# N705UP: 1968 Douglas DC-8-71F, registration cancelled 2010-03-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 30, 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: [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: 45949
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 14, 1985
- Certificate issued: June 18, 1985
- Last registry action: September 15, 2009
- Mode S code: A968F1
- 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/N705UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=705UP
- Page: https://openairdocs.org/deregistered/N705UP-2010-03-30

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-8-71F: https://openairdocs.org/model/douglas-dc-8-71f.md

## Service difficulty reports (188, newest 50)

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

- [SDR UPS07851215](https://openairdocs.org/sdr/UPS07851215), Nov 26, 2007: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, SYSTEM OPS CHECKS GOOD PER MM 33-50-01-2.
- [SDR UPS07850983](https://openairdocs.org/sdr/UPS07850983), Oct 23, 2007: ENGINE. FLAMED OUT. NNNDURING CRUISE FLT W/ENG ANTI-ICE ON (TAT -1), NR 4 ENGINE FLAMED OUT. ENG INDICATIONS WERE NORMAL. RESTART ACCOMPLISHED. ENG OPERATED NORMALLY FOR REMAINDER 
- [SDR UPS07850131](https://openairdocs.org/sdr/UPS07850131), Jun 29, 2007: BULKHEAD. CRACKED. INSPECTION TYPE:C3 MAIN CABIN AFT PRESS BULKHEAD CRACKED 2 INCHES LONG AT STA 1766 BETWEEN L10L AND L11L, LBL 30. CUT OUT DAMAGED AREA OF PRESS BULKHEAD STA 176
- [SDR UPS07850212](https://openairdocs.org/sdr/UPS07850212), Jun 26, 2007: FLOORBEAM. CRACKED. INSPECTION TYPE:C3 CRACKED FLOORBEAM SUPPORT FITTING FS 340 RBL 60 A-PIT DOOR UPPER CUTOUT L21 CUSP AREA. REMOVED AND REPLACED FLOORBEAM SUPPORT FITTING AT STA 
- [SDR UPS07850168](https://openairdocs.org/sdr/UPS07850168), Jun 23, 2007: DOUBLER. CRACKED. INSPECTION TYPE:C3 LT/WING OUTBOARD L/E INNER DOUBLER CRACKED AT STA XFS 597. REMOVED CRACKED INNER DOUBLER AT LT/WING OUTBOARD L/E AT STA XFS 597. FABRICATED A
- [SDR UPS07850123](https://openairdocs.org/sdr/UPS07850123), Jun 23, 2007: DOOR FRAME. DAMAGED. INSPECTION TYPE:C3 DOUBLE DRILLED HOLES IN WEB AT LWR AFT CORNER OF L2 DOOR JAMB STA 1667. TRIMMED OUT DAMAGED AREA OF WEB AND FRAME SEGMENT OF L2 DOOR LWR AFT 
- [SDR UPS07850088](https://openairdocs.org/sdr/UPS07850088), Jun 23, 2007: DOUBLER. CRACKED. INSPECTION TYPE:C3 L/WING OUTBD L/E UPPER INNER DOUBLER CRACKED AT STA XW 761. REMOVED INNER DOUBLER ON L/WING OUTBD L/E AT STA XW 761 IAW SRM 51-1-21. FABRICAT
- [SDR UPS07850053](https://openairdocs.org/sdr/UPS07850053), Jun 23, 2007: RIB. CRACKED. INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE AT STA XFS 641 IS CRACKED. STOP DRILLED CRACK AT STA XFS 641 L/WING LEADING EDGE IAW SRM 57-2- 0 FIG 002. FABRICATE
- [SDR UPS07850052](https://openairdocs.org/sdr/UPS07850052), Jun 23, 2007: RIB. CRACKED. INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE RIB CRACKED AT STA XFS 672. STOP DRILLED CRACK AT STA XFS 672 L/WING LEADING EDGE IAW SRM 57-2- 0 FIG 002. FABRICAT
- [SDR UPS07850051](https://openairdocs.org/sdr/UPS07850051), Jun 23, 2007: RIB. CRACKED. INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE UPPER RIB CRACKED AT XFS 678. STOP DRILLED CRACK AT STA XFS 678 L/WING LEADING EDGE IAW SRM 57-02-00-0 FIG 002. FAB
- [SDR UPS07850050](https://openairdocs.org/sdr/UPS07850050), Jun 23, 2007: RIB. CRACKED. C3 L/WING LEADING EDGE OUTBD LWR RIB CRACKED AT STA XFS 772. STOP DRILLED CRACK ON RIB AT STA XFS 772 L/WING LEADING EDGE IAW SRM 57-02-00 FIG 002. FABRICATED A
- [SDR UPS07850195](https://openairdocs.org/sdr/UPS07850195), Jun 22, 2007: RIB. CRACKED. INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 697. STOP DRILLED CRACK AT XFS 697 RIGHT WING IAW SRM 51-1-21. INSTALLED DOUBLER IAW SRM
- [SDR UPS07850097](https://openairdocs.org/sdr/UPS07850097), Jun 22, 2007: FITTING. CRACKED. INSPECTION TYPE:C3 LONGERON END FITTING AT STA 1770 L10R IS CRACKED. REMOVED CRACKED END FITTING AT STA 1770 L10R IAW SRM 51-1-21. LOCATED, DRILLED-UP, AND INST
- [SDR UPS07850096](https://openairdocs.org/sdr/UPS07850096), Jun 22, 2007: DOUBLER. CRACKED. INSPECTION TYPE:C3 R/WING CENTER L/E INNER DOUBLER CRACKED AT DRAIN HOLE AT STA XFS 334. REMOVED CRACKED INNER DOUBLER AT R/WING STA XFS 334 IAW SRM 51-1-21. FA
- [SDR UPS07850081](https://openairdocs.org/sdr/UPS07850081), Jun 22, 2007: DOUBLER. CRACKED. INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER AND LWR INNER DOUBLER CRACKED AT STA XW 761. REMOVED CRACKED DOUBLERS AT R/WIND L/E STA XW 761 IAW SRM 51-1-21. FABRIC
- [SDR UPS07850080](https://openairdocs.org/sdr/UPS07850080), Jun 22, 2007: CHANNEL. CRACKED. INSPECTION TYPE:C3 R/WING CENTER L/E OUTBD T CHANNEL IS CRACKED. STOP DRILLED CRACKED T CHANNEL AT R/WING STA X 501 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTA
- [SDR UPS07850079](https://openairdocs.org/sdr/UPS07850079), Jun 22, 2007: RIB. CRACKED. INSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 360. STOPPED DRILLED CRACKED RIB AT R/WING L/E STA XFS 360 IAW SRM 57-03 -03-0 FIG 7. FABRICAT
- [SDR UPS07850078](https://openairdocs.org/sdr/UPS07850078), Jun 22, 2007: RIB. CRACKED. INSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 461 STOPPED DRILLED CRACK RIB AT STA XFS 461 IAW SRM 57-03-03-0 FIG 7. FABRICATED AND INSTALLE
- [SDR UPS07850077](https://openairdocs.org/sdr/UPS07850077), Jun 22, 2007: RIB. CRACKED. INSPECTION TYPE:C3 L/WING OUTBD L/E LWR RIB CRACKED AT STA XFS 734. STOPPED DRILLED CRACKED RIB AT L/WING LE STA XFS 734 IAW SRM 57-02- 0 FIG 2. FABRICATED AND 
- [SDR UPS07850076](https://openairdocs.org/sdr/UPS07850076), Jun 22, 2007: RIB. CRACKED. INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 816. STOPPED DRILLED CRACK AT R/WING L/E STA XFS 816 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED R
- [SDR UPS07850075](https://openairdocs.org/sdr/UPS07850075), Jun 22, 2007: RIB. CRACKED. INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 734. STOP DRILLED CRACK ON R/WING UPPER OUTBD L/E AT STA XFS 734 IAW SRM 57-03-03-0. FABRICATED AND
- [SDR UPS07850211](https://openairdocs.org/sdr/UPS07850211), Jun 21, 2007: FLOORBEAM. CRACKED. INSPECTION TYPE:C3 INTERCOSTAL CORRODED AROUND AND UNDER NUT PLATE AT FS 50 AND RBL 30. REPAIRED INTERCOSTAL AND FLOORBEAM AT STA 55 RBL 10 TO RBL 28 IAW SAA EA
- [SDR UPS07850149](https://openairdocs.org/sdr/UPS07850149), Jun 21, 2007: CUSP WEB. CRACKED. INSPECTION TYPE:C3 L21L UPPER CUSP BETWEEN STA 1160-1140 CRACKED. CUT OUT CRACKED CUSP SEGMENT AT STA 1130-1160 L21L IAW SRM 53-02-05 FIG 15A. FABRICATED AND IN
- [SDR UPS07850095](https://openairdocs.org/sdr/UPS07850095), Jun 19, 2007: SKIN. CRACKED. INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1742 L17L. CUT OUT DAMAGED AREA OF FUSELAGE SKIN AT STA 1742 L17L IAW SRM 53-02-01-0 FIG 7. FABRICATED 
- [SDR UPS07850082](https://openairdocs.org/sdr/UPS07850082), Jun 19, 2007: SKIN. CRACKED. INSPECTION TYPE:C3 R/WING INBD L/E (AUX TANK) INBD LWR CORNER CRACKED. CUT OUT DAMAGED AREA ON R/WING L/E AUX TANK IAW SRM 57-02-00 FIG 6. FABRICATED AND INSTAL
- [SDR UPS07850234](https://openairdocs.org/sdr/UPS07850234), Jun 18, 2007: SKIN. CRACKED. INSPECTION TYPE:C3 LEFT WING UPPER FRONT SPAR SKIN CRACKED 2 INCHES LONG AT XRS -36.000. REPAIRED LEFT WING UPPER FRONT SPAR SKIN AT STA XRS -36.000 IAW SAA EA 
- [SDR UPS07850129](https://openairdocs.org/sdr/UPS07850129), Jun 17, 2007: SKIN. DENTED. INSPECTION TYPE:C3 LEFT ELEVATOR LWR INBOARD SKIN HAS DEEP DENT. CUT OUT DAMAGED AREA ON L/ELEV INBOARD SKIN IAW SRM 55-02-01 FIG 010, FABRICATED AND INSTALLED 
- [SDR UPS07850124](https://openairdocs.org/sdr/UPS07850124), Jun 17, 2007: SKIN. CANNING. INSPECTION TYPE:C3 L/ELEVATOR UPPER MIDDLE SKIN HAS OIL CANNING ON O/B SIDE. CUT OUT DAMAGED SKIN SECTION FROM L/ELEVATOR, UPPER MIDDLE STA 219 - 234 IAW SRM 55
- [SDR UPS07849967](https://openairdocs.org/sdr/UPS07849967), Jun 13, 2007: WINDOW. DIRTY. INSPECTION TYPE:N/A ESCAPE SLIDE VIEWING WINDOW INOP. REMOVED COVER FROM SLIDE. CLEANED WINDOW, SECURED SLIDE TO DOOR & VERIFIED PROPER CYLINDER PRESSURE, REF M
- [SDR UPS07849724](https://openairdocs.org/sdr/UPS07849724), Apr 30, 2007: BATTERY PACK. WEAK. DURING PDC, FOUND EMERGENCY LIGHTING DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. OPS CHECK GOOD.
- [SDR UPS07849499](https://openairdocs.org/sdr/UPS07849499), Mar 14, 2007: INDICATOR. DISLODGED. DOOR SLIDE PRESS INDICATOR SLIDE OUT OF SIGHT. CANNOT READ. REPACKED/REPOSITIONED SLIDE INDICATOR, NOW IN VIEW.
- [SDR UPS06848800](https://openairdocs.org/sdr/UPS06848800), Dec 23, 2006: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A CENTER LIGHT UNDER GLARESHIELD FOR EMERGENCY LIGHT ARM INOP. ACCOMPLISHED OPERATIONAL TEST, NO DISCREPANCY NOTED IAW MM 33-50-01.
- [SDR UPS06847708](https://openairdocs.org/sdr/UPS06847708), Aug 15, 2006: GAUGE. OUT OF POSITION. FOUND ESCAPE SLIDE PRESSURE GAUGE NOT IN VIEW. REPOSITIONED SLIDE PACK. OK FOR SERVICE.
- [SDR UPS06847184](https://openairdocs.org/sdr/UPS06847184), Jun 22, 2006: COALESCER BAG. DIRTY. INSPECTION TYPE:N/A STRONG BURNING ODOR WHEN LEFT PACK OPERATED WITH MIX VALVE IN FULL COLD POSITION. REMOVED AND CLEANED LT PACK COALESCER BAG IAW MM 21-55-03-
- [SDR UPS06845928](https://openairdocs.org/sdr/UPS06845928), Jan 9, 2006: SMOKE GOGGLES. SCRATCHED. F/O SMOKE GOGGLES SCRATCHED. REPLACED F/O SMOKE GOGGLES. OPS NORMAL.
- [SDR UPS06845925](https://openairdocs.org/sdr/UPS06845925), Jan 7, 2006: SKIN. CORRODED. FUSELAGE HAS A BULGED AREA 25" FWD OF PIT 31 LWR FWD CORNER MARKED AND ADVISED BY MX. GAINED ACCESS TO THE BACKSIDE OF AREA NO CORROSION OR DEFECTS FOUND AT THI
- [SDR UPS05844805](https://openairdocs.org/sdr/UPS05844805), Jun 25, 2005: INTERCOSTAL. CORRODED. INSPECTION TYPE:C-2, INTERCOSTAL AT STA 980 HAS CORROSION. CORROSION OUT OF LIMITS PER SRM 53-2-0. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-21, AND SRM
- [SDR UPS05844803](https://openairdocs.org/sdr/UPS05844803), Jun 20, 2005: LONGERON. CRACKED. INSPECTION TYPE:C-2, LONGERON 24L CRACKED ON O/B FLANGE. REMOVED AND REPLACED LONGERON 24L IAW SRM 51-3-2, 51-1-8, AND 51-1-20D.
- [SDR UPS05844771](https://openairdocs.org/sdr/UPS05844771), Jun 8, 2005: FITTING. CRACKED. INSPECTION TYPE:C-2. BANANA FITTING CRACKED AT STA 340 L33R. REMOVED AND REPLACED BANANA FITTING AT STA 340 L33R IAW SRM 51-1-20D.
- [SDR UPS05844770](https://openairdocs.org/sdr/UPS05844770), Jun 8, 2005: FRAME. CORRODED. INSPECTION TYPE:C-2. MAIN CARGO STA 1700 RBL 24 SEVERE CORROSION AT TOP OF FRAME ON UNDERSIDE AND CONTINUES OUTBD TO RBL48. CUT OUT DAMAGED AREA PER SRM 51-2-1 
- [SDR UPS05844767](https://openairdocs.org/sdr/UPS05844767), Jun 8, 2005: SEAT TRACK. CORRODED. INSPECTION TYPE:C-2. HEAVY CORROSION IN SEAT TRACK ALONG RBL 59 STA 375-420. REMOVED AND FABRICATED SEAT TRACK PER DWG S2400463. INSTALLED FABBED SEAT TRACK AT 
- [SDR UPS05844766](https://openairdocs.org/sdr/UPS05844766), Jun 8, 2005: FITTING. CORRODED. INSPECTION TYPE:C-2. A-PIT AT STA 320 L33R, BATH TUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BATH TUB FITTING AT A-PIT STA 320 L33R IAW SRM 53-2-0 FIG
- [SDR UPS05844763](https://openairdocs.org/sdr/UPS05844763), Jun 8, 2005: SEAT TRACK. CORRODED. C2 SEAT TRACK HEAVILY CORRODED AT STA 420 LBL 25. REMOVED AND REPLACED SEAT TRACK AT STA 360-560 LBL 25 IAW SRM 51-3-0, 51-3-2, 53B-003-501.
- [SDR UPS05844761](https://openairdocs.org/sdr/UPS05844761), Jun 8, 2005: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK HAS HEAVY CORROSION, STA 1480 RBL 50. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1460-1580 RBL 50 IAW SRM 51-3-0.
- [SDR UPS05844935](https://openairdocs.org/sdr/UPS05844935), Jun 7, 2005: FITTING. CRACKED. INSPECTION TYPE: C2, B-PIT BETWEEN STA 460-440 L28R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IN B-PIT AT STA 460-440, L28R IAW SRM 51-1-21D A
- [SDR UPS05844772](https://openairdocs.org/sdr/UPS05844772), Jun 7, 2005: SKIN. DAMAGED. INSPECTION TYPE:C-2. UPPER PORTION OF RUDDER ON RT SIDE JUST ABOVE LOGO, OIL CANNING OF SKIN. REMOVED AND REPLACED SKIN ON RT SIDE OF RUDDER JUST ABOVE LOGO IAW
- [SDR UPS05844768](https://openairdocs.org/sdr/UPS05844768), Jun 7, 2005: FLOOR SUPPORT. CRACKED. INSPECTION TYPE:C-2. MAIN CABIN STA 759 LBL24 UNDER SEAT TRACK. SEAT TRACK FLOOR SUPPORT FITTING CRACKED. REMOVED AND REPLACED SUPPORT FITTING AT STA 759 LBL24 
- [SDR UPS05844769](https://openairdocs.org/sdr/UPS05844769), Jun 5, 2005: FITTING. CORRODED. INSPECTION TYPE C-2, CORNER FITTING CRACKED AND HEAVILY CORRODED, RT W/W STA 980 CEILING O/B CORNER NEXT TO L24R. REMOVED FITTING IAW SRM 51-1-20D. FABRICATED D
- [SDR UPS05844765](https://openairdocs.org/sdr/UPS05844765), Jun 5, 2005: SKIN. CRACKED. INSPECTION TYPE:C-2. LT ELEVATOR CONTROL TAB SKIN AND DOUBLER CRACKED AT INBD EYEBOLT ACCESS HOLE LWR SKIN. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB ASSY PE
- [SDR UPS05844762](https://openairdocs.org/sdr/UPS05844762), Jun 5, 2005: RIB. CRACKED. LT HORIZ STAB L/E 2ND INBD LWR RIB REPAIR HAS DOUBLER AND TRIPLER CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 55-2-0, 51-1-21

All 188: https://openairdocs.org/deregistered/N705UP-2010-03-30/reports.md

## FAA accident and incident reports (2)

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 19950217008429I](https://openairdocs.org/incident/19950217008429I), Feb 17, 1995: Doug DC871F (N705UP), Atlanta, GA. Narrative: aircraft exited the end of the runway, due to excessive rollout speed.
- [Incident 19900927048999I](https://openairdocs.org/incident/19900927048999I), Sep 27, 1990: Doug DC871F (N705UP), Wichita, KS. Forward cargo door warning at cruise. Some pressure lost. Landed safely.

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