- Registered owner
- United Parcel Service Co
- Location
- Louisville, KY
- Owner type
- Corporation
- Serial number
- 23852
- Year built
- 1988
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 30, 1988
- Certificate issued
- October 13, 1988
- Expires
- August 31, 2028
- Mode S code
- A4DD5E
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 15
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2001 | 1 |
| 2002 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 2 |
| 2012 | 1 |
| 2014 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2019 | 1 |
| 2021 | 1 |
| 2024 | 1 |
| 2026 | 1 |
Engine · Pratt & Whitney PW2040
AD 2026-07-06Turbine SectionAD 2024-12-04Turbine SectionAD 2021-14-13Turbine SectionInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N412UPMatched 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 757-24APF aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 248
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR IPXA2026092882672Evas Unit · dislodgedCAPTAIN (LEFT) SIDE EVAS CONTAINER LID DISLODGED AND EVAS EXPOSED. INSTALLED CAPTAIN (LEFT) SIDE EVAS PER AMM 25-60-00.SDR IPXA2026092382672Evas Unit · dislodgedCAPTAIN (LEFT) SIDE EVAS CONTAINER LID DISLODGED AND EVAS EXPOSED, DEFERRAL REMAINSSDR IPXA2026060280694Skin · damagedAFTER REMOVAL OF DME ANTENNA, FOUND SIGNS OF CORROSION. CHECKED LIMITS AT FUSELAGE SKIN AREA ORIGINAL THICKNESS .080 IAW DWG# 143N3471 BLENDED DIMENSIONS L=5.500'', W=2'', X=.004'' MAXIMUM ALLOWABLE X=15%=.012'' AREA FOUND TO BE WITHIN LIMITS IAW B757-200PF S
See all 248 reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.