# N806UP: 1968 Douglas DC-8-73F, registration cancelled 2010-08-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 12, 2010
- Status when cancelled: Sale reported
- 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: 46006
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 21, 1997
- Last registry action: August 12, 2010
- Mode S code: AAF9F7
- Location: [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables)
- Owner type: Individual
- Owner's area on the map: 25.7533° N, 80.2704° W: Placed by OpenAirDocs at the center of ZIP code 33134, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N806UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=806UP
- Page: https://openairdocs.org/deregistered/N806UP-2010-08-12

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 (343, newest 50)

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

- [SDR UPS08852686](https://openairdocs.org/sdr/UPS08852686), Jul 7, 2008: SKIN. CORRODED. CORROSION RT LWR FUSE AFT OF THE E&E DOOR APPROX. STA 70. STARTED ECA FORM 011382. INSTALLED TIME LIMITED REPAIR IAW EO DC8-5330-29905A. ALL WORK PERFORMED ON E
- [SDR UPS08852628](https://openairdocs.org/sdr/UPS08852628), Jul 2, 2008: BATTERY PACK. FAILED. ON PRE-DEPARTURE CK, EMERGENCY EXIT LIGHT CK FAILED. FOUND SW IN ON POSITION. REPLACED AND TESTED BATTERY PACK IAW 33-50-01-2 CKS OK.
- [SDR UPS08852014](https://openairdocs.org/sdr/UPS08852014), Apr 11, 2008: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01-2 PARA 4. OPS CHECK GOOD.
- [SDR UPS08851953](https://openairdocs.org/sdr/UPS08851953), Mar 31, 2008: LIGHT. INTERMITTENT. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INTERMITTENT ON OPS CHECK. PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MM 33-50-02-2. OPS CHECK.
- [SDR UPS07851308](https://openairdocs.org/sdr/UPS07851308), Dec 14, 2007: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-01-2 AND TESTED.
- [SDR UPS07851275](https://openairdocs.org/sdr/UPS07851275), Dec 8, 2007: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-02-2.
- [SDR UPS07851058](https://openairdocs.org/sdr/UPS07851058), Oct 26, 2007: SLIDE. UNSECURE. ESCAPE SLIDE CAME LOOSE. RESECURED ESCAPE SLIDE TO FWD ENTRY DOOR B DC8 25-60.
- [SDR UPS07848853](https://openairdocs.org/sdr/UPS07848853), Jan 11, 2007: LIGHT. NO TEST. EMERGENCY LIGHTS WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY AND RELAY UNIT ASSY PER AMM 33-50-01. OPS CK NORMAL.
- [SDR UPS07848852](https://openairdocs.org/sdr/UPS07848852), Jan 2, 2007: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND TESTED OK PER MM 33-50-01-2.
- [SDR UPS06848801](https://openairdocs.org/sdr/UPS06848801), Dec 27, 2006: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD PER MM 3-50-01-2.
- [SDR UPS06847782](https://openairdocs.org/sdr/UPS06847782), Aug 22, 2006: DOUBLER. GOUGED. INSPECTION TYPE:C1-3 STA 219 LT FLAP FOUND O/B VERT DOUBLER AND LWR ATTACH ANGLE GOUGED OUT OF LIMITS. REMOVED DAMAGED DOUBLER AND ATTACH ANGLE AT LT FLAP STA 2
- [SDR UPS06847665](https://openairdocs.org/sdr/UPS06847665), Jul 31, 2006: FITTING. CRACKED. INSPECTION TYPE-C1-3 BOTH STRINGER END FITTINGS ON STRINGER 51 AT XRS 74 ARE CRACKED NR 2 MAIN TANK. REMOVED BOTH STRINGER END FITTINGS AT STR 51 XRS 74 NR 2 MA
- [SDR UPS06847663](https://openairdocs.org/sdr/UPS06847663), Jul 29, 2006: FITTING. CORRODED. BATH TUB FITTING EXFOLIATED OUT OF LIMITS AT A-PIT TORQUE BOX STA 280 L33L-L34L. REMOVED BATHTUB FITTING AT STA 280 L33L-L34L IAW SRM 53-02-00, AND SRM 51-1-20D
- [SDR UPS06847710](https://openairdocs.org/sdr/UPS06847710), Jul 27, 2006: SKIN. CORRODED. INSPECTION TYPE: C1-3 D-PIT BELLY SKIN REQUIRES REPLACEMENT DUE TO OUT OF LIMITS CORROSION AT L35R-36 STA 1490-1350. REMOVED AND REPLACED BELLY SKIN AT STA 1490
- [SDR UPS06847648](https://openairdocs.org/sdr/UPS06847648), Jul 26, 2006: ATTACH FITTING. CRACKED. INSPECTION TYPE:C1/3 NR 1 MAIN TANK REAR SPAR ATTACH TEE FITTING AT XW-408 HAS A 4 INCH CRACK. REMOVED AND REPLACED ATTACH TEE FITTING AT XCW-408 NR1 MAIN TANK.
- [SDR UPS06847640](https://openairdocs.org/sdr/UPS06847640), Jul 25, 2006: SPLICE. CRACKED. INSPECTION TYPE: C1,3 LONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L35L. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D
- [SDR UPS06847603](https://openairdocs.org/sdr/UPS06847603), Jul 21, 2006: FITTING. CRACKED. INSPECTION TYPE:C1-3 60 HOLE APPROX STA 1800 LONGERON 24L END FITTING IS CRACKED. REMOVED DRILLED UP, AND INSTALLED END FITTING AT STA 1800 L24L IAW SRM 51-1-21
- [SDR UPS06847574](https://openairdocs.org/sdr/UPS06847574), Jul 21, 2006: LONGERON. CRACKED. INSPECTION TYPE:C1-3 CRACKED LONGERON L34R FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 - 1350 L34R IAW SRM 51-1-20D.
- [SDR UPS06847651](https://openairdocs.org/sdr/UPS06847651), Jul 19, 2006: DRAG ANGLE. CRACKED. INSPECTION TYPE:C1, 3 POSSIBLE CRACKS ON BULKHEAD FWD OF CENTER SPAR UPPER BOLT IB DRAG ANGLE. REMOVED, FABRICATED AND INSTALLED DRAG ANGLE IAW SRM 51-1-21, DWG
- [SDR UPS06847521](https://openairdocs.org/sdr/UPS06847521), Jul 18, 2006: LONGERON. CRACKED. INSPECTION TYPE:C1-3 MAIN CABIN LONGERON END FITTING CRACKED AT STA 905 L9L. REMOVED AND REPLACED LONGERON END FITTING AT STA 905 L9L IAW SRM 51-1-20D, AND SRM 
- [SDR UPS06847441](https://openairdocs.org/sdr/UPS06847441), Jul 18, 2006: LONGERON SPLICE. CRACKED. INSPECTION TYPE:C1-3 LONGERON SPLICE FITTING CRACKED AT STA 900 TO 920 L1. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 900 TO 920 LONGERON 1 IAW SRM 51-
- [SDR UPS06847583](https://openairdocs.org/sdr/UPS06847583), Jul 17, 2006: LONGERON. CRACKED. INSPECTION TYPE:C1-3 CRACKED LONGERON L35L FS 1270 C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 L35L IAW SRM 51-1-20D.
- [SDR UPS06847581](https://openairdocs.org/sdr/UPS06847581), Jul 17, 2006: LONGERON. CRACKED. INSPECTION TYPE:C1-3 CRACKED LONGERON AT L36 FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON FROM STA 1270 - 1350 L36 IAW SRM 51-1-20D.
- [SDR UPS06847522](https://openairdocs.org/sdr/UPS06847522), Jul 17, 2006: FINGER DOUBLER. CORRODED. INSPECTION TYPE:C1-3 9 SHEARED RIVETS ON FINGER DOUBLER IN COCKPIT SUBFLOOR, STA -130 LBL 20. REMOVED CORRODED FINGER DOUBLER IN COCKPIT SUBFLOOR AT STA -130 LB
- [SDR UPS06847747](https://openairdocs.org/sdr/UPS06847747), Jul 16, 2006: SKIN. CORRODED. INSPECTION TYPE:C1 3 HEAVY CORROSION BETWEEN FUSE SKIN AND FINGER DOUBLER AT STA 1670 L31R IN AFT ACC COMPT. REPAIRED FUSELAGE SKIN FROM FS 1660 TO 1680 IAW SAA
- [SDR UPS06847639](https://openairdocs.org/sdr/UPS06847639), Jul 15, 2006: FITTING. CRACKED. INSPECTION TYPE: C1, 3 CRACKED BATHTUB FITTING AT FS 270 L34R IN A-PIT. REMOVED AND REPLACED BATHTUB FITTING. IAW SRM 51-1-20D
- [SDR UPS06847638](https://openairdocs.org/sdr/UPS06847638), Jul 15, 2006: LONGERON. CORRODED. INSPECTION TYPE: C1,3 AT STA. 270 L33L IS BLOWN OUT. REMOVED WEB, BATHTUB FITTING AND LONGERON. FABRICATED AND INSTALLED LONGERON, SPLICE FITTING,BATHTUB FITTIN
- [SDR UPS06847526](https://openairdocs.org/sdr/UPS06847526), Jul 15, 2006: SPLICE. CRACKED. INSPECTION TYPE:C1-3 L31L AT STA 200 TO STA 180 SPLICE IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 200-180 L31L IAW SRM 51-1-20D, AND SRM 51-03-02.
- [SDR UPS06847646](https://openairdocs.org/sdr/UPS06847646), Jul 14, 2006: DOUBLER. BROKEN. INSPECTION TYPE: C1/3 INTERNAL DOUBLER BROKEN AT 6:00 AND 12:00 POSITION UNDER EXTERIOR MAIN CARGO DOOR ACCESS PLATE FOR NR 4 LATCH FABRICATED AND INSTALLED -1 
- [SDR UPS06847584](https://openairdocs.org/sdr/UPS06847584), Jul 14, 2006: SHEAR TIE. CRACKED. INSPECTION TYPE:C1-3 MAIN CABIN STA 1740 L14L SHEAR TIE CRACKED. REMOVED SHEAR TIE AT STA 1740 L14L IAW SRM 51-01-20D. FABRICATED AND INSTALLED SHEAR TIE AT STA
- [SDR UPS06847439](https://openairdocs.org/sdr/UPS06847439), Jul 14, 2006: SEAT TRACK. WORN. C1-3 FE'S FWD SEAT TRACK LOCK PINS HOLES WORN. REMOVED AND REPLACED FE'S FWD SEAT TRACK IAW SRM 51-03-00,51-01-22 AND SRM 51-03-00.
- [SDR UPS06847435](https://openairdocs.org/sdr/UPS06847435), Jul 14, 2006: SEAT TRACK. WORN. C1-3 2ND OBSERVERS AFT SEAT TRACK LOCKPIN HOLES WORN. REMOVED AND REPLACED 2ND OBSERVERS AFT SEAT TRACK IAW SRM 51-3-0 51-01-24.
- [SDR UPS06847696](https://openairdocs.org/sdr/UPS06847696), Jul 13, 2006: SPAR CAP. CRACKED. INSPECTION TYPE:C1-3 LT MLG WHEEL WELL FRONT SPAR CAP STA 857 LBL 36 HAS A CRACK BETWEEN BOLTS. REPAIRED LT MLG WHEEL WELL FRONT SPAR CAP AT STA 857 LBL 36 IAW 
- [SDR UPS06847641](https://openairdocs.org/sdr/UPS06847641), Jul 13, 2006: LONGERON. CORRODED. INSPECTION TYPE: C1,3 AIR CONDITIONING COMPT, L36 IS CORRODED AND CRACKED AT STA.35. REMOVED, FABRICATED AND INSTALLED LONGERON AT FS 35 L36.
- [SDR UPS06847582](https://openairdocs.org/sdr/UPS06847582), Jul 13, 2006: FITTING. CRACKED. INSPECTION TYPE:C1-3 LONGERON END FITTING CRACKED AT STA 65 L31L. REMOVED AND REPLACED LONGERON END FITTING AT STA 65 L31L IAW SRM 51-3-0, 51-1-21, AND SRM 51-3
- [SDR UPS06847527](https://openairdocs.org/sdr/UPS06847527), Jul 13, 2006: RIB. CRACKED. INSPECTION TYPE:C1-3 LT CENTER WING L/E UPPER RIB CRACKED AT XFS 497. STOP DRILLED CRACKED RIB AT LT L/E WING STA XFS 497 IAW SRM 57-02-00 FIG 002. FABRICATED A
- [SDR UPS06847447](https://openairdocs.org/sdr/UPS06847447), Jul 13, 2006: RIB. CRACKED. RT CENTER L/E UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK ON RIB AT LT L/E STA XFS 415 IAW SRM 57-2-0. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E 
- [SDR UPS06847446](https://openairdocs.org/sdr/UPS06847446), Jul 13, 2006: LONGERON. CRACKED. INSPECTION TYPE:C1-3 RT AFT MAIN CABIN FS 1750 L14R CRACKED AT CANTED FRAME REMOVED CRACKED LONGERON SECTION AT STA 1750 L14R IAW SRM 53-02-02-0 FI FIG 10. FABR
- [SDR UPS06847444](https://openairdocs.org/sdr/UPS06847444), Jul 13, 2006: RIB. CRACKED. LEFT WING CENTER L/E RIB CRACKED AT XFS 328. STOP DRILLED CRACK AT LT WING L/E RIB AT STA XFS 328 IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLES AT LT
- [SDR UPS06847438](https://openairdocs.org/sdr/UPS06847438), Jul 13, 2006: RIB. CRACKED. LT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK ON RIB ANGLE IAW SRM 57-2-0 AT STA XFS 304. FABRICATED AND INSTALLED REPAIR ANGLES AT STA L/WING S
- [SDR UPS06847410](https://openairdocs.org/sdr/UPS06847410), Jul 13, 2006: RIB. CRACKED. FOUND LT CTR LE UPPER RIB CRACKED AT XS 491. SET HOLE TERMINATED CRACK. FABRICATED AND INSTALLED 2. REPAIR DOUBLERS IAW SRM 57-02-00 FIG 002 SHT 2, 51-01-20D AN
- [SDR UPS06847409](https://openairdocs.org/sdr/UPS06847409), Jul 13, 2006: RIB. CRACKED. INSPECTION TYPE:C1,3 LT WING CTR LE LWR IB CRACKED AT XFS 347. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002, 57-02-03 FIG 
- [SDR UPS06847407](https://openairdocs.org/sdr/UPS06847407), Jul 13, 2006: RIB. CRACKED. RT CENTER LE UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 002, 51-1-21 AND 51-1-20D. SAT PREVIO
- [SDR UPS06847406](https://openairdocs.org/sdr/UPS06847406), Jul 13, 2006: RIB. CRACKED. LT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES 2 IAW SRM 57-02-00 FIG 002, 57-03-03 FIG 005 AND 51-1-20D.
- [SDR UPS06847405](https://openairdocs.org/sdr/UPS06847405), Jul 13, 2006: RIB. CRACKED. FOUND LT CENTER LE UPPER RIB CRACKED AT XS454. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2 AND 51-1-20A.
- [SDR UPS06847371](https://openairdocs.org/sdr/UPS06847371), Jul 13, 2006: RIB. CRACKED. C1, 3 RT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS409. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 51-1-21, 57-02-00 FIG 2, 57-03-03 F
- [SDR UPS06847647](https://openairdocs.org/sdr/UPS06847647), Jul 12, 2006: FITTING. CRACKED. INSPECTION TYPE: C 1-3 MAIN CABIN STA.1690 LONGERON 35L END FITTING CRACKED REMOVED AND REPLACED LONGERON 35L END FITTING AT STA.1690 IAW SRM 51-1-21 AND SRM 51
- [SDR UPS06847602](https://openairdocs.org/sdr/UPS06847602), Jul 12, 2006: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C1-3 LT MLG WHEEL WELL STA 940 LBL 63 PRESSURE DECK SKIN IS CORRODED AND CRACKED. CUT OUT DAMAGED AREA IAW SRM 53-2-0. FABRICATED AND INSTALLED 
- [SDR UPS06847572](https://openairdocs.org/sdr/UPS06847572), Jul 12, 2006: FITTING. CRACKED. INSPECTION TYPE:C1-3 LT MAIN CABIN FS 680 FWD LONG END FITTING 6L IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L6L IAW SRM 51-03-00, 51-1-20
- [SDR UPS06847370](https://openairdocs.org/sdr/UPS06847370), Jul 12, 2006: RIB. CRACKED. C1, 3 LT OB LEADING EDGE RIB CRACKED AT XFS 746 UPPER RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EACH DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 2, 51-01-20D 

All 343: https://openairdocs.org/deregistered/N806UP-2010-08-12/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 20080214012409I](https://openairdocs.org/incident/20080214012409I), Feb 14, 2008: Doug DC873F (N806UP), Greensboro, NC, Minor damage. (-23) On 2/14/2008 at Greensboro, NC (gso), aircraft N806UP began its take-off roll on rwy 5 at 2327. Approximately 800 ft into the takeoff roll, at a speed of…

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