N566AS
Service difficulty reports · 575
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 = 'N566AS' 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 = 'N566AS' 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 ASAA2023073044320Unknown · unknownFWD CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL. LIGHT EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. GROUNDED - YES. (RESOLVED ON W/O: 1963596 TASKCARD: N/R-00001 ) RAN BITE PROCEDURE PER F.I.M MANUAL 21-62 TASK 801 NO CURRENT FAULTS FOUND AT THIS TIME. NO HSDR ASAA2023070843988Valve · faultedTECH SERVICES FOLLOW UP REQUEST FOR FREQUENT #2 IDG SERVICING(#PRI2/ETOPS) ****** ETOPS SIGNIFICANT SYSTEM *******. GROUNDED - YES. (RESOLVED ON W/O: 1961078 TASKCARD: N/R-00002 ) AFTER ACCOMPLISHING #2 ENGINE IDG FILTER AND OIL CHANGE PER T/C 7842400. REMOVEDSDR ASAA2023060143423Blade · peelingREF ASA T/C # 78472010 CFM56-7 FAN BLADE LUBRICATION FOUND #2 PLATFORM RUBBER SEAL PEELED OFF. GROUNDED - YES. REMOVED AND REPLACED TWO PLATFORMS ON THE #2 ENGINE PER TASK CARD 78472010 AND PERFORMED VIBRATION SURVEY PER B737-800 AMM 71-00-00. CHECKS GOOD.SDR ASAA2023052243331Eec · inoperative# 2 ENGINE SHORT TIME MSG# 73-11282 (NOT ENERGIZED WITH ALTERNATOR VOLTAGE) DEFER PER ASA T/C # 78273000. GROUNDED - YES. C/W BITE TEST OF ENG #2 EEC = FC 73-11282 EEC CHANNEL IS NOT ENERGIZED WITH THE ALTERNATOR VOLTAGE, 73-20012 / INTERNAL EEC FAULT, & 73-20SDR ASAA2023052243324Switch · faulty#2 AFT FUEL PUMP LOW PRESSURE LIGHT NOT ILLUMINATED WITH #2 AFT PUMP OFF. GROUNDED - YES. REMOVED AND REPLACED PRESSURE SWITCH OF THE RIGHT AFT FUEL BOOST PUMP REF B737-800 AMM TASK 28-42-11-420-801.SDR ASAA2023050143070Unknown · unknownWHILE PERFORMING ASA T/C 78273000 FOUND LONG TIME FAULT 73-20042 ENGINE #2 INTERNAL EEC FAULT. GROUNDED - YES. ACCOMPLISHED EEC TEST REF B737-800 AMM 73-21-00-700-804-F00. NO FAULTS FOUND IN RECENT OR FAULT HISTORY.SDR ASAA2023050143069Unknown · unknownWHILE PERFORMING ASA T/C 78273000 FOUND SHORT TIME FAULT 73-20012 ON ENGINE #2 INTERNAL EEC FAULT. GROUNDED - YES. ACCOMPLISHED EEC TEST REF B737-800 AMM 73-21-00-700- 804-F00. NO FAULTS IN RECENT OR FAULT HISTORY. RELOADED EEC SOFTWARE REF AMM 73-21-60-470-8SDR ASAA2023042743056Panel · delaminatedREF ASA T/C #78472000 #1 ENG. INLET AND FAN BLADES - DETAILED INSPT. FOUND #5 I/B AT 5 O'CLOCK POS. STRUT PANEL HAS 1 EACH FASTENER INSERT DELAMINATED FROM PANEL. (M) ALF AFT UPPER INSERT. GROUNDED - YES. REMOVED AND REPLACED #5 FAN DUCT PANEL REF B737-800 AMMSDR ASAA2023042243004Unknown · unknownWHILE PERFORMING T/C 78273000 FOUND LONG TIME FAULT 73-20042 ON #2 ENGINE INTERNAL EEC FAULT. GROUNDED - YES. ACCOMPLISHED TASK CARD #7827300 NO CURRENT AND FAULT HISTORY FOR ENG #2. PER B737-800 FIM 73-21 TASK 801 THE FAULT WAS INTERMITENT FAULT. PERFORMED GOSDR ASAA2023042243003Unknown · unknownWHILE PERFORMING TASK CARD 78273000 FOUND SHORT TIME FAULT 73-20012 ON #2 ENGINE ENGINE INTERNAL EEC FAULT. GROUNDED - YES. ACCOMPLISHED TASK CARD #7827300 NO CURRENT AND FAULT HISTORY FOR ENG #2. PER B737-800 FIM 73-21 TASK 801 THE FAULT WAS INTERMITTENT FAULSDR ASAA2023033142666Unknown · unknownFC GALLEY GUST LOCK- DIFFICULT TO DEPRESS LATCH- HAD TO JIMMY DOOR. GROUNDED - YES. OPS CHECK FC GALLEY GUST LOCK. OPS CHECK GOOD NO DEFECTS NOTED.SDR ASAA2023031442362Unknown · unknownAUTOPILOT B WOULD NOT ENGAGE IN CLIMBOUT. GROUNDED - YES. FOUND "AFCS SYS B ENGAGE INTLK" C/B (P6-2 B4) OPEN. PERFORMED GVI OF C/B, NO DEFECTS NOTED, RESET C/B REF B737-800 AMM 20-60-01. PERFORMED B737-800 FIM 22-11 TASK 856, FOUND MAINTENANCE MESSAGE 22-11282SDR ASAA2023030442744Start Valve · faulty#1 ENGINE WOULD NOT START. GOOD DUCT PRESSURE AT 38 PSI BUT NO ROTATION WHEN STARTER WAS ENGAGED. GROUNDED - YES. REMOVED AND REPLACED #1 ENG START VALVE REF IAW B737-800 AMM 80-11-03.SDR ASAA2023022842167Unknown · unknownON RECALL, OBSERVED AMBER " ZONE TEMP" ON CONT CABIN. GROUNDED - YES. ZONE TEMP CONT-2 SHOWS FLT DECK TRIM VALVE ON BIT & PREV FLT, GREEN GO FOR VERIFY, MSG REST. RAN PACKS RE-CONFIRM BITE, OPS NML NO HISTORY PAST 30 DAYS.SDR ASAA2023021842023Indicator · inoperativeRIGHT WING #2 TANK INDICATOR ON RE-FUELING PANEL IS NOT FUNCTIONING. GROUNDED - YES. REMOVED AND REPLACED #2 REFUEL QUANTITY INDICATOR. IAW B737-800 AMM 28-41-61. OPS CHECK GOOD.SDR ASAA2023021841988Unknown · unknownRIGHT WING, #2 FUEL TANK RE-FUELING PANEL INDICATOR IS NOT FUNCTIONING. GROUNDED - YES. FOUND RIGHT WING #2 FUEL TANK REFUELING PANEL INDICATOR BLANK NOT DISPLAYING. PERFORMED RESET OF #2 FUEL TANK INDICATION REF B737-800 AMM 28-00-00. OPS CK GOOD.SDR ASAA2023021441938None · faultyON LANDING RECEIVED "SINGLE FMC OPERATION" SCRATCHPAD MESSAGE. FO ND SHOWED MAP FLAG, VTK, NO ANP/RNP. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 801 FOUND R FMCS FAILED PREVIOUS FLT LEGS, REPLACED NEW FMCS #2 WITH TRANSFERRED & VERIFIED SOFTWARE, UPDATSDR ASAA2023021341937Unknown · unknownF/O NAV DISPLAY SHOWS MAP FLAG. NO ANP/RNP NO VSPD FLAG. GROUNDED - YES. SWITCHED FMC TO BOTH ON LEFT AND THEN BACK TO NORMAL. F/O NAV DISPLAY RESET AND BACK TO NORMAL AND NO FLAGS NOTED. REF B737-800 FIM 34-61-00-810-836.SDR ASAA2023020941904Computer · failedRIGHT FMC FAILED ON CLIMB OUT (VTK & MAP) RECOVERED IN 5 MIN. GROUNDED - YES. REPLACED FMC #2 PER B737-800 AMM 34-61-02-401, VERIFIED LDDB-557362-004, ADDB-ASA1007A, OPS-559775-001, OPC-BCG01T-62, MEDB- BCG-01T-A0 SOFTWARE INSTALLED. FMC SWITCH PLACED INTO NORSDR ASAA2023013041846Detector · faultyENG #1 FIRE LOOP 'A' WILL NOT TEST. GROUNDED - YES. REF B737-800 FIM 26-10 TASK 801, ENG/APU FIRE/OVHT DETECTION CONTROL MODULE BITE TEST SHOWS ENGINE 1 - LOOP A - FAN UPPER DETECTOR FAULT AND ENGINE 1 - LOOP A - CORE RIGHT DETECTOR FAULT. PER FIM 26-10 TASK 8SDR ASAA2023013041742None · noneVTK ANNUNCIATED ON APPROACH FOR APPROX 45 SEC. ON GROUND WARNING CLEARED. GROUNDED - YES. PER B737-800 FIM 34-61 TASK 801 AND 824. IN FMC-R INFLIGHT FAULTS LEG 1 HAD: ADIRS-R DISCRETE 270 AND ADIRS-R PRES POS LAT. THESE WERE CAUSED BY THE ADIRU-R. REMOVED AND SDR ASAA2023013024667Idg · failedLH GENERATOR FAILED ON DEPARTURE THROUGH 90KTS ON TO ROLL. GROUNDED - YES. DIVERSION TIME 44 MINUTESRMVD & RPLCD LH IDG REF B737-800 AMM 24-11-11.SDR ASAA2023011241532Fmc · faultedFMC DISAGREE GROUNDED - YES. PROCEDURE RUN ON THE GROUNDSDR ASAA2023010961446Fan · inoperativeFOUND WX RADAR BLOWER FAN INOP. GROUNDED - YES. REPLACED WEATHER RADAR R/T BLOWER FAN IAW B737-800 AMM 34-43-51/401.SDR ASAA2022121041094Fmc · intermittent#2 FMC FAIL (VTK LNAV DISCONNECT, SIGLE FMC OPERATION) DESCENDING THRU 10,000 MSL. SEEMED TO SELF CORRECT BUT AND WAS SLOW TO RECEIVER. POSITION SHIFT TO THE RIGHT WAS VISUALLY EVIDENT ON FINAL TO 35 EVEN THROUGH AND WAS WITHIN LIMITS FOR THE 2ULU RNWY APPROACSDR ASAA2022120141006Wire Harness · faultedOVERHEAT DETECTION LOOP A SHOWS A FAULT. GROUNDED - YES. PERFORMED B737-800 FIM 26-10 TASK 805. MW0325 HARNESS BAD. REMOVED AND REPLACED ENGINE 1 CORE FIRE DETECTION HARNESS MW0325 REF B737-800 AMM REF 26-11-02/401. ENGINE FIRE DETECTION OPS TEST OK. ETOPS GROSDR ASAA2022112640972Fire Detector · faultedON FIRE TEST FOUND FAULT ON ENG1 "A" LOOP. GROUNDED - YES. REMOVED AND REPLACED UPPER FAN DETECTOR PER B737-800 AMM 26-11-01 OPS CHECKED NORMAL. ORIGINAL SUBMISSION DATE: 11/30/2022SDR ASAA2022112540938Warning Message · false indicationR/O FMC FAILED DURING DESCENT: SINGLE FMC OPS. VTK AND MAR FLAGS ON F/O ND F/O FMC RESET ON ITS OWN, ANP INCREASED TO 0.54 NM PRIOR TO REDUCING TO 0.10 NM WITHIN 15 MINUTES APPROX. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 836 FO FMC OPS TEST GOOD.SDR ASAA2022112540935Control Panel · faultedCAPT WX RADAR TILT CONTROL DIAL DOES NOT MATCH ACTUAL TILT SHOWN ON ND FOR WX RADAR IN MANUAL MODE ON CAPTAIN'S DISPLAY. GROUNDED - YES. FOUND SHAFT OF CAPT'S TILT KNOB LOOSE. R & RD WX RADAR CONT PNL PER B737-800 AMM 34-43-91. SYS OPS CKS NML PER SAME. GND VESDR ASAA2022112540934Lens · detachedF/A REPORT EMERGENCY EXIT SIGN FELL IN CABIN. GROUNDED - YES. EXIT LIGHT LENS, CEILING, MID CABIN, FELL OFF. RECLIPPED LENS BACK IN POSITION.SDR ASAA2022112440939Warning Message · false indicationF/O FMC FAIL, SINGLE OPS. GROUNDED - YES. FMC OPERATIONAL ON ARRIVAL TO AIRCRAFT. PERFORMED B737-800 FIM 34-61 TASK 836. OPS TEST GOOD. BOTH FMCS OPERATE NORMAL AND RESET SUCCESSFULLY. PER FIM NO ACTION NECESSSRY.SDR ASAA2022102640499Wire · damagedR2 DOOR LOWER AFT EXIT SIGN IS INOP. GROUNDED - YES. REPAIRED WIRES W4142-0412-20 AND W4142-0452-20 IAW B737-800 WDM 33-51-22 AND BSWPM 20-30-12.OPERATIONAL TEST OF R2 LOWER EXIT SIGN CHECK GOOD.SDR ASAA2022100740403Intercostal · corrodedFORWARD WET AREA, MAIN CABIN FLOOR STEP INTERCOSTAL, PART # 141A5214-5 AT STA 259.565 TO STA 277.12, LBL 11.20, WL 207.5 IS CORRODED IN THE UPPER FLANGE. GROUNDED - YES. REMOVED CORROSION ON THE UPPER SURFACE OF THE INTERCOSTAL LOCATED IN THE FORWARD WET AREA SDR ASAA2022100340248Shield · corrodedAFT CARGO COMPARTMENT - RH FLOOR TRANSITION PANEL - STA 847- 867 CORRORED IN AND AROUND FASTENER HOLES. (RED MARKED). GROUNDED - YES. EVALUATED SHIELD & FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN. REMOVED OLD SHIELD, LOCATED & DRILLED NEW SHIELD P/N:146ASDR ASAA2022100340264Shield · corrodedAFT CARGO COMPARTMENT - RH FLOOR TRANSITION PANEL - STA. 767 -787 CORRORED IN AND AROUND FASTENER HOLES.(RED MARKED). GROUNDED - YES. EVALUATED SHIELD & FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN.REMOVED OLD SHIELD, LCOATED & DRILLED NEW SHIELD P/N: 143ASDR ASAA2022100340263Shield · corrodedRH TRANSITION PANEL STA. 480-500A - CORROSION IN AND AROUND FASTENER HOLDS. (RED MARKED). GROUNDED - YES. EVALUATED SHIELD & FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN.REMOVED OLD SHIELD, LCOATED & DRILLED NEW SHIELD P/N: 143A8126U21 P.O. 1042480.1 & INSSDR ASAA2022100340262Shield · corrodedRH TRANSITION PANEL STA. 420-440 - CORROSION FOUND - BARE METAL AREAS EXPOSED.(RED MARKED). GROUNDED - YES. REMOVED CORROSION.ORIG, THICKNESS= .040REMOVED .009"REMAINING = .031."FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2.REMOVED OLD SHIELD, CLOCASDR ASAA2022100340261Shield · corrodedAFT CARGO COMPARTMENT -RH FLOOR TRANSITION PANEL - STA 847- 867 CORRORED IN AND AROUND FASTENER HOLES. (RED MARKED). GROUNDED - YES. EVALUATED SHIELD & FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN.REMOVED OLD SHIELD, LOCATED & DRILLED NEW SHIELD P/N:146A81SDR ASAA2022100340260Transition Panel · corrodedRH TRANSITION PANEL FROM STA. 500B - 500C BULKHEAD- CORROSION IN AND AROUND FASTENER HOLSE.PREVIOUS BLEND OUT REPAIR AREA. (RED MARKED). GROUNDED - YES. REMOVED CORROSION.ORIG THICKNESS =.40"REMOVED =.10"REMAINING +.030"FOUND TO BE OUT OF LIMITS IAW B737-800 SSDR ASAA2022100340259Transition Panel · corrodedRH TRANSITION PANEL FROM STA.500D - 500I BULKHEAD- CORROSION IN AND AROUND FASTENER HOLES.PREVIOUS BLENDED AREA REPAIR. (RED MARKED). GROUNDED - YES. REMOVED CORROSIONORIG THICKNESS=.040".REMOVED .010"REMAINING .030".FOUND TO BE OUT OF LIMITS IAW B737-800 SRM SDR ASAA2022100140402Floorbeam · corrodedAFT MAIN CABIN FLOOR SUPPORT BEAM UPPER SKIN HAS CORROSION AT SEVERAL SPOTS BETWEEN LBL-45-LBL15, BS986.5. GROUNDED - YES. REMOVED CORROSION FROM THE UPPER SURFACE OF THE PASSENGER FLOOR BEAM AT STATION 986.5, LBL15 -LBL 45, ORIGINAL THICKNESS 0.150", REMOVED SDR ASAA2022100140401Door Sill · corrodedFWD MAIN CABIN FLOOR SUPPORT, FWD ENTRY DOOR CUTOUT LOWER SILL, Z-CHANNEL UPPER SKIN HAS CORROSION, LBL-60, BS326. GROUNDED - YES. REMOVED CORROSION FROM THE FORWARD MAIN CABIN, FORWARD ENTRY DOOR LOWER MAIN SILL, INNER CHORD:ORIGINAL THICKNESS 0.090",REMOVED SDR ASAA2022100140400Intercostal · corrodedFWD MAIN CABIN FLOOR SUPPORT, U-CHANNEL UPPER SKIN HAS CORROSION , LBL 11.16, BS 270- BS277. GROUNDED - YES. REMOVED CORROSION FROM THE UPPER SURFACE OF THE INTERCOSTAL LOCATED IN THE FORWARD WET AREA AT STA 270- STA 277, LBL 11.16, WL 208.10, ORIGINAL THICKNESDR ASAA2022100140225Intercostal · corrodedFWD MAIN CABIN FLOOR SUPPORT, STRAP UPPER SKIN HAS CORROSION AROUND FSTNR HOLE, LBL-13, BS326. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPPORT AT STA. LBL-13 BS326,ORIGINAL THICKNESS .080 REMAINING THICKNESS .054 REMOVED .026 FOUND TO BE OUT OF LIMITS PER BSDR ASAA2022100140193Floorbeam · corrodedAFT MAIN CABIN FLOOR SUPPORT BEAM UPPER SKIN HAS CORROSION AROUND FSTNR HOLE, RBL -44, BS986.5. GROUNDED - YES. REMOVED CORROSION FROM THE FLOORBEAM AT STATION 986.5, RBL 44 ORIGINAL THICKNESS 0.150",REMOVED 0.058",REMAINING THICKNESS 0.092"FOUND OUT OF LIMITSSDR ASAA2022100140177Support Beam · corrodedAFT MAIN CABIN FLOOR SUPPORT BEAM, PREVIOUS REPAIR LOWER SPLICE STRAP HAS CORROSION AT SEVERAL SPOTS LBL-10, BS947.5. GROUNDED - YES. REMOVED LOWER SPLICE STRAPS 2EA FROM PREVIOUS REPAIR AT BS947.5 LBL-10 IAW B737-800 SRM 51-40-02.FABRICATED. LOCATED, DRILLED SDR ASAA2022093040399Floorboard · damagedFWD AREA FLOOR BOARD PN: 141A5810-155 DAMAGED. GROUNDED - YES. REPAIRED FWD AREA FLOOR BOARD PN 141A5810-155 IAW B737 SRM 53-00-50.SDR ASAA2022093040224Floor Panel · damagedAFT WET AREA FLOOR BOARD PN:147A5810-27 DAMAGED. GROUNDED - YES. EVALUATED PANEL IAW B737-800 SRM 53-00-50-1A-1 FOUND DAMAGE NEEDING REPAIR. REPAIRED FLOOR BOARD PN: 147A5810-27 AFT WET AREA IAW B737-800 SRM 53-00-50-2R-1 AND B737-800 SRM 53-00-50-2R-0.SDR ASAA2022093040223Floor Panel · damagedAFT WET AREA FLOOR BOARD PN:147A5810-28 DAMAGED. GROUNDED - YES. EVALUATED AND REPAIRED FLOOR PANEL IAW B737-800 SRM 53-00-50-1A-1 AND B737-800 SRM 53-00-50-2R-1 AND B737-800 SRM 53-00-50-2R-0.SDR ASAA2022093040222Floor Panel · delaminatedAFT WET AREA FLOOR BOARD PN:147A5810-136 DAMAGED. GROUNDED - YES. EVALUATED PANEL IAW B737-800 SRM 53-00--50-1A-1 FOUND DAMAGE NEEDING REPAIR. REPAIRED IAW B737-800 SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.
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