- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 36880
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 29, 2016
- Certificate issued
- June 18, 2025
- Expires
- June 30, 2032
- Mode S code
- A42A14
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-7B27/3 model are included below.
On this page
Airworthiness directives that may apply · 11
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1998 | 1 |
|---|---|
| 2007 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2014 | 1 |
| 2015 | 2 |
| 2018 | 4 |
| 2019 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
Engine · CFM International CFM56-7B27/3 series
AD 2023-05-05Turbine Engine Compressor SectionAD 2022-02-03Turbine Engine Accessory DriveAD 2018-26-01Turbine Engine Compressor SectionInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · CFM International CFM56-7B27/3 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairNTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N368ARMatched 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 737-86J aircraft
Service difficulty reports · 19
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2025F00008Exchanger · leakingON FLIGHT ENGINE OIL CONSUMPTION HIGHSDR 2023F00093Flap · failedFLAPS TRANSIT LIGHT AMBER WITH TRAILING EDGE FLAPS EXTENDED AND THEY AGREE WITH FLAP HANDLE POSITION 27808001/08SDR 2023F00076None · noneFUEL DRIP ENGINE 2 DURING STAR, WAS ACCOMPLISHED TEST IDLE POWER LEACK CHECK IAW AMM. 71-00-00-700-801-F00, ENGINE VENTS AND DRAINS
See all 19 reportsSTCs that may be installed · 2
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · CFM International CFM56-7B27/3 series
STC SE04840NYInstallation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engineSTC SE03036CHApplication of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision.