# N802UP: 1969 Douglas DC-8-73F, registration cancelled 2010-07-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 2, 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: 46100
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 29, 1990
- Last registry action: June 17, 2010
- Mode S code: AAEB1B
- 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/N802UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=802UP
- Page: https://openairdocs.org/deregistered/N802UP-2010-07-02

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 UPS09854304](https://openairdocs.org/sdr/UPS09854304), Jan 7, 2009: GIRT BAR. BROKEN. EMERGENCY ESCAPE SLIDE INOP, GIRT BAR CLIP BROKEN. REPLACED FWD GIRT BAR CLIP IAW DPS 1.07-2.
- [SDR UPS09854279](https://openairdocs.org/sdr/UPS09854279), Jan 3, 2009: LATCH. BROKEN. ESCAPE SLIDE CONTAINER CLOSURE CLIP BROKEN CONTAINER WILL NOT STAY CLOSED. M391960, DEFERRED IAW MEL 52-7-4. REMOVED SLIDE AND SECURED ENCLOSURE PLACARD INSTALL
- [SDR UPS08854080](https://openairdocs.org/sdr/UPS08854080), Dec 2, 2008: ENGINE. FLAMED OUT. INSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT. ENGINE RELIT ON IT'S OWN. PERFORMED FIRST FOUR STEPS OF DC-8 M/M 71-00-00-1 FIG 139 UP TO INSPECT FUEL FILTER. FILTE
- [SDR UPS08852457](https://openairdocs.org/sdr/UPS08852457), Jun 8, 2008: FLOORBOARD. DAMAGED. INSPECTION TYPE:C2 FLOORBOARD F81 HAS ONE EACH SCREW HOLE BROKEN OUT. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-3 FIG 10, 51-1-8, 51-1-21
- [SDR UPS08852570](https://openairdocs.org/sdr/UPS08852570), Jun 5, 2008: SUPPORT ANGLE. CHAFED. INSPECTION TYPE:C2 RT WING INBD SLOT VANE HAS A DEEP CHAFING MARK AT SUPPORT ANGLE AT OTBD SIDE. REMOVED AND REPLACED SUPPORT ANGLE IAW AMM, 51-1-24, 27-80-00.
- [SDR UPS08852572](https://openairdocs.org/sdr/UPS08852572), Jun 4, 2008: INTERCOSTAL. CRACKED. INSPECTION TYPE:C2 INTERCOSTAL CRACKED AT STA -84 L21L BELOW SUB-FLOOR. REMOVED AND REPLACED INTERCOSTAL IAW, SRM, 51-1-20D ,51-1-8, 51-1-21
- [SDR UPS08852432](https://openairdocs.org/sdr/UPS08852432), May 31, 2008: SKIN. GOUGED. INSPECTION TYPE:C2 C-PIT CROSS SLIDE DOOR INTERIOR SKIN IS GOUGED, FWD LWR AREA. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-21, 52-2-0 FIG 2.
- [SDR UPS08852567](https://openairdocs.org/sdr/UPS08852567), May 30, 2008: ATTACH FITTING. CORRODED. INSPECTION TYPE:C2 C PIT STA 1230 L27L ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED LONGERON ATTACH FITTING IAW DC8 SRM 51-01-20D.
- [SDR UPS08852566](https://openairdocs.org/sdr/UPS08852566), May 30, 2008: FITTING. CRACKED. INSPECTION TYPE:C2 D PIT STA 1360 L35L SPLICE FITTING CRACKED AND CORRODED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-03-01 AND 51-01-20D.
- [SDR UPS08852733](https://openairdocs.org/sdr/UPS08852733), May 29, 2008: ATTACH ANGLE. CRACKED. INSPECTION TYPE-C2 POSSIBLE CRACK IN RADIUS OF INTERCOSTAL ATTACH ANGLE, AT BOTTOM J-BEAM, AFT SIDE OF APB, 60 COMPT RT BS 1771. REMOVED INTERCOSTAL ATTACH ANGL
- [SDR UPS08852414](https://openairdocs.org/sdr/UPS08852414), May 29, 2008: SHEAR TIE. CRACKED. INSPECTION TYPE:C2 LARGE SHEAR TIE CRACKED IN RADIUS, 60 COMARTMENT CEILING, STA 1800 L4R. STOP DRILLED, FABBED AND INSTALLED REPAIR ANGLE IAW, SRM 51-1-21, 53-
- [SDR UPS08852438](https://openairdocs.org/sdr/UPS08852438), May 29, 2008: FITTING. CORRODED. INSPECTION TYPE:C2 END FITTING BLOWN OUT, L30L, STA 1759 DIFFICULT ACCESS. REMOVED AND REPLACED CORRODED FITTING IAW SRM 51-1-21, 51-1-8, 51-1-24 , 51-3-0.
- [SDR UPS08852577](https://openairdocs.org/sdr/UPS08852577), May 28, 2008: ATTACH FITTING. CORRODED. INSPECTION TYPE:C2 AFT ACCESSORY COMPT STA 1580, L21L FLOORBEAM ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED END FITTING IAW SRM, 51-1-8, 51-1-20D, 51-3-1
- [SDR UPS08852603](https://openairdocs.org/sdr/UPS08852603), May 28, 2008: FRAME. CORRODED. INSPECTION TYPE:C2 FLIGHT DECK STA -52 RT SIDE FRAME HAS CORROSION BY SUBFLOOR AREA. REPAIRED FLT DECK FRAME AT STA -52 AND SUBFLOOR AREA IAW EA 008- 5310-01-A1
- [SDR UPS08852427](https://openairdocs.org/sdr/UPS08852427), May 28, 2008: SKIN. GOUGED. INSPECTION TYPE:C2 RIGHT ELEVATOR UPPER SKIN IS DENTED AND GOUGED, FWD OF GEARED TAB. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-0, 55 51-
- [SDR UPS08852571](https://openairdocs.org/sdr/UPS08852571), May 28, 2008: LONGERON. CRACKED. INSPECTION TYPE:C2 MAIN CABIN, L-15L CRACKED AT CANT FRAME STA 1746. REMOVED, FABBED AND INSTALLED LONGERON SLICE IAW SRM, 51-1-8, 53-2-2 FIG 10, 53-5-1 FIG 7, 
- [SDR UPS08852568](https://openairdocs.org/sdr/UPS08852568), May 28, 2008: SKIN. CORRODED. INSPECTION TYPE:C2 RUDDER RT SIDE EXTERIOR SKIN HAS CORROSION, POPPED RIVETS AND BEADED SKIN IS SEPARATED. REMOVED AND REPLACED 2 RUDDER SKINS IAW DC8 SRM 51-1-
- [SDR UPS08852565](https://openairdocs.org/sdr/UPS08852565), May 27, 2008: SEAT TRACK. WORN. INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK STA 1460, 0BL 2 EACH HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK PLUG IAW SRM, 51-3-00.
- [SDR UPS08852564](https://openairdocs.org/sdr/UPS08852564), May 27, 2008: SEAT TRACK. WORN. INSPECTION TYPE:C2 COPILOT REAR LT AND RT SEAT TRACKS SHOWS ELONGATION. REMOVED AND REPLACED SEAT TRACKS IAW SRM, 51-1-20D, 51-3-1, 51-1-24 AN D 25-11-1.
- [SDR UPS08852578](https://openairdocs.org/sdr/UPS08852578), May 25, 2008: HINGE FITTING. GOUGED. INSPECTION TYPE:C2 LEFT WING NR 1 SPOILER HINGE FITTING GOUGED NEAR STA XW38. REMOVED AND REPLACED HINGE FITTING IAW SRM, 51-1-8, 51-3-0, 51-3-2.
- [SDR UPS08852444](https://openairdocs.org/sdr/UPS08852444), May 25, 2008: STRUCTURE. DAMAGED. INSPECTION TYPE:C2 MAIN CABIN, FLOORBOARD TIEDOWN BULGED AND FASTENERS PULLING STA 350 LBL 35. REMOVED, DAMAGED RECEPTICLE, FABBED AND INSTALLED REPAIR DOUBLER 
- [SDR UPS08852536](https://openairdocs.org/sdr/UPS08852536), May 25, 2008: FLOORBOARD. CRACKED. INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD CRACKED, STA 45 RBL 47. FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 53-2-00, 53-2-3, 510108, 51-1-26, 51-1-21.
- [SDR UPS08852606](https://openairdocs.org/sdr/UPS08852606), May 24, 2008: FITTING. CRACKED. INSPECTION TYPE:C2 RIGHT WHEEL WELL AT UPPER FWD BULKHEAD, HYDRAULIC MANIFOLD PULLEY BRACKET IS CRACKED. REMOVED CRACKED FITTING, REPAIRED AND RE-INSTALLED FITT
- [SDR UPS08852433](https://openairdocs.org/sdr/UPS08852433), May 24, 2008: SEAT TRACK. DAMAGED. INSPECTION TYPE:C2 COCKPIT, SECOND OBSERVER SEAT TRACKS SHOW ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-3-0, 51-1-2, 51-1-8.
- [SDR UPS08852462](https://openairdocs.org/sdr/UPS08852462), May 24, 2008: SEAT TRACK. WORN. INSPECTION TYPE:C2 COCKPIT SECOND OBSERVER SEAT TRACKS SHOWS ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-8, 51-3-0, 51-1-24.
- [SDR UPS08852535](https://openairdocs.org/sdr/UPS08852535), May 24, 2008: SEAT TRACK. WORN. INSPECTION TYPE:C2 PILOT REAR LT AND RT SEAT TRACKS SHOW ELONGATIONS REMOVED AND REPLACED 2 EACH SEAT TRACKS IAW SRM, 51-1-20D, 51-1-24.
- [SDR UPS08852463](https://openairdocs.org/sdr/UPS08852463), May 23, 2008: FRAME. CHAFED. INSPECTION TYPE:C2 NR 2 PYLON UPPER PANEL FRAME, WORN BEYOND LIMITS, DEEP CHAFED DAMAGE BETWEEN PANELS 293A/B AND 294A/B. FABBED AND INSTALLED NEW PANEL FRAME I
- [SDR UPS08852461](https://openairdocs.org/sdr/UPS08852461), May 22, 2008: FITTING. CRACKED. INSPECTION TYPE:C2 MAIN CARGO COMP STA 980, L22R ATTACHING FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20, 51-1-20D, 51-1-8.
- [SDR UPS08852579](https://openairdocs.org/sdr/UPS08852579), May 21, 2008: FLAP. DAMAGED. INSPECTION TYPE:C2 INTERIM REPAIR TO RT INBOARD FLAP AT TRAILING EDGE XM-75. REMOVED INTERIM REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-2
- [SDR UPS08852022](https://openairdocs.org/sdr/UPS08852022), Apr 13, 2008: BULB. INOPERATIVE. EMERGENCY EXIT LIGHT AT THE C1 DOOR HAS 2 BULBS OUT. REMOVED AND REPLACED 2 BULBS FOR THE EMERGENCY EXIT LIGHTING AS NEEDED.
- [SDR UPS08851978](https://openairdocs.org/sdr/UPS08851978), Apr 8, 2008: LIMITER. INOPERATIVE. EMERGENCY LIGHTS DISARM LIGHT WAS NOT ILLUMINATED. FOUND BATTERY BUS 30 AMP CURRENT LIMITER BAD. REPLACED SAME AND PERFORMED EMERGENCY LIGHT TEST IAW DC8 AMM 33
- [SDR UPS08851880](https://openairdocs.org/sdr/UPS08851880), Mar 16, 2008: DOOR. CRACKED. INSPECTION TYPE:N/A PIT 32 DOOR CRACKED. ACCOMPLISHED HFEC INSPECTION PER EO DC8-5230-28827 PAR 6 A2. ACCOMPLISHED STOP DRILL PER EO DC8-5230-28827 PAR 6 A3-A4.
- [SDR UPS08851552](https://openairdocs.org/sdr/UPS08851552), Jan 24, 2008: LIGHT. INOPERATIVE. GLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD.
- [SDR UPS07851217](https://openairdocs.org/sdr/UPS07851217), Nov 27, 2007: ENGINE. FLAMED OUT. NR 3 ENGINE FLAME OUT. INFLIGHT RESTART ACCOMPLISHED AFTER DESCENT TO FL220. NORMAL ENGINE INDICATIONS AFTER RESTART. A/C IS CURRENTLY OUT OF SERVICE. PERFORMED
- [SDR UPS07851100](https://openairdocs.org/sdr/UPS07851100), Nov 6, 2007: BATTERY. WEAK. EMERGENCY EXIT LIGHTS ARE VERY DIM AND FLIGHT DECK LIGHT GOES OUT IN APPROX 2 MINUTES. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW DC8 AMM 33-50-01-2
- [SDR UPS07850639](https://openairdocs.org/sdr/UPS07850639), Sep 11, 2007: DOOR. LOOSE. INSPECTION TYPE:N/A CAPT ESCAPE ROPE DOOR LOOSE, ROPE FELL OUT. ROLLED, INSTALLED ESCAPE ROPE. RESECURED ESCAPE ROPE DOOR, OK TO CONTINUE.
- [SDR UPS07849225](https://openairdocs.org/sdr/UPS07849225), Feb 20, 2007: LIGHT. FAULTY. INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT DISARM. RELAMPED DISARM INDICATION LIGHT. OPS CHECK OK.
- [SDR UPS07849215](https://openairdocs.org/sdr/UPS07849215), Feb 18, 2007: SWITCH. STIFF. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH HARD TO MOVE TO DISARM CHECK POSITION. REPLACED EMERGENCY EXIT LIGHT SWITCH PER IPC 33-50-00-003. OPS CHECK OK P
- [SDR UPS06848716](https://openairdocs.org/sdr/UPS06848716), Nov 23, 2006: PACKING. WORN. INSPECTION TYPE:N/A FLIGHT LEVEL 370 .79 MACH AT CRUISE ENGINE 3 FLAMED OUT AND WITH IGNITION ON RESTARTED ALL INDICATIONS NORMAL. PERFORMED AMM 71-00-00-1 UP T
- [SDR UPS06848567](https://openairdocs.org/sdr/UPS06848567), Nov 9, 2006: BAR. DEFECTIVE. CAPTAIN'S CLEARVIEW WINDOW STUCK CLOSED. REMOVED AND REPLACED CAPT'S SLIDING WINDOW UPPER LOCK BAR W/REF TO DC8 AMM 56-10-03-5 CAPTAIN'S CLEARVIEW WINDOW OPS NO
- [SDR UPS06848515](https://openairdocs.org/sdr/UPS06848515), Nov 3, 2006: WINDOW. JAMMED. CAPT CLEARVIEW WINDOW WILL NOT OPEN. FOUND WINDOW TRIM ON AFT OF SLIDING WINDOW JAMMING WINDOW MOTION. REMOVED WINDOW TRIM FROM AFT OF WINDOW. WINDOW OPS CK NOR
- [SDR UPS06847940](https://openairdocs.org/sdr/UPS06847940), Aug 23, 2006: FITTING. CRACKED. INSPECTION TYPE:C3 END FITTING FOR STRINGER 51 OUTBOARD OF XRS 74 NR 2 MAIN TANK. REMOVED STRINGER END FITTING 51 AT STA XRS 74 NR 2 MAIN TANK IAW SRM 51-3-0. L
- [SDR UPS06847787](https://openairdocs.org/sdr/UPS06847787), Aug 22, 2006: RIB. CRACKED. INSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACKED RIB AT LT L/E STA XFS 460 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED R
- [SDR UPS06847995](https://openairdocs.org/sdr/UPS06847995), Aug 18, 2006: LONGERON. CORRODED. INSPECTION TYPE-C3 AFTER REMOVED FUSELAGE BELLY SKIN FROM FS -22 TO 70 L31L-L31R, FOUND LONGERON HAS HEAVY CORROSION AT STA 55 TO 70 L36. FABRICATED AND INSTALL
- [SDR UPS06847892](https://openairdocs.org/sdr/UPS06847892), Aug 18, 2006: ATTACH ANGLE. CORRODED. INSPECTION TYPE-C3 STA 857 RBL 53 UPPER HORIZONTAL ATTACH ANGLE, CENTER FUEL TANK, FWD BULKHEAD HAS EXFOLIATED CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR
- [SDR UPS06847894](https://openairdocs.org/sdr/UPS06847894), Aug 17, 2006: LONGERON. CORRODED. INSPECTION TYPE-C3 STA.1766 LONGERON 28R CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF LONGERON 28R FROM STA 1752 TO 1766 IAW SRM 53-02-02-0 FIG 10 AND SRM 5
- [SDR UPS06847893](https://openairdocs.org/sdr/UPS06847893), Aug 17, 2006: FITTING. CRACKED. INSPECTION TYPE-C3 STA 1766 LONGERON 28R END FITTING CORRODED. END FITTING FOUND TO BE CORRODED AND CRACKED. REMOVED AND REPLACED STA 1766 LONGERON 28R END FITT
- [SDR UPS06847891](https://openairdocs.org/sdr/UPS06847891), Aug 17, 2006: FITTING. CRACKED. INSPECTION TYPE-C3 STA 1760 LONGERON 14R END FITTING CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 1760 LONGERON 14R IAW SRM 51-01-21, SRM 51-03-00,
- [SDR UPS06847768](https://openairdocs.org/sdr/UPS06847768), Aug 17, 2006: RIB. CRACKED. INSPECTION TYPE:C3 LEFT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-3-3, 57-0
- [SDR UPS06847871](https://openairdocs.org/sdr/UPS06847871), Aug 16, 2006: SKIN. CORRODED. FOUND CORROSION BETWEEN SKIN AND DOUBLER AT L36 STA 1180, EXTERIOR BULGED. CUT OUT DAMAGED AREA AT STA 1180 L36 IAW SAA EA 008-5320-01-A0381. FABRICATED AND INS

All 268: https://openairdocs.org/deregistered/N802UP-2010-07-02/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 20020430009029I](https://openairdocs.org/incident/20020430009029I), Apr 30, 2002: Doug DC873F (N802UP), Kansas City, MO. (-23) On April 30, 2002, at approximately 2219 CDT, ups flight 673, a DC-8, N802UP, aborted takeoff at Kansas City International Airport, Kansas City, MO.…
- [Incident 20000218002919I](https://openairdocs.org/incident/20000218002919I), Feb 18, 2000: Doug DC873F (N802UP), Pittsburgh, PA. On February 18, 2000, at 0535E, a DC-8-73F, s/n 46100, registered as N802UP and operated as ups (ipxa) flight #172, was enroute from "sdf" to "MDT" when the…

## Other aircraft with N802UP

- [Registered now](https://openairdocs.org/aircraft/N802UP): Beechcraft B300, S/N FL-885, built 2013

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