Boeing 727-2S2F
Service difficulty reports · 842
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '7272S2F' 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.
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 aircraft_model_key = '7272S2F' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VGCA20260917001Engine · making metalENGINE OIL BYPASS INDICATION. METAL IN OIL FILTERSDR VGCA20251024009Skin Panel · damagedR/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21SDR VGCA20251024020Frame · puncturedFUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R.SDR VGCA20251024019Frame · puncturedFUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28RSDR VGCA20251024018Frame · dentedFUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29RSDR VGCA20251024017Frame · dentedFUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28RSDR VGCA20251024016Floorbeam · corrodedFUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94SDR VGCA20251024015Frame · gougedFUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28LSDR VGCA20251024014Frame · gougedFUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28LSDR VGCA20251024013Frame · puncturedFUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28LSDR VGCA20251024012Skin · dentedFUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20LSDR VGCA20251024011Frame · puncturedFUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29LSDR VGCA20251024010Shear Tie · corrodedFUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R.SDR VGC2025F00000Frame · corrodedFUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29RSDR VGCA202511254009Skin Panel · damagedR/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED I.A.W. V1 AEROSPACE DOC. NO. R24-02464-001, REVISION 6 ,DATE OCTOBER 03.2025SDR VGCA202511254008Skin Panel · damagedRIGHT HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20658-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED IAW. R24-02464-001, REVISION 6 ,DATE OCTOBER 03.2025.SDR VGCA20251024007Beam · corrodedR/H SIDE H-STAB. TRAILING EDGE BEAM UPPER SURFACE CORROSION REPAIRED BY REPLACEMENT OF R/H TRAILING EDGE UPPER BEAM ENTIRE LENGTH BETWEEN ELEVATOR STATION 10 AND ELEVATOR STATION 209.90 I.A.W BOEING DRAWING 65-22987, SHEET 5, REVISION C.SDR VGCA20251024006Floorbeam · corrodedFUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62SDR VGCA20251024005Frame · dentedFUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28LSDR VGCA20251024004Frame · crackedFUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27RSDR VGCA20251024003Frame · crackedFUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27RSDR VGCA20251024002Frame · dentedFUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28RSDR VGCA20251024001Frame · dentedFUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28RSDR VGCA20250805029Spar Web · elongatedELONGATED HOLE ON VERTICAL STIFFENER WEB IN CENTER FUEL TANK FRONT SPAR AT LBL40SDR VGCA20250805028Skin · crackedCRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WINGSDR VGCA20250805027Bear Strap · corrodedCORROSION ON BEAR STRAP, DOUBLER, AND FUSLAGE EXTERNAL SKIN AT AFT CONER OF AFT CARGO DOOR FROM FS965 TO FS1010 AND STR S-21R TO S-29LSDR VGCA20250805026Beam · corrodedRIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30SDR VGCA20250815025Floorbeam · corrodedFORWARD UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER AND LOWER CHORDS CORROSION AT BS720 FROM LBL65-RBL50SDR VGCA20250815024Fastener · wrong partNONPRODUCTION FASTENER INSTALLED @ AFT LOWER FUSELAGE FRAME REPAIRED AT BS1166 FROM S-25L TO S-28LSDR VGCA20250805023Frame · misrepairedNON-PRODUCTION FASTENERS INSTALLED .AFT LOWER FUSELAGE FRAME REPAIRED AT BS1050 FROM S-25L TO S-28LSDR VGCA20250805022Floorbeam · corrodedAFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORRODED AT BS1030 FROM LBL10 TO LBL20.SDR VGCA20250805021Vertical Beam · corrodedVERTICAL BEAM CORRODED AT LOWER END. REPAIRED AT BL 0 BS 1183.SDR VGCA20250805020Frame · puncturedAFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1148 FROM S-25R TO S-28R.SDR VGCA20250805019Window Frame · corrodedAFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14RSDR VGCA20250805018Structure · corrodedCORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660SDR VGCA20250805017Floorbeam · corrodedAFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORROSION AT BS1148 FROM LBL45 TO LBL55SDR VGCA20250805016None · noneBMS3-27 IS NO LONGER PROCURABLE. BOEING SR KFC-GUC-24-0105-09B APPROVED THE USE OF BMS3-38 AS AN ALTERNATE.SDR VGCA20250805015Spar · corrodedCORROSION ON RH HORIZONTAL STAB REAR SPAR UPPER CHORD AT STAB STATION 104.25 THRU 123.25 AND 141.5 THRU 160.5SDR VGCA20250805014Skin · corrodedCORROSION ON FUSELAGE SKIN AT BS1028 TO 1055 AND S-29L TO S-29RSDR VGCA20250808013Keelbeam · corrodedKEEL BEAM BREATHER WEB CORRODED AT SEVERAL LOCATIONS ON THE UPPER SURFACE FROM BS740 TO 795 AND LBL13 TO RBL13SDR VGCA20250805012Frame · dentedAFT LOWER FUSELAGE FRAME INNER CHORD DENTED AT BS1110 FROM S-24L TO S-28LSDR VGCA20250805011Frame · puncturedAFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1090 FROM S-24L TO S-28LSDR VGCA20250805010Frame · puncturedFRAME INNER CHORD PUNCTURE AT BS 1090 BETWEEN S26R AND S28R.SDR VGCA20250805009Frame · puncturedAFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1130 FROM S-25L TO S-29L.SDR VGCA20250805008Frame · crackedFT LOWER FUSELAGE FRAME CRACKED AT BS1070 FROM S-26R TO S-28RSDR VGCA20250805007Frame · crackedFORWARD LOWER FUSELAGE FRAME UPPER CHORD CRACKED AT BS700 FROM S-28L TO S-28RSDR VGCA20250805006Skin Panel · corrodedAFT LOWER FUSELAGE SKIN CORROSION FROM BS990-1010 AT S-26LSDR VGCA20250805005Shear Web · crackedAFT UPPER FUSELAGE FLOOR SHEAR WEB CRACK NEAR BS1166-1176.9 AND RBL8 TO RBL17.87SDR VGCA20250805004Spar · corrodedWING CENTER BOX FRONT SPAR CORRODED IN MULTIPLE PLACES ON VERTICAL AND HORIZONTAL CHORD FLANGES AT BS740 FROM LBL70.5 TO RBL70.5SDR VGCA20250805003Flap Track · crackedCRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.
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