# N295UP: 1992 Mcdonnell Douglas MD-11F, registration cancelled 2025-07-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 23, 2025
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas MD-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f) (registry code 3023600)
- Engine: [Pratt & Whitney PW4460](https://openairdocs.org/engine/pratt-whitney-pw4460) (registry code 51673)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (OpenAirDocs)
- Serial number: 48475
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 12, 2008
- Certificate issued: March 31, 2006
- Last registry action: September 15, 2023
- Mode S code: A309DD
- 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/N295UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=295UP
- Page: https://openairdocs.org/deregistered/N295UP-2025-07-23

From the FAA registry file of October 31, 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 Mcdonnell Douglas MD-11F: https://openairdocs.org/model/mcdonnell-douglas-md-11f.md

## Service difficulty reports (322, newest 50)

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

- [SDR IPXA2023120733928](https://openairdocs.org/sdr/IPXA2023120733928), Dec 6, 2023: UNKNOWN. UNKNOWN. LATCH FOR COCKPIT DOOR WILL NOT KEEP DOOR LATCHED OPEN REPLACED LATCH, OP CKS NORMAL. DOCUMENT REFERENCE: 25-00-00
- [SDR IPXA2023120633928](https://openairdocs.org/sdr/IPXA2023120633928), Dec 6, 2023: UNKNOWN. UNKNOWN. LATCH FOR COCKPIT DOOR WILL NOT KEEP DOOR LATCHED OPEN REPLACED LATCH, OP CKS NORMAL.
- [SDR IPXA2023100939811](https://openairdocs.org/sdr/IPXA2023100939811), Oct 6, 2023: UNKNOWN. UNKNOWN. WHILE OPENING ENG #2 FAN COWL TO FOM FOUND R/H FAN COWL DELAMINATED (SEE ATTACHMENT) R+R #2 ENGINE R/H FAN COWL PER AMM 71-12-01. REFERENCE HYUNG CHOE LABOR ROW
- [SDR IPXA2023100639811](https://openairdocs.org/sdr/IPXA2023100639811), Oct 6, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** WHILE OPENING ENG #2 FAN COWL TO FOM FOUND R/H FAN COWL DELAMINATED (SEE ATTACHMENT)
- [SDR IPXA2022112488399](https://openairdocs.org/sdr/IPXA2022112488399), Nov 24, 2022: DOUBLER. DAMAGED. INSPECTION TYPE:N/AFUSELAGE SKIN PREVIOUS REPAIR DOUBLER DAMAGED AT PLANE 25, BL 0REPLACED DOUBLER IAW E.O. MD11-553-85332-A
- [SDR IPXA2022101487140](https://openairdocs.org/sdr/IPXA2022101487140), Oct 14, 2022: BATTERY. DISCHARGED. INSPECTION TYPE:N/AEMERGENCY LIGHT BATTERY TESTS LOWR2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-01. OPS TEST GOOD
- [SDR IPXA2022091486256](https://openairdocs.org/sdr/IPXA2022091486256), Sep 14, 2022: SKIN PANEL. PUNCTURED. INSPECTION TYPE:SVTRANSFERRED FROM LOGPAGE 439463 ITM 1 RH WING OTBD FLAP LOWER SKIN IS PUNCTURED.ACCOMPLISHED PERMANENT MAJOR REPAIR ON RH WING OTBD FLAP LOWER
- [SDR IPXA2022033080667](https://openairdocs.org/sdr/IPXA2022033080667), Mar 16, 2022: FORMER. CRACKED. INSPECTION TYPE:C1L/H O/B WING L/E HAS A FORMER THAT IS CRACK JUST I/B OF THE #9 SLAT TRACK.REMOVED, FAB, REPLACED CRACK FORMER IAW DWG ARB2931 AND SRM 51-33-01
- [SDR IPXA2022032780562](https://openairdocs.org/sdr/IPXA2022032780562), Mar 16, 2022: DOUBLER. CRACKED. INSPECTION TYPE:1CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 537.2 TO 547.5.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. 
- [SDR IPXA2022032180309](https://openairdocs.org/sdr/IPXA2022032180309), Mar 14, 2022: STIFFENER. CRACKED. INSPECTION TYPE:1CRT MLG W/W 3RD STIFFENER CRACK AT LOWER END O/B AFT.REMOVED AND REPLACED CRACK STIFFENER IAW SRM 51-35-01 AND 51-35-02 (MINOR).
- [SDR IPXA2022012478222](https://openairdocs.org/sdr/IPXA2022012478222), Jan 24, 2022: NONE. DENTED. INSPECTION TYPE:N/ASMALL DENT ON RIGHT WING INBOARD FLAP LOWER SURFACE T/E AREA BETWEEN STA XIFH 124 AND XW 291MAJOR REPAIR COMPLETED PER E.O. MD11-575080336-A 
- [SDR IPXA2021082873233](https://openairdocs.org/sdr/IPXA2021082873233), Aug 28, 2021: DOOR. INOPERATIVE. INSPECTION TYPE:N/AUPON ENTERING A/C FOUND L1 DOOR ELECTRIC ACTUATION TO BE INTERMITTENTT/S IAW FIM 34-46-00 & AMM 34-46-00. OPS TEST GOOD AT THIS TIME. THIS CL
- [SDR IPXA2021090173373](https://openairdocs.org/sdr/IPXA2021090173373), Aug 24, 2021: PULLEY. INOPERATIVE. INSPECTION TYPE:N/AL1 DOOR FWD TOP DRIVE CABLE IDLER PULLEY DAMAGEDR&R LA DOOR FWD TOP DRIVE CABLE IDLER PULLEY REF AMM 52-11-03, BOEING DRAWING ABA7788, & BOEI
- [SDR IPXA2021082473097](https://openairdocs.org/sdr/IPXA2021082473097), Aug 23, 2021: PULLEY. DAMAGED. INSPECTION TYPE:N/AL1 DOOR AFT TOP CABLE TENSION PULLEY DAMAGED.INSTALLED NEW PULLEY IN TRUNION. AWAITING PART IN ITEM 2 THIS LOG FOR REINSTALLATION. REF MM 52 
- [SDR IPXA2021081322676](https://openairdocs.org/sdr/IPXA2021081322676), Aug 12, 2021: CABLE. BROKEN. FUELING SUPERVISOR REPORTED L1 DOOR WOULD NOT CLOSE INSPECT L1 DOOR AND FOUND AFT LIFT. LOWERING CABLES BROKEN. INSTALLED LOWER L1 DOOR CABLE UP TO AND INCLUDIN
- [SDR IPXA2021060870293](https://openairdocs.org/sdr/IPXA2021060870293), Jun 8, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTING IN COURIER AREA REMAINS PARTIALLY ILLUMINATED WITH EMERGENCY LIGHT. TEST PASSED ANE WITHOUT INDICATION EAD. DEFERRED EMERGENCY LIGHTS PER MEL
- [SDR IPXA2021012564839](https://openairdocs.org/sdr/IPXA2021012564839), Jan 25, 2021: ROLLER. LACK OF LUBE. L1 DOOR DOES NOT CLOSE/SEAL COMPLETELY ON FORWARD SIDE. THE DOOR DOES NOT OPERATE SMOOTHLY DURING THE LAST HALF OF THE CLOSING EITHER. ITEM DEFERRED PER MEL 52-
- [SDR IPXA2020050154778](https://openairdocs.org/sdr/IPXA2020050154778), Apr 29, 2020: SUPPORT FITTING. CRACKED. INSPECTION TYPE:2C CRACK ON NLG LH TRUNNION SUPPORT FITTING AT FUSELAGE STA Y=582.5 , Z= -114 & X = 24.00.REPAIRED CRACKED LH NLG TRUNNION SUPPORT FITTING AT FU
- [SDR IPXA2020042954772](https://openairdocs.org/sdr/IPXA2020042954772), Apr 29, 2020: LONGERON. CORRODED. INSPECTION TYPE:2CCORROSION ON LONGERON 52 AT FWD EXTENDED FUSELAGE SECTION STA Y=6-73.ACCOMPLISHED SPLICE REPAIR ON LONGERON 52 BETWEEN Y= 6-60.00 - Y= 6-80 IA
- [SDR IPXA2020051555288](https://openairdocs.org/sdr/IPXA2020051555288), Apr 13, 2020: BULKHEAD. CORRODED. INSPECTION TYPE:2C#3 ENG. PYLON AFT BULKHEAD ASSY. HAS CORROSION COMMON TO THE INNER BORE LUG OF BULKHEAD P/N AUB7502-507 & AUB 7502-509.REPAIRED #3 ENG. PYLON 
- [SDR IPXA2020051855346](https://openairdocs.org/sdr/IPXA2020051855346), Apr 8, 2020: STRINGER. CRACKED. INSPECTION TYPE:4CR/H WING TANK AT STA XORS 330.890, STRINGER # 41 IS CRACKED.ACOMPLISHED REPAIR TO R/H WING TANK AT STA XORS 330.890, STRINGER # 41 IAW VT-SAA 
- [SDR IPXA2020051155098](https://openairdocs.org/sdr/IPXA2020051155098), Apr 7, 2020: MOUNT FITTING. DAMAGED. INSPECTION TYPE:4CRT I/B AILERON #2 MOUNT BOTH I/B AND O/B BUSHINGS ARE MIGRATED.REPAIRED DAMAGED RT I/B AILERON #2 MOUNT FITTING I/B AND O/B LUG BUSHING BORES 
- [SDR IPXA2020051555324](https://openairdocs.org/sdr/IPXA2020051555324), Apr 6, 2020: BARRIER. CORRODED. INSPECTION TYPE:2CRIGID CARGO BARRIER WALL HAS CORROSION ON LOWER FACE.REMOVED AND REPLACED RIGID CARGO BARRIER WALL IAW AMM 25-59-13-00-801 AND 25-59-13-400-80
- [SDR IPXA2020051355030](https://openairdocs.org/sdr/IPXA2020051355030), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:4CMAIN CABIN SEAT TRACK AT X=-47.5 BETWEEN STA. 475 AND STA. 488 HAS CORROSION.REPAIRED CORRODED MAIN CABIN SEAT TRACK AT X=-47.5 BETWEEN STA. 4
- [SDR IPXA2020051355214](https://openairdocs.org/sdr/IPXA2020051355214), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:2CMAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA. 459-485 AND X=50 TO X=62.REPAIRED CORRODED SEAT TRACK MBETWEEN STA. 459-485 AND X=50 TO X=62 IA
- [SDR IPXA2020051355266](https://openairdocs.org/sdr/IPXA2020051355266), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:4CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440 - 488 AT X=19.0.REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA. 440 - 488 AT X=19.0 
- [SDR IPXA2020051355210](https://openairdocs.org/sdr/IPXA2020051355210), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 459-480 AND X=77REMOVED AND REPLACED SEAT TRACK AT SAID LOCATION IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2020051355034](https://openairdocs.org/sdr/IPXA2020051355034), Apr 6, 2020: FLOOR PANEL. CORRODED. INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 AND X=75.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 AND X=75.25 IAW VT-SAA EA 011-
- [SDR IPXA2020051355035](https://openairdocs.org/sdr/IPXA2020051355035), Apr 6, 2020: FLOOR PANEL. CORRODED. INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 AND BETWEEN X=47.5 TO X=75.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 AND BETWEEN 
- [SDR IPXA2020050655022](https://openairdocs.org/sdr/IPXA2020050655022), Apr 6, 2020: FLOOR PANEL. CORRODED. INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA. 475 BETWEEN X=-47.5 TO X=-72.25 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA. 475 BETWEEN X=-4
- [SDR IPXA2020050655021](https://openairdocs.org/sdr/IPXA2020050655021), Apr 6, 2020: FLOOR PANEL. CORRODED. INSPECTION TYPE:4CMAIN CABIN FLOOR PANEL AT STA 475 BETWEEN X=-27.5 TO X=-36 HAS CORROSION.REPAIRED CORRODED MAIN CABIN FLOOR PANEL AT STA 475 BETWEEN X=-27.5 T
- [SDR IPXA2020050654983](https://openairdocs.org/sdr/IPXA2020050654983), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:4CSEAT TRACK AT X=-27.5 BETWEEN STA 437 AND STA 479 HAS CORROSION.REPAIRED CORRODED SEAT TRACK AT X=-27.5 BETWEEN STA 437 AND STA 479 IAW VT-SAA
- [SDR IPXA2020050654986](https://openairdocs.org/sdr/IPXA2020050654986), Apr 6, 2020: FLOORBEAM. CORRODED. INSPECTION TYPE:4CFLOOR SUPPORT AT STA 421.578 BETWEEN X=-65 & X=-78 HAS CORROSION.REMOVED AND REPLACED CORRODED FLOOR SUPPORT AT STA 421.578 BETWEEN X=-65 & X=
- [SDR IPXA2020050154808](https://openairdocs.org/sdr/IPXA2020050154808), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 459-475 AT X= 36.0.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 459-475 AT X= 36.0 IAW VT-SAA EA
- [SDR IPXA2020050154807](https://openairdocs.org/sdr/IPXA2020050154807), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440-488 AT X= -17.REPAIRED CORRODED SEAT TRACK BETWEEN STA 440-488 AT X= -17 IAW VT-SAA EA 01
- [SDR IPXA2020050154806](https://openairdocs.org/sdr/IPXA2020050154806), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 421.578-488 AT X=0.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 421.578-488 AT X=0 IAW VT-SAA EA
- [SDR IPXA2020050154805](https://openairdocs.org/sdr/IPXA2020050154805), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 440-488 AT X= -36.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 440-488 AT X= -36 IAW VT-SAA EA 0
- [SDR IPXA2020050154804](https://openairdocs.org/sdr/IPXA2020050154804), Apr 6, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:2CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 475-515 AT X= 47.5.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 475-515 AT X=47.5 IAW VT-SAA EA 
- [SDR IPXA2020051355253](https://openairdocs.org/sdr/IPXA2020051355253), Apr 5, 2020: LONGERON. CRACKED. INSPECTION TYPE:2CCENTER CARGO LONGERON # 52 IS CRACKED BETWEEN STA. 1681-1701.REPAIRED CRACKED CENTER CARGO LONGERON # 52 BETWEEN STA. 1641 TO 1701 IAW VT=SAA 
- [SDR IPXA2020051355211](https://openairdocs.org/sdr/IPXA2020051355211), Apr 5, 2020: DOOR FRAME. CHAFED. INSPECTION TYPE:2CCENTER LANDING GEAR R/H DOOR UPPER AFT CORNER FRAME IS CHAFED.REMOVED FABRICATED AND REPLACED DOOR FRAME IAW DWG. ANB7384 AND SRM 51-31-01. (M
- [SDR IPXA2020051355037](https://openairdocs.org/sdr/IPXA2020051355037), Apr 4, 2020: LONGERON. CRACKED. INSPECTION TYPE:4CMAIN CABIN INTERUPTED LONGERON 16L IS CRACKED BETWEEN STA. 1139 - 1159.REMOVED AND REPLACED CRACKED MAIN CABIN INTERUPTED LONGERON 16L BETWEEN
- [SDR IPXA2020051355268](https://openairdocs.org/sdr/IPXA2020051355268), Apr 4, 2020: STRINGER SPLICE. CRACKED. INSPECTION TYPE:4CCENTER CARGO LONGERON 29R SPLICE IS CRACKED BETWEEN STA. 1661 AND 1681.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 29R SPLICE BETWEEN S
- [SDR IPXA2020051355065](https://openairdocs.org/sdr/IPXA2020051355065), Apr 4, 2020: SPLICE. CRACKED. INSPECTION TYPE:4CCENTER CARGO R/H TUNNEL UPPER AREA SPLICE AT L28R HAS 2 CRACKS.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 28R SPLICE AND CRACKED LONGE
- [SDR IPXA2020051155097](https://openairdocs.org/sdr/IPXA2020051155097), Apr 4, 2020: SUPPORT ANGLE. CRACKED. INSPECTION TYPE:4CCENTER CARGO SLOPE PANEL SUPPORT ANGLE AT STA. 1951 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO SLOPE PANEL SUPPORT ANGLE AT STA. 195
- [SDR IPXA2020050654991](https://openairdocs.org/sdr/IPXA2020050654991), Apr 4, 2020: LONGERON. CRACKED. INSPECTION TYPE:2CCENTER CARGO LONGERON # 42 R/H IS CRACKED BETWEEN STA. 1641-1661.REPAIRED CRACKED CENTER CARGO LONGERON # 42 R/H BETWEEN STA. 1630 TO 1650.130
- [SDR IPXA2020050654990](https://openairdocs.org/sdr/IPXA2020050654990), Apr 4, 2020: LONGERON. CRACKED. INSPECTION TYPE:2CCENTER CARGO LONGERON # 38 R/H IS CRACKED BETWEEN STA. 1661-1681.REPAIRED CRACKED CENTER CARGO LONGERON # 38 R/H BETWEEN STA. 1641 TO 1681 IAW
- [SDR IPXA2020050654989](https://openairdocs.org/sdr/IPXA2020050654989), Apr 4, 2020: LONGERON. CRACKED. INSPECTION TYPE:2CCENTER CARGO LONGERON # 37 R/H IS CRACKED BETWEEN STA. 1661-1681.REPAIRED CRACKED CENTER CARGO LONGERON # 37 R/H BETWEEN STA. 1641 TO 1681 IAW
- [SDR IPXA2020050454884](https://openairdocs.org/sdr/IPXA2020050454884), Apr 4, 2020: LONGERON. CRACKED. INSPECTION TYPE:2CTAIL CONE R/H UPPER LONGERON BEAM IS CRACKED AT THE FWD. END.REPAIRED TAIL CONE R/H UPPER LONGERON BEAM IAW UPS EO MD11-5350-66790-A. (MINOR)
- [SDR IPXA2020050154830](https://openairdocs.org/sdr/IPXA2020050154830), Apr 4, 2020: DOUBLER. WORN. INSPECTION TYPE:2CTAIL CONE LH UPPER LONGERON @ PRODUTION DOUBLER IS WORN THRU.REPAIRED TAILCONE LONGERON / INTERNAL DOUBLER IAW EO MD11-5350-66790-A. (MINOR)
- [SDR IPXA2020050154829](https://openairdocs.org/sdr/IPXA2020050154829), Apr 4, 2020: FRAME. CRACKED. INSPECTION TYPE:2CTAIL CONE FWD. R/H FRAME IS CRACKED AT THE CENTER GUIDE PIN HOLE.REPAIRED TAIL CONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG. 201. (MINOR)

All 322: https://openairdocs.org/deregistered/N295UP-2025-07-23/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 20121015024649I](https://openairdocs.org/incident/20121015024649I), Oct 15, 2012: Mcdonnell Douglas MD-11F (N295UP), Louisville, KY, Minor damage. During a cat iii flight confidence check while landing at sdf, the aircraft flared normally, touched down, but nose continued to rise. The pilot regained…

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