGAIN PASSES NORMAL NO FAULTS BUT SPEED TRIM FAIL ILLUMINATES AGAIN REF B737-80SDR ASAA2021120736867Fire Loop · no testDURING OVERHEAT DETECTION/FIRE TEST, #1 ENGINE WOULD NOT ILLUMINATE ON LOOP B. LOOP A OPERATES NORMALLY. GROUNDED - YES. PERFORMED OPERATIONAL TEST OF OVERHEAD FIRE DETECTION. PERFORMED ENGINE FIRE DETECTION BITE PROCEDURE B737-800 FIM 26-10 TASK 801, NO FAULSDR ASAA2021102136381Detector · noneAPU DET INOP LIGHT ILLUMINATED. GROUNDED - YES. REMOVED AND REPLACED APU OVERHEAT DETECTOR ASSEMBLY (TAILCONE) REF B737-800 AMM 26-15-01. REVERSED MAINT PROC FOR MEL 26-8D. OPS CHECK GOOD. ALL TEST PASS REF AMM 26-15-00. THIS CLEARS MEL 26-8D C/N: 21024529 SEASDR ASAA2021100736218None · leakingDURING WALK AROUND NOTED #1 IDG OIL COOLER LEAKING. GROUNDED - YES. REMOVED & REPLACED #1 ENG IDG OIL COOLER REF M/M 73-11-06 LEAK CKS GOOD.SDR ASAA2021092936107Platform · tornPER T/C 78472010 #1 ENG FAN BLADE LUBE #9 PLATFORM SIDE IS TORN. GROUNDED - YES. REMOVED AND REPLACED #1 ENG #9 PLATFORM REF T/C 78472010.SDR ASAA2021092936106Blade · nonePER T/C 78472010 #1 ENG FAN BLADE LUBE #6 FAN BLADE CU-NI-IN COATING IS MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #6 FAN BLADE REF T/C 78472010.SDR ASAA2021092936105Blade · nonePER T/C 78472010 #1 ENG FAN BLADE LUBE #14 FAN BLADE CU-NI-IN COATING IS MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #14 FAN BLADE REF T/C 78472010.SDR ASAA2021092936104Blade · nonePER T/C 78472010 #1 ENG FAN BLADE LUBE #10 FAN BLADE CU-NI-IN COATING IS MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #10 FAN BLADE REF T/C 78472010.SDR ASAA2021092936103Blade · nonePER T/C 78472010 #1 ENG FAN BLADE LUBE #24 FAN BLADE CU-NI-IN COATING IS MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #24 FAN BLADE FOR WEAR, REMOVED #12 AS A PAIR REF T/C 78472010.SDR ASAA2021092936102Blade · nonePER T/C 78472010 #1 ENG FAN BLADE LUBE #18 FAN BLADE CU-NI-IN COATING IS MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #18 FAN BLADE REF T/C 78472010.SDR ASAA2021091735977Terminal · brokenWHILE CHANGING FUEL NOZZLES, FOUND BROKEN TERMINAL LUG ON WIRE HARNESS. GROUNDED - YES. REMOVED AND REPLACED WIRE HARNESS MW0326 ON #1 ENGINE REF B737-800 AMM 26-11-02. ACCOMPLISHED ENGINE FIRE DETECTION OPERATIONAL TEST, NO FAULTS NOTED, REF AMM 26-11-00-710-SDR ASAA2021082835825Switch · faulty#1 REVERSER LIGHT ILLUMINATED ON OVERHEAD PANEL AFTER START. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 75-32 TASK 812. NO FAULTS FOUND. REMOVED AND INSTALLED NEW #1 SWITCH PACK ASSEMBLY PER B737-800 MM 76-11-07/401, OPS NORMAL. GROUND VERIFICATION SUCCESSFUL. SDR ASAA2021082635805Outflow Valve · failedONE HOUR INTO CRUISE AT FL380 CABIN PRESSURIZATION SUDDENLY WENT TO 3500-4000 FPM DESCENT FOR APPROXIMATELY 20 SECONDS . DURING THIS TIME THE CABIN DIFFERENTIAL ROSE FROM BOTTOM OF "ORANGE BAND" TO JUST BELOW "RED MAX" LINE. CONTINUED FLT AT FL340; ACFT CONTINSDR ASAA2021080735659O-Ring · worn#1 ENGINE OIL TREND DATA SHOWS OIL CONSUMPTION TREND INCREASING ON RECENT FLIGHTS. GROUNDED - YES. ACCOMPLISHED STEP 1 OF TSR FOUND #1 ENGINE DRY PAD LEAKING, AND FOUND OUTER SEALS ON LUBRICATION UNIT LEAKING. REMOVED AND REPLACED #1 ENG DRY PAD "O" RINGS PERSDR ASAA2021072135461Module · faultyLANDING GEAR EXTENDED WHEN LANDING GEAR LEVER WAS MOVED TO THE OFF POSITION DURING THE AFTER TAKE CHECK LIST. RAN THE GEAR DISAGREE QRH AND GEAR RETRACTED NORMALLY. LANDING GEAR LEVER WAS LEFT IN THE UP POSITION IN ACORDANCE TO THE CHECKLIST. GROUNDED - YES. DSDR ASAA2021070335242Fmc · malfunctionedIN CLIMB OUT WITH FO F/D ON MASTER VNAV DISENGAGED AND LNAV TRACK DISAPPEARED FROM FO NAV DISPLAY. "SINGLE FMC OPERATION" IN FO SCRATCHPAD WITHOUT ANY INDICATIONS OTHER THAN FMC P/RST. FMC RESTORED ON ITS OWN WITHIN APPROX 3 MIN. GROUNDED - YES. DFCS HISTORY BSDR ASAA2021062135164Sensor · faultedDURING TASK CARD #78273000 ACCOMPLISHMENT, FOUND FAULT CODE 77-11172 ON # 2 ENGINE, THE N1 SIGNAL IS OUT OF RANGE, THIS IS A LONG TIME FAULT. GROUNDED - YES. VERIFIED DEFECT, FAULT LOGGED ON EVERY LEG. REMOVED AND REPLACED #2 ENG N1 SPEED SENSOR REF B737-800 ASDR ASAA2021061635111Pump · leaking#1 HYD ENG PUMP IS LEAKING 1 DROP PER MINUTE. YOU ARE ALLOWED 1 DROP EVERY 10 MINS. LEAKING AT CASE HALF. ENG HYD PUMP NEEDS TO BE REPLACED. GROUNDED - YES. REMOVED POWER FROM A&B HYD SYSTEM PER B737-800 AMM 29-11-00-860-805. DEPRESSURIZATION OF HYD RESERVOIRSSDR ASAA2021040634524Transceiver · failedWXR FAIL INDICATION ON BOTH CA & RO ND'S WHEN WXR IS SELECTED ON THE EFIS CONTROL PANELS. NO TEST PATTERN OBSERVED WHEN TESTIS SELECTED ON THE WEATHER RADAR CONTROL PANEL. GROUNDED - YES. (RESOLVED ON W/O: 1869328 TASKCARD: N/R-00001 ) REMOVED AND REPLACED WEASDR ASAA2021040334503Lamp · burned outEMERG EXIT LIGHT @ 9 LH/OVHD BIN INOP. GROUNDED - YES. RELAMPED EMERGENCY EXIT LIGHT AT 9 LH OVERHEAD BIN AND OPS TESTS GOOD IAW B737-800 AMM 33-51-03-960-801.SDR ASAA2021030834460Transition Panel · corrodedAFT PIT LEFT FLOOR TRANSITION PANEL HAS CORROSION THROUGHOUT BS727 -BS787. GROUNDED - YES. CUSTOMER REF. ONLY; SEE CUSTOMER CARDS G1553675, G153678, G1553679, G1553682AND G1553752 FOR MAT ORIG. LOSS AND REMAINING TRACKING PURPOSES. REMOVED LEFT TRANSITION PASDR ASAA2021030434459Cargo Track · corrodedAFT CARGO COMPARTMENT BILGE INT, FLOOR SUPPORT RAIL HAS CORROSION IN SEVERAL SPOTS, BS787-807, RBL13.84. GROUNDED - YES. REMOVED DAMAGED TRACK; FABRICATED NEW TRACK AND INSTALLED NEW TRACK PER B737-800 SRM 53-00-53-2R-3. BLENDED CORROSION ON TRACK AT BL-13.84SDR ASAA2021030334483Floorbeam · corrodedCORROSION ON FLOORBEAM STA 947.5 JUST O/B OF LAV D INBOARD AFTMOUNT FITTING. DOT Z617. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-70-51-1A.1. ORIG MAT. IS .180, REMAINING MAT IS .095. MAT LOSS OF .085 IS BEYOND ALLOWABLE LIMITS. REMOVEDUPPER T-CAP CSDR ASAA2021030334439Floorbeam · corrodedFLOORBEAM AT STATION 986 @R2 DOOR AREA CORRODED AT MOUNT FITTING. GROUNDED - YES. REMOVED DAMAGE PER B737-800 SRM 53-70-15 ORIG THICKNESS .040, MAT LOSS .015NEW THICKNESS .025, AREA OUT OF LIMITS PER B737-800 SRM 53-70-15. REMOVED WEB PER B737-800 SRM 51-40-02SDR ASAA2021030334438Floorbeam · corrodedMAIN CABIN AFT @ L2 DOOR. FLOORBEAM CORRODED AT STATION 986. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 53-70-51. ORIG MAT IS .150, REMAINING MAT IS .103. MAT LOSS OF .047 IS BEYOND ALLOWABLE LIMITS. REMOVED UPPER T-CAP CHORD AND INSTALLED NEW T-CAP CHSDR ASAA2021030334316Floor Support · corrodedAFT WET AREA INTERCOSTAL HAS A GOUGE JUST FWD OF FLOORBEAM AT STA 967 RBL16 DOT N253DOT:N253. GROUNDED - YES. REMOVED CORROSION - ORIGINAL THICKNESS .080, REMOVED .025, REMAINING .055 AND FOUND TO BE OUT OF LIMITS IW B737-800 SRM 53-70-51-1A-1. REMOVED AND REPSDR ASAA2021030334315Mount · corrodedMAIN CABIN AFT RIGHT HAND SIDE @ OR ABOUT STATION 1016 GALLEY MOUNT RAILCORRODED.DOT: N166. GROUNDED - YES. REMOVED CORROSION - ORIGINAL THICKNESS .050, REM0VED .025, REMAINING .025 AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-15. REMOVED AND REPLACED SDR ASAA2021030334314Web · corrodedAFT CARGO DOOR LOWER CUT OUT HAS CORROSION STA.787 TO STA.847 AS MARKED.DOT:C570. GROUNDED - YES. REMOVED CORROSION FROM LOWER SILL UPPER WEB ORIG. THICKNESS 0.050, REMOVED 0.050, 100% MAT LOSS FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-60-15-1A-1; REMOVED SDR ASAA2021020834063Warning Light · false activationAFTER PUSH, FO FD AMBER FLAG ILLUMINATED ALONG WITH MCP ALTITUDE GOING TO 50,000 AND COULD NOT BE MOVED. AFTER ENGINE START TO TAXI BACK IN, CONDITIONS RETURNED TO NORMAL. GROUNDED - YES. ELEC PWR SWITCHOVER - DFCS NO FAULT/FAULT HISTORY - DFCS AND FMCS R-T-S SDR ASAA2021012933979Warning Message · false activationON TAKEOFFROLL AFTER HITTING TOGA BUT BEFORE ENGINES WERE STABILIZED AT 2TK BUMP POWER, THE MASTER CAUTION LIGHT ILLUMINATED. AFTER A VERY QUICK SCAN OF THE OVERHEAD PANEL, CAPT ABORTED TAKEOFF. NO ASSOCIATED LIGHTS ON THE SIX-PACK AND NO LIGHTS ON OVERHEAD PASDR ASAA2021012733975Modulating Valve · faultyAFTER ENGINE START FOLLOWING MASTER CAUTION RECALL, THE CONT CABIN ZONE TEMP LITE ILLUMINATED. THIS LIGHT EXTINGUISHED ON MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED CONTROL CABIN TRIM AIR MODULATING VALVE REF B737-800 AMM 21-61-21. LEAK CHESDR ASAA2020121333698Fcu · faultedAPU FAILED TO START, MTX FAULT MESSAGE 49-31016. GROUNDED-YES. REMOVED AND REPLACED APU FUEL CONTROL UNIT, PER B737-800 AMM 49-31-11. OPERATIONS AND NO LEAKS NOTED.SDR ASAA2020092933238Warning Message · false activationAFTER STARTING BOTH ENGINES, THE MESSAGE PWS FAIL APPEARED ON BOTH F/O AND CAPT WHEN F/O SELECTED WXR INSTEAD OF TERR. THEN WXR FAIL MESSAGE APPEARED AS WELL. AT ONE POINT DURING POWER SWAPS TO THE APU, THE ERROR MESSAGE RT APPEARED BELOW THE WXR FAIL. GROUSDR ASAA2020092533226Bleed Valve · no testREF TC N8010004 ITEM F(6). NR 1 ENG BLEED AIR CROSSOVER CHECK FAILED. GROUNDED-YES. ACCOMPLISHED GVI OF ENGINE BLEED AIR DUCTS RELATIVE TO THE CORE FOR LOOSE SENSE LINES OR POSSIBLE LOOSE CLAMPS, NONE FOUND. ACCOMPLISHED TASK CARD NUMBER NG-36WC-00001 ENGI
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