JASC 5414

Service difficulty reports · 4,361

Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 jasc_code = '5414'
  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 UPS402748Skin · crackedWHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND NR 4 PYLON OUTER SKIN CRACKED AT NAC STA 221. FABRICATED AND INSTALLED REPAIR PER SRM 54-30-03.Mar 29, 1995 · N676UP · Boeing 747123FSDR DLL17951347Panel · crackedDURING HMV, FOUND PYLON STRUCTURE AT AFT O/B CORNER FASTENER FOR FWD PYLON PANEL 451TZ IS CRACKED. WELDED THE CRACK PER SRM 54-11-00 PG 812.Mar 23, 1995 · N764DA · Lkheed 10113853SDR 95ZZZX1493Skin · cracksNUMEROUS LOOSE RIVETS IN LEFT AND RIGHT WING LOWER PYLON SKINS (AFT). ORIGINAL SKIN THICKNESS .025 INCH 2024T3. SKIN TOO THIN FOR RIVET REPLACEMENT EFFECTIVELY. REPLACED LEFT AND RIGHT LOWER PANEL SKINS WITH .032 INCH 2024T3 PANELS FABRICATED. (SEE 337 DATMar 15, 1995 · N1564B · Beech 400BEECHSDR 95ZZZX1492Skin · cracksNUMEROUS LOOSE RIVETS IN LEFT AND RIGHT WING LOWER PYLON SKINS (AFT). ORIGINAL SKIN THICKNESS .025 INCH 2024T3. SKIN TOO THIN FOR RIVET REPLACEMENT EFFECTIVELY. REPLACED LEFT AND RIGHT LOWER PANEL SKINS WITH .032 INCH 2024T3 PANELS FABRICATED. (SEE 337 DATMar 15, 1995 · N1564B · Beech 400BEECHSDR 95ZZZZ181Skin · corrosionDURING D-CHECK, CORROSION IN 'S' DUCT ON SKIN INT AT RIB 27 BLR 3 INCHES. INSTALLED REPAIR 7075-T6 .080 INCH 4 INCHES BY 7 INCHES AS PER SRM 54-10-3. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9SDR 95ZZZZ180Skin · corrosionDURING D-CHECK, CORROSION IN 'S' DUCT ON SKIN INT AT RIB 20 BLR 3 INCH. REMOVED CORROSION APPROX 3 INCH BY 3 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 54-10-3, DOUBLER APPROX 6 INCHES BY 10 INCHES 7075-T6. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9SDR DL72S950990Skin · crackedFOUND ON CV2 CHECK .25 INCH CRACKS IN SKIN AT FASTNER HOLES (4 PLACES) RT SIDE ABOVE FWD VERTICAL SPAR AND FWD OF PANEL 95012) FASTNERS LOOSE FWD OF PANEL 9501 REPAIR-1) REPAIR PER MM 54-30-0 PG801/FIG801 2).Feb 27, 1995 · N468DA · Boeing 727232SDR 9504606305Skin · crackedDURING OVERNIGHT LINE CHECK, A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON INBOARD SKIN AT THE FORWARD UPPER CORNER OF THE NR 452 PANEL CUTOUT. STOP DRILLED CRACK AND REPAIRED PER EA 63-96730.Feb 18, 1995 · N665US · Boeing 747451SDR 9504426623Skin · wornDURING PERIODIC CHECK, THE NR 4 PYLON RIGHT SKIN PANEL AND UPPER CAP SKIN WAS FOUND WORN ADJACENT TO THE WING TO PYLON FAIRING ATTACH ANGLE. PYLON SKIN AND UPPER CAP SKIN ARE MADE FROM .063 INCHES 2024-T3 AND .025: DOUBLER PLUS .032 INCH TRIPLER. MADE REPAIRFeb 1, 1995 · N623US · Boeing 747251BSDR 9504046304Skin · crackedDURING OVERNIGHT INSPECTION, A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON SKIN AT THE NR 452 ER CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLERS PER EA 63-96605.Jan 25, 1995 · N664US · Boeing 747451SDR DL72S950045Skin · crackedDURING LETTER CHECK, THE NR 2 ENGINE S DUCT HOUSING RIGHT SIDE OUTER SKIN WAS FOUND WITH A 1.25 INCH CRACK EXTENDING UP FROM ACCESS PANEL 9524. REPAIRED PER MM 54-30-0 PG 803.Jan 4, 1995 · N484DA · Boeing 727232
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