# N819UP: Douglas DC-8-73F, registration cancelled 2011-03-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 24, 2011
- 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: 46019
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 7, 1986
- Certificate issued: October 25, 1985
- Last registry action: September 15, 2009
- Mode S code: AB2C9B
- 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/N819UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=819UP
- Page: https://openairdocs.org/deregistered/N819UP-2011-03-24

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 (205, newest 50)

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

- [SDR UPS08854213](https://openairdocs.org/sdr/UPS08854213), Dec 17, 2008: ROD. BROKEN. F/O MADE UNEVENTFUL LANDING WITH NORMAL BRAKING. EXITED RUNWAY & HAD NO BRAKES AT 55 KTS. NOSE WHEEL STEERING WORKED, BUT HAD TO USE EMERGENCY AIR BRAKES. R&R N
- [SDR UPS08853383](https://openairdocs.org/sdr/UPS08853383), Sep 20, 2008: DOUBLER. DAMAGED. INSPECTION TYPE:N/A REPAIR DOUBLER AT FUSELAGE FRAME 50 AND STRINGER 24L REQUIRED REPLACEM MENT D385232. REMOVED DOUBLER, ACCOMPLISHED STEPS APPENDIX-A (1) THRU
- [SDR UPS08853382](https://openairdocs.org/sdr/UPS08853382), Sep 20, 2008: DOUBLER. DAMAGED. INSPECTION TYPE:N/A DOUBLER AT FUSELAGE STATION 902, LT SIDE OF FUSELAGE REQUIRES REPLACEMENT. REMOVED EXISTING DOUBLER AND SHIM PER SRM 51-1-00, C/W EO DC8-533
- [SDR UPS07851177](https://openairdocs.org/sdr/UPS07851177), Nov 15, 2007: SLIDE. DISLODGED. INSPECTION TYPE:N/A THE MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE NEEDS TO BE ADJUSTED IN THE HOLDING CASE AS IT APPEARS TO BE SLIDING OUT AND IT IS DIFFICULT TO R
- [SDR UPS07850551](https://openairdocs.org/sdr/UPS07850551), Aug 29, 2007: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2 AND CHECKS GOOD PER SAME.
- [SDR UPS07850350](https://openairdocs.org/sdr/UPS07850350), Jul 24, 2007: BATTERY. DISCHARGED. INSPECTION TYPE:N/A ON PREFLIGHT AIRCRAFT FAILED EMERGENCY EXIT LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY & RELAY PACK IAW DC8 MM 33-50-1-2.
- [SDR UPS07849803](https://openairdocs.org/sdr/UPS07849803), Apr 20, 2007: SKIN. CRACKED. INSPECTION TYPE:C1 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE C-4 (D-PIT) UPPER FWD DOOR JAMB CORNER. CRACK RUNS FROM FASTENER HOLE TO EDGE OF CUTOUT. REM
- [SDR UPS07849763](https://openairdocs.org/sdr/UPS07849763), Apr 17, 2007: BRACKET. CRACKED. INSPECTION TYPE:C1 LOWER FRONT SPAR CAP BRACKET IS CRACKED IN 2 PLACES BETWEEN XRS 463-428 NR 1 ALT. REMOVED, FABRICATED AND INSTALLED BRACKET IN NR 1 ALT TANK 
- [SDR UPS07849683](https://openairdocs.org/sdr/UPS07849683), Apr 15, 2007: FINGER DOUBLER. CORRODED. INSPECTION TYPE:C1 CORROSION AND POSSIBLE STRESS CRACK ON FINGER DOUBLER COCKPIT SUB FLOOR FS -25 TO 8 RBL 22. REMOVED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW
- [SDR UPS07849681](https://openairdocs.org/sdr/UPS07849681), Apr 15, 2007: FINGER DOUBLER. CORRODED. INSPECTION TYPE:C1 SEVERAL AREAS OF CORROSION AND POSSIBLE CRACK IN FINGER DOUBLER COCKPIT SUBFLOOR FS -60, RBL 22. REMOVED CORRODED FINGER DOUBLER AT STA -60 R
- [SDR UPS07849761](https://openairdocs.org/sdr/UPS07849761), Apr 14, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 855 L10R. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0.
- [SDR UPS07849729](https://openairdocs.org/sdr/UPS07849729), Apr 14, 2007: ATTACH FITTING. CRACKED. INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 756 L13L. REMOVED END FITTING AT STA 756 L13L IAW SRM 51-1-20D. LOCATED, DRILLED UP AND INSTALLED REPLACEMENT F
- [SDR UPS07849728](https://openairdocs.org/sdr/UPS07849728), Apr 14, 2007: ATTACH FITTING. CRACKED. INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 697 L18L. REMOVED CRACKED END FITTING AT STA 697 L18L IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED END 
- [SDR UPS07849727](https://openairdocs.org/sdr/UPS07849727), Apr 14, 2007: ATTACH FITTING. CRACKED. INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 901 L19R. REMOVED CRACKED FITTING AT STA 901 L19R IAW SRM 51-1-20D. LOCATED DRILLED UP, AND INSTALLED REPLACEME
- [SDR UPS07849713](https://openairdocs.org/sdr/UPS07849713), Apr 14, 2007: FITTING. CORRODED. INSPECTION TYPE:C1 BOOT FITTING CORRODED AT STA 759 L22R. REMOVED CORRODED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-20D. PROCURED, LOCATED, DRILLED UP, AND INS
- [SDR UPS07849685](https://openairdocs.org/sdr/UPS07849685), Apr 14, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 T-BOLT BACKUP FITTING CRACKED IN C-PIT TORQUE BOX, STA 1177 L33R UPPER AND LWR FLANGES. REMOVED DAMAGED FITTING AT STA 1177 L33R IAW SRM 51-1
- [SDR UPS07849671](https://openairdocs.org/sdr/UPS07849671), Apr 14, 2007: FITTING. CRACKED. INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 822 L22L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
- [SDR UPS07849670](https://openairdocs.org/sdr/UPS07849670), Apr 14, 2007: FITTING. GOUGED. INSPECTION TYPE:C1 LOWER FWD T-BOLT FITTING GOUGED AT C-PIT DOOR JAM. REMOVED AND REPLACED LWR FWD T-BOLT FITTING IAW SRM 51-3-2.
- [SDR UPS07849765](https://openairdocs.org/sdr/UPS07849765), Apr 12, 2007: DOOR FRAME. MISREPAIRED. INSPECTION TYPE:C1 L1 DOOR CUTOUT HAS RIVET WITH NO ED AT LWR HINGE CUTOUT. REMOVED, FABRICATED, AND INSTALLED L1 DOOR JAMB FRAME IAW SRM 51-1-21, 0D, 51-03-02,
- [SDR UPS07849684](https://openairdocs.org/sdr/UPS07849684), Apr 12, 2007: CHANNEL. CRACKED. INSPECTION TYPE:C1 T-CHANNEL CRACKED UPPER SURFACE AT XRS 204 BETWEEN STRINGERS 60 AND 59. STOPPED DRILLED CRACK AT XRS 204 BETWEEN STRINGERS 59 & 60 IN NR 4 MA
- [SDR UPS07849826](https://openairdocs.org/sdr/UPS07849826), Apr 11, 2007: SKIN. CRACKED. INSPECTION TYPE:C1 LEFT WING UPPER REAR SPAR SKIN CRACKED 5 INCHES AT STA XCW 69. REPAIRED LEFT WING UPPER AFT SPAR AT STA XCW 69.5 IAW SAA EA 008- 5710-01-A083
- [SDR UPS07849791](https://openairdocs.org/sdr/UPS07849791), Apr 11, 2007: SPAR CAP. CRACKED. INSPECTION TYPE:C1 CRACK ON LWR CENTER SPAR CAP FLANGE NEAR XRS 172 NR 2 MAIN TANK. REPAIRED WING CENTER LWR CAP AND WEB AT STA XRS 168 NR 2 MAIN TANK IAW SAA E
- [SDR UPS07849790](https://openairdocs.org/sdr/UPS07849790), Apr 11, 2007: ANGLE. CRACKED. INSPECTION TYPE:C1 CENTER SECTION EXTERIOR L-ANGLE CRACKED THRU STOP DRILLED HOLE AT STA 855 LBL 65. REMOVED CRACKED L-ANGLE AT STA 855 LBL 65 IAW SRM 51-1-20D.
- [SDR UPS07849745](https://openairdocs.org/sdr/UPS07849745), Apr 10, 2007: SKIN. CORRODED. INSPECTION TYPE:C1 EVIDENCE OF CORROSION UNDER VERT STAB SKIN, RIGHT SIDE LARGE AREA OF PILLOWED SKIN WITH SEVERAL FAILED RIVETS. EXTERIOR ZR252-296 ALONG REAR 
- [SDR UPS07849586](https://openairdocs.org/sdr/UPS07849586), Apr 3, 2007: RELEASE MECH. CONTAMINATED. INSPECTION TYPE:N/A DIVERSION - LEFT NOSE GEAR DOOR OPEN IN FLIGHT. FOUND LEFT NOSE GEAR DOOR RELEASE TRIGGER JAMMED WITH DEBRIS. CLEANED TRIGGER IAW MM 32-20-0
- [SDR UPS07849680](https://openairdocs.org/sdr/UPS07849680), Jan 14, 2007: ATTACH FITTING. CRACKED. INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 787 L13R. REMOVED FITTING AT STA 787 L13R IAW SRM 51-1-20D. FABRICATED AND INSTALLED LONGERON END FITTING AT ST
- [SDR UPS06848712](https://openairdocs.org/sdr/UPS06848712), Nov 15, 2006: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT VERY DIM. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND UNIT IAW MM 33-50-01-2-4. OPS CHECK GOOD.
- [SDR UPS06848345](https://openairdocs.org/sdr/UPS06848345), Oct 20, 2006: WINDOW. STICKING. CAPTAIN SIDE WINDOW HARD TO SLIDE. CLEARED DEBRIS FROM WINDOW TRACK. OPERATES AS REQUIRED, REF DC8 MM 56-10-00-0.
- [SDR UPS06847986](https://openairdocs.org/sdr/UPS06847986), Sep 13, 2006: LINE. LEAKING. LOST HYD FLUID - DROPPED TO AUX - FOLLOWED BY MAIN SYSTEM PRESS FLUCTU ATIONS + - 1500 - 2000 PSI. DIVERT TO RICKENBACKER AFB (THIS INFO DIRE CTLY OFF LOGPAGE A
- [SDR UPS06847948](https://openairdocs.org/sdr/UPS06847948), Sep 6, 2006: WINDOW. OBSTRUCTED. CAPTAIN'S EMERGENCY WINDOW WILL NOT FULLY OPEN. REMOVED TRIM ON L3 WINDOW AND DEFERRED PER GMM 3-6-10. WINDOW OPERATES NORMALLY. OK TO CONTINUE D332951.
- [SDR UPS05845844](https://openairdocs.org/sdr/UPS05845844), Nov 30, 2005: LIGHT. MALFUNCTIONED. EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT, BREAKER POPPED, BREAKER RESET LIGHTS OPERATING NORMAL. OPS CK NORMAL ON GROUND PER MM 33-50-00, OK TO CONTINUE SERVI
- [SDR UPS05844301](https://openairdocs.org/sdr/UPS05844301), Apr 11, 2005: SPAR. CRACKED. INSPECTION TYPE: C2, FOUND POSSIBLE CRACK JUST I/B OF XCW 46 ON LOWER FRONT SPAR CAP VERTICAL ANGLE INSIDE RT CTR FUEL TANK. NDT VERIFIED CRACK APPROX 3 INCH LO
- [SDR UPS05844289](https://openairdocs.org/sdr/UPS05844289), Apr 10, 2005: SKIN. CRACKED. INSPECTION TYPE:C2 C-PIT DOOR UPPER AFT CORNER HAS CRACK IN FIRST FASTENER HOLE ABOVE FITTING ATTACH LIP UNDER INTERIOR SKIN. REPAIRED C-PIT DOOR IAW DC-8 SRM 5
- [SDR UPS05844261](https://openairdocs.org/sdr/UPS05844261), Mar 30, 2005: FITTING. CRACKED. INSPECTION TYPE: C2, STRINGER END FITTING FWD INSIDE ACCESS PANEL 505E NR 3 MAIN CRACKED AT STRINGER 51. REMOVED AND REPLACED STRINGER 51 END FITTING IAW DC-8 S
- [SDR UPS05844267](https://openairdocs.org/sdr/UPS05844267), Mar 25, 2005: STRINGER. CRACKED. C2 FOUND STRINGER CRACKED INSIDE FUEL PANEL 506B NR 2 MAIN STRINGER 71. REMOVED CRACKED SECTION OF STRINGER; FABRICATED AND INSTALLED REPLACEMENT SECTION OF STR
- [SDR UPS05844299](https://openairdocs.org/sdr/UPS05844299), Mar 24, 2005: SUPPORT FITTING. CRACKED. INSPECTION TYPE: C2, 62 COMPARTMENT FITTING FOR "POGO STICK" CRACKED AT FWD RT ATTACH BOLT STA 1875. REMOVED AND REPLACED FITTING FOR "POGO STICK" IAW DC-8 SRM 
- [SDR UPS05844268](https://openairdocs.org/sdr/UPS05844268), Mar 24, 2005: FITTING. CRACKED. C2 CRACKED CORNER FITTING IN C-PIT DOOR UPPER AFT CORNER. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-21A, AND 51-1- 20D.
- [SDR UPS05844256](https://openairdocs.org/sdr/UPS05844256), Mar 24, 2005: FITTING. CORRODED. INSPECTION TYPE: C2, AFT CARGO DOOR -C- LOWER DOOR JAMB CUTOUT AFT REAR LOWER CORNER CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F.
- [SDR UPS05844246](https://openairdocs.org/sdr/UPS05844246), Mar 24, 2005: LONGERON. CRACKED. INSPECTION TYPE: C2, 60 COMPT, 6 INCHES CRACK IN L-17L STA 1770. REMOVED LONGERON 17L IAW DC-8 SRM 51-1-21. FABRICATED LONGERON IAW DC- 8 SRM 53-5-3 AND SRM 51-
- [SDR UPS05844245](https://openairdocs.org/sdr/UPS05844245), Mar 24, 2005: FITTING. CRACKED. INSPECTION TYPE: C2, AFT CARGO PIT STA 1200 LONGERON 34R BATHTUB FITTING CRACKED IN FWD AND AFT CORNERS. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-
- [SDR UPS05844259](https://openairdocs.org/sdr/UPS05844259), Mar 22, 2005: FITTING. CRACKED. INSPECTION TYPE:C2 "A" PIT CARGO DOOR ENTRANCE L33R FWD CORNER BOTTOM BANANA FITTING HAS .400 INCH LONG CRACK. ROMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 
- [SDR UPS05844298](https://openairdocs.org/sdr/UPS05844298), Mar 21, 2005: FITTING. CRACKED. INSPECTION TYPE:C2 RIGHT FLAP STA 3 SUPPORT FITTING HAS APPROX 6.125 INCH CRACK ON BOTTOM OF FITTING. REMOVED AND REPLACED RIGHT FLAP STA 3 SUPPORT FITTING IAW 
- [SDR UPS05844258](https://openairdocs.org/sdr/UPS05844258), Mar 21, 2005: RIB. CRACKED. C2 VER. FIN L/E HAS CRACKED RIB 3/4 INCH AT ACCESS PNL 51I. STOP DRILLED CRACK IAW DC-8 SRM 55-02-00. REPAIRED RIB IAW 55-02-00, 51 -1-20D, AND 51-3-0.
- [SDR UPS05844251](https://openairdocs.org/sdr/UPS05844251), Mar 21, 2005: RIB. CRACKED. INSPECTION TYPE: C2, VERTICAL FIN L/E HAS CRACKED RIB .75 INCH AT ACCESS PNL 51F. REPAIRED VERTICAL FIN RIB IAW DC-8 SRM 55-02-00 FIG 002 AND SRM 51-1-20D.
- [SDR UPS05844243](https://openairdocs.org/sdr/UPS05844243), Mar 21, 2005: FITTING. CRACKED. INSPECTION TYPE:C2 RT WING FLAP WELL STA 230 UPPER AREA HAS CRACKED WEB TO INTERCOSTAL ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING IAW DC-8 SRM 51-1-21D
- [SDR UPS05844293](https://openairdocs.org/sdr/UPS05844293), Mar 20, 2005: RIB. DAMAGED. INSPECTION TYPE:C2 RIGHT STA 3 AFT LINK TO FLAP HINGE BOLT FROZEN & NUT PLATE BROKEN. REMOVED DAMAGED RIB, REMOVED AND REPLACED NUT PLATE, AND FABRICATED & INST
- [SDR UPS05844291](https://openairdocs.org/sdr/UPS05844291), Mar 20, 2005: SPAR. CRACKED. INSPECTION TYPE:C2 POSSIBLE CRACK BETWEEN VERTICAL FASTENERS ON RT WING REAR SPAR LOWER T-CAP RIGHT W/W STA 857 RBL 28-32. NDT DETECTED A 4 INCH CRACK PER NDT S
- [SDR UPS05844269](https://openairdocs.org/sdr/UPS05844269), Mar 20, 2005: CHANNEL. CORRODED. C2 CEILING RIB CORRODED WITH CORROSION UNDER RADIUS FILLER RT W/W ABOVE FLAP BUSS DIRECTION CHANGE PULLEYS STA 930 RBL 58. REMOVED AND REPLACED HAT CHANNEL, STI
- [SDR UPS05844260](https://openairdocs.org/sdr/UPS05844260), Mar 20, 2005: RIB. CRACKED. INSPECTION TYPE: C2, CRACKED LOWER RIB ON L/H HORIZONTAL LEADING EDGE 40 INCHES FROM IB END. STOPDRILLED CRACK IAW DC-8 SRM 55-2-0 FIG.2. REPAIRED CRACKED RIB I
- [SDR UPS05844265](https://openairdocs.org/sdr/UPS05844265), Mar 19, 2005: LONGERON. CRACKED. INSPECTION TYPE: C2, LONGERON 15R IS CRACKED AT F/S 1730 & F/S 1750 AT CANTED FRAMES. REMOVED AND REPLACED LONGERON SECTION IAW DC-8 SRM53-2-2 FIG. 10, 51-1 -21

All 205: https://openairdocs.org/deregistered/N819UP-2011-03-24/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 20080213012489I](https://openairdocs.org/incident/20080213012489I), Feb 13, 2008: Doug DC873F (N819UP), Charlotte, NC, Minor damage. (-23) Flight 1285, N819UP, departed kclt enroute to ksdf. While taking off, crew overheard ATC issue a windshear advisory on the approach end of the runway.…
- [Incident 19930618021559I](https://openairdocs.org/incident/19930618021559I), Jun 18, 1993: Doug DC871F (N819UP), Baltimore, MD. Ground personnel overcome by vapors from leaking container. Found hazardous material in cargo bay.

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