N592AS

Service difficulty reports · 435

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 = 'N592AS' 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.

SDR ASAA11510833Unknown · malfunctionedDURING TAXI OUT OGG "FMS DISAGREE" MESSAGE DISPLAYED ACCOMPLISHED QRH PROCEDURE FMS OPERATIONS RETURNED TO NORMAL. CURRENTLY NR 1 AND NR 2 FMS SYSTEM GROUND FUNCTIONAL TEST GOOD IAW AMM 34 61 00 SYSTEM READY FOR CONTINUED SERVICE.Dec 20, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510752Idg · malfunctionedNR 2 ENGINE DRIVE LIGHT INOP. REPLACED NR 2 ENGINE IDG ASSY REF M/M 24 11 11 090 801C3 AND 24 11 11 400 801 OPS AND LEAK CHECKS GOOD.Dec 2, 2011 · N592AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA11510659Exciter · faultyAPU FAIL TO START WITH FAULT LIGHT ILLUMINATING. ACCOMPLISHED FIM 49 40 00 810 802. VERIFIED FAULT 49 41011 STILL ACTIVE. APU GOES THROUGH START SEQUENCE DOOR OPEN CRANKING AND FUEL FOG AT TAILPIPE BUT NO IGNITION SOUND NOTED. REPLACED APU EXCITER REF MM49Nov 13, 2011 · N592AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA11510618Control Unit · malfunctionedELECTRIC LIGHT ILLUMINATED AFTER ENGINE START. PER BITE PROCEDURE ELEC LIGHT MESSAGE 24 31 TASK 801 FOUND SPCU TO BE INOP. ACCOMP FAULT ISOLATION OF SPCU PER FIM TASK 24 34 00 810 802 BY CYCLING C/B`S SPCU NORMAL & SPCU STANDBY. REACCOMP BITE PROCEDURE & ELNov 6, 2011 · N592AS · Boeing 737890 · DC Generating SystemSDR ASAA11510591Valve · failedDURING CLIMB, AT FL300. DUCT PRESSURE SPLIT. AT CRUISE 350 EACH CLIMB WOULD GIVE ANOTHER SPLIT GREATER THAN 20 PSI. ON DEFERRAL.Oct 26, 2011 · N592AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA11510546Unknown · malfunctionedFMC DISAGREE LIGHT ILLUMINATED ON GROUND AFTER FLAPS EXTENDED. PERFORMED QRH PROCEDURE. LIGHT RESET. OPS NORMAL.Oct 18, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510422Unknown · malfunctionedFMC DISSAGREE, MESSAGE AFTER START. ACCOMPLISHED QRH PROCEDURE. LIGHT RESET. OPS NORMAL.Sep 27, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510350Actuator · failedRT SPAR VALVE CLOSED LIGHT ILLUMINATED BRIGHT IN FLIGHT. DIVERSION TIME: 1H 53M. REPLACED RT SPAR VALVE ACTUATOR PER MM 28 22 11 OPS CHECK NORMAL. VERIFICATION FLIGHT SATISFACTORY.Sep 10, 2011 · N592AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA11510346Inlet Bullet · damagedFOUND FWD SPINNER FOR FAN BLADES ON NR 1 ENGINE BLACK ANODIZED COATING MISSING GREATER THAN 50 PERCENT. REMOVED AND REPLACED FWD SPINNER FOR FAN BLADES ON NUMBER 1 ENGINE PER MM 72 21 01 400 801 F00.Sep 6, 2011 · N592AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA1159913Wire Harness · defectiveNR 1 ENGINE TREND DATA SHOWS GREATER THAN NORMAL VIBRATION DATA SCATTER FROM THE FORWARD (NOB) SENSOR. ACCOMPLISHED AVM SYS OPS TEST NO FAULTS LOGGED BEFORE AND AFTER HARNESS CHANGED. REPLACED ENGINE NACELLE WIRING HARNESS MW0313 REF MM 71 51 03 000/400 801 Jun 22, 2011 · N592AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA1159734Fmc · malfunctionedMAP+VTK DISPLAYED ON F/O'S INBD DISPLAY. RESET NR 2 FMC COMPUTER. BITE PASSES FLAGS REMOVED FROM F/O'S DISPLAY. OPS OK REF MM 34 61 TSK 801 FIM.Jun 1, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159692Control Panel · failedFAULT AND APU DET INOP LIGHTS ON PRE FLIGHT TEST ILLUMINATED ONLY CAPT'S MASTER CAUTION. REPLACED ENGINE AND APU FIRE CONTROL PANEL PER AMM REF 26 00 01 00 801/ 26 00 01 400 801. ALL INSTALLATION TESTS PASS.May 26, 2011 · N592AS · Boeing 737890 · Fire DetectionSDR ASAA1159631Unknown · malfunctionedAFTER ENG START PRIOR TO TAXI AN FMC DISAGREE MESSAGE CAME UP ON BOTH FMC'S. PERFORMED QRC PROCEDURE 11.2. AFTER PUSHING CB'S IN FMC'S RESUMED NORMAL OPERATIONS.May 10, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159535Unknown · malfunctionedLNAV WILL NOT ENGAGE. ACCOMPLISHED FMCS BITE CHECK PER FIM 34 61 TASK 801. FMCS LEFT AND RIGHT SENSOR STATUS ALL OK. FMCS LEFT IN FLT FAULTS FLT LEG 1 FMC RIGHT SHOWS LEFT FAIL. ACCOMPLISHED FIM 34 61 TASK 807 TO FMC LEFT FMC PROMPTS SHOW TASK PASSED. ACCApr 23, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159419Unknown · malfunctionedFMC DISAGREE ILLUMINATED ON CAPT & F/O MAP DISPLAYS. ACCOMPLISHED QRH PROCEDURE, OPS NORMAL.Apr 11, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159418Unknown · malfunctionedFMC DISAGREE LIGHT CAME ON. PERFORMED QRH PROCEDURE ON GROUND. LIGHT WENT AWAY.Apr 11, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159249Circuit Breaker · poppedAFTER LEVEL OFF AT CRUISE ALT MASTER CAUTION ILLUMINATED AND THE STBY PWR OFF LIGHT ALSO ILLUMINATED. RAN QRH. ALSO NOTICED CB C2 POPPED. RESET STBY BUS SECT 2 C/B. STBY PWR SYS TESTS GOOD REF TASK 24 34 00 710 802. NO HISTORY.Mar 14, 2011 · N592AS · Boeing 737890 · DC Power Distribution SystemSDR ASAA1159166Relief Valve · malfunctionedOUTBOARD (RT) POSITIVE PRESS RELIEF VALVE FAILED TEST LOOSE SEAL INSIDE VALVE. REMOVED AND REPLACED POSITIVE PRESSURE RELIEF VALVE REF B737NG AMM 21 32 01. POSITIVE PRESSURE RELIEF VALVE SYSTEM TEST GOOD REF B737NG AMM 21 32 01 700 801.Mar 2, 2011 · N592AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA1159075Fan · noisyFWD CABIN TEMP SENSE FAN LOUD. REMOVED AND REPLACED CABIN TEMP SENSE FAN REF MM 21 61 11.Feb 23, 2011 · N592AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1158968Filter Element · cloggedAPU DROP OFF LINE MAINTENANCE SHUTDOWN MESSAGE 49 94299 OIL FILTER SHOWS CLOGGED. TROUBLESHOT PER FIM 49 90 00 810 819. MAG PLUG CK GD. REMOVED AND REPLACED LUBE FILTER AND STARTER GEN. FILTERS AND FILTER BYPASS SWITCH REF FIM 49 90 00 810 819. OPS AND LEFeb 5, 2011 · N592AS · Boeing 737890 · APU Oil SystemSDR ASAA1158804Fmc · failedLEFT FMC INOP. VTK FLAG ON MAP DISPLAY. COULD NOT RESTORE NORM OP. NO FMC CARROT ON MENU PAGE W/XFER SW IN "NORM" OR "BOTH ON LT". NR 1 FMC CMPTR "PWR" & "FMC VALID" GREEN LIGHTS NOT ILLUM C/B'S ARE IN. SUSPECT FMC CMPTR. REPLACED LEFT FMS COMPUTER REF MJan 16, 2011 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1058699Switch · failedAPU STARTS NORMALLY BUT WILL NOT POWER MAIN BUSSES. REPLACED APU GENERATOR PER MM 49 41 21, NO HELP. FOUND BAD S16 SWITCH AT P28 PANEL PER FIM TASK 24 21 00 810 820. REPLACED APU REMOTE FIRE SWITCH PER CHAPTER 20 STANDARD PRACTICES. TESTED APU AC GENERATIODec 24, 2010 · N592AS · Boeing 737890 · Extinguishing SystemSDR ASAA1058665Unknown · malfunctionedFMC DISAGREE AFTER PUSH BACK. ACCOMPLISHED FMC DISAGREE FAULT ISOLATION PER FIM 34 61 00 810 835, NO FAULT AFTER 5 MIN A/C OK FOR SERVICE.Dec 19, 2010 · N592AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1058653Converter · failedDURING THE EEP CHECK THE APU GEN VOLTS & FREQS SHOWING 0 FREQS AND 2 VOLTS. DIVERSION TIME 121 MINUTES. VERIFIED DISCREPANCY. PERFORMED APU AND GCU BITE. NO FAULTS NOTED. REMOVED AND REPLACED APU START CONVERTER PER AMM 49 41 61. OPS NORMAL. APU GEN BUS Dec 19, 2010 · N592AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA1058641Unknown · malfunctionedUPON RECALL LEFT PACK LIGHT ILLUMINATED. RESET VIA MASTER CAUTION RESET BUTTON OK. LIGHT ILLUMINATES ON RECALL. NR 1 TEMP CTRLR SHOWS "TCV THIS PACK" FAULT ON BIT AND LAST FLT. VERIFY TEST GO. RESET FAULT. FAULT DID NOT RETURN. FUNCT CHECK LT PACK GOOD. Dec 16, 2010 · N592AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058532Unknown · malfunctioned"CONT CAB" ZONE TEMP LIGHT ILLUMINATES ON MASTER CAUTION RECALL. LIGHT CLEAR WHEN PUSH TO RESET IN PUSHED. PERFORMED FIM 21 62/842 FOUND FLT DECK TRIM VALUE FAULT ON NR 2 TEMP CONT ON BIT & LAST FLT BUT VERFIY CK "GO". OPERATED LT PACK FOR SEVERAL MIN. ZONNov 22, 2010 · N592AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058490Idg · failedNR 1 ENGINE DRIVE LIGHT NOT ILLUMINATED DURING PRE FLT. FOUND VERY HIGH RESISTANCE AT PIN 5 AND 6 ON PLUG DP 1306 ON NR 1 IDG PRESS A/W REF SSM 24 11 11. REMOVED AND REPLACED NR 1 ENG IDG PER AMM 24 11 11. IDG OPERATIONAL CHECKED GOOD PER AMM 24 11 11.Nov 9, 2010 · N592AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1058468Pan · damagedAFT CARGO DOOR HANDLE PAN DAMAGE OUT OF LIMITS. REMOVED AND REPLACED HOUSING PAN REF SRM 51 40 02.Oct 29, 2010 · N592AS · Boeing 737890 · Cargo/Baggage DoorsSDR ASAA1058462Packing · leakingRT AND LT MAIN FUEL TANK SUMP DRAIN VALVES LEAKING. REPLACED PRIMARY DRAIN SEAL O-RING ON RT AND LT MAIN FUEL TANK SUMP DRAIN VALVES REF MM 28 11 61 600 80. OP AND LEAK CHEAK GOOD.Oct 29, 2010 · N592AS · Boeing 737890 · Fuel StorageSDR ASAA1058408Handle · dirtyNR 1 ENGINE FIRE/OVERHEAT (FIRE HANDLE) WILL NOT ILLUMINATE DURING FIRE/OVERHEAT TEST. FAULT LIGHT IS ILLUMINATED DURING FIRE/OVERHEAT TEST. ALL SWITCHES POSITIONED TO "NORMAL". FIRE DET MOD. BITE REVEALED NR 1 ENG B-LOOP FAULT. CYCLED FIRE HANDLE IN RIGHOct 18, 2010 · N592AS · Boeing 737890 · Fire DetectionSDR ASAA1058325Tape · looseFOUND LOOSE / TORN ANTISKATE FOIL ON AFT GATE OF OUT FLOW VALVE. REMOVED LOOSE ANTISKATE FOIL FROM OUT FLOW VALVE REF EA 2130 01028. NO TIME LIMITATION REQUIRED. SEAMC CONTACTED.Oct 4, 2010 · N592AS · Boeing 737890 · Pressure Regulator/Outflow ValveSDR ASAA1058263Hf Comm · malfunctionedMCDU SCREEN INDICATES HF RADIO TRANSMITTING WHILE ON GROUND "HF IN PROG" MSG SHOWN. UNABLE TO DUPLICATE MSG 'HF IN PROG' ON MCDU WHILE A/C IS ON GROUND. ACCOMPLISHED NR 1 AND NR 2 HF XCVR BITE IAW FIM TASK 23 11 00 810 801 LRU STATUS GOOD, NO FAULTS NOTED. Sep 10, 2010 · N592AS · Boeing 737890 · HF Communications SystemSDR ASAA1058250Control Valve · failedL PACK PRESS DECREASES AS ALTITUDE INCREASES. AT 10K L40/R45 15K L37/R45 AT 20K L33/R45 25K L30/R45 30K L25/R45 35KL21/R45 37KL19/R45 CRUISE FL380 L21/45. FOUND BOTH THE PRECOOLER CONT VALVE & THE HIGH STAGE REGULATOR ON THE NR 1 ENG FAILED TO REGULATE THE PRSep 3, 2010 · N592AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058231Hf Comm · no testHF NR 1 TEST OK HF NR 2 TEST NOT OK. (UNABLE TO GET ANY RESPONSE USING HF NR 2 AND ATTEMPTING MULTIPLE HF FREQUENCIES). OPERATIONAL CHECK OF HF NR 1 AND HF NR 2 IS GOOD. NO DISCREPANCIES NOTED BITE CHECK OF NR 1 AND NR 2 HF TRANSCEIVERS GOOD. GROUND VERIFIAug 27, 2010 · N592AS · Boeing 737890 · HF Communications SystemSDR ASAA0956358Panel · puncturedPANEL 194FR IS PUNCTURED. REPAIRED PANEL 194FR.Aug 4, 2009 · N592AS · Boeing 737890 · Fuselage Main, Plate/Skin
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