N579AS
Service difficulty reports · 587
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 = 'N579AS' 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 = 'N579AS' 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 ASAA2022083039742Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-23 DELAM. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 147A5810-23 IAW B737-800 SRM 53-00-50-2R0, SRM 53-00-50-2R2, SRM 53-00-50-2R1.SDR ASAA2022083039740Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-137 DELAM. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 147A5810-137 IAW B737-800 SRM 53-00-50-2R-0, 53-00-50-2R2, SRM 53-00-50-2R1.SDR ASAA2022081339769Floor Support · corrodedLEFT SIDE CABIN BETWEEN STATION -900 LBL -1 FLOOR BEAM HAS CORROSION. GROUNDED - YES. EVALED CORROSION.FASTENER HOLE ELONGATED BEYOND ALLOWABLE LIMITS IAW B737-800 SRM 53-70-51-1A-1.LOCATED DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW BOEING DWG 147A5700 REV B SDR ASAA2022081339768Door Sill · corrodedRIGHT SIDE CABIN STATION -993 RBL-45 DOOR SILL AREA HAS CORROSION. GROUNDED - YES. EVALED CORROSION. ORIG T .080"REMOVED .017".REMAINING .068"FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 DETAIL D.LOCATED DRILLED, AND INSTALLED NEW MOP SILL IAW BOEISDR ASAA2022081339767Pressure Deck · corrodedRIGHT SIDE CABIN STATION -988 RBL-44 PRESSURE DECK HAS CORROSION. GROUNDED - YES. EVALED CORROSION.ORIG T .040"REMOVED .008".REMAINING .032"FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 LOCATED DRILLED, AND INSTALLED NEW PRESSURE DECK / SHEAR WEB IASDR ASAA2022081339766Floorbeam · corrodedLEFT SIDE CABIN STATION -986 RBL - 30 T-CAP HAS CORROSION. GROUNDED - YES. EVALED CORROSION.ORIG T .150"REMOVED .060".REMAINING .090"FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 REMOVED ADJACENT STRUCTURE. ACCOMPLISHED FULL TCAP REPAIR IAW B737-800SDR ASAA2022081339765Support · corrodedRIGHT SIDE CABIN STATION 1014 RBL 31 AROUND AFT GALLEY MOUNT AREA HAS CORROSION. GROUNDED - YES. EVALED CORROSION.ORIG T .050"REMOVED .020".REMAINING .030"FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 DETAIL C.LOCATED DRILLED, AND INSTALLED NEW WALLSDR ASAA2022081339764Support · corrodedLEFT SIDE CABIN STATION -1014 LBL-31 AROUND GALLEY MOUNT AREA HAS CORROSION. GROUNDED - YES. EVALED CORROSION.ORIG T .050"REMOVED .024".REMAINING .026"FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 DETAIL C.LOCATED DRILLED, AND INSTALLED NEW WALL SUPSDR ASAA2022081339745Angle · corrodedR1 DOOR THRESHOLD SUPPORT STRAP - STA.312 THRU 344- UPPER SURFACE & ROUND FASTENER HOLES HAS AREAS OF SURFACE CORROSION .RED CIRCLED. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02.ORIG THICKNESS 0.080REMVOED 0.016REMAINING MAT 0.064FOUND TO BE OUSDR ASAA2022081339727Transition Panel · crackedAFT PIT R/H TRANSITION PANEL IS CRACKED AT STA 727J+14. (STREAMER ATTACHED). GROUNDED - YES. EVAL'D AFT PIT R/H TRAHSITION PANEL AT STA 727J+14 CRACK IS TO FASTENER HOLE, OUT OF LIMITS,REMOVED FROM STA 727J+12 - STA 767,LOCATE AND DRILLED USING MAT I.D. BAC 14SDR ASAA2022081339610Support Angle · corrodedAFT PIT R/H SHIELD SUPPORT P/N 146A8125-53 IS CORRODED. GROUNDED - YES. EVALUATED AFT PIT RH SHIELD SUPPORT P/N 146A8125-53ORIGINAL THICKNESS .050" PER BAC DWG 146A8123-18 REV A SHEET.MAT REMOVED .006',.044" REMAINING.OUT OF LIMITS PER B737-800 SRM 53-60-15-1ASDR ASAA2022081339557Transition Panel · crackedAFT PIT R/H TRANSITION PANEL IS CRACKED AT STA 727J+14. (STREAMER ATTACHED). GROUNDED - YES. EVAL'D AFT PIT R/H TRAHSITION PANEL AT STA 727J+14 CRACK IS TO FASTENER HOLE, OUT OF LIMITS,REMOVED FROM STA 727J+12 - STA 767,LOCATE AND DRILLED USING MAT I.D. BAC 14SDR ASAA2022081339552Intercostal · crackedFWD WET AREA: INTERCOSTAL BETWEEN BS 312 AND BS328 RBL 31 IS CRACKED AT FASTENER HOLES. GROUNDED - YES. REMOVED INTERCOSTAL IAW B737-800 SRM 51-40-02.LOCATED AND DRILLED NEW INTERCOSTAL IAW BOEING DRAWING 141A5400 REV-. INSTALLED NEW INTERCOSTAL IAW BOEING DRASDR ASAA2022081239739Floor Panel · delaminatedFLOOR PANEL P/N 141A5810-236 DELAM. GROUNDED - YES. REPAIRED DELAM ON FLOOR PANEL P/N: 141A5810-236 IAW B737-800 SRM: 53-00-50-2R-0 & 53-00-50-2R-7.SDR ASAA2022081239714Transition Panel · noneAFT PIT L/H TRANSITION PANEL PUNCTURED @ STA 747. GROUNDED - YES. EVALUATED AFT PIT L/H TRANSITION PANEL @ STA 747.PUNCTURE OUT OF LIMITS PER B737-800 SRM 53-00-53-1A-2 DUE TO PROXIMITY OF PUNCTURE TO FASTENER HOLE.REMOVED DAMAGED SECTION AT STA 727I TO STA 76SDR ASAA2022081239553Transition Panel · puncturedAFT PIT L/H TRANSITION PANEL PUNCTURED @ STA 747. GROUNDED - YES. EVALUATED AFT PIT L/H TRANSITION PANEL @ STA 747.PUNCTURE OUT OF LIMITS PER B737-800 SRM 53-00-53-1A-2 DUE TO PROXIMITY OF PUNCTURE TO FASTENER HOLE.REMOVED DAMAGED SECTION AT STA 727I TO STA 76SDR ASAA2022081139741Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-28 DELAM. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR TO FLOOR PANEL 147A5810-28 IAW B737NG SRM 53-00-50-2R-0.SDR ASAA2022081139738Floor Panel · delaminatedFLOOR PANEL P/N 141A5810-286 DELAM. GROUNDED - YES. REPAIRED DELAM ON FLOOR PANEL P/N:141A5810-28C IAW B737-800 SRM:53-00-50-2R-7, 53-00-50-2R-0.SDR ASAA2022081139737Floor Panel · delaminatedFLOOR PANEL P/N 141A5810-558 DELAM. GROUNDED - YES. REPAIRED DELAM ON FLOOR PANEL O/N: 141A5810-558 IAW B737-800SRM:53-00-50-2R-0 & 53-00-50-2R-7.SDR ASAA2022081139736Floor Panel · noneFLOOR PANEL P/N 141A5810-454 DELAM. GROUNDED - YES. REPAIRED DELAM ON FLOOR PANEL 141A5810-454 IAW B737-800SRM:53-00-50-2R-0 & 53-00-50-2R-7.SDR ASAA2022081139735Floor Panel · noneFLOOR PANEL P/N 141A5810-470 DELAM. GROUNDED - YES. REPAIRED DELAM ON FLOOR PANEL P/N:14185810-470 IAW B737-800 SRM:53-00-50-2R & 53-00-2R-7.SDR ASAA2022081139734Floor Panel · noneFLOOR PANEL P/N 141A5810-155 DELAM. GROUNDED - YES. REPAIRED DELAM ON FLOOR PANEL P/N:141A5810-155 IAW B737-800 SRM:53-00-50-2R-0 & 53-00-50-2R-7.SDR ASAA2022081139732Floor Panel · delaminatedFLOOR PANEL P/N 141A5810-175 DELAM. GROUNDED - YES. REPAIRED DELAM ON FLOOR PANEL 141A5810-175 IAW B737-800 SRM 53-00-50-2R AND 53-00-50-2R-7.SDR ASAA2022071239057Start Valve · degraded#2 ENGINE SLUGGISH TO START. N2 ACCELERATES TO 21-22% IN OVER 30 SEC AND DOES NOT INCREASE BEYOND THAT WITHIN THE START PARAMETERS. EGT T NORMAL DURING START. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE START VALVE REF B737-800 AMM 80-11-03. OPS CHECK GOOD.SDR ASAA2022071139027Detector · faulty#1 ENGINE S3 EGT SHOWS DASHES. GROUNDED - YES. REMOVED AND REPLACED S3 DETECTOR REF. B737-800 AMM 77-21-01. REMOVED AND REPLACED CJ10 HARNESS REF. AMM 73-21-06.SDR ASAA2022071038989Overheat · warning lightON CLIMBOUT, L SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED, ACCOMPLISHED QRH & LIGHT EXTINGUISHED. GROUNDED - YES. PERFORMED BITE TEST OF WHCU IAW B737-800 FIM 30-41 TASK 801. NO CURRENT FAULTS PRESENT.SDR ASAA2022061138615Heater · warning lightLEFT SIDE WINDOW HEAT OVERHEAT LIGHT CAME ON DURING FLIGHT QRH DIRECT US TO TURN OFF (FOR 5 MINS) THEN TURN BACK ON, OVERHEAT LIGHT EXTINGUISHED. OPERATED NORMAL FOR REST OF FLIGHT. QRH DIRECTED INFORMATION ONLY WRITE UP. GROUNDED - YES. PERFORMED OPERATIONAL SDR ASAA2022051638352Radar · failedPWS FAIL AND WXR FAIL INDICATED ON F/O ND. GROUNDED - YES. ACCOMPLISHED A/C POWER RESET PER B737-800 AMM 20-60-01. ACCOMPLISHED WXR OPS TEST PER AMM 34-43-00. OPS CHECKS NORMAL.SDR ASAA2022051638351Cover · missingFA REPORTS EXIT SIGN COVER BY L2 DOOR MISSING. GROUNDED - YES. REPLACED COVER REF B737-800 AMM 33-51-01.SDR ASAA2022050838240Fmc · faultedON TAXI IN WE NOTICED WE LOST BOTH FMC'S AND ALL DATA. GROUNDED - YES. VERIFIED F/H FMC HAD A PGM FAULT, R/H FMC NO FAULTS LAST FLT. REF B737-800 FIM 34-61 TASK 801 & 807 ACCOMP FMC'S BOTH C/B CYCLING OPEN & CLOSED. ACCOMP SENSOR TEST, BOTH FMC'S SHOW OK REF BSDR ASAA2022050338193Blower · inoperativeREF AD20211420-MULTI-21-1. FOUND WEATHER RADAR COOLING BLOWER INOP. GROUNDED - YES. REPLACED WEATHER RADAR T/R MOUNT BLOWER ASSY WITH SERVICEABLE UNIT. OPS CHECKS OK. WEATHER RADAR SYS OPS TEST OK. REF B737-800 AMM 34-43-51.SDR ASAA2022042838155Spacer · unknownPER T/C 78472010 #2 ENG. FAN BLADE LUBE SPACERS # 4, 5, 7, 8, 9, AND 22 ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FAN BLADE SPACERS # 4, 5, 7, 8, 9, AND 22 REF T/C 78472010.SDR ASAA2022042838154Platform · unknownPER T/C 78472010 #2 ENG. FAN BLADE LUBE PLATFORM #8 PN 340-001-817-0 NOT PAIRED 180 DEGREES APART. GROUNDED - YES. REMOVED AND REPLACED ENG #2 FAN BLADE PLATFORM #8, NEW PART #340-001-816-0, PLATFORMS NOW PAIRED REF ASA T/C 78472010.SDR ASAA2022042838152Unknown · wornPER T/C 78472010 #2 ENG FAN BLADE LUBE FRONT SPINNER CONE 6 WASHER GROOVES ARE WORN. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FRONT CONE WASHER REF ASA T/C 78472010. REMOVED AND REPLACED #2 ENG FRONT SPINNER CONE BOLTS SAME REF.SDR ASAA2022042338103Lamp · failedTASK CARD 78233008 - FLT DECK EMERGENCY DOME LT IS VERY DIM. GROUNDED - YES. RELAMPED FLT DECK EMERGENCY DOME LT, OPS CHECKS OK. REF B737-800 AMM 33-51-00.SDR ASAA2022041838140Switchpack · warning light#2 ENGINE "REVERSER" LIGHT ILLUMINATED ON ON OVERHEAD PANEL. GROUNDED - YES. REMOVED AND REPLACED R/H AUTOTHROTTLE SWITCHPACK REF B737-800 AMM 76-11-07/401. OPS CHECK OK. REMOVED 4 SLEEVE PINS, REMOVED LOCKWIRE FROM #2 T/R HANDLE, RESET 2 C/BS.SDR ASAA2022040237873None · inoperativeFMC SCREEN BLANKED W/ FAULT LIGHT AFTER 3-5 SECONDS FMC ACTIVATED W/ BLUE LINE THROUGH SCREEN. GROUNDED - YES. REMOVED AND REPLACED FO'S FMC CDU REF B737-800 AMM 34-61-01. OPS CHECK GOOD.SDR ASAA2022030637656Modulating Valve · inoperativeUPON OPS PROCEDURE FOR MEL 21-21G, RIGHT PACK LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED TROUBLESHOOTING PER B737-800 FIM TASK 21-62-00-810-831 FOUND RIGHT TEMP CONTROL VALVE BAD. REMOVED AND REPLACED RIGHT TEMP CONTROL VALVE IAW B737-800 21-51-10. PERFORMEDSDR ASAA2022030537658Modulating Valve · inoperativeAFTER PUSH BACK AND COMPLETION OF "AFTER START" CHECKLIST ON - RECALL MASTER & CONT CAB ZONE TEMP LIGHT ILLUMINATED CAUTION. GROUNDED - YES. PERFORMED TROUBLESHOOTING PER B737-800 FIM TASK 21-62-00-810-831 FOUND RIGHT TEMP CONTROL VALVE BAD. REMOVED AND REPLASDR ASAA2022020737399Modulating Valve · faultyCONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. CONFIRMED FAULT, #2 PACK/ZONE TEMP CONTROLLER SHOWS "FLIGHT DECK TCV (V143) FAIL & CONT CAB ZONE TEMP LIGHT ILLUMINATE WHEN RECALL. REMOVED & REPLACED SAME PERSDR ASAA2022020637378Hmu · faultyWHILE PERFORMING TASK CARD 78273000, #1 ENG HAS SHORT TIME FAULT 73-30351 THE FMV POSITION SIGNAL DISAGREE, ON MULTIPLE FLIGHT LEGS. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 73-25 TASK 804, ALL CONTINUITY CHECKS GOOD. REMOVED AND REPLACED HMU PER TASK CARDS NSDR ASAA2022013037302Start Valve · inoperative#1 START VALVE WON'T OPEN. GROUNDED - YES. REMOVED & REPLACED #1 START VALVE PER B737-800 AMM 80-11-03. OPS CHECK GOOD.SDR ASAA2022011537152Unknown · unknownR PACK LT ILLUMINATED ON RECALL. GROUNDED - YES. C/W BITE PROCEDURE B737-800 FIM 21-62-TASK 801 FOR LEFT AND RIGHT PACK / ZONE TEMPERATURE CONTROLLERS, R PACK TCV LIGHT ON PREV FLT, GREEN ON VERIFY AND RESET. C/W FIM 21-62 TASK 831 RIGHT PZTC-2 RESET. FOUND DISDR ASAA2022011437162Unknown · unknownL2 WINDOW OVERHEAT LIGHT ILLUMINATED. ACCOMP QRH PROCEDURE-LIGHT REMAINED OFF AFTER 5 MIN COOLING PERIOD. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 30-41 TASK 801 PERFORMED BITE CHK, GOOD. NO DEFECTS NOTED.SDR ASAA2021111736680Engine · faulty#1 ENGINE TREND DATA SHOWS A SHIFT IN DEGT, HDM, DELTA FUEL FLOW, DELTA CORE SPEED AND VSV POSITION DIVERGENCE WITH EXCESSIVE VSV SCATTER. (#PRI1/ETOPS)SEA ONLY. GROUNDED - YES. REMOVED BORESCOPE PLUGS 2 THROUGH 9, BORO PLUG 13,15 AND 17. REMOVED DRIVE PAD COVSDR ASAA2021111136557Coupler · failedHF 1 TRANSMIT AND RECEIVE NORMALLY HF2 UNABLE TO TRANSMIT OR RECEIVE. GROUNDED - YES. REMOVED AND REPLACED #2 HF COUPLER IAW B737-800 AMM 23-11-61/401. VERIFIED #2 HF TRANSMIT AND RECEIVED OK ON GROUND.SDR ASAA2021110936561Transceiver · failedIN FLIGHT UNABLE TO XMIT ON EITHER HF. RETUNED NUMEROUS TIMES, MADE CONTACT W/SFO AIRINC AND 2 GOOD SELCALS. DURING FLIGHT HOURS IN, RETRIED HF 2 & HF1 RECEIVE BUT ONLY HF 2 XMITTED INTERMITTENTLY. GROUNDED - YES. CYCLED POWER TO BOTH HF'S #1 HF OPS RESTORED, SDR ASAA2021102936449Unknown · unknownHF 2 WILL RECEIVE BUT NOT TRANSMIT. GROUNDED - YES. (RESOLVED ON W/O: 1889819 TASKCARD: N/R-00001 ) ACCOMPLISHED HF OPS CHECK REF B737-800 AMM 23-11-00 COULD TRANSMIT AND RECEIVE CLEARLY WITH NO FAULTS FOUND. ACCOMPLISHED BITE CHECK OF HF #2 TRANSCEIVER WITH NSDR ASAA2021101636324Lens · detachedL/H FWD OVERWING EXIT, EXIT SIGN COVER MISSING. GROUNDED - YES. INSTALLED NEW EXIT SIGN COVER. OPS CHECK GOOD.SDR ASAA2021101336279Shim · wornWHILE PERFORMING FAN LUBE T/C 78472010 ON #1 ENGINE FOUND ALL SHIMS TO HAVE MOLYDAG COATING LOSS BETWEEN 25 TO 100%. GROUNDED - YES. REINSTALLED EXISTING SHIMS DUE NO NEW SHIMS AVAILABLE. SHIMS OK TO REMAIN IN SERVICE REF B737-800 AMM 72-21-02 SECTION L. REPL
Back to N579AS