- Registered owner
- C C & E I LLC
- Location
- Louisville, KY
- Owner type
- LLC
- Serial number
- 37874
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 19, 2012
- Certificate issued
- May 4, 2012
- Expires
- May 31, 2028
- Mode S code
- A3EA54
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 1 |
|---|---|
| 1991 | 4 |
| 1993 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 4 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 3 |
| 2008 | 1 |
| 2009 | 4 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2020 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 2023 | 1 |
See all 47 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N351UPMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 767-34AF aircraft
FAA incident reports
No FAA accident or incident reports matched to N351UPMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 767-34AF aircraft
Service difficulty reports · 44
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR IPXA2026101806238Skin · puncturedDURING WALKAROUND, FOUND A PUNCTURE AT SLAT NR 10 (WS 624). SLAT CRACKED AT SEVERAL SPOTS, NUMEROUS RIVETS SHEARED. R/R SLAT #10 (STATION 624) IAW MM 27-81-02-024. ACCOMPLISHED OPS TEST PER MM 27-81-02/501 TEST FAIL. DUE TO NO SLAT TARGETS. S296,S310 SENSOR TASDR IPXA2026033018198Counterbalance · out of adjustFORWARD ENTRY DOOR IS HEAVIER AND HARDER TO OPEN THAN OTHER FORWARD ENTRY DOORS. ADJUSTED THE COUNTERBALANCE IAW AMM 52-12-16.SDR IPXA2026032379778Door · bindingFORWARD ENTRY DOOR IS VERY HEAVY TO LIFT. PERFORMED COUNTERBALANCE SYSTEM TEST PER AMM 52-12-16-735 , LUBED DOOR TRACKS , OPS CHECK GOOD.
See all 44 reportsSTCs that may be installed · 5
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · GE CF6-80C2B6F
STC SE01543CHReplace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve.STC SE01478CHInstallation of Cook Airtomic alignment joint p/n AIR 22912.STC SE01471ATReplace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine.STC SE00463LAInstall fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220STC SA2227SOInstallation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES