# N874UP: 1969 Douglas DC-8-73F, registration cancelled 2011-04-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 5, 2011 - Status when cancelled: Triennial form not returned - 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: 46074 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 21, 1986 - Certificate issued: December 20, 1985 - Last registry action: September 15, 2009 - Mode S code: AC0702 - Owner when cancelled: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO) - Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville) - Owner type: Corporation - Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N874UP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=874UP - Page: https://openairdocs.org/deregistered/N874UP-2011-04-05 From the FAA registry file of November 3, 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 (244, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UPS09854290](https://openairdocs.org/sdr/UPS09854290), Jan 7, 2009: ENGINE. FLAMED OUT. INSPECTION TYPE:N/A, NR 3 ENGINE FLAMEOUT. ***SDR FILED OPEN*** - [SDR UPS08854209](https://openairdocs.org/sdr/UPS08854209), Dec 16, 2008: FUEL. CONTAMINATED. INSPECTION TYPE:N/A IFSD - NR 1 ENGINE FLAMED OUT AS POWER WAS BROUGHT TO IDLE FOR DESCENT OUT OF 380. PERFORMED FLAME OUT CK LIST AT FL 240 ENGINE STARTED AND - [SDR UPS08852991](https://openairdocs.org/sdr/UPS08852991), Aug 5, 2008: FITTING. INOPERATIVE. IN CRUISE, HYD QTY DROPPING RUN CK LIST, STOPPED AT AUX PUMP LEVEL. PRESS NEVER BELOW 3000 PSI. R/R HYD FITTING AT LT MLG AFT HYD MANIFOLD, FAR OB POS FOR BOGIE - [SDR UPS08852001](https://openairdocs.org/sdr/UPS08852001), Apr 9, 2008: SEAL. MISSING. INSPECTION TYPE:N/A CREW PBE MISSING THE UPPER GREEN LOCKED SEAL. REPLACED LOCK SEAL. - [SDR UPS08851446](https://openairdocs.org/sdr/UPS08851446), Jan 16, 2008: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK GOOD, REF AMM 33-50-01-2, P/N ON 60-1223-5, S/N ON 341. - [SDR UPS08851677](https://openairdocs.org/sdr/UPS08851677), Jan 2, 2008: BATTERY PACK. NOT SEATED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT ARM. RESEATED BATTERY PACK. OPS CHECK NORMAL. - [SDR UPS07851240](https://openairdocs.org/sdr/UPS07851240), Dec 3, 2007: BRACKET. CRACKED. INSPECTION TYPE:SP BRACKET CRACKED AT 3 BOLT HOLES L/WING FRONT SPAR UPPER INBD CORNER STA 680. REMOVED, FABRICATED, AND INSTALLED REPAIR BRACKET AT L/WING FRON - [SDR UPS07851239](https://openairdocs.org/sdr/UPS07851239), Dec 2, 2007: BRACKET. BROKEN. INSPECTION TYPE:SP BROKEN BRACKET ON FUSELAGE ABOVE LEADING EDGE AUX TANK, L/WING. REMOVED, FABRICATED AND INSTALLED REPAIR BRACKET ON L/WING AUX TANK STA XCW 6 - [SDR UPS07851013](https://openairdocs.org/sdr/UPS07851013), Oct 26, 2007: HOUSING. OPEN. ESCAPE SLIDE HOUSING IS PARTIALLY OPEN. SECURED ESCAPE SLIDE HOUSING PER MM 25-60-01-2. - [SDR UPS07850683](https://openairdocs.org/sdr/UPS07850683), Sep 6, 2007: SKIN. CORRODED. INSPECTION TYPE:C1 CORROSION ON FUSELAGE EXTERIOR L35L, STA 1075. REPAIRED DAMAGED EXTERIOR FUSELAGE SKIN AT STA L35L, STA 1075 IAW SAA EA 008-5330-01-A1087, UP - [SDR UPS07850481](https://openairdocs.org/sdr/UPS07850481), Aug 11, 2007: FLOORBEAM. CORRODED. INSPECTION TYPE:C1 FLOORBEAM AT STA 240 BL-0 HAS CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 240 BL 0 IAW SRM 53-02-00 FIG 001. FABRICATED - [SDR UPS07850462](https://openairdocs.org/sdr/UPS07850462), Aug 11, 2007: INTERCOSTAL. CRACKED. INSPECTION TYPE:C1 INTERCOSTAL CRACKED AT STA 1650 LBL 3. STOP DRILLED CRACKED INTERCOSTAL AT STA 1650 LBL 3 IAW SRM 51-1-21, FABRICATED AND INSTALLED REPAIR DO - [SDR UPS07850664](https://openairdocs.org/sdr/UPS07850664), Aug 9, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 MAIN CABIN FRAME FITTING CRACKED AT STA 980 L19L. REPAIRED MAIN CABIN FRAME FITTING AT STA 980 L19L IAW SAA EA 008- 5310-01-A1020, UPS RAA DC - [SDR UPS07850611](https://openairdocs.org/sdr/UPS07850611), Aug 9, 2007: FITTING. CORRODED. INSPECTION TYPE:C1 MAIN CABIN FRAME FITTING HAS EXFOLIATION CORROSION AND CRACK AT STA 940 L21L. REPAIRED FRAME FITTING AT STA 940 L21L IAW SAA EA 008-5310-01-A - [SDR UPS07850504](https://openairdocs.org/sdr/UPS07850504), Aug 9, 2007: LONGERON SPLICE. CRACKED. INSPECTION TYPE:C1 .25 INCH CRACK LWR ROW STA 1749 ON L28R SPLICE AND EXISTING REPAIR THAT IS NOT PER SRO8530032. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AR - [SDR UPS07850503](https://openairdocs.org/sdr/UPS07850503), Aug 8, 2007: SKIN. CORRODED. INSPECTION TYPE:C1 MAJOR CORROSION BETWEEN STA 1620 - 1640 L31L - L31R, BETWEEN SKIN AND INTERNAL DOUBLER, CORROSION AROUND OUTFLOW VALVE. REMOVED AND REPLACED - [SDR UPS07850477](https://openairdocs.org/sdr/UPS07850477), Aug 7, 2007: SUPPORT ANGLE. CORRODED. INSPECTION TYPE:C1 CORROSION UNDER NUT PLATES IN AFT CABIN SUBFLOOR, STA 1746-1756 ALONG RBL 17. REMOVED SUPPORT, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. - [SDR UPS07850484](https://openairdocs.org/sdr/UPS07850484), Aug 6, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 FITTING CRACKED AT STA 1260 L20R. REMOVED AND REPLACED FITTING AT STA 1260 L20R IAW SRM 51-01-20D AND SRM 51-3-2. - [SDR UPS07850483](https://openairdocs.org/sdr/UPS07850483), Aug 6, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 STA 1060 FRAME FITTING IS GOUGED. REMOVED FRAME FITTING AT STA 1060 IAW SRM 51-3-0. LOCATED, DRILLED UP AND INSTALLED NEW FRAME FITTING AT ST - [SDR UPS07850465](https://openairdocs.org/sdr/UPS07850465), Aug 6, 2007: WEB. CRACKED. INSPECTION TYPE:C1 FWD LWR CORNER OF FWD RIGHT SERVICE DOOR HAS CRACK IN WEB. CUT OUT DAMAGED AREA ON FWD LWR CORNER WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02 - [SDR UPS07850464](https://openairdocs.org/sdr/UPS07850464), Aug 6, 2007: WEB. DAMAGED. INSPECTION TYPE:C1 LARGE PUNCTURE AND 2EA CRACKS IN WEB AT AFT UPPER SECTION OF INTERIOR OF RIGHT FWD SERVICE DOOR. CUT OUT DAMAGED AREA FROM WEB ON RIGHT FWD S - [SDR UPS07850463](https://openairdocs.org/sdr/UPS07850463), Aug 6, 2007: WEB. DAMAGED. INSPECTION TYPE:C1 HOLE DRILLED THROUGH FASTENER AND INTO FWD CENTER WEB OF RIGHT FWD SERVICE DOOR INTERIOR. CUT OUT DAMAGED AREA FROM CENTER WEB ON RIGHT FWD S - [SDR UPS07850461](https://openairdocs.org/sdr/UPS07850461), Aug 6, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 FITTING CRACKED AT STA 1240 L20R. REMOVED CRACKED FITTING AT STA 1240 L20R IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPAIR FITTING AT STA - [SDR UPS07850451](https://openairdocs.org/sdr/UPS07850451), Aug 6, 2007: WEB. PUNCTURED. INSPECTION TYPE:C1 HOLE PUNCTURED IN INTERIOR WEB OF RIGHT FWD SERVICE DOOR FWD CENTER AREA. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM - [SDR UPS07850442](https://openairdocs.org/sdr/UPS07850442), Aug 6, 2007: FINGER DOUBLER. CRACKED. INSPECTION TYPE:C1 CENTER WING BOX SUBFLOOR FINGER DOUBLER CRACKED AT STA 890 LBL 5. REMOVED CRACKED FINGER DOUBLER AT STA 890 LBL 5 IAW SRM 51-1-20D, FABRICATE - [SDR UPS07850432](https://openairdocs.org/sdr/UPS07850432), Aug 5, 2007: WEB. CRACKED. INSPECTION TYPE:C1 WEB CRACKED ON RIGHT AFT SERVICE DOOR AFT SIDE BELOW BAYONET. STOP DRILLED END OF CRACK ON WEB IAW SRM 52-02-00 FIG 02. FABRICATED AND INSTAL - [SDR UPS07850592](https://openairdocs.org/sdr/UPS07850592), Aug 4, 2007: SEAT TRACK. GOUGED. INSPECTION TYPE:C1 SEAT TRACK GOUGED AT STA 317 RBL 60. REMOVED DAMAGED SEAT TRACK AT STA 317 RBL 60 IAW EO DC8-5340-7779. INSTALLED SEAT TRACK PLUG AT STA 317 - [SDR UPS07850506](https://openairdocs.org/sdr/UPS07850506), Aug 4, 2007: SEAT TRACK. GOUGED. INSPECTION TYPE:C1 SEAT TRACK GOUGED OUT OF LIMITS AT STA 240 BL 0. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 230-250 BL 0 IAW SRM 53-02-03-0 FIG 014, 53 - [SDR UPS07850466](https://openairdocs.org/sdr/UPS07850466), Aug 4, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 FITTING CRACKED AT STA 1230 TO STA 1240 L19R. REMOVED CRACKED FITTING AT STA 1230 TO 1240 L19R IAW SRM 51-01-20D, FABRICATED AND INSTALLED RE - [SDR UPS07850482](https://openairdocs.org/sdr/UPS07850482), Aug 3, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L9L FWD. REMOVED CRACKED END FITTING AT STA 680 L9L IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALL - [SDR UPS07850431](https://openairdocs.org/sdr/UPS07850431), Aug 3, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 902 L9L AFT. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L9L AFT IAW SRM 51-1-20D, AND SRM 51-3- - [SDR UPS07850427](https://openairdocs.org/sdr/UPS07850427), Aug 3, 2007: BULKHEAD. CRACKED. INSPECTION TYPE:C1 AFT PRESS BULKHEAD CRACKED RBL 24 L10R TO L12R. CUT OUT DAMAGED AREA ON AFT PRESS BULKHEAD STA 1766 RBL 24 L10R TO L12R IAW SRM 53-2-5. FABRI - [SDR UPS07850419](https://openairdocs.org/sdr/UPS07850419), Aug 3, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L10R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L10R FWD IAW SRM 51-3-0, SRM 51-1-21D, - [SDR UPS07850426](https://openairdocs.org/sdr/UPS07850426), Jul 4, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 FITTING CRACKED AT STA 1160 L19R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 1160 L19R IAW SRM 51-1-20D, AND SRM 51-01-24. - [SDR UPS07849138](https://openairdocs.org/sdr/UPS07849138), Feb 7, 2007: GIRT BAR. STIFF. INSPECTION TYPE:N/A THE EMERGENCY ESCAPE SLIDE GIRT BAR IS VERY DIFFICULT TO ENGAGE & DISENGAGE. REPACKED EMERGENCY ESCAPE SLIDE IN ITS CONTAINER. GIRT BAR STOW - [SDR UPS06847287](https://openairdocs.org/sdr/UPS06847287), Jul 3, 2006: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY LIGHTS DISARM CHECK FAIL. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK & CHARGED. OPS CHECKS NORMAL. - [SDR UPS06846246](https://openairdocs.org/sdr/UPS06846246), Feb 22, 2006: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY DEAD. FOUND DURING PRE-DEPARTURE CHECK. REPLACED PER MM 33-50-01-2, CHECKS OK. - [SDR UPS05845864](https://openairdocs.org/sdr/UPS05845864), Dec 7, 2005: BATTERY PACK. ACTIVATED. EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-01. - [SDR UPS05845862](https://openairdocs.org/sdr/UPS05845862), Dec 6, 2005: LIGHT. INOPERATIVE. EMERGENCY LIGHTS DISARM CHECK LIGHT INOP. RELAMPED IAW 33-15-00-2. OPS CK GOOD. - [SDR UPS05845642](https://openairdocs.org/sdr/UPS05845642), Oct 20, 2005: FLAP SYSTEM. SPLIT. RIGHT HAND INBD FLAP OUTBD HINGE BRACKET COVER FWD PANEL CRACKED. INSTALLED INTERIM AIRWORTHY PANEL IAW EO DC8-5720-23117-A. DEFERRAL D312507 PER EO. REPLACED P - [SDR UPS05845450](https://openairdocs.org/sdr/UPS05845450), Sep 13, 2005: RIB. CRACKED. INSPECTION TYPE:C3 WHILE WORKING NR 808576, FOUND LT WING I/B FLAP LWR O/B SIDE 3RD RIB FROM LWR AT XW120 CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM - [SDR UPS05845541](https://openairdocs.org/sdr/UPS05845541), Sep 12, 2005: FITTING. CORRODED. INSPECTION TYPE: C3, DEEP CORROSION PITTING AROUND LOWER FASTENER THRU BATHTUB FITTING AT STA. 1153 ABOVE L33R. REMOVED BATHTUB FITTING, FABRICATED SPLICE ANGLE - [SDR UPS05845531](https://openairdocs.org/sdr/UPS05845531), Sep 12, 2005: LONGERON. CRACKED. C3 - CRACKED LONGERON AT STA 1736 L15R. CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, 53-2-2 FIG 10 AND DWG - [SDR UPS05845530](https://openairdocs.org/sdr/UPS05845530), Sep 12, 2005: FITTING. CRACKED. C3 - D-PIT DOOR INTERIOR FWD UPPER ANGLE CRACKED JUST BELOW UPPER STOP. REMOVED AND REPLACED DOOR UPPER ANGLE SUPPORT FITTING IAW SRM 51-1-2 AND 51-3-0. - [SDR UPS05845491](https://openairdocs.org/sdr/UPS05845491), Sep 12, 2005: LONGERON. CRACKED. FOUND CRACKED LONGERON AT STA 1756 L14L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-3-0, 53-2-2 FIG 11 AND 51-1-20D. - [SDR UPS05845553](https://openairdocs.org/sdr/UPS05845553), Sep 11, 2005: FITTING. CORRODED. INSPECTION TYPE:C3 CORROSION ON BACK UP FITTING AT STA 320 BETWEEN L33R-L34R. REMOVED BACK UP FITTING AND INSTALLED REPLACEMENT FITTING AND CLIPS IAW SRM 51-1-2 - [SDR UPS05845517](https://openairdocs.org/sdr/UPS05845517), Sep 11, 2005: FITTING. CORRODED. INSPECTION TYPE:C3 DEEP CORROSION PIT OR DRILL START IN BATHTUB FITTING TA STA 315 BETWEEN L33R AND L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D, - [SDR UPS05845516](https://openairdocs.org/sdr/UPS05845516), Sep 11, 2005: INTERCOSTAL. CORRODED. INSPECTION TYPE:C3 HEAVY CORROSION ON INTERCOSTAL AT STA 1079 L35L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW 51-1-20D AND DWG 9758 507. - [SDR UPS05845515](https://openairdocs.org/sdr/UPS05845515), Sep 10, 2005: FITTING. CRACKED. INSPECTION TYPE:C3 INSIDE 60 HOLE, LONGERON END FITTING CRACKED 2" LONG AT STA 1766 L10R. REMOVED AND REPLACED END FITTING IAW SRM 51-3-0, 51-1-21 AND 51-1-20D. - [SDR UPS05845490](https://openairdocs.org/sdr/UPS05845490), Sep 10, 2005: FITTING. CRACKED. RT WING FUEL TANK NR 4 ALTERNATE STA XW 408 LWR STR NR 58 END FITTING CRACKED 2" LONG. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D. All 244: https://openairdocs.org/deregistered/N874UP-2011-04-05/reports.md ## Other aircraft with N874UP - [Cancelled 2025-09-04](https://openairdocs.org/deregistered/N874UP-2025-09-04): Textron B300, S/N FL-1119, built 2017. Exported to Benin. Owner: [Asi Aircraft Corp](https://openairdocs.org/faa-owner/ASI%20AIRCRAFT%20CORP), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) --- 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.