# N2674U: 1969 Douglas DC-8-73F, registration cancelled 2005-04-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 26, 2005 - Status when cancelled: Sale reported - Airframe: [Douglas DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f) (registry code 302199F) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46062 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 26, 1984 - Last registry action: February 28, 2003 - Mode S code: A29BF5 - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N2674U - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2674U - Page: https://openairdocs.org/deregistered/N2674U-2005-04-26 From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Douglas DC-8-73F: https://openairdocs.org/model/douglas-dc-8-73f.md ## Service difficulty reports (78, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RRXA010030](https://openairdocs.org/sdr/RRXA010030), Mar 28, 2001: INDICATOR. FAULTY. 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 NOS - [SDR RRXA000545](https://openairdocs.org/sdr/RRXA000545), Jun 10, 2000: CURRENT LIMITER. BURNED OUT. 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), May 9, 2000: WEB. CRACKED. 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 ARE - [SDR RRXA001759](https://openairdocs.org/sdr/RRXA001759), May 9, 2000: FLOORBEAM. CRACKED. 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 - [SDR RRXA001758](https://openairdocs.org/sdr/RRXA001758), May 9, 2000: RIB. CRACKED. 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, - [SDR RRXA001757](https://openairdocs.org/sdr/RRXA001757), May 9, 2000: ANGLE. CRACKED. 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 D - [SDR RRXA001740](https://openairdocs.org/sdr/RRXA001740), May 9, 2000: ANGLE. CORRODED. 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 - [SDR RRXA001739](https://openairdocs.org/sdr/RRXA001739), May 9, 2000: STRINGER CLIP. CORRODED. 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- - [SDR RRXA001738](https://openairdocs.org/sdr/RRXA001738), May 9, 2000: DOUBLER. CORRODED. 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 - [SDR RRXA001737](https://openairdocs.org/sdr/RRXA001737), May 9, 2000: STIFFENER. CORRODED. 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, TRE - [SDR RRXA001735](https://openairdocs.org/sdr/RRXA001735), May 9, 2000: FLOORBEAM. CORRODED. 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 DAM - [SDR RRXA001756](https://openairdocs.org/sdr/RRXA001756), May 8, 2000: WEB. CRACKED. 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 - [SDR RRXA001755](https://openairdocs.org/sdr/RRXA001755), May 8, 2000: SKIN. CRACKED. 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- - [SDR RRXA001754](https://openairdocs.org/sdr/RRXA001754), May 8, 2000: SKIN. CRACKED. 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 - [SDR RRXA001753](https://openairdocs.org/sdr/RRXA001753), May 8, 2000: SKIN. CRACKED. 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 SR - [SDR RRXA001752](https://openairdocs.org/sdr/RRXA001752), May 8, 2000: SKIN. CRACKED. 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 LIM - [SDR RRXA001736](https://openairdocs.org/sdr/RRXA001736), May 8, 2000: PRESSURE PANEL. CORRODED. 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 - [SDR RRXA001734](https://openairdocs.org/sdr/RRXA001734), May 8, 2000: PRESSURE PANEL. CORRODED. 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. REMOVE - [SDR RRXA001751](https://openairdocs.org/sdr/RRXA001751), May 1, 2000: FLOORBEAM. CRACKED. 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 LIMITATI - [SDR RRXA001733](https://openairdocs.org/sdr/RRXA001733), May 1, 2000: FLOORBEAM. CORRODED. 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. REM - [SDR RRXA001742](https://openairdocs.org/sdr/RRXA001742), Apr 24, 2000: SKIN. CRACKED. 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 - [SDR RRXA001741](https://openairdocs.org/sdr/RRXA001741), Apr 24, 2000: FRAME. CRACKED. 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 - [SDR RRXA001729](https://openairdocs.org/sdr/RRXA001729), Apr 24, 2000: SKIN. BULGED. 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 - [SDR RRXA001750](https://openairdocs.org/sdr/RRXA001750), Apr 3, 2000: SKIN. CRACKED. 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 - [SDR RRXA001749](https://openairdocs.org/sdr/RRXA001749), Apr 3, 2000: SKIN. CRACKED. 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 - [SDR RRXA001748](https://openairdocs.org/sdr/RRXA001748), Apr 3, 2000: ANGLE. CRACKED. 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. RE - [SDR RRXA001747](https://openairdocs.org/sdr/RRXA001747), Apr 3, 2000: FLOORBOARD. CRACKED. 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. - [SDR RRXA001732](https://openairdocs.org/sdr/RRXA001732), Apr 3, 2000: FLOORBOARD. CORRODED. 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. REMOV - [SDR RRXA001731](https://openairdocs.org/sdr/RRXA001731), Apr 3, 2000: WEB. CORRODED. 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- - [SDR RRXA002155](https://openairdocs.org/sdr/RRXA002155), Mar 20, 2000: DOOR FRAME. CRACKED. 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 I - [SDR RRXA002154](https://openairdocs.org/sdr/RRXA002154), Mar 20, 2000: DOOR FRAME. CRACKED. 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 I - [SDR RRXA002150](https://openairdocs.org/sdr/RRXA002150), Mar 20, 2000: SKIN. BULGED. 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 - [SDR RRXA002149](https://openairdocs.org/sdr/RRXA002149), Mar 20, 2000: PRESSURE PANEL. CORRODED. 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. R - [SDR RRXA002161](https://openairdocs.org/sdr/RRXA002161), Mar 13, 2000: SKIN. CRACKED. 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- - [SDR RRXA002160](https://openairdocs.org/sdr/RRXA002160), Mar 13, 2000: SKIN. CRACKED. 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 S - [SDR RRXA002159](https://openairdocs.org/sdr/RRXA002159), Mar 13, 2000: SKIN. CRACKED. 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 LIMITATION - [SDR RRXA002158](https://openairdocs.org/sdr/RRXA002158), Mar 13, 2000: BULKHEAD. CRACKED. 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. - [SDR RRXA002157](https://openairdocs.org/sdr/RRXA002157), Mar 13, 2000: SKIN. CRACKED. 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 - [SDR RRXA002156](https://openairdocs.org/sdr/RRXA002156), Mar 13, 2000: ANGLE. CRACKED. 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 LIMITA - [SDR RRXA002151](https://openairdocs.org/sdr/RRXA002151), Mar 13, 2000: WEB. CORRODED. 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. - [SDR RRXA001743](https://openairdocs.org/sdr/RRXA001743), Mar 13, 2000: BULKHEAD. CRACKED. 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. - [SDR RRXA002164](https://openairdocs.org/sdr/RRXA002164), Mar 10, 2000: SKIN. CRACKED. 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 LIMITATION - [SDR RRXA002163](https://openairdocs.org/sdr/RRXA002163), Mar 10, 2000: FLOOR PANEL. CRACKED. 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. REMO - [SDR RRXA002162](https://openairdocs.org/sdr/RRXA002162), Mar 10, 2000: FLOOR PANEL. CRACKED. 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. R - [SDR RRXA002153](https://openairdocs.org/sdr/RRXA002153), Mar 10, 2000: FLOOR PANEL. CORRODED. 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 D - [SDR RRXA002152](https://openairdocs.org/sdr/RRXA002152), Mar 10, 2000: FLOOR PANEL. CORRODED. 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 D - [SDR RRXA001745](https://openairdocs.org/sdr/RRXA001745), Mar 10, 2000: SKIN. CRACKED. 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 D - [SDR RRXA001744](https://openairdocs.org/sdr/RRXA001744), Mar 10, 2000: FLOORBOARD. CRACKED. 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 - [SDR RRXA001730](https://openairdocs.org/sdr/RRXA001730), Mar 10, 2000: FLOORBOARD. CORRODED. 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. REMOV - [SDR RRXA002165](https://openairdocs.org/sdr/RRXA002165), Mar 9, 2000: WEB. CRACKED. 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, DA All 78: https://openairdocs.org/deregistered/N2674U-2005-04-26/reports.md ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20010316003589I](https://openairdocs.org/incident/20010316003589I), Mar 16, 2001: Doug DC873F (N2674U), Newburgh, NY. (-23) On March 16, 2001 emery flight 349 inbound for swf reported a loss of oil quantity on #1 engine. The engine was shutdown in flight. Maintenance found the… - [Incident 19881208065339I](https://openairdocs.org/incident/19881208065339I), Dec 8, 1988: Doug DC873F (N2674U), Ontario, CA, Minor damage. Nr 1 engine nacelle damaged during landing. Discovered by maintenance during post flight inspection. - [Incident 19850215026469I](https://openairdocs.org/incident/19850215026469I), Feb 15, 1985: Doug DC873F (N2674U), Chicago, IL, Minor damage. Wingtip struck radome of parked aal aircraft during taxi. Misinterpretation of ground persons signals. ## Other aircraft with N2674U - [Cancelled 1963-09-04](https://openairdocs.org/deregistered/N2674U-1963-09-04): Cessna 172D, S/N 17250274. Exported to Germany. Owner: [Lake Air Corp](https://openairdocs.org/faa-owner/LAKE%20AIR%20CORP), [Michigan City, IN](https://openairdocs.org/faa-place/IN/Michigan%20City) --- 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.