# Service difficulty reports: N2674U, cancelled Apr 26, 2005 A list on [N2674U, cancelled Apr 26, 2005](https://openairdocs.org/deregistered/N2674U-2005-04-26.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 78 reports - [SDR RRXA010030](https://openairdocs.org/sdr/RRXA010030.md): Indicator · faulty · Mar 28, 2001 · N2674U · Doug DC873F · Attitude and Direction Data System > IN 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. - [SDR RRXA000545](https://openairdocs.org/sdr/RRXA000545.md): Current Limiter · burned out · Jun 10, 2000 · N2674U · Doug DC873F · Hydraulic Pump, Auxiliary > ELEC 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 REQUIRED - [SDR RRXA001760](https://openairdocs.org/sdr/RRXA001760.md): Web · cracked · May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA001759](https://openairdocs.org/sdr/RRXA001759.md): Floorbeam · cracked · May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor Beam > DURING 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. - [SDR RRXA001758](https://openairdocs.org/sdr/RRXA001758.md): Rib · cracked · May 9, 2000 · N2674U · Doug DC873F · Wing, Rib/Bulkhead > DURING 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. - [SDR RRXA001757](https://openairdocs.org/sdr/RRXA001757.md): Angle · cracked · May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure > DURING 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 51-1-2 - [SDR RRXA001740](https://openairdocs.org/sdr/RRXA001740.md): Angle · corroded · May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure > DURING 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- - [SDR RRXA001739](https://openairdocs.org/sdr/RRXA001739.md): Stringer Clip · corroded · May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure > DURING 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 D - [SDR RRXA001738](https://openairdocs.org/sdr/RRXA001738.md): Doubler · corroded · May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/Skin > DURING 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. - [SDR RRXA001737](https://openairdocs.org/sdr/RRXA001737.md): Stiffener · corroded · May 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA001735](https://openairdocs.org/sdr/RRXA001735.md): Floorbeam · corroded · May 9, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor Beam > DURING 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. - [SDR RRXA001756](https://openairdocs.org/sdr/RRXA001756.md): Web · cracked · May 8, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure > DURING 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 51-1 - [SDR RRXA001755](https://openairdocs.org/sdr/RRXA001755.md): Skin · cracked · May 8, 2000 · N2674U · Doug DC873F · Leading Edge Devices > DURING 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. - [SDR RRXA001754](https://openairdocs.org/sdr/RRXA001754.md): Skin · cracked · May 8, 2000 · N2674U · Doug DC873F · Leading Edge Devices > DURING 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. - [SDR RRXA001753](https://openairdocs.org/sdr/RRXA001753.md): Skin · cracked · May 8, 2000 · N2674U · Doug DC873F · Leading Edge Devices > DURING 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. - [SDR RRXA001752](https://openairdocs.org/sdr/RRXA001752.md): Skin · cracked · May 8, 2000 · N2674U · Doug DC873F · Leading Edge Devices > DURING 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. - [SDR RRXA001736](https://openairdocs.org/sdr/RRXA001736.md): Pressure Panel · corroded · May 8, 2000 · N2674U · Doug DC873F · Fuselage Main, Bulkhead > DURING 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. - [SDR RRXA001734](https://openairdocs.org/sdr/RRXA001734.md): Pressure Panel · corroded · May 8, 2000 · N2674U · Doug DC873F · Fuselage Main, Bulkhead > DURING 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. - [SDR RRXA001751](https://openairdocs.org/sdr/RRXA001751.md): Floorbeam · cracked · May 1, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor Beam > DURING 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 RE - [SDR RRXA001733](https://openairdocs.org/sdr/RRXA001733.md): Floorbeam · corroded · May 1, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor Beam > DURING 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. - [SDR RRXA001742](https://openairdocs.org/sdr/RRXA001742.md): Skin · cracked · Apr 24, 2000 · N2674U · Doug DC873F · Cargo/Baggage Doors > DURING 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. - [SDR RRXA001741](https://openairdocs.org/sdr/RRXA001741.md): Frame · cracked · Apr 24, 2000 · N2674U · Doug DC873F · Cargo/Baggage Doors > DURING 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. - [SDR RRXA001729](https://openairdocs.org/sdr/RRXA001729.md): Skin · bulged · Apr 24, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/Skin > DURING 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. - [SDR RRXA001750](https://openairdocs.org/sdr/RRXA001750.md): Skin · cracked · Apr 3, 2000 · N2674U · Doug DC873F · Leading Edge Devices > DURING 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 IAW - [SDR RRXA001749](https://openairdocs.org/sdr/RRXA001749.md): Skin · cracked · Apr 3, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/Skin > DURING 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-8 - [SDR RRXA001748](https://openairdocs.org/sdr/RRXA001748.md): Angle · cracked · Apr 3, 2000 · N2674U · Doug DC873F · Nacelle/Pylon Structure > DURING 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 S - [SDR RRXA001747](https://openairdocs.org/sdr/RRXA001747.md): Floorboard · cracked · Apr 3, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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 S - [SDR RRXA001732](https://openairdocs.org/sdr/RRXA001732.md): Floorboard · corroded · Apr 3, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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- - [SDR RRXA001731](https://openairdocs.org/sdr/RRXA001731.md): Web · corroded · Apr 3, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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 WEB - [SDR RRXA002155](https://openairdocs.org/sdr/RRXA002155.md): Door Frame · cracked · Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Main, Structure > DURING 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. - [SDR RRXA002154](https://openairdocs.org/sdr/RRXA002154.md): Door Frame · cracked · Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Main, Structure > DURING 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. - [SDR RRXA002150](https://openairdocs.org/sdr/RRXA002150.md): Skin · bulged · Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/Skin > DURING 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. - [SDR RRXA002149](https://openairdocs.org/sdr/RRXA002149.md): Pressure Panel · corroded · Mar 20, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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. - [SDR RRXA002161](https://openairdocs.org/sdr/RRXA002161.md): Skin · cracked · Mar 13, 2000 · N2674U · Doug DC873F · Cargo/Baggage Doors > DURING 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. - [SDR RRXA002160](https://openairdocs.org/sdr/RRXA002160.md): Skin · cracked · Mar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/Skin > DURING 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, - [SDR RRXA002159](https://openairdocs.org/sdr/RRXA002159.md): Skin · cracked · Mar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/Skin > DURING 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 I - [SDR RRXA002158](https://openairdocs.org/sdr/RRXA002158.md): Bulkhead · cracked · Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, Bulkhead > DURING 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, 51-1 - [SDR RRXA002157](https://openairdocs.org/sdr/RRXA002157.md): Skin · cracked · Mar 13, 2000 · N2674U · Doug DC873F · Wing, Plate/Skin > DURING 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 IAW - [SDR RRXA002156](https://openairdocs.org/sdr/RRXA002156.md): Angle · cracked · Mar 13, 2000 · N2674U · Doug DC873F · Wing Miscellaneous Structure > DURING 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 INSTALL - [SDR RRXA002151](https://openairdocs.org/sdr/RRXA002151.md): Web · corroded · Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, Floor Beam > DURING 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. - [SDR RRXA001743](https://openairdocs.org/sdr/RRXA001743.md): Bulkhead · cracked · Mar 13, 2000 · N2674U · Doug DC873F · Fuselage Main, Bulkhead > DURING 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- - [SDR RRXA002164](https://openairdocs.org/sdr/RRXA002164.md): Skin · cracked · Mar 10, 2000 · N2674U · Doug DC873F · Wing, Plate/Skin > DURING 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 IA - [SDR RRXA002163](https://openairdocs.org/sdr/RRXA002163.md): Floor Panel · cracked · Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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, 51-1-20D - [SDR RRXA002162](https://openairdocs.org/sdr/RRXA002162.md): Floor Panel · cracked · Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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- - [SDR RRXA002153](https://openairdocs.org/sdr/RRXA002153.md): Floor Panel · corroded · Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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. - [SDR RRXA002152](https://openairdocs.org/sdr/RRXA002152.md): Floor Panel · corroded · Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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. - [SDR RRXA001745](https://openairdocs.org/sdr/RRXA001745.md): Skin · cracked · Mar 10, 2000 · N2674U · Doug DC873F · Leading Edge Devices > DURING 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 - [SDR RRXA001744](https://openairdocs.org/sdr/RRXA001744.md): Floorboard · cracked · Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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 I - [SDR RRXA001730](https://openairdocs.org/sdr/RRXA001730.md): Floorboard · corroded · Mar 10, 2000 · N2674U · Doug DC873F · Fuselage Floor Panel > DURING 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 D - [SDR RRXA002165](https://openairdocs.org/sdr/RRXA002165.md): Web · cracked · Mar 9, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous Structure > DURING 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. FABRICATE Next page: https://openairdocs.org/deregistered/N2674U-2005-04-26/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N2674U-2005-04-26/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.