N560AS

Service difficulty reports · 562

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 = 'N560AS' 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 ASAA0956424Filter · dirtyUNABLE TO ADEQUATELY CONTROL CABIN TEMP AFT OF ROW 20 WITHOUT MOVING CONTROL. PAX COMPLAINED OF EXTREME HOT AND COLD OSCILLATION. DUPLICATED DEFECT. ACCOMPLISHED FIM 21 61/863. FOUND AFT CABIN TEMP SENSOR DIRTY. REPLACED FILTER AFT CABIN REF MM 21 61 00. Aug 19, 2009 · N560AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0956253Regulator · failedNUMBER 2 ENGINE BLEED AIR REGULATOR FAILED HEALTH CHECK. REMOVED AND REPLACED NR 2 ENGINE BLEED AIR REGULATOR PER MM 36 11 03 000 801 AND MM 36 11 03 400 801. ACCOMPLISHED NR 2 ENGINE BLEED AIR REGULATOR PER MM 36 11 03 400 801 STEP E, TESTS GOOD.Jul 22, 2009 · N560AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA0956254Valve · failedNUMBER 2 ENGINE HIGH STAGE VALVE FAILED HEALTH CHECK. REMOVED AND REPLACED HIGH STAGE VALVE ON NR 2 ENGINE PER MM 36 11 06 000 801 AND MM 36 11 06 400 801. ACCOMPLISHED NR 2 ENGINE HIGH STAGE VALVE INSTALLATION TEST PER MM 36 11 06 400 801 STEP G, TESTS GOODJul 22, 2009 · N560AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA0956252Regulator · failedNUMBER 1 ENGINE BLEED AIR REGULATOR FAILED HEALTH CHECK. REMOVED AND REPLACED NR 1 ENG BLEED AIR REGULATOR PER AMM 36 11 03 400 801 STEP D (1) (5) AND MM 36 11 03 000 81. ACCOMPLISHED NR 1 ENGINE BLEED AIR REGULATOR INSTALLATION TEST PER MM 36 11 03 400 801 Jul 22, 2009 · N560AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA0956251Regulator · failedNUMBER 1 ENGINE HIGH STAGE REGULATOR FAILED HEALTH CHECK. REMOVED AND REPLACED NR 1 ENGINE HIGH STAGE REGULATOR PER MM 36 11 02 000 801 AND MM 36 11 02 400 801. ACCOMPLISHED NR 1 ENGINE HIGH STAGE REGULATOR INSTALLATION TEST PER MM 36 11 02 400 801 STEP F, TJul 22, 2009 · N560AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA0956250Shutoff Valve · failedNUMBER 1 ENGINE PRSOV FAILED HEALTH CHECK. REMOVED AND REPLACED NUMBER 1 ENG PRSOV VALVE IAW 737 NG AMM 36 11 04 000 801 AND AMM 36 11 04 400 801 A,B,C (1)(2)(4)(9) A,B,C,D,E AND F (1)(2)(3) G (1)(8). ACCOMPLISHED NR 1 ENGINE PRSOV INSTALLATION TEST PER MM 3Jul 22, 2009 · N560AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA0956220Support · crackedLT WING UPPER TE PANEL SUPPORT AT RSS 289 CRACKED ON VERTICAL EDGE LOWER HOLE. REPLACED CRACKED FITTING.Jul 21, 2009 · N560AS · Boeing 737890 · Wing Miscellaneous StructureSDR ASAA0956204Support · corrodedSEVERAL AREAS OF CORROSION FOUND ON FLOOR TO SIDEWALL SUPPORT LBL 23 FROM STA 727D+10 787. REMOVED AND REPLACED FLOOR TO SIDEWLL SUPPORT.Jul 17, 2009 · N560AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA0956221Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK FAILED DEEP CYCLE. REMOVED AND REPLACED BATTERY PACK.Jul 16, 2009 · N560AS · Boeing 737890 · Emergency LightingSDR ASAA0955930Indicator · malfunctionedAPU DELTA P INDICATOR ON LUBE FILTER HOUSING EXTENDED. REPLACED LUBE FILTER ELEMENT AND REST DELTA P INDICATOR ON LUBE FILTER HOUSING. NO CONTAMINANTS FOUND IN FILTER. REF MM 49 91 12. OPS CHECK GOOD.Jun 10, 2009 · N560AS · Boeing 737890 · APU Oil SystemSDR ASAA0955842Spinner · damagedWHILE ACCOMPLISHING ASA T/C 78472002 ON NR 2 ENGINE FOUND FRONT SPINNER CONE MISSING ANODIZED COATING (BLACK SULFURIC ANODIZING) GREATER THAN 20 PERCENT. PARTS NOT AVAILABLE. NR SPINNER CONE REPLACEMENT TO BE ACCOMPLISHED AT NEXT "C" CHECK PER TC 78472002. Jun 3, 2009 · N560AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0955838Shim · damagedWHILE ACCOMPLISHING ASA T/C 78472002 ON NR 2 ENGINE FOUND 24 EACH SHIMS MISSING MOLYDAG COATING GREATER THAN 25 PERCENT. REF MM 72 21 02 200 801 F00 PARA L. REMOVED AND REPLACED 24 EACH SHIMS, INSTALLED SHIM P/N 340 252 307 0 PER T/C 78472002.Jun 3, 2009 · N560AS · Boeing 737890 · Turbine Engine Compressor Section
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