N216WE

Service difficulty reports · 43

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 = 'N216WE' 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 VGCA20250805029Spar Web · elongatedELONGATED HOLE ON VERTICAL STIFFENER WEB IN CENTER FUEL TANK FRONT SPAR AT LBL40Aug 5, 2025 · N216WE · Boeing 7272S2F · Wing SparSDR VGCA20250805028Skin · crackedCRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WINGAug 5, 2025 · N216WE · Boeing 7272S2F · Wing, Plate/SkinSDR 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-29LAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR VGCA20250805026Beam · corrodedRIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, StructureSDR VGCA20250815025Floorbeam · corrodedFORWARD UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER AND LOWER CHORDS CORROSION AT BS720 FROM LBL65-RBL50Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR VGCA20250815024Fastener · wrong partNONPRODUCTION FASTENER INSTALLED @ AFT LOWER FUSELAGE FRAME REPAIRED AT BS1166 FROM S-25L TO S-28LAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805023Frame · misrepairedNON-PRODUCTION FASTENERS INSTALLED .AFT LOWER FUSELAGE FRAME REPAIRED AT BS1050 FROM S-25L TO S-28LAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805022Floorbeam · corrodedAFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORRODED AT BS1030 FROM LBL10 TO LBL20.Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR VGCA20250805021Vertical Beam · corrodedVERTICAL BEAM CORRODED AT LOWER END. REPAIRED AT BL 0 BS 1183.Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, BulkheadSDR VGCA20250805020Frame · puncturedAFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1148 FROM S-25R TO S-28R.Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805019Window Frame · corrodedAFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14RAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, StructureSDR VGCA20250805018Structure · corrodedCORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, StructureSDR VGCA20250805017Floorbeam · corrodedAFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORROSION AT BS1148 FROM LBL45 TO LBL55Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR VGCA20250805016None · noneBMS3-27 IS NO LONGER PROCURABLE. BOEING SR KFC-GUC-24-0105-09B APPROVED THE USE OF BMS3-38 AS AN ALTERNATE.Aug 5, 2025 · N216WE · Boeing 7272S2F · Standard Practices/StructuresSDR VGCA20250805015Spar · corrodedCORROSION ON RH HORIZONTAL STAB REAR SPAR UPPER CHORD AT STAB STATION 104.25 THRU 123.25 AND 141.5 THRU 160.5Aug 5, 2025 · N216WE · Boeing 7272S2F · Horizontal Stabilizer, Spar/RibSDR VGCA20250805014Skin · corrodedCORROSION ON FUSELAGE SKIN AT BS1028 TO 1055 AND S-29L TO S-29RAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR VGCA20250808013Keelbeam · corrodedKEEL BEAM BREATHER WEB CORRODED AT SEVERAL LOCATIONS ON THE UPPER SURFACE FROM BS740 TO 795 AND LBL13 TO RBL13Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, KeelSDR VGCA20250805012Frame · dentedAFT LOWER FUSELAGE FRAME INNER CHORD DENTED AT BS1110 FROM S-24L TO S-28LAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805011Frame · puncturedAFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1090 FROM S-24L TO S-28LAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805010Frame · puncturedFRAME INNER CHORD PUNCTURE AT BS 1090 BETWEEN S26R AND S28R.Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805009Frame · puncturedAFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1130 FROM S-25L TO S-29L.Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805008Frame · crackedFT LOWER FUSELAGE FRAME CRACKED AT BS1070 FROM S-26R TO S-28RAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805007Frame · crackedFORWARD LOWER FUSELAGE FRAME UPPER CHORD CRACKED AT BS700 FROM S-28L TO S-28RAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805006Skin Panel · corrodedAFT LOWER FUSELAGE SKIN CORROSION FROM BS990-1010 AT S-26LAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR VGCA20250805005Shear Web · crackedAFT UPPER FUSELAGE FLOOR SHEAR WEB CRACK NEAR BS1166-1176.9 AND RBL8 TO RBL17.87Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR VGCA20250805004Spar · corrodedWING CENTER BOX FRONT SPAR CORRODED IN MULTIPLE PLACES ON VERTICAL AND HORIZONTAL CHORD FLANGES AT BS740 FROM LBL70.5 TO RBL70.5Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20250805003Flap Track · crackedCRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.Aug 5, 2025 · N216WE · Boeing 7272S2F · Trailing Edge FlapsSDR VGCA20250805002Skin Panel · corrodedAFT LOWER FUSELAGE SKIN PANEL CORROSION FROM BS1148-1166 AND S-18L TO S-20L.Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR VGCA20250805001Keelbeam · corrodedCENTER FUSELAGE SECTION RH DELTA BEAM LOWER CHORD CORRODED FROM BS720F-755 AND S-27L TO S-27RAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, KeelSDR VGCA20211113001None · noneDURING CLIMB WHILE PASSING THROUGH FL250 THE AIRCRAFT EXPERIENCED A RAPID DECOMPRESSON THAT WAS NOT CONTROLLABLE FROM THE FLIGHT DECK. EMERGENCY DECENT WAS INITATED AND AIRCRAFT RETURNED WITHOUT FURTHER INCIDENTNov 13, 2021 · N216WE · Boeing 7272S2F · Cabin Pressure Control SystemSDR VGCA2020072016001Cabin Pressure · abnormalLOST CABIN PRESSUURIZATION AT FLIGHT LEVEL 30000, CABIN ALTITUDE WARNING HORN SOUNDED AT 10000 FEET CABIN PRESSURE. UNABLE TO CONTROL CABIN PRESSURE WITH OUTFLOW VALVE CLOSED.Jul 16, 2020 · N216WE · Boeing 7272S2F · Cabin Pressure Control SystemSDR VGCA2020041309007Seat Track · gougedSEAT TRACK GOUGED IN MAIN CARGO DEK FLOOR AT BS. 625, RBL 62.5. FOUND BEYOND ALLOWABLE DAMAGE. SEGEMENT OF SEAT TRACK REPLACED IN ACCORDANCE WITH B727 SRMApr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR VGCA2020041309006Pressure Panel · puncturedPRESSURE PAN WEB PUNCHTURED BETWEEN BS. 880 - 890 AND LBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH PART IN ACCORDANCE WITH B727 SRM.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage Main, StructureSDR VGCA2020041309005Pressure Panel · puncturedPRESSURE PAN WEB PUNCTURED BETWEEN BS. 880 - 890 AND RBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH NEW PART IN ACCORDANCE WITH B727 SRMApr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage Main, StructureSDR VGCA2020041309004Seat Track · crackedSEAT TRACK FLANGE CRACKED IN MAIN CARGO DECK FLOOR AT BS. 870, LBL, 62.5. FOUND BEYOND ALLOWABLE DAMAGE. SEAT TRACK SEGMENT REPLACED IN ACCORDANCE WITH B727 SRM.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR VGCA2020041309003Seat Track · gougedSEAT TRACK FLANGE GOUGED IN MAIN CARGO DECK FLOOR AT BS. 870, LBL 45.5. FOUND BEYOND ALLOWABLE DAMAGE. SEAT TRACK SEGMENT REPLACED IN ACCORDANCE WITH B727 SRM.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR VGCA2020041309002Panel · dentedHORIZONTAL STABILIZER LH SIDE LEADING EDGE PANEL #9122 REWORKED (BLEND OUT) DENT FOUND BEYOND ALLOWABLE DAMAGE, REPAIRED IN ACCORDANCE WITH B727-200 SRMApr 9, 2020 · N216WE · Boeing 7272S2F · Horizontal Stabilizer, Plate/SkinSDR VGCA2020041309001Web · crackedWEB TANGS CRACKED AT BS. 600 AND BS 620 BETWEEN STR. 3L AND STR. 4L, ABOVE MAIN CARGO DOOR. PART REPLACEMENT REQUIRED.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR VGCA20150901001Light · dimCOCKPIT EMER EXIT LIGHTS DIM. REPLACED EMER EXIT LIGHT UNIT.Sep 1, 2015 · N216WE · Boeing 7272S2F · Emergency LightingSDR VGCA20140620001Service Panel · departedNUMBER 1 ENG VIBRATION IN FLIGHT, AFTER LANDING PERFORMED WALK AROUND AT WHICH POINT DISCOVERED THE LT HYD ACCESS PANEL MISSING & DENT IN LT INLET COWLING RESULTING IN SUSPECTED FOD DAMAGE.Jun 20, 2014 · N216WE · Boeing 7272S2F · Hydraulic Compartment DoorsSDR VGCA20140425001Slat · damagedRIGHT HAND SLAT TE NR 5 DAMAGED.Apr 25, 2014 · N216WE · Boeing 7272S2F · Leading Edge DevicesSDR VGCA201205100001Fire Loop · shortedINTERMITTENT FIRE WARNING.May 10, 2012 · N216WE · Boeing 7272S2F · Fire DetectionSDR VGCA201201090001Sill · corrodedDOOR SILL HAS CORROSION, REPAIRED.Jan 9, 2012 · N216WE · Boeing 7272S2F · Fuselage Miscellaneous Structure
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