# N807UP: 1968 Douglas DC-8-73F, registration cancelled 2010-09-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 13, 2010
- 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: 46007
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, showing compliance
- Airworthiness date: September 30, 1982
- Certificate issued: March 10, 1983
- Last registry action: October 20, 2009
- Mode S code: AAFDAE
- 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/N807UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807UP
- Page: https://openairdocs.org/deregistered/N807UP-2010-09-13

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 (268, newest 50)

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

- [SDR UPS08854052](https://openairdocs.org/sdr/UPS08854052), Nov 28, 2008: SKIN. CORRODED. INSPECTION TYPE:N/A AREA OF CORROSION CAUSING RIVET HEADS TO DEFORM ON A/C SKIN LOWER CENTERLINE LOCATED NEAR VHF BLADE ANTENNA. INSTALLED INTERIM REPAIR DOUBLE
- [SDR UPS08853915](https://openairdocs.org/sdr/UPS08853915), Nov 13, 2008: DOOR. OUT OF RIG. INSPECTION TYPE:N/A L1 DOOR EXTREMELY HARD TO OPEN OR CLOSE. RERIGGED L-1 DOOR. OPS CHECK NORMAL.
- [SDR UPS08853700](https://openairdocs.org/sdr/UPS08853700), Oct 20, 2008: BATTERY. DISCHARGED. INSPECTION TYPE:N/A DURING EMERGENCY LIGHT CHECK, EMERGENCY STANDBY LIGHTS FAILED TO ILLUMINATE. REMOVED & REPLACED EMERGENCY LIGHT BATTERY / RELAY ASSY PER MM 
- [SDR UPS08852736](https://openairdocs.org/sdr/UPS08852736), Jul 11, 2008: FRAME. CRACKED. PITS 32 AND 34 CARGO DOOR INNER CRACKS. ISSUED DEFERRAL D380080 IAW EO DC8-5230-29933-A. DAMAGE CONSISTS OF 2.0" LONG CRACK LOCATED ON THE INSIDE RADIUS OF FRAM
- [SDR UPS08851759](https://openairdocs.org/sdr/UPS08851759), Mar 4, 2008: DOOR FRAME. DENTED. MAIN ENTRY DOOR HAD DENT WITH CREASE JUST OUTBD OF BAYONET FITTING DENT MEASURES 1.25 LENGTH BY .750 WIDE AND .150 DEEP. CON'T ON ECA FORM 011317: FABRICATED DO
- [SDR UPS08851697](https://openairdocs.org/sdr/UPS08851697), Feb 21, 2008: ENGINE. FLAMED OUT. INSPECTION TYPE:N/A NR 3 ENGINE FLAMEOUT AT CRUISE. FLT LVL 360, SPEED MACH .81, FUEL NORMAL AND BALANCED. ATTEMPTED RESTART AT FL 300 UNSUCCESSFUL. ATTEMPTED 2
- [SDR UPS08851569](https://openairdocs.org/sdr/UPS08851569), Jan 29, 2008: HOSE. CHAFED. THE CREW EXPERIENCED A HYDRAULIC LEAK. AFTER RUNNING THE CHECKLIST, DECLARED AN EMERGENCY AND CONTINUED TO PHL. AFTER APPROX 20 MIN IN CRUISE, LOST HYD QTY DOWN
- [SDR UPS07851280](https://openairdocs.org/sdr/UPS07851280), Dec 8, 2007: INERTIA REEL. STICKS. CAPTAIN'S LEFT SHOULDER HARNESS INERTIAL REEL IS STICKY. REMOVED AND REPLACED CAPTAIN'S INERTIA REEL. OPS CHECK GOOD.
- [SDR UPS07850686](https://openairdocs.org/sdr/UPS07850686), Sep 17, 2007: BATTERY. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER 33-50-01-2, DC8 AMM. LIGHTS OP'S OK.
- [SDR UPS07850620](https://openairdocs.org/sdr/UPS07850620), Sep 6, 2007: CONTROL PANEL. INOPERATIVE. INSPECTION TYPE:N/A F/E PANEL EMERGENCY CONTROL LIGHT PANEL HAS 4 OR 6 LIGHTS INOP. DEF 358150 ASSIGNED. *SDR FILED OPEN* DEFERRED F/E EMERGENCY ELECT CONTROL L
- [SDR UPS07850380](https://openairdocs.org/sdr/UPS07850380), Jul 14, 2007: SKIN. GOUGED. INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN HAS DEEP GOUGE AND DENT AT STA 160 L21L TO L22L. REPAIR EXTERIOR SKIN IAW SAA EA 008-5330-01-A0966, UPS RAA DC8-53-206
- [SDR UPS07850225](https://openairdocs.org/sdr/UPS07850225), Jul 14, 2007: DOOR FRAME. CRACKED. INSPECTION TYPE:C2 L-1 DOOR FRAME SEGMENT CRACKED IN BAYONETTE AREA. STOP DRILLED CRACK IN FRAME SEGMENT AT L-1 DOOR IAW SRM 52-2-0. FABRICATED AND INSTALLED RE
- [SDR UPS07850227](https://openairdocs.org/sdr/UPS07850227), Jul 11, 2007: FITTING. CRACKED. INSPECTION TYPE:C2 STA 1180 L27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED BANANA FITTING AT STA 1180 L27L IAW SRM 51-01-20D, AND SRM 51-3-2.
- [SDR UPS07850216](https://openairdocs.org/sdr/UPS07850216), Jul 10, 2007: LONGERON. CRACKED. INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L34R. REMOVED END FITTING AT STA 1140 L34R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT
- [SDR UPS07850191](https://openairdocs.org/sdr/UPS07850191), Jul 10, 2007: FITTING. CRACKED. INSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT STA 1140 L35L. REMOVED L35L END FITTING AT STA 1140 IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED L35L
- [SDR UPS07850185](https://openairdocs.org/sdr/UPS07850185), Jul 10, 2007: FITTING. CRACKED. INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L33R. REMOVED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND IN
- [SDR UPS07850192](https://openairdocs.org/sdr/UPS07850192), Jul 8, 2007: SKIN. CORRODED. INSPECTION TYPE:C2 LEFT SIDE OF RUDDER SKIN ZR 251 HAS CORROSION. REMOVED SKIN PANEL ON LEFT SIDE OF RUDDER STA ZR 251 IAW SRM 51-1-21. FABRICATED AND INSTALLED
- [SDR UPS07850178](https://openairdocs.org/sdr/UPS07850178), Jul 8, 2007: SKIN. CANNING. INSPECTION TYPE:C2 RIGHT SIDE OF RUDDER SKIN ZR 271 HAS OIL CANNING. REMOVED SKIN PANEL ON RT/SIDE OF RUDDER AT ZR 271 IAW SRM 51-1-21. FABRICATED AND INSTALLED
- [SDR UPS07850184](https://openairdocs.org/sdr/UPS07850184), Jul 7, 2007: FLOORBEAM. CORRODED. INSPECTION TYPE:C2 HEAVY CORROSION ON TOP OF FLOORBEAM IN C-PIT TUNNEL AT STA 1300 LBL 51. REMOVED CORROSION FROM FLOORBEAM, FOUND TO BE OUT OF LIMITS IAW SRM 5
- [SDR UPS07850166](https://openairdocs.org/sdr/UPS07850166), Jul 5, 2007: SKIN. DENTED. INSPECTION TYPE:C2 DENTS ON NLG RT/STRUT DOOR EXTERIOR SKIN. CUT OUT DAMAGED AREA ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR D
- [SDR UPS07850172](https://openairdocs.org/sdr/UPS07850172), Jul 3, 2007: SKIN. CRACKED. INSPECTION TYPE:C2 CRACK ON EXTERIOR FUSE SKIN AT STA 1740 L19R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN AT STA 1740 L19R IAW SRM 53-02-01 FIG 7. FABRICATED AND I
- [SDR UPS07849886](https://openairdocs.org/sdr/UPS07849886), Jun 6, 2007: SLIDE. LOOSE. INSPECTION TYPE:N/A CABIN ESCAPE SLIDE WILL NOT STOW. INSTALLED RETAINING PIN IN SLIDE PER AMM 25-60-01-2.
- [SDR UPS07849749](https://openairdocs.org/sdr/UPS07849749), May 3, 2007: SLIDE. MISSING. INSPECTION TYPE:N/A ESCAPE SLIDE NOT IN DOOR. INSTALLED ESCAPE SLIDE ON DOOR IAW MM 25-60-01-2.
- [SDR UPS07849501](https://openairdocs.org/sdr/UPS07849501), Mar 15, 2007: BULB. BURNED OUT. PILOTS OVERHEAD PANEL EMERGENCY LIGHTS DISARMED LIGHT INOP. FOUND BULB BURNED OUT. REPLACED BULB, CHECKS OK.
- [SDR UPS06848791](https://openairdocs.org/sdr/UPS06848791), Dec 20, 2006: SLIDE. UNWANTED DEPLOY. INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE DEPLOYED INADVERTENTLY. DEFERRAL M340403 ASSIGNED. CLEARED MEL 52-7-4 M340403. INSPECTED AND REINSTALLED ORIGINAL DOO
- [SDR UPS06848527](https://openairdocs.org/sdr/UPS06848527), Nov 8, 2006: BATTERY. DISCHARGED. EMERGENCY EXIT LTS INOP. REMOVED ADN REPLACED EMERGENCY EXIT BATT/RELAY PACK IAW MM 33-50-01-2. OPS CK GOOD.
- [SDR UPS06847468](https://openairdocs.org/sdr/UPS06847468), Jul 28, 2006: ODOR. DETECTED. ELECTRICAL ODOR ON F/O'S SIDE OF COCKPIT TROUBLESHOOTING IN PROGRESS COULD NOT SMELL ANY TYPE OF ELECTRICAL ODOR WHEN OPERATING ALL FOUR ENGINES.
- [SDR UPS05845146](https://openairdocs.org/sdr/UPS05845146), Jul 29, 2005: FITTING. CRACKED. WHILE WORKING N/R 859104 FOUND LONG 31L END FITTING CRACKED. REMOVED AND REPLACED LONG END FITTING AT STA 106 IAW SRM 51-3-0 51-1-21, AND SRM 51-1-20D.
- [SDR UPS05845112](https://openairdocs.org/sdr/UPS05845112), Jul 29, 2005: FRAME. CRACKED. INSPECTION TYPE:C1 WHILE ACCOMPLISHMENT OF MCD FWD HINGE REPLACEMENT AFTER REMOVAL OF THE ACTUATOR CLOSE OUT PNL FOUND A 1" CRACK ON THE FWD UPPER MAIN FRAME CR
- [SDR UPS05845003](https://openairdocs.org/sdr/UPS05845003), Jul 23, 2005: FITTING. CORRODED. A/C COMPT LONGERON END FITTING CORRODED AROUND FASTENER HOLE AT STA 70 L32R. REMOVED AND REPLACED LONG END FITTING AT STA 70 L32R IAW SRM 57-1-20D, AND 51-3-2.
- [SDR UPS05844997](https://openairdocs.org/sdr/UPS05844997), Jul 22, 2005: FINGER DOUBLER. CORRODED. INSPECTION TYPE: C1, SKIN SPLICE AT FS 1350 INTERIOR FINGER DOUBLER HAS PITTED CORROSION FROM L31R TO L31L. REMOVED FINGER DOUBLER AT FS 1350 IAW SRM 51-1-21 AN
- [SDR UPS05845188](https://openairdocs.org/sdr/UPS05845188), Jul 20, 2005: HINGE PIN. WORN. INSPECTION TYPE:C1 REMOVE MAIN CARGO DOOR HINGE TO ACCOMPLISH FWD HINGE REPLACEMENT, CRACKED, FOUND DURING DOUBLER REMOVAL. REMOVED MAIN CARGO DOOR AND HINGE, M
- [SDR UPS05845121](https://openairdocs.org/sdr/UPS05845121), Jul 16, 2005: SKIN. CORRODED. INSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE TO FOM FOR NDT INSPECTION TO COMPLY WITH EO DC8-5330-20206 FOUND CORROSION ON FUSELAGE SKIN FS 1395 TO 1445
- [SDR UPS05844965](https://openairdocs.org/sdr/UPS05844965), Jul 16, 2005: LONGERON. CORRODED. INSPECTION TYPE:C1 AFTER REMOVAL OF INTERCOSTAL ON N/R 858794 FS 1473 L34R FOUND CORROSION AT LONGERON UNDER STRAP REMOVED LONGERON 34R STA 1350 TO 1490 IAW DC8
- [SDR UPS05845183](https://openairdocs.org/sdr/UPS05845183), Jul 14, 2005: SKIN. CRACKED. REPLACE SKIN PANEL AT STA 70 TO -21.92 LONG 31R-L31L. REMOVED AND REPLACED FWD BELLY SKIN AT STA -21.92 TO STA LONG 31L TO LONG 31R IAW EO DC8-5330-8942-D.
- [SDR UPS05845182](https://openairdocs.org/sdr/UPS05845182), Jul 13, 2005: PLATE. CRACKED. MAIN CARGO DOOR LWR AFT CORNER, THE DOOR JAMB CORNER INTERNAL SUPPORT PLATE IS CRACKED. REMOVED FILLET IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT FIL
- [SDR UPS05845120](https://openairdocs.org/sdr/UPS05845120), Jul 13, 2005: FITTING. CRACKED. INSPECTION TYPE:C1 LONG 31R SPLICE FITTING CRACKED FROM 1040-1060. REMOVED AND REPLACED LONG SPLICE FITTING IAW SRM 53-1-0 AND 51-1-20 AT STA 1040-1060 LONG 31R
- [SDR UPS05845115](https://openairdocs.org/sdr/UPS05845115), Jul 13, 2005: FITTING. CRACKED. INSPECTION TYPE:C1 BATHTUB FITTING CRACKED AT C-PIT DOOR JAMB STA 1200 L33R-L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 53-2-0 AND SRM 53-2-0 FIG 02G.
- [SDR UPS05845046](https://openairdocs.org/sdr/UPS05845046), Jul 13, 2005: FLOORBEAM. CRACKED. F/S 960 LBL 60 FLOORBEAM AT LIGHTING HOLE ON VERT FLANGE AT CENTER OF HOLE HAS A 5" CRACK GOING AT HORIZ ANGLE. STOP DRILLED CRACKED FLOORBEAM, FABRICATED AND I
- [SDR UPS05844966](https://openairdocs.org/sdr/UPS05844966), Jul 13, 2005: FITTING. CRACKED. INSPECTION TYPE:C1 SPLICE FITTING CRACKED AT STA 610, L35L REMOVED CRACKED SPLICE FITTING AT STA 610, LONG 35L IAW SRM 51-1-20D. FABRICATED REPLACEMENT FITTING 
- [SDR UPS05845145](https://openairdocs.org/sdr/UPS05845145), Jul 12, 2005: FITTING. CORRODED. A-PIT CENTER TORQUE BOX BATHTUB FITTING AT FS 360 BETWEEN TORQUE BOX FRAME AND LONGERON34R HAS CORROSION. REMOVED CORROSION FROM BATH TUB FITTING AT STA 360 LON
- [SDR UPS05844995](https://openairdocs.org/sdr/UPS05844995), Jul 12, 2005: LONGERON. CRACKED. FS 1488 LONG 32L CRACKED ON BACKSIDE OF SPLICE END. REMOVED LONG 32L AND SPLICE END FITTING AT FS 1488 IAW SRM 51-1-21, FABRICATED LONG 32L AND SPLICE END FITTI
- [SDR UPS05844949](https://openairdocs.org/sdr/UPS05844949), Jul 12, 2005: FITTING. CORRODED. INSPECTION TYPE: C1, EXFOILIATED CORROSION ON VERTICAL L-FITTING FWD BULKHEAD RT NOSE TUNNEL. REMOVED VERTICAL L-FITTING, FABRICATED AND INSTALLED REPLACEMENT F
- [SDR UPS05845125](https://openairdocs.org/sdr/UPS05845125), Jul 11, 2005: STRUCTURE. ELONGATED. INSPECTION TYPE: C1, D-PIT DOOR AFT WEB HAS SEVERAL ELONGATED HOLES AND LITE CORROSION AROUND FASTENER. REMOVED DAMAGED WEB IAW SRM 51-1-21, FABRICATED DOOR JAM
- [SDR UPS05845123](https://openairdocs.org/sdr/UPS05845123), Jul 11, 2005: FITTING. CRACKED. INSPECTION TYPE:C1 60 COMPT L17L AT 1770 HAS 6 INCH CRACK AT END FITTING. REMOVED FITTING AND SUPPORT FROM STA 1770 L17L IAW SRM 51-1-20D, FABRICATED AND INSTAL
- [SDR UPS05845122](https://openairdocs.org/sdr/UPS05845122), Jul 11, 2005: INTERCOSTAL. CORRODED. INSPECTION TYPE:C1 D-PIT FS 1473 LONG 34R LWR RETURN FLANGE ON INTERCOSTAL IN LONGERON HAS HEAVY EXFOLIATION 4.00". REMOVED INTERCOSTAL ATTACH ANGLE AT STA 1473
- [SDR UPS05845111](https://openairdocs.org/sdr/UPS05845111), Jul 11, 2005: FITTING. CRACKED. INSPECTION TYPE: C1, LONGERON END FITTING CRACKED AT STA 690 L4L. REMOVED CRACKED END FITTING AT STA 690 L4L IAW SRM 53-2-2. REPLACED END FITTING AT STA 690 L4L
- [SDR UPS05845050](https://openairdocs.org/sdr/UPS05845050), Jul 11, 2005: FITTING. CRACKED. LONGERON END FITTING CRACKED AT STA 902 L7L. REMOVED AND REPLACED LONGERON END FITTING IAW 51-1-20D, 51-1-21 AND 51-3-0.
- [SDR UPS05845005](https://openairdocs.org/sdr/UPS05845005), Jul 11, 2005: FITTING. CORRODED. INSPECTION TYPE: C1, MAIN CARGO DOOR JAMB AFT LATCH SPOOL FITTING FWD ANGLE HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED MCD LATCH SPOOL FITTING IAW 51-3-0
- [SDR UPS05845006](https://openairdocs.org/sdr/UPS05845006), Jul 11, 2005: FINGER DOUBLER. CORRODED. FINGER DOUBLER BLOWN OUT IN COCKPIT SUBFLOOR AT STA -67 TO -81. REMOVED FINGER DOUBLER AT STA -67 TO -81. FABRICATED FINGER DOUBLER AND INSTALLED IAW SRM 53-3-1

All 268: https://openairdocs.org/deregistered/N807UP-2010-09-13/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 19910823051429I](https://openairdocs.org/incident/19910823051429I), Aug 23, 1991: Doug DC871F (N807UP), Ontario, CA. Hydraulic fluid loss en route. Continued to destination. NR2 engine hydraulic pump had a cracked housing.
- [Incident 19881215065889I](https://openairdocs.org/incident/19881215065889I), Dec 15, 1988: Doug DC873F (N807UP), Des Moines, IA, Minor damage. Plane rolled forward during start of NR4 engine. Pilot unaware chocks pulled. Had hydraulic leaks from brake systems

## Other aircraft with N807UP

- [Registered now](https://openairdocs.org/aircraft/N807UP): Beechcraft B300, S/N FL-892, built 2013

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