# N836UP: 1968 Douglas DC-8-73F, registration cancelled 2008-12-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 24, 2008
- 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: 45936
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 5, 1984
- Certificate issued: December 4, 1984
- Last registry action: September 19, 2006
- Mode S code: AB7074
- 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/N836UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=836UP
- Page: https://openairdocs.org/deregistered/N836UP-2008-12-24

From the FAA registry file of October 29, 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 (164, newest 50)

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

- [SDR UPS03840659](https://openairdocs.org/sdr/UPS03840659), May 8, 2003: SKIN. CRACKED. RT INBD FLAP INBD WEB CRACKED. REMOVED ONE AREA OF CRACKED SKIN. D. RIEKE. 75838 5-8-03. REMOVED WEB. FABRICATED NEW WEB FROM 2024-T3 .040" PER SAMPLE. STARTED 
- [SDR UPS02839977](https://openairdocs.org/sdr/UPS02839977), Dec 10, 2002: CONNECTOR. FAILED. INSPECTION TYPE: PFLT, EMERGENCY LIGHT DISARM CHECK INOPERATIVE. REPLACED CONNECTOR PLUG P01-1345. SYSTEM CHECKS GOOD IAW M/M 33-50-01
- [SDR UPS02839951](https://openairdocs.org/sdr/UPS02839951), Dec 1, 2002: LIGHT. INOPERATIVE. INSPECTION TYPE: ASV, EMERGENCY LIGHTS INOPERATIVE. REPAIRED OPEN AT P1-1345 PIN 11 AS REQUIRED REF WDW 33-50-01. SYSTEM OPS NORMAL.
- [SDR UPS02837816](https://openairdocs.org/sdr/UPS02837816), Mar 11, 2002: BATTERY PACK. DISCHARGED. INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS BATTERY DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY SYSTEM, OPS CHECKS NORMAL PER MM 33-50-01.
- [SDR UPS02837388](https://openairdocs.org/sdr/UPS02837388), Jan 2, 2002: BATTERY PACK. DISCHARGED. INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, LIGHTS OPS CHECKED OK.
- [SDR UPS01837366](https://openairdocs.org/sdr/UPS01837366), Dec 13, 2001: BATTERY PACK. DISCHARGED. INSPECTION TYPE:AS EMERGENCY LIGHTS ARE INOP IN TEST. REMOVED, REPLACED, AND TESTED EMERGENCY BATTERY PACK IAW MM 33-50-01.
- [SDR UPS01837362](https://openairdocs.org/sdr/UPS01837362), Dec 7, 2001: BATTERY PACK. DISCHARGED. INSPECTION TYPE:IN NO ILLUM OF EMERGENCY LIGHTS. REMOVED AND REPLACED BATTERY (EMERGENCY) PACK, OPS CHECK GOOD 33-50.
- [SDR UPS01837152](https://openairdocs.org/sdr/UPS01837152), Oct 20, 2001: SEAT TRACK. CRACKED. INSPECTION TYPE:C23 STA 1520 LBL 55 SEAT TRACK IS CRACKED. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.
- [SDR UPS01837142](https://openairdocs.org/sdr/UPS01837142), Oct 15, 2001: INTERCOSTAL. CRACKED. INSPECTION TYPE:C23 FWD ENTRY DOOR AFT TORQUE BOX HAS A CRACKED INTERCOSTAL STA 60-70 BETWEEN LONG 14L-15L. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5597646, AN
- [SDR UPS01837145](https://openairdocs.org/sdr/UPS01837145), Oct 12, 2001: FRAME. CORRODED. INSPECTION TYPE:C23 STA 1240 FRAME IS CORRODED BEYOND LIMITS LONG 35R-36. REPAIRED FRAME IAW 8110-3 APPROVED DH SK 836-901, BY INSTALLING A REPAIR STRAP IAW DH 
- [SDR UPS01837108](https://openairdocs.org/sdr/UPS01837108), Oct 10, 2001: FITTING. CRACKED. INSPECTION TYPE:C23 RIGHT WING STRINGER 64 SPLICE FITTING IS CRACKED AT APPROX XRS 510. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3644046 AND SRM 51-1-2
- [SDR UPS01837144](https://openairdocs.org/sdr/UPS01837144), Oct 6, 2001: FINGER DOUBLER. CORRODED. INSPECTION TYPE:C23 STA 70-120 LONG 31R FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5779916, AND SRM 51-1-20D, 5
- [SDR UPS01837141](https://openairdocs.org/sdr/UPS01837141), Oct 6, 2001: FRAME. CRACKED. INSPECTION TYPE:C23 STA 55 RT SIDE FRAME IS CRACKED ABOVE FITTING AT CUSP. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.
- [SDR UPS01837109](https://openairdocs.org/sdr/UPS01837109), Oct 6, 2001: ANGLE. CRACKED. INSPECTION TYPE:C23 LEFT HORIZONTAL STAB T/E UPPER ANGLE IS CRACKED AT XE 29. REPAIRED ANGLE IAW SRM 55-2-0 FIG 2.
- [SDR UPS01837110](https://openairdocs.org/sdr/UPS01837110), Oct 5, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT HORIZONTAL STAB LOWER RIB IS CRACKED AT XFS 135. REPAIRED RIB IAW SRM 55-2-0 FIG 2.
- [SDR UPS01837148](https://openairdocs.org/sdr/UPS01837148), Oct 5, 2001: SEAT TRACK. CORRODED. INSPECTION TYPE:C23 SEAT TRACK STA 1020-1040 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.
- [SDR UPS01837147](https://openairdocs.org/sdr/UPS01837147), Oct 5, 2001: SEAT TRACK. CORRODED. INSPECTION TYPE:C23 SEAT TRACK STA 1400-1540 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.
- [SDR UPS01837146](https://openairdocs.org/sdr/UPS01837146), Oct 5, 2001: FRAME. CORRODED. INSPECTION TYPE:C23 STA 12 FRAME AND WEB ARE CORRODED BEYOND LIMITS AT RBL 48. REPAIRED FRAME BY INSTALLING FILLER AND ANGLE DOUBLER IAW 8110-3 APPROVED DH SK 8
- [SDR UPS01837143](https://openairdocs.org/sdr/UPS01837143), Oct 5, 2001: SEAT TRACK. CORRODED. INSPECTION TYPE:C23 SEAT TRACK IS CORRODED BEYOND LIMITS STA 1130-1150 AT LBL 60. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A, AND DC8-53B-003-501.
- [SDR UPS01837135](https://openairdocs.org/sdr/UPS01837135), Oct 5, 2001: FITTING. CRACKED. INSPECTION TYPE:C23 LEFT HORIZONTAL STAB LOWER FLANGE FITTING AT FRONT SPAR IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D.
- [SDR UPS01837140](https://openairdocs.org/sdr/UPS01837140), Oct 4, 2001: ANGLE. CRACKED. INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB ANGLE IS CRACKED AT XS 472.099. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5770170, AND SRM 51-1-20D, 51-1-21.
- [SDR UPS01837134](https://openairdocs.org/sdr/UPS01837134), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837132](https://openairdocs.org/sdr/UPS01837132), Oct 4, 2001: SPLICE. CRACKED. INSPECTION TYPE:C23 STA 440 - 460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.
- [SDR UPS01837120](https://openairdocs.org/sdr/UPS01837120), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 404. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837119](https://openairdocs.org/sdr/UPS01837119), Oct 4, 2001: CLIP. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED CLIP IAW DWG 5769589, AND SRM 51-1-21.
- [SDR UPS01837118](https://openairdocs.org/sdr/UPS01837118), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837117](https://openairdocs.org/sdr/UPS01837117), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 491.193. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837116](https://openairdocs.org/sdr/UPS01837116), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837115](https://openairdocs.org/sdr/UPS01837115), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 366.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837114](https://openairdocs.org/sdr/UPS01837114), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837113](https://openairdocs.org/sdr/UPS01837113), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 515.72. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837112](https://openairdocs.org/sdr/UPS01837112), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837111](https://openairdocs.org/sdr/UPS01837111), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 834. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837107](https://openairdocs.org/sdr/UPS01837107), Oct 4, 2001: FITTING. CRACKED. INSPECTION TYPE:C23 STA 280 LONG 21R FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754032, AND SRM 51-1-20D.
- [SDR UPS01837096](https://openairdocs.org/sdr/UPS01837096), Oct 4, 2001: FITTING. CRACKED. INSPECTION TYPE:C23 STA 610 LONG 26R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51-1-20D, 53-1-0.
- [SDR UPS01837032](https://openairdocs.org/sdr/UPS01837032), Oct 4, 2001: DOUBLER. CORRODED. INSPECTION TYPE:C23 RIGHT WING L/E STALL WARNING DOUBLER IS CORRODED BEYOND LIMITS AT XFS 373. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SR
- [SDR UPS01837027](https://openairdocs.org/sdr/UPS01837027), Oct 4, 2001: SPLICE. CRACKED. INSPECTION TYPE:C23 STA 600-620 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D, 51-3-0.
- [SDR UPS01837026](https://openairdocs.org/sdr/UPS01837026), Oct 4, 2001: ANGLE. CRACKED. INSPECTION TYPE:C23 NR 2 STUB WING VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0
- [SDR UPS01837021](https://openairdocs.org/sdr/UPS01837021), Oct 4, 2001: DOUBLER. CRACKED. INSPECTION TYPE:C23 LEFT WING L/E INBOARD WRAP-AROUND DOUBLER IS CRACKED AT XFS 304. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D
- [SDR UPS01837013](https://openairdocs.org/sdr/UPS01837013), Oct 4, 2001: CLIP. CRACKED. INSPECTION TYPE: C23, LEFT WING L/E. INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED,FABRICATED,AND REPLACED CLIP I.A.W.DWG. 5769589,AND SRM. 51- 1-2
- [SDR UPS01837011](https://openairdocs.org/sdr/UPS01837011), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 354 AND XFS 379 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01837010](https://openairdocs.org/sdr/UPS01837010), Oct 4, 2001: RIB. CRACKED. INSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 297.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01837007](https://openairdocs.org/sdr/UPS01837007), Oct 4, 2001: FITTING. CRACKED. INSPECTION TYPE: C23, STA. 440-460 LONG. 31R SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3750257,AND SRM. 51-1-20D
- [SDR UPS01837006](https://openairdocs.org/sdr/UPS01837006), Oct 4, 2001: DOUBLER. CRACKED. INSPECTION TYPE: C23, LEFT WING L/E. LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.25 REMOVED,FABRICATED,AND REPLACED DOUBLER I.A.W. DWG. 5769589,A
- [SDR UPS01837155](https://openairdocs.org/sdr/UPS01837155), Oct 3, 2001: SKIN. CRACKED. INSPECTION TYPE:C23 R-2 DOOR UPPER AFT CORNER OF OPENING SKIN, INTERNAL DOUBLER, AND LONGERON 11R ARE CRACKED AT STA 1654. REPAIRED SKIN AND INTERNAL DOUBLER, A
- [SDR UPS01837139](https://openairdocs.org/sdr/UPS01837139), Oct 3, 2001: RIB. CRACKED. INSPECTION TYPE:C23 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75, XFS 835. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837138](https://openairdocs.org/sdr/UPS01837138), Oct 3, 2001: SPLICE. CRACKED. INSPECTION TYPE:C23 STA 210 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754220, AND SRM 51-1-20D.
- [SDR UPS01837137](https://openairdocs.org/sdr/UPS01837137), Oct 3, 2001: RIB. CRACKED. INSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 628.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837136](https://openairdocs.org/sdr/UPS01837136), Oct 3, 2001: RIB. CRACKED. INSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 578.75, XFS 585. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.
- [SDR UPS01837104](https://openairdocs.org/sdr/UPS01837104), Oct 3, 2001: DOUBLER. CRACKED. INSPECTION TYPE:C23 LEFT WING L/E INTERNAL WRAP AROUND DOUBLER IS CRACKED AT XFS 566.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1

All 164: https://openairdocs.org/deregistered/N836UP-2008-12-24/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 19870312009439I](https://openairdocs.org/incident/19870312009439I), Mar 12, 1987: Doug DC873F (N836UP), Des Moines, IA. Landed long and during turn around on overrun, landing gear broke through the asphalt.

## Other aircraft with N836UP

- [Registered now](https://openairdocs.org/aircraft/N836UP): Beechcraft B300, S/N FL-966, built 2014

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