N128UP

Service difficulty reports · 215

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 = 'N128UP' 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 UPS06146187Shear Plate · crackedINSPECTION TYPE:5YR, SHEAR PLATE AT FS 79L, FLOOR LEVEL, IS CRACKED. REMOVED AND REPLACED SHEAR PLATE PER A300 SRM 51-40-21 AND 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622R · Fuselage Main, StructureSDR UPS06146186Shear Plate · crackedINSPECTION TYPE:5YR SHEAR PLATE AT FS 79 R , FLOOR LEVEL, IS CRACKED. REMOVED AND REPLACED SHEAR PLATE PER A300 SRM 51-40-21 AND 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622R · Fuselage Main, StructureSDR UPS06146185Angle · crackedINSPECTION TYPE:5YR, NR 1 ENGINE PYLON STRINGER FAIRING, CRACKED STIFFENER, OUTBOARD, AFT MOST. REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR UPS06146184Angle · crackedINSPECTION TYPE:5YR, NR 1 ENGINE PYLON STRINGER, CRACKED STIFFENER, INBD, AFT MOST. REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR UPS06146203Rib · crackedINSPECTION TYPE:5YR RT WING KRUEGER FLAP BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED AND REPLACED DOUBLER PER A300 SRM 51-40-00.Feb 7, 2006 · N128UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR UPS06146190Floorbeam · crackedINSPECTION TYPE:5YR, AVIONICS COMPARTMENT FLOOR PANEL NR 121TF BETWEEN AVIONICS RACKS HAS CRACKED FLOORBRACE. REMOVED AND REPLACED FLOORBRACE PER A300 SRM 51-40-21.Feb 7, 2006 · N128UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR UPS06146189Bracket · crackedINSPECTION TYPE:5YR, AFT CARGO FWD BULKHEAD LT SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER A300 SRM 51-40-21 AND 51-40-00.Feb 7, 2006 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146188Bracket · crackedINSPECTION TYPE:5YR AFT CARGO FWD BULKHEAD CENTER SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER A300 SRM 51-40-21 AND 51-40-00.Feb 7, 2006 · N128UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR UPS06146183Rib · crackedINSPECTION TYPE:5YR LT WING KRUGER FLAP BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED AND REPLACED DOUBLER PER A300 SRM 51-40-00.Feb 7, 2006 · N128UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR UPS05144871Bulb · inoperativeINSPECTION TYPE:N/A LAV EMERGENCY LIGHT INOP. RELAMPED, WORKED OK.Jul 8, 2005 · N128UP · Airbus A300B4622R · Emergency LightingSDR UPS05144435Slide · malfunctionedSLIDE HARD TO ARM HAD TO RECYCLE ARMING HANDLE SEVERAL TIMES IN ORDER TO GET A SLIDE ON ECAM. CYCLED EMERGENCY ESCAPE SLIDE RELEASE HANDLE SEVERAL TIMES WITH SLIDE APPEARING ON ECAM HANDLE WAS SMOOTH IN OPERATION IN REF TO MM 52-73-00-0.May 10, 2005 · N128UP · Airbus A300B4622R · Escape SlideSDR UPS04142860Light · inoperativeLAV EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT.Jul 23, 2004 · N128UP · Airbus A300F4622R · Emergency LightingSDR UPS04142326Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. R&R EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY PER MM 33-51-14, CHECKS OK.Apr 30, 2004 · N128UP · Airbus A300F4622R · Emergency LightingSDR UPS01136402Coalescer Bag · contaminatedINSPECTION TYPE:N/A CREW REPORTED THAT THEY HAD A SMOKE SMELL IN THE COCKPIT AND THAT THE NR 1 IDG WHICH AS ON DEFERRAL WAS READING 120C ON THE OIL TEMP WHILE THE NR 2 OIL TEMP WAS READING 90C. R&R LT PACK COALESCER BAG IAW MM 21-51-16, REF TSM 21-20-00, FIG 2Jul 25, 2001 · N128UP · Airbus A300F4622R · Humidity Control SystemSDR UPS01135474Warning System · activatedIN FLT, ECAM MSG AUTO TRIM TANK SYS INOP / FUEL GRAVITY FWD TRANSFER ONLY. ITEM TRANSFERED TO MEL M212201. PLACARD INSTALLED. ITEM CLEARED, PLACARD REMOVED. NOW AIRCRAFT RESTORED TO NORMAL OPERATING CONFIGURATION.Mar 29, 2001 · N128UP · Airbus A300F4622R · Fuel Indicating System
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