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.

SDR ASAA0956495Idg · faultyFOLLOW UP TO NR 2 IDG FREQUENT SERVICING. REMOVED AND REPLACED NR 2 ENGINE IDG REF AMM 24 11 11 000 801 24 11 11 400 801.Aug 28, 2009 · N566AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0956399Circuit Breaker · poppedCABIN PRESSURE AUTO FAIL LIGHT AND ALTERNATE LIGHTS ON. VERIFIED AUTO FAIL LIGHT AND ALTERNATE LIGHTS ON. FOUND AUTO PRESS CONTROL NR 2 MANUAL C/B OUT. RESET SAME C/B. NR 2 AUTO PRESSURE CONTROL SYSTEM OPS CHECK GOOD PER M/M FIM TASK 21 31 TASK 801. SEAMCAug 14, 2009 · N566AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA0956193Valve · inoperativeLEFT SPAR VALVE CLOSED LIGHT ILLUMINATED BRIGHT IN FLIGHT. DIVERSION TIME 1 HOUR 39 MINUTES. FOUND LEFT SPAR VALVE INOP. REMOVED AND REPLACED LEFT SPAR VALVE REF AMM 28 22 11 400 804. P/N MA30A1001 VERIFIED SEAMC. PERFORMED OPS CHECK AMM 28 22 00 710 801.Jul 11, 2009 · N566AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA0956114Idg · malfunctionedNR 2 IDG HAS RECENT HISTORY OF FREQUENT SERVICING, GROUNDED, YES. ACCOMPLISHED TSR 904797, RAN ENGINE FOR 10 MIN NO LEAKS NOTED. REPLACED VENT VALVE AND FILL PORT VALVE REF MM 24-11-00-700-804 SEAM C.Jul 1, 2009 · N566AS · Boeing 737890 · Alternator-Generator DriveSDR ASAA0956091Warning System · false activationDURING FLIGHT RT SIDE WINDOW HEAT LIGHT OVERHEAT ILLUM. CYCLED OFF THEN ON AFTER 3 MIN. DID NOT RE-ILLUMINATE. THEN AFTER LANDING RT SIDE WINDOW HEAT LIGHT WAS NOT ILLUM. COULD NOT DUPLICATE. NO HISTORY IN 90 DAYS. PERFORMED WINDOW HEAT TEST ON RT SIDE WJun 30, 2009 · N566AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0955859Transceiver · inoperativeCIRCUIT BREAKER FOR HF 1 IS POPPED. INSPECTED HF NR 1 CIRCUIT FOUND NORMAL RESET HF NR 1 C/B. FOUND NR 1 HF TRANSCEIVER INOP. REPLACED HF NR 1 TRANSCEIVER GROUND VERIFICATION SUCCESSFUL REF 23 11 21. PART VERIFIED WITH SEAMC IPC 23 11 21 11.Jun 6, 2009 · N566AS · Boeing 737890 · HF Communications SystemSDR ASAA0955801Drive Unit · failedTHE "PWS FAIL" DISPLAYED ON CAPTAIN'S NAVIGATIONAL DISPLAY ON APPROACH. FOLLOWED FIM 34 43 TASK 815 UNABLE TO DUPLICATE, NO FAULTS. WXR TEST PASSED REF MM 34 43 00. FIRST VERIFICATION FLIGHT FAILED. REPLACED WEATHER RADAR ANT DRIVE UNIT OPS CK GOOD PER MM May 28, 2009 · N566AS · Boeing 737890 · Weather Radar SystemSDR ASAA0955653Cdu · damagedCOPILOTS FMC LINE SELECT BUTTON FOR "6L" IS CHIPPED AND HALF MISSING. GROUNDED YES. REMOVED/INSTALLED F/O'S FMC CDU REF 34 61 01.May 14, 2009 · N566AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0955497Filter Element · defectiveAPU OIL FILTER DELTA P INDICATION IS POPPED ON FILTER HOUSING. REMOVED AND REPLACED FILTER REF AMM 49 91 11 RESET OIL FILTER INDICATOR REF AMM 49 91 13 SEAMC NOTIFIED PARTS CONFIRMED. OPS CHECK NORMAL.May 5, 2009 · N566AS · Boeing 737890 · APU Oil SystemSDR ASAA0954677Computer · malfunctionedSINGLE FMC OPS ON BOTH SCRATCH PADS AND VTK DISPLAYED ON RIGHT NAV DISPLAY. COMPLIED WITH QRH PROCEDURE, UNABLE TO RESTORE DUAL FMC OPS. RT FMC LOGGED 1 INFLT FAULT. NO HISTORY LAST 90 DAYS. NO CURRENT FAULTS. PERFORMED FIM 34 61 TASK 801 FMC BITE CHECK PMar 9, 2009 · N566AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0954430Controller · faultyAFTER START AUTO FAIL LIGHT ILLUMINATED. FOUND FAULT ON NR 2 DCPC. PERFORMED FIM TASK 21 31 00 800 801 ON NR 1 AND NR 2 DCPD, NO FAULTS FOUND ON GROUND TEST. NO HISTORY FOR PAST 30 DAYS.Feb 13, 2009 · N566AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA0954386Oil System · faultedFOUND APU LUBE FILTER DELTA "P" BUTTON EXTENDED. APU LUBE FILTER DIFFERENTIAL PRESSURE INDICATOR HAS HISTORY OF INDICATOR FOUND EXTENDED WITH FILTER FOUND CLEAN. GROUNDED YES. REMOVED APU LUBE FILTER INSPECTED AND FOUND NO CONTAMINANTS IN FILTER OR BOWL. IFeb 8, 2009 · N566AS · Boeing 737890 · APU Oil SystemSDR ASAA0954378Oil Filter · leakingTHE APU IS LEAKING OIL FROM THE DRAIN MAST AND THE OIL FILTER INDICATOR IS EXTENDED. GROUNDED YES. ACCOMPLISHED FIM 49 16 11 200 801 NO LEAKS FOUND AT THIS TIME. ACCOMPLISHED MM 49 91 13 600 801 MAG CHIP DETECTOR CLEAN & FILTER CLEAN. REPLACED FILTER. LEAFeb 5, 2009 · N566AS · Boeing 737890 · APU Oil SystemSDR ASAA0954304Engine · oil consumptionPER SEAMC ACFT RESTRICTED FROM ETOPS SERVICE UNTIL BOTH ENGINE OIL CONSUMPTION RATES ARE WITHIN ETOPS LIMITS. GROUNDED YES. PER SEMAC DAVE TOP DEFERRAL HAS BEEN REMOVED. ENGINE OIL CONSUMPTION RATE HAS RETURNED TO NORMAL.Jan 26, 2009 · N566AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA0954306Pump · failedFOUND ENG PUMP DEPRESS VALVE 1 C/B OUT. GROUNDED YES. R&R NR 1 HYD PUMP (EDP) PER MM 29-11-11.Jan 26, 2009 · N566AS · Boeing 737890 · Hydraulic Pump (Electric/Engine), MainSDR ASAA0954266Coupling · leakingNR 1 IDG IS REQUIRING INCREASINGLY FREQUENT SERVICING. GROUNDED YES. COMPLIED WITH REF 24 11 001 PERFORMED LEAK CK FOUND SERVICE COUPLING LEAKING. INSTALLED NEW PACKING AND COUPLING REF 24 11 61MM. PERFORMED LK CK FOUND NO PRESS DROP AND LEAK @ COUPLING/PORJan 21, 2009 · N566AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0954245Autoland Sys · malfunctionedAUTOLAND PERFORMED ON RWY 16R. ACFT LANDED APPROXIMATELY 30 FT LT OF CENTERLINE. GROUNDED YES. PERFORMED FIM 22 11 TASK 825 LAND VERIFY TEST AMM TASK 22 11 00 700 801 ACCOMPLISHED WITH NO DISCREP. OPS CHK GOOD. ACFT APPROACH SURVEY COMPLETED ON D/P 664601Jan 15, 2009 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA0954242Filter · dirtyF/A REPORTS AIRCRAFT WARMS UP TO ROW 9 ROW 9 AFT STAYS VERY COLD STAYS COLD UNTIL AFT 4B ZONE TEMP CONTROLLER IS NEAR FULL WARM ON. PAST 3 O'CLOCK POSITION. IN THIS POSITION AFT CABIN TEMP & SUPPLY DUCT BOTH SHOW 30DEGS ON A/C PANEL BUT DOES NOT FEEL WARM IN Jan 15, 2009 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0954207Housing · defectiveFOUND APU OIL FILTER INDICATOR EXTENDED. GROUNDED YES. PERFORMED MAGNETIC DRAIN PLUG INSPECTION PER MM 49 91 81 200 801 NO METAL PARTICLES FOUND. REPLACED LUBE FILTER ELEMENT PER MM 49 91 12. PERFORMED LEAK CHECK. LEAK CHECK GOOD. FILTER INDICATOR WOULD NJan 14, 2009 · N566AS · Boeing 737890 · APU Oil SystemSDR ASAA0954214Engine · oil consumptionACFT 566 TOPPED FOR ENG. OIL SPIKE FOR NR 1 ENG INSUFFICIENT DATA AVAILABLE FOR RE CALCULATING SPIKE REC. GROUNDED YES. ETOPS CONSUMPTION RATE IS NOW WITHIN ETOPS OPS LIMITS AT NR 1 ENG. 12 NR 2 ENG. 06 APU .00. ACFT RELEASED FROM TOP DEFERRAL SEAMC JERRY Jan 11, 2009 · N566AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA0954206Starter Gen · faultyAPU MX LIGHT ON MX MSG 49 41244. GROUNDED YES. STARTER/GENERATOR HAS BAD DIODE. ETOPS PARTS VERIFICATION: STARTER PN/28B545 7 START CONVERTER PN/452466 250. SEAMC MIKE NOTIFIED. 08675. INSTALLED NEW APU STARTER GENERATOR PN/28B545 7 PER MM 49-41-21 400 80Jan 11, 2009 · N566AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA0954197Engine · overspeedCLIMBOUT THROUGH FL330, LT ENG RPM ROLLED BACK TOWARDS IDLE, UNCOMMANDED. LT THROTTLE REDUCED TO IDLE AND ENG INDICATIONS STABILIZED. BRIEF EXHAUST SMELL THROUGH A/C PACKS WHICH CLEARS IMMEDIATELY AFTER SHUTDOWN. RED BOX AROUND LT N2 INDICATION AND N1 INDICATIJan 9, 2009 · N566AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA0854080Module · failedNR 2 ZONE/TEMP CONTROLLER BITE TEST FAILS FLIGHT DECK TRIM VALVE GROUNDED YES. R&R FLIGHT DECK TRIM VALVE. BITE CHECK OK. REF MM 21 61 21/401. REQUIRES LEAK CHECK. 3922 INSTALLED PART NR VERIFIED BY SEAMC PAT. BATCH NR 867780. LEAK CHECK GOOD.Dec 18, 2008 · N566AS · Boeing 737890 · Cabin Temperature ControllerSDR ASAA0853035Intercostal · crackedCRACK IN FWD PIT RT SIDE STRAP AFT OF CARGO PIT DOOR 8 INCHES UP SIDEWALL FROM CARGO NET FLOOR ATTACH POINT. STOP DRILLED CRACK. REPLACED STRAP (INTERCOSTAL WEB) WITH FABRICATED REPAIR PART IAW BOEING DWG NR 143A9403 AND SRM 51 30 01 51 40 05 AND 53 30 15.5.Jun 2, 2008 · N566AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA0752057Skin · damagedRAMP CREW STRUCK FWD PIT SCUFF PLATE WITH BELT LOADER. TWO SMALL SCRATCHES ON EDGE OF SKIN AND BEAR STRAP. BLENDED EDGE OF BEAR STRAP AND SKIN PERFORMED HFEC INSPECTION ARE CRACK FREE. REPLACED DAMAGED FWD AND CTR SCUFF PLATES IAW EA 5330 02237.Sep 18, 2007 · N566AS · Boeing 737890 · Fuselage Main, Plate/Skin
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