# N283UP: 1991 Mcdonnell Douglas MD-11F, registration cancelled 2025-04-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 4, 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: 48484
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 22, 2006
- Certificate issued: December 28, 2005
- Last registry action: July 18, 2023
- Mode S code: A2DAF0
- 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/N283UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=283UP
- Page: https://openairdocs.org/deregistered/N283UP-2025-04-04

From the FAA registry file of November 3, 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 (335, newest 50)

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

- [SDR IPXA2022112288362](https://openairdocs.org/sdr/IPXA2022112288362), Nov 22, 2022: BOTTLE. LOW PRESSURE. INSPECTION TYPE:NAR1 DOOR PNEUMATIC CYLINDER PRESSURE LOW.SERVICED DOOR PNEUMATIC CYLINDER IAW AMM 12-25-04-3.
- [SDR IPXA2022102287368](https://openairdocs.org/sdr/IPXA2022102287368), Oct 18, 2022: CAP. DAMAGED. INSPECTION TYPE:3CREPAIR UPPER AFT RUDDER UPPER CAP.REMOVED,FABRICATED, REPLACED UPPER CAP IAW DWG AMC7339 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2022012178118](https://openairdocs.org/sdr/IPXA2022012178118), Jan 20, 2022: SLAT SYSTEM. FAULT MESSAGE. EMERG DECL'D* NO EQUIP USED, A/C LANDED UNEVENTFULLY*ON SHORT FINAL WE GOT A SLAT DISAG WENT AROUND ON DOWN WINDW WITH SLATS EXTENDED THE SLAT DISAG LEVELWOULD 
- [SDR IPXA2021090873721](https://openairdocs.org/sdr/IPXA2021090873721), Sep 6, 2021: PUMP. INOPERATIVE. AIR TURNBACK, RECEIVED LEVEL 1 HYD 2 OFF ALERT ENG 2 HYD PUMPS INOP AUTO SYSTEM TURNED PUMPS OFF. REPLACED 2R HYD PUMP REF AMM 29-11-20. PERFORMED OPS & LEAK CH
- [SDR IPXA2021082473079](https://openairdocs.org/sdr/IPXA2021082473079), Aug 23, 2021: BATTERY PACK. NO TEST. EMERGENCY LIGHTING BATTERY 1 LOW, DURING EMERGENCY LIGHT TEST. R & R EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-50-01-401.
- [SDR IPXA2021070871438](https://openairdocs.org/sdr/IPXA2021070871438), Jul 6, 2021: BATTERY PACK. MISINSTALLED. EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT PWR SUPPLY BATTERY REVERSED DMP 33-50-04. OPS AND TEST GOOD IAW AMM 33-51-01.
- [SDR IPXA2021070171165](https://openairdocs.org/sdr/IPXA2021070171165), Jun 30, 2021: HINGE. CORRODED. INSPECTION TYPE:CR/H I/B FLAP O/B AFT HINGE #7 LUG BORE AND O/B FACE HAS PITTINGCORROSION REMOVED PER CMM 57-52-03. PERFORMED DETAILED, FPI, HFEC TO ENSURE NO C
- [SDR IPXA2021070171164](https://openairdocs.org/sdr/IPXA2021070171164), Jun 30, 2021: HINGE. CORRODED. INSPECTION TYPE:CL/H I/B FLAP O/B AFT HINGE #6 LUG BORE HOLE AND I/B FACE HAS PITTINGREMOVED PITTING AND CORROSION FROM FLAP LUG BORE IAW CMM 57-52-03. PERFORME
- [SDR IPXA2021070171175](https://openairdocs.org/sdr/IPXA2021070171175), Jun 14, 2021: HINGE BRACKET. CORRODED. INSPECTION TYPE:3CLT I/B FLAP FWD HINGE BRACKET CORRODED AT #3 LUG.REPAIRED CORRODED HINGE BRACKET IAW VT-SAA EA 011-5740-01-A91998 REV I/R AND UPS EO MD11-5740
- [SDR IPXA2021062370892](https://openairdocs.org/sdr/IPXA2021062370892), Jun 8, 2021: TEE ANGLE. CRACKED. INSPECTION TYPE:3CRT WING O/B FLAP I/B AFT HINGE FAIRING FWD END TEE ANGLE IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B AFT HINGE FAIRING FWD EN
- [SDR IPXA2021070171171](https://openairdocs.org/sdr/IPXA2021070171171), Jun 7, 2021: HINGE BRACKET. CORRODED. INSPECTION TYPE:3CLT WING I/B FLAP O/B AFT HINGE BRACKET LUGS HAS CORROSION.REPAIRED CORRODED LT WING I/B FLAP O/B AFT HINGE BRACKET LUGS IAW VT-SAA EA 011-5740
- [SDR IPXA2021070171170](https://openairdocs.org/sdr/IPXA2021070171170), Jun 7, 2021: HINGE BRACKET. CORRODED. INSPECTION TYPE:3CRT WING I/B FLAP O/B FWD HINGE BRACKET LUGS HAS PITTING CORROSION.REPAIRED CORRODED RT WING I/B FLAP O/B FWD HINGE BRACKET LUGS IAW VT-SAA EA 
- [SDR IPXA2021070171168](https://openairdocs.org/sdr/IPXA2021070171168), Jun 7, 2021: HINGE BRACKET. CORRODED. INSPECTION TYPE:3CRT WING I/B FLAP O/B AFT HINGE BRACKET LUG BORES HAS PITTING CORROSION.REPAIRED CORRODED RT WING I/B FLAP O/B AFT HINGE BRACKET LUGS IAW VT-SA
- [SDR IPXA2021063071152](https://openairdocs.org/sdr/IPXA2021063071152), Jun 7, 2021: HINGE BRACKET. CORRODED. INSPECTION TYPE:3CR/H WING O/B FLAP O/B HINGE BRACKET ASSY. O/B LUG ON A/C SIDE HAS CORROSION ON LUG BORE AND FACE.REPAIRED HINGE BRACKET ASSY. IAW VT-SAA EA 01
- [SDR IPXA2021063071151](https://openairdocs.org/sdr/IPXA2021063071151), Jun 7, 2021: HINGE BRACKET. CORRODED. INSPECTION TYPE:3CR/H WING O/B FLAP HINGE BRACKET ASSY ON A/C SIDE HAS CORROSION ON LUG BORE AND FACE.REPAIRED HINGE BRACKET ASSY IAW VT-SAA EA 011-5700-01-A918
- [SDR IPXA2021062971104](https://openairdocs.org/sdr/IPXA2021062971104), Jun 7, 2021: HINGE. CORRODED. INSPECTION TYPE:3CLH O/B FLAP O/B AFT HINGE #7 LUG HOLE HAS PITTING CORROSION.REPAIRED CORRODED LH O/B FLAP LUG HOLE IAW CMM 57-52-04 (MINOR)
- [SDR IPXA2021062971102](https://openairdocs.org/sdr/IPXA2021062971102), Jun 7, 2021: HINGE. CORRODED. INSPECTION TYPE:3CLT O/B FLAP O/B FWD HINGE #2 LUG HOLE HAS PITTING CORROSION.REPAIRED CORRODED LT O/B FLAP HINGE IAW CMM 57-44-09 PG 602 (MINOR)
- [SDR IPXA2021062570959](https://openairdocs.org/sdr/IPXA2021062570959), Jun 7, 2021: HINGE BRACKET. CORRODED. INSPECTION TYPE:3CLT WING O/B FLAP O/B FWD HINGE #1 LUG BORE HOLE HAS PITTING.REPAIRED CORRODED LT WING O/B FLAP O/B FWD HINGE BRACKET LUG AT STA. XW 638.31 IAW
- [SDR IPXA2021070171180](https://openairdocs.org/sdr/IPXA2021070171180), Jun 3, 2021: FRAME. DENTED. INSPECTION TYPE:3CMAIN CABIN FUSELAGE FRAME AT STA 740 & LONGERON 12R IS DENTED.REPAIRED DENTED MAIN CABIN FUSELAGE FRAME AT STA 740 & LONGERON 12R IAW VT-SAA E
- [SDR IPXA2021061870730](https://openairdocs.org/sdr/IPXA2021061870730), Jun 3, 2021: LONGERON SPLICE. CRACKED. INSPECTION TYPE:3CMAIN CABIN CEILING AREA HAS A PRODUCTION SPLICE THAT IS CRACKED AT STA. 1531 ON LONG. 7 R/H.REMOVED, FABRICATED AND REPLACED SPLICE IAW DWG. A
- [SDR IPXA2021061870729](https://openairdocs.org/sdr/IPXA2021061870729), Jun 3, 2021: ANGLE. CRACKED. INSPECTION TYPE:3CMAIN CABIN LONGERON 15 R/H T ANGLE IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REP[LACED T ANGLE IAW DWG. AEA7588 AND SRM 51-33-01. (MINOR
- [SDR IPXA2021061570633](https://openairdocs.org/sdr/IPXA2021061570633), Jun 3, 2021: SUPPORT BRACKET. CRACKED. INSPECTION TYPE:C3MAIN CABIN SUPPORT BRACKET CRACK AT STA.1341 LON 15R.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT BRACKET IAW SRM 51-33-01 AND 51-31-01 (MI
- [SDR IPXA2021062971124](https://openairdocs.org/sdr/IPXA2021062971124), Jun 2, 2021: FRAME. GOUGED. INSPECTION TYPE:3CMAIN CARGO DOOR AFT FRAME IS GOUGED AT MID SECTION.REPAIRED GOUGED MAIN CARGO DOOR AFT PAN AT STA 765.375 BETWEEN Z= 30 AND Z= 40 IAW VT-SAA E
- [SDR IPXA2021062971107](https://openairdocs.org/sdr/IPXA2021062971107), Jun 2, 2021: INTERCOSTAL. CRACKED. INSPECTION TYPE:3CLOWER VERTICAL STABILIZER REAR CENTER SPAR INTERCOSTAL IS CRACKED AT STA. YID= 375, XID= 7.1 AND ZID= 65.REPAIRED CRACKED LOWER VERTICAL STABI
- [SDR IPXA2021062971103](https://openairdocs.org/sdr/IPXA2021062971103), Jun 2, 2021: BEAM. CRACKED. INSPECTION TYPE:3CL3 DOOR PLUG UPPER HORIZONTAL BEAM IS CRACK AT AFT END.REMOVED AND REPLACED CRACKED HORZ BEAM IAW SRM 51-35-01,51-33-01 AND 51-31-01 (MINOR).
- [SDR IPXA2021062871034](https://openairdocs.org/sdr/IPXA2021062871034), Jun 2, 2021: SKIN. CORRODED. INSPECTION TYPE:3CL/H EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA. 2153 TO 2163 AND BETWEEN L33L TO 35L.REPAIRED CORRODED FUSELAGE SKIN BETWEEN STA. 2153 T
- [SDR IPXA2021062370909](https://openairdocs.org/sdr/IPXA2021062370909), Jun 2, 2021: STRINGER. CRACKED. INSPECTION TYPE:2CCENTER WING UPPER AUX TANK STRINGER 52 CRACKED BETWEEN STA.XCW 35 TO XCW 59.75.REPAIRED CRACKED CENTER WING UPPER AUX TANK STRINGER 52 BETWEEN
- [SDR IPXA2021062370891](https://openairdocs.org/sdr/IPXA2021062370891), Jun 2, 2021: CHANNEL. CRACKED. INSPECTION TYPE:3CUPPER FUSELAGE SUPPORT ANGLE (CHANNEL) INSIDE VERTICAL STAB PANEL 364FR IS CRACKED.REMOVED AND REPLACED CRACKED SUPPORT ANGLE (CHANNEL) INSIDE
- [SDR IPXA2021062370890](https://openairdocs.org/sdr/IPXA2021062370890), Jun 2, 2021: BEAM. CRACKED. INSPECTION TYPE:3CMAIN CABIN L3 DOOR PLUG LOWER HORIZONTAL BEAM IS CRACKED AT FWD END.REMOVED AND REPLACED CRACKED MAIN CABIN L3 DOOR PLUG LOWER HORIZONTAL BEAM
- [SDR IPXA2021061570618](https://openairdocs.org/sdr/IPXA2021061570618), Jun 2, 2021: INTERCOSTAL. CRACKED. INSPECTION TYPE:C3FWD CARGO COMPARTMNET INTERCOSTAL CRACK AT RH STA.6-50 BETWEEN LON 42R-43R.REMOVED,FABRICATED AND REPLACED CRACKED INTERCOSTAL IAW SRM 51-35-0
- [SDR IPXA2021070171174](https://openairdocs.org/sdr/IPXA2021070171174), Jun 1, 2021: RUB STRIP. CRACKED. INSPECTION TYPE:3CRT WING #2 SLAT LOWER RUB STRIP CRACK AT O/B T/E STA.XIS 358.005.REPAIRED CRACKED RUB STRIP IAW VT-SAA EA 011-5754-01-A9197 REV I/R AND UPS EO
- [SDR IPXA2021070171178](https://openairdocs.org/sdr/IPXA2021070171178), Jun 1, 2021: FLOORBEAM. CORRODED. INSPECTION TYPE:3CAFT CARGO FLOOR BEAM SUPPORT AT STA. 1841 AND X= 46 IS CORRODED.REPAIRED CORRODED AFT CARGO FLOOR BEAM SUPPORT AT STA 1841 AND X= 46 IAW EA 01
- [SDR IPXA2021062570958](https://openairdocs.org/sdr/IPXA2021062570958), Jun 1, 2021: TEE FITTING. CORRODED. INSPECTION TYPE:3CR/H AFT LOWER WING TO BODY FAIRING SUPPORT FRAME AT STA 1521 IS CORRODED.REPAIRED CORRODED R/H AFT LOWER WING TO BODY FAIRING SUPPORT FRAME TE
- [SDR IPXA2021062871036](https://openairdocs.org/sdr/IPXA2021062871036), Jun 1, 2021: SEAT TRACK. CRACKED. INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CRACKED AT STA. 1421 AT X= 27.50.REAPIRED CRACKED SEAT TRACK BETWEEN STA. 1411 TO 1431 AT X= 27.50 IAW SRM 53-00-52 R
- [SDR IPXA2021061870728](https://openairdocs.org/sdr/IPXA2021061870728), Jun 1, 2021: TRUSS. CRACKED. INSPECTION TYPE:3CLONGERON 27R/H TRUSS FITTING IS CRACKED AT STA. 1159.REMOVED, FABRICATED AND REPLACED TRUSS FITTING IAW DWG. AFA7605 AND SRM 51-31-01. (MINOR)
- [SDR IPXA2021061570623](https://openairdocs.org/sdr/IPXA2021061570623), Jun 1, 2021: ANGLE. CRACKED. INSPECTION TYPE:C3FWD CARGO COMPARTMENT STRUT TO FLOOR BEAM TEE ANGLE CRACK AT STA. 6-75 RBL 58".REMOVED,FABRICATED AND REPLACED CRACKED TEE ANGLE IAW SRM 51-33
- [SDR IPXA2021061570621](https://openairdocs.org/sdr/IPXA2021061570621), Jun 1, 2021: ATTACH ANGLE. CRACKED. INSPECTION TYPE:C3CENTER CARGO COMPARTMENT SLOPE PANEL SUPPORT ANGLE CRACK AT STA.1561 RH SIDE.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-
- [SDR IPXA2021061570620](https://openairdocs.org/sdr/IPXA2021061570620), Jun 1, 2021: SUPPORT ANGLE. CRACKED. INSPECTION TYPE:C3CENTER CARGO COMPARTMENT FRAME SUPPORT ANGLE CRACK AT STA. 5-53 LON 41L.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-35-01
- [SDR IPXA2021061570619](https://openairdocs.org/sdr/IPXA2021061570619), Jun 1, 2021: INTERCOSTAL. CRACKED. INSPECTION TYPE:C3FWD CARGO COMPARTMENT INTERCOSTAL CRACK AT STA. 6-50 BETWEEN LON 42L-43L.REMOVED,FABRICATED AND REPLACED CRACKED INTERCOSTAL IAW SRM 51-35-01 
- [SDR IPXA2021061570614](https://openairdocs.org/sdr/IPXA2021061570614), Jun 1, 2021: BRACKET. RUSTED. INSPECTION TYPE:3CR/H WING O/B FLAP I/B FWD. HINGE O/B SIDE LOAD FITTING HAS RUST COMING OUT.REMOVED AND REPLACED SIDE LOAD FITTING/BRACKET IAW AMM 57-53-01-400
- [SDR IPXA2021061570613](https://openairdocs.org/sdr/IPXA2021061570613), Jun 1, 2021: ATTACH ANGLE. CRACKED. INSPECTION TYPE:3CR/H UPPER WING TO BODY FAIRING SUPPORT ATTACH ANGLE IS CRACKED AT STA. 1361.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AEA0553 AND SRM 51
- [SDR IPXA2021061570611](https://openairdocs.org/sdr/IPXA2021061570611), Jun 1, 2021: SUPPORT. CRACKED. INSPECTION TYPE:3CCENTER CARGO FRAME ANGLE/SUPPORT IS CRACKED AT STA. 1761 AND LONG. 41L.REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG ADA0130 AND SRM 51-35-
- [SDR IPXA2021061170413](https://openairdocs.org/sdr/IPXA2021061170413), Jun 1, 2021: FRAME ANGLE. CRACKED. INSPECTION TYPE:C3CENTER CARGO FRAME ANGLE CRACK AT STA.1701 LON 41L.REMOVED,FABRICATED AND REPLACED CRACKED FRAME ANGLE IAW SRM 51-31-01 AND 51-35-01 (MINOR).
- [SDR IPXA2021070171177](https://openairdocs.org/sdr/IPXA2021070171177), May 29, 2021: SPAR CAP. CORRODED. INSPECTION TYPE:3C, RT WING UPPER T/E PANELS ARE BULGED AT REAR SPAR APPROX. XORS 980.REPAIRED CORRODED RT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 964 
- [SDR IPXA2021062971112](https://openairdocs.org/sdr/IPXA2021062971112), May 29, 2021: SKIN. CORRODED. INSPECTION TYPE:3CRT WING UPPER SKIN BETWEEN XORS 97 TO XORS 130.40 AT STRINGER 15 IS CORRODED.REPAIRED CORRODED RT WING UPPER SKIN BETWEEN XORS 97 TO XORS 130.
- [SDR IPXA2021062570957](https://openairdocs.org/sdr/IPXA2021062570957), May 29, 2021: SPAR CAP. CORRODED. INSPECTION TYPE:3CRT WING UPPER T/E PANEL IS BULGED AT REAR SPAR & APPROX. XORS 813.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 769.25
- [SDR IPXA2021062570956](https://openairdocs.org/sdr/IPXA2021062570956), May 29, 2021: SPAR CAP. CORRODED. INSPECTION TYPE:3CRT WING UPPER T/E PANEL IS BULGED JUST FWD OF #5 SPOILER O/B HINGE.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 769.2
- [SDR IPXA2021062570955](https://openairdocs.org/sdr/IPXA2021062570955), May 29, 2021: SKIN. CORRODED. INSPECTION TYPE:3CRT WING UPPER SURFACE BETWEEN STA. XORS 372 - XORS 402 AT STRINGER 6 IS CORRODED.REPAIRED CORRODED RT WING UPPER SURFACE BETWEEN STA. XORS 372
- [SDR IPXA2021062871035](https://openairdocs.org/sdr/IPXA2021062871035), May 29, 2021: SKIN. CORRODED. INSPECTION TYPE:3CL/H WING UPPER SKIN HAS CORROSION BETWEEN STA. XORS. 185 TO XORS. 196.5 AT STR. 11.REPAIRED CORRODED L/H WING UPPER SKIN BETWEEN STA. XORS. 18
- [SDR IPXA2021062871033](https://openairdocs.org/sdr/IPXA2021062871033), May 29, 2021: SKIN. GOUGED. INSPECTION TYPE:3CR/H WING FIXED L/E UPPER SKIN IS GOUGED BETWEEN STA. XOS. 1187 TO 1191 & 10" FWD FROM AFT EDGE.REPAIRED R/H WING FIXED L/E UPPER SKIN BETWEEN 

All 335: https://openairdocs.org/deregistered/N283UP-2025-04-04/reports.md

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