N2674U, cancelled Apr 26, 2005

Service difficulty reports · 78

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 = 'N2674U' AND deregistration_id = 'N2674U-2005-04-26'
  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 RRXA010030Indicator · faultyIN FLIGHT, SAI SHOWS A 20 DEG RIGHT BANK AND 5 DEG TO 6 DEG NOSE UP IN LEVEL FLIGHT. SAI WILL THEN RETURN TO A 3 DEG RIGHT BANK AND 5 DEG''''S TO 6 DEG''''S NOSE UP. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR. OPS CHECKS NORMAL IAW MM CH 34-00-00.Mar 28, 2001 · N2674U · Doug DC873F · Attitude and Direction Data SystemSDR RRXA000545Current Limiter · burned outELEC BURNING SMELL ON DESCENT "CREW OPENED AUX PUMP C/B AS A PRECAUTION" (SMELL STARTED TO DISIPATE). FOUND 3 EA CURRENT LIMITERS BURNT, R&R AS REQUIREDJun 10, 2000 · N2674U · Doug DC873F · Hydraulic Pump, AuxiliarySDR RRXA001760Web · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE MAIN CABIN CUSP WEB AT FS 268 AND RBL 50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001759Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MAIN CABIN FLOORBEAM AT FS 1750 AND BL 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FLOORBEAM IAW DC-8 SRM 51-1-20D.May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA001758Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIB AT THE RT STUB WING OVER NR 3 PYLON AT XFS 207.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0.May 9, 2000 · N2674U · Doug DC873F · Wing, Rib/BulkheadSDR RRXA001757Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE MAIN CARGO DOOR THRESHOLD SUPPORT ANGLES AT FS 200 AND 220, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLES IAW DC-8 SRM 51-1-2May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001740Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE MAIN CARGO DOOR SCUFF PLATE AREA BRACKET AT FS 260, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001739Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN STRINGER TIE END AT FS 1688 TO 1690 AND STR 26L AND 28L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PART IAW DMay 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001738Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE DOUBLER ON LONGERON L28L AT FS 600 , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-3-0.May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001737Stiffener · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE BULKHEAD STIFFENER AT FS 129 AND RBL 40, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED STIFFENER IAW DC-8 SRM 51-1-20D.May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001735Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE UPPER FWD FLANGE FLOORBEAM AT FS 680 AND RBL 52, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA001756Web · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT MLG DOOR UPLOCK TORQUE BOX VERTICALLY IN THE RADIUS OF THE ATTACH FLANGE APPROX. 2 INCHES LONG AT THE FWD WEB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1May 8, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001755Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE OF THE RT WING LE SKIN 2 INCHES FWD OF THE WING SPAR AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001754Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001753Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN ON UPPER SIDE AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001752Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE SKIN ON UPPER SIDE 2 INCHES FWD OF THE WING SPAR AT THE RT WING LEADING EDGE AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001736Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LEFT WHEEL WELL PRESSURE PANEL AT FS 915 TO 925 AND LBL 58 TO 65, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR RRXA001734Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WW PRESSURE PANEL, FS 857 TO 879 AND LBL 58 TO 65, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR RRXA001751Floorbeam · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ALONG THE RADIUS OF THE UPPER FLANGE IN THE MAIN CABIN FLOORBEAM AT FS 1660 AND RBL 48, WL-1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REMay 1, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA001733Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOORBEAM UPPER CAP, FS 760 AND LBL 24 TO 44, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED IAW DALFORT AEROSPACE, L.May 1, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA001742Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CARGO DOOR AFT EDGE OF SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 52-2-0.Apr 24, 2000 · N2674U · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001741Frame · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE MAIN CARGO DOOR LOWER AFT CORNER FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 52-2-0.Apr 24, 2000 · N2674U · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001729Skin · bulgedDURING A MAINTENANCE VISIT, FOUND COOROSION DAMAGE TO THE FUSELAGE SKIN AT BS 320 AND STR 28L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1.Apr 24, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001750Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE LWR SURFACE AT THE LT WING LE SKIN 5 INCHES FWD OF THE WING SPAR AT XFS 335, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAWApr 3, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001749Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE AFT END OF THE CENTER WING BOX LWR SKIN EXTERIOR AT FS 855 AND BL 68R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8Apr 3, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001748Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE INBD DRAG ANGLE ON FOR NR 3 PYLON 1 INCH AFT WING SPAR AT XRS 198, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW DRAG ANGLE IAW DC-8 SApr 3, 2000 · N2674U · Doug DC873F · Nacelle/Pylon StructureSDR RRXA001747Floorboard · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE DRAIN PLUG HOLE ON THE MAIN CABIN FLOOR PANEL, AT BS 1200 AND RBL 10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SApr 3, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA001732Floorboard · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOORBOARD, FS 987 TO 990 AND LBL 16 TO 19, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-Apr 3, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA001731Web · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE MAIN CABIN COURIER AREA FLOOR WEB AT FS 25 TO 45 AND LBL 48 TO 75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR WEBApr 3, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA002155Door Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MAIN CARGO DOOR LOWER AFT CORNER FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 53-2-3.Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Main, StructureSDR RRXA002154Door Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MAIN CARGO DOOR UPPER AFT CORNER FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 53-2-3.Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Main, StructureSDR RRXA002150Skin · bulgedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE SKIN AT STR 28L AND BS 320, DAMAGE EXCEEDED LIMITATIONS IAW DC-8S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-1.Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA002149Pressure Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEFT WHEEL WELL PRESSURE FLOOR AT FS 857-879 AND LBL 58-65, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW XEA-X8-53-874.Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA002161Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT AFT EDGE OF SKIN IN "D" BAG BIN DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, 51-1-20D.Mar 13, 2000 · N2674U · Doug DC873F · Cargo/Baggage DoorsSDR RRXA002160Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK 2 INCHES FWD OF THE WING SPAR ON THE RIGHT WING LEADING EDGE SKIN AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, Mar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/SkinSDR RRXA002159Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE UPPER SIDE 2 INCHES FWD OF THE WING SPAR ON THE RT WING LEADING EDGE SKIN AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IMar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/SkinSDR RRXA002158Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LIGHTNING HOLE BELOW THE LEFT HINGE ON THE RADOME BULKHEAD AT FS 156, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, 51-1Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR RRXA002157Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK 5 INCHES FWD OF THE WING SPAR ON THE LEFT WING LEADING EDGE SKIN LOWER SURFACE AT XFS 335, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAWMar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/SkinSDR RRXA002156Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE ON THE AFT END OF THE CENTER WING BOX LOWER SKIN EXTERIOR AT FS 855 AND XCW 68 RT., DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLMar 13, 2000 · N2674U · Doug DC873F · Wing Miscellaneous StructureSDR RRXA002151Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN COURIER AREA FLOOR WEB AT FS 25-45 AND RBL 48-75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-4.Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA001743Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LIGHTNING HOLE BELOW THE LEFT HINGE ON THE RADOME BULKHEAD AT FS 156, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW DC-Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, BulkheadSDR RRXA002164Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING LEADING EDGE SKIN AT THE INBD PRESSURE FUELING RECEPTICAL CUT OUT AT XRS 261, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAMar 10, 2000 · N2674U · Doug DC873F · Wing, Plate/SkinSDR RRXA002163Floor Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN 2 PLACES TO THE MAIN CABIN FLOOR PANEL AT FWD ENTRY DOOR AT FS 25-45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, 51-1-20DMar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA002162Floor Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE DRAIN PLUG HOLE ON THE MAIN CABIN FLOOR PLANK AT BS 1200 AND RBL 10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, 51-1-Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA002153Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOOR PLANK AT FS 850-879 AND LBL 26-27, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 53-2-3.Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA002152Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOOR PLANK AT FS 987-990 AND LBL 16-19, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 53-2-3.Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA001745Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT WING LEADING EDGE SKIN AT THE INBD PRESSURE FUELING RECEPTICAL AT XRS 261, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW Mar 10, 2000 · N2674U · Doug DC873F · Leading Edge DevicesSDR RRXA001744Floorboard · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK IN TWO PLACES TO THE MAIN CABIN FLOOR PANEL AT FWD ENTRY DOOR AT FS 25 TO 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IMar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA001730Floorboard · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOORBOARD, FS 850 TO 879 AND LBL 26 TO 27, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DMar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA002165Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK APPROX. 2 IN. LONG ON THE FWD WEB OF THE RT MAIN LANDING GEAR DOOR UPLOCK TORQUE BOX IN RADIUS OF THE ATTACH FLANGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEMar 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure
Back to N2674U, cancelled Apr 26, 2005