# N750UP: 1968 Douglas DC-8-71F, registration cancelled 2010-04-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 19, 2010
- Status when cancelled: Triennial form not returned
- Airframe: [Douglas DC-8-71F](https://openairdocs.org/model/douglas-dc-8-71f) (registry code 302199D)
- Engine: [Pratt & Whitney JT3D-3&3B](https://openairdocs.org/engine/pratt-whitney-jt3d-3-3b) (registry code 52039)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 45950
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 26, 1968
- Certificate issued: October 15, 1985
- Last registry action: September 15, 2009
- Mode S code: AA1BD9
- 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/N750UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=750UP
- Page: https://openairdocs.org/deregistered/N750UP-2010-04-19

From the FAA registry file of October 31, 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-8-71F: https://openairdocs.org/model/douglas-dc-8-71f.md

## Service difficulty reports (261, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UPS07850577](https://openairdocs.org/sdr/UPS07850577), Sep 1, 2007: STARTER. LEAKING. INSPECTION TYPE:N/A IFSD - NR 1 ENG SHUTDOWN IN CLIMB PASSING 25000 DUE TO OIL QTY GOING TO ZERO. OIL PRESSURE WAS 12 PSI. SERVICED OIL, RAN ENGINE, FOUND OIL L
- [SDR UPS07849884](https://openairdocs.org/sdr/UPS07849884), Jun 4, 2007: SKIN. CORRODED. EVIDENCE OF CORROSION BETWEEN FUSELAGE SKIN, FINGER DOUBLER AND LONGERON 31R, STARTING AT STA 70 AND EXTENDING APPROX 6 FEET REFERENCE D351779 AND FERRY PERMIT 
- [SDR UPS07849428](https://openairdocs.org/sdr/UPS07849428), Mar 14, 2007: LIGHT. INOPERATIVE. ON CREW PREFLIGHT, FOUND EMERGENCY LIGHTS INOP AWAITING CLOSING LP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33-50-01-2. CHECKS GOOD.
- [SDR UPS07849093](https://openairdocs.org/sdr/UPS07849093), Jan 31, 2007: RELAY. INOPERATIVE. INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY/RELAY UNIT. NOW OPS OK. REF 33-50-01-2.
- [SDR UPS07849092](https://openairdocs.org/sdr/UPS07849092), Jan 31, 2007: RELAY. INOPERATIVE. INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTT BATTERY/RELAY UNIT. NOW OPS OK. REF 33-50-01-2.
- [SDR UPS07848864](https://openairdocs.org/sdr/UPS07848864), Jan 14, 2007: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK ASSY IAW MM 33-50-01-2.
- [SDR UPS06848786](https://openairdocs.org/sdr/UPS06848786), Dec 18, 2006: BATTERY PACK. INOPERATIVE. INSPECTION TYPE:N/A ON PRE-DEPARTURE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-01-2.
- [SDR UPS06848341](https://openairdocs.org/sdr/UPS06848341), Oct 24, 2006: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK EMERGENCY EXIT LIGHTS. OPS CHECKS GOOD.
- [SDR UPS06848323](https://openairdocs.org/sdr/UPS06848323), Oct 24, 2006: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS. OPS CKS GOOD.
- [SDR UPS06847301](https://openairdocs.org/sdr/UPS06847301), Jul 7, 2006: FUSE. BLOWN. INSPECTION TYPE:N/A SMOKE AND ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACKGROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE (5AMP) OP'S CHE
- [SDR UPS06847293](https://openairdocs.org/sdr/UPS06847293), Jul 7, 2006: FUSE. BLOWN. SMOKE & ELECTRICAL ODOR CAME FROM BEHIND ENGINEERS PANEL. ALL BACK GROUND LIGHTS ON F/E PANEL WENT OUT. REPLACED BLOWN FUSE-5 AMP. OP'S CHECK NORMAL ON BACKGROU
- [SDR UPS05845559](https://openairdocs.org/sdr/UPS05845559), Oct 7, 2005: GROUND WIRE. SHORTED. CARGO SMOKE LIGHT ILLUMINATED - ALL POSITIONS. T/S SYS FOUND & REPAIRED BAD GROUND WIRE 8M OHMS ON SMOKE DETECTOR UNIT NR 1. FOUND & REPAIRED BAD GND WIRE ON SD
- [SDR UPS05845283](https://openairdocs.org/sdr/UPS05845283), Aug 19, 2005: DOUBLER. CRACKED. NOSE SECTION FUSELAGE SKIN HAS 3/8" CRACK AT AFT HINGE ACCESS DOOR. REMOVED CRACKED DOUBLER AT NOSE EXTERIOR AFT SKIN IAW SRM 51-1-21. FABRICATED AND INSTALLED 
- [SDR UPS05845421](https://openairdocs.org/sdr/UPS05845421), Aug 16, 2005: SPAR. CRACKED. INSPECTION TYPE:C1 RIGHT KEEL BEAM AT FS 857 2.5 INCH CRACK ON LWR SPAR. STOP DRILLED CRACK AT XCW 4.0 IAW SRM 51-1-20D NDT HFEC IAW NDTSPM 06-10-01.001 NO CRAC
- [SDR UPS05845275](https://openairdocs.org/sdr/UPS05845275), Aug 16, 2005: FINGER DOUBLER. CORRODED. COCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEAR HEAD RIVETS AND CORRODED AT STA -67 TO -80 RBL 60. REMOVED FINGER DOUBLER IAW SRM 51-1-21 AND 51-3-0. REMOVED 
- [SDR UPS05845241](https://openairdocs.org/sdr/UPS05845241), Aug 16, 2005: FRAME. CRACKED. FRAME ON 62 DOOR OPENING IS CRACKED INSIDE OPENING RT SIDE. FAB`D DOUBLER AND REPAIRED IAW SRM 53-05-01 AND 51-1-21A.
- [SDR UPS05845236](https://openairdocs.org/sdr/UPS05845236), Aug 16, 2005: FITTING. CORRODED. HEAVY CORROSION ON SPLICE FITTING STA 210 L7R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
- [SDR UPS05845369](https://openairdocs.org/sdr/UPS05845369), Aug 15, 2005: FLOORBEAM. CRACKED. INSPECTION TYPE:C1 FLOORBEAM CRACKED AT FS 55 LBL 12. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 TEMP REV 53-152, FABRICATED DOUBLER AND FILLER AND INSTAL
- [SDR UPS05845285](https://openairdocs.org/sdr/UPS05845285), Aug 15, 2005: FITTING. CRACKED. FS -8 AT L33L BULKHEAD HAS CRACKED END FITTING A/C COMPT. REMOVED AND REPLACED END FITTING AT FS -8 L33L IAW SRM 51-3-0,51-3-2 PG 1 AND 51-1-21.
- [SDR UPS05845282](https://openairdocs.org/sdr/UPS05845282), Aug 15, 2005: FITTING. CRACKED. STA 280 RBL 50 END FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 280 RBL 50 IAW DWG 9754022 AND SRM 51-1-20D.
- [SDR UPS05845256](https://openairdocs.org/sdr/UPS05845256), Aug 15, 2005: FITTING. CRACKED. END FITTING CRACKED LONG 17R FS 1768. REMOVED AND REPLACED END FITTING AT STA 1768 LONG 17R IAW DWG 4772397 AND SRM51-1-20D.
- [SDR UPS05845383](https://openairdocs.org/sdr/UPS05845383), Aug 14, 2005: SPLICE. CRACKED. INSPECTION TYPE:C1 CRACKED SPLICE ANGLE INSIDE CHANNEL AT FS 450 L33R. REMOVED CRACKED SPLICE ANGLE IAW SRM 51-1-21D, MACHINED AND INSTALLED LONGERON SPLICE AT 
- [SDR UPS05845368](https://openairdocs.org/sdr/UPS05845368), Aug 14, 2005: SPLICE. CRACKED. INSPECTION TYPE:C1 SPLICE FITTING AT FS 450 L31R IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31R IAW DWG 5754814 AND SRM 51-1-20D.
- [SDR UPS05845385](https://openairdocs.org/sdr/UPS05845385), Aug 13, 2005: FITTING. CRACKED. INSPECTION TYPE:C1 C-PIT FS 1150 L33R I/B SIDE, FITTING HAS 2EA PLUGGED FASTENERS LOOSE. REMOVED INTERCOSTAL AT FS 1150 L33R IAW SRM 51-1-20D, FABRICATED AND IN
- [SDR UPS05845292](https://openairdocs.org/sdr/UPS05845292), Aug 13, 2005: FITTING. CORRODED. LWR CARGO FS 1230 L32R ZEE FITTING CORRODED AND CRACKED .500 INCH LONG AROUND FASTNER HOLE. REMOVED ZEE FITTING IAW SRM 51-1-21 AND 51-1-20D. REPLACED ZEE FITTI
- [SDR UPS05845255](https://openairdocs.org/sdr/UPS05845255), Aug 13, 2005: SKIN. CRACKED. LT WING AILERON LE UPPER SURFACE AROUND FASTENER HAS 1/4" LONG CRACK PCU AREA. STOP DRILLED CRACK NDT HFEC VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED R
- [SDR UPS05845242](https://openairdocs.org/sdr/UPS05845242), Aug 13, 2005: RIB. CRACKED. LT LE UPPER RIB CRACKED AT XFS 766.250. FAB`D DOUBLER AND REPAIRED IAW DWG 5769470 AND SRM57-02-00 FIG 2.
- [SDR UPS05845240](https://openairdocs.org/sdr/UPS05845240), Aug 13, 2005: RIB. CRACKED. LT WING LE UPPER RIB CRACKED AT XFS 707. FABED DOUBLER AND REPAIRED RIB IAW DWG 5769466, AND SRM 57-2-0 FIG 2.
- [SDR UPS05845239](https://openairdocs.org/sdr/UPS05845239), Aug 13, 2005: FINGER DOUBLER. CORRODED. COCKPIT SUBFLOOR FINGER DOUBLER HAS SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER DOUBLER AT FS -67 TO -52 LBL24. REMOVED AND REPLACED FINGER DOUBLER IAW 
- [SDR UPS05845420](https://openairdocs.org/sdr/UPS05845420), Aug 12, 2005: CUSP WEB. CRACKED. INSPECTION TYPE:C1 CUSP CRACKED FS 1100 L21R. REMOVED CUSP DOUBLER AT FS 1100 L21R AND REMOVED DAMAGED SECTION OF L21R IAW SRM 51-1-20A AND SRM 53-2-5 FIG 15. F
- [SDR UPS05845384](https://openairdocs.org/sdr/UPS05845384), Aug 12, 2005: PAN. CRACKED. INSPECTION TYPE:C1 L1 DOOR LWR AFT CORNER JAMB INSIDE WEB CRACKED 2 INCHES LONG. REMOVED DOOR JAMB AND WEB CUT OUT DAMAGED AREA IAW DWG 5597646, FABRICATED DOUB
- [SDR UPS05845294](https://openairdocs.org/sdr/UPS05845294), Aug 12, 2005: CUSP WEB. CRACKED. CUSP HAS SHEAR HEAD FASTENER AND CRACK 1 INCH LONG FS 1420 L21R. REMOVED DAMAGED CUSP FROM BS 1390-1430 L21R IAW SRM 51-1-20D AND 51-1-2. FABRICATED AND INSTALL
- [SDR UPS05845257](https://openairdocs.org/sdr/UPS05845257), Aug 12, 2005: LONGERON. CRACKED. LONGERON 7R CRACKED AT FS 1746. REMOVED DAMAGED AREA IAW SRM 53-02-02 FIG 11, FABRICATED AND INSTALLED REPAIR SPLICE FILLER AND REPAIR ANGLES IAW SRM 53-02-02 F
- [SDR UPS05845254](https://openairdocs.org/sdr/UPS05845254), Aug 12, 2005: LONGERON. CRACKED. LONG 15L CRACKED AT FS 1726. REMOVED DAMAGED AREA IAW SRM 53-2-2 FIG 11. FABRICATED REPAIR SPLICE FILLER AND REPAIR ANGLES AND INSTALLED IAW SRM 53-02-02 FIG 11
- [SDR UPS05845252](https://openairdocs.org/sdr/UPS05845252), Aug 12, 2005: ANGLE. CRACKED. C1 ANGLE CRACKED AT FS 1766 LONG 6L. REMOVED ANGLE IAW SRM 51-1-20D AT FS 1766 LONG 6L. FABRICATED AND INSTALLED ANGLE AT FS 1766 LONG 6L DWG 5773844 AND SRM 51
- [SDR UPS05845251](https://openairdocs.org/sdr/UPS05845251), Aug 12, 2005: ANGLE. CRACKED. C1 ANGLE CRACKED AT FS 1766 LONG 6R. REMOVED CRACKED ANGLE AT FS 1766 L6R IAW SRM 51-1-20D. FABRICATED AND INSTALLED ANGLE AT FS 1766 L6R IAW SRM DWG 5773844 AN
- [SDR UPS05845229](https://openairdocs.org/sdr/UPS05845229), Aug 12, 2005: FITTING. CRACKED. MAIN CABIN LONGERON END FITTING CRACKED AFT SIDE OF STA 680 L2L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-3-0 .
- [SDR UPS05845228](https://openairdocs.org/sdr/UPS05845228), Aug 12, 2005: LONGERON. CRACKED. LONGERON 14R CRACKED FS 1746. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 11.
- [SDR UPS05845227](https://openairdocs.org/sdr/UPS05845227), Aug 12, 2005: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD CRACKED 1.5" LONG FS 1766 RBL 48 L11R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAE DWG SRO 8530007.
- [SDR UPS05845219](https://openairdocs.org/sdr/UPS05845219), Aug 12, 2005: FITTING. CRACKED. FITTING CRACKED AT FS 1150 L19R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.
- [SDR UPS05845371](https://openairdocs.org/sdr/UPS05845371), Aug 11, 2005: FITTING. CRACKED. INSPECTION TYPE:C1 CENTER WING SUB FLOOR FS 759 LBL 48 L-FITTING CRACKED. REMOVED CRACKED L-FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED L-FITTING IAW DWG
- [SDR UPS05845366](https://openairdocs.org/sdr/UPS05845366), Aug 11, 2005: FITTING. CRACKED. INSPECTION TYPE:C1, FITTING CRACKED AT FS 759 L18R AFT SIDE. REMOVED AND REPLACED FITTING AT FS 759 L18R IAW SRM 51-1-20D,51-1-24, AND 51-1-8
- [SDR UPS05845293](https://openairdocs.org/sdr/UPS05845293), Aug 11, 2005: FITTING. CRACKED. FITTING CRACKED AT FS 857.125 L18R AFT SIDE. REMOVED AND REPLACED END FITTING AT FS 857.125 L18R IAW SRM 51-1-20D AND DWG 4750420.
- [SDR UPS05845281](https://openairdocs.org/sdr/UPS05845281), Aug 11, 2005: FITTING. CORRODED. MAIN CABIN TEE FITTING CORRODED AT FS 980 LBL 40. REMOVED CORROSION ON TEE FITTING AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED TEE FITTIN
- [SDR UPS05845280](https://openairdocs.org/sdr/UPS05845280), Aug 11, 2005: FITTING. CRACKED. LONGERON END FITTING CRACKED AT FS 857.125 L10L. REMOVED AND REPLACED LONG END FITTING AT FS 857.125 L10L IAW SRM 51-1-8,51-1-20, 51-3-01 AND 53-3-0.
- [SDR UPS05845279](https://openairdocs.org/sdr/UPS05845279), Aug 11, 2005: FITTING. CRACKED. LONGERON END FITTING CRACKED AT FS 867.125 L5L. REMOVED AND REPLACED LONGERON END FITTING AT FS 857.125 L5L IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.
- [SDR UPS05845277](https://openairdocs.org/sdr/UPS05845277), Aug 11, 2005: FITTING. CRACKED. CRACK ON SPLICE FITTING ON LONG 1L STA 680. REMOVED CRACKED FITTING AND LONGERON SPLICE IAW SRM 51-1-20D, INSTALLED FITTING, SPLICE AND STRAPS IAW SRM 51-1-21,5
- [SDR UPS05845276](https://openairdocs.org/sdr/UPS05845276), Aug 11, 2005: FITTING. CRACKED. MAIN CABIN CENTER SUBFLOOR STA 923 L22L "T" FITTING AROUND FASTNERS AREA HAS HEAVY CORROSION. REMOVED CORROSION FROM "T" FITTING AND VISUALLY FOUND CRACK IAW SR
- [SDR UPS05845274](https://openairdocs.org/sdr/UPS05845274), Aug 11, 2005: FITTING. CRACKED. FS 834.500 L18R FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME FITTING AT STA 834.500 L18R IAW SRM 51-1-20 D, SRM 51-3-2.
- [SDR UPS05845258](https://openairdocs.org/sdr/UPS05845258), Aug 11, 2005: ANGLE. CRACKED. CENTER WING BOX SUB FLOOR "L" ANGLE CRACKED AT FS 798 LBL 48. REMOVED AND REPLACED "L" ANGLE AT FS 798 LBL 48 IAW SRM 51-3-2 AND SRM 51-1-20D.

All 261: https://openairdocs.org/deregistered/N750UP-2010-04-19/reports.md

## FAA accident and incident reports (1)

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 19860103006139I](https://openairdocs.org/incident/19860103006139I), Jan 3, 1986: Doug DC861F (N750UP), Huntingburg, IN. Climbed above assigned altitude due to malfunction as autopilot was engaged. Less than standard separation.

## Other aircraft with N750UP

- [Registered now](https://openairdocs.org/aircraft/N750UP): Pacific Aerospace 750XL, S/N 133, built 2007

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