# N368AR: 2011 Boeing 737-86J

- Status: Valid registration
- Airframe: [Boeing 737-86J](https://openairdocs.org/model/boeing-737-86j) (registry code 13844CT, 149 seats)
- Engine: [CFM International CFM56-7B27/3 series](https://openairdocs.org/engine/cfm-international-cfm56-7b27-3-series) (registry code 13805)
- Serial number: 36880
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2016
- Certificate issued: June 18, 2025
- Expires: June 30, 2032
- Mode S code: A42A14
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=368AR
- Page: https://openairdocs.org/aircraft/N368AR

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B27/3 model are included.

## ADs that may apply (OpenAirDocs): 11 in force

### Matched by airframe (Boeing 737-86J)

None in force.

### Matched by engine (CFM International CFM56-7B27/3 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

### Historical (superseded or no longer in force)

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014

## Information bulletins (advisory) (1 in force)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA17WA168](https://openairdocs.org/ntsb/DCA17WA168), Aug 1, 2017: Boeing 737 (N368AR), Tijuana, Mexico, incident, no damage

## FAA accident and incident reports

None matched to N368AR.

## Service difficulty reports (19)

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

- [SDR 2025F00008](https://openairdocs.org/sdr/2025F00008), Jan 2, 2025: EXCHANGER. LEAKING. ON FLIGHT ENGINE OIL CONSUMPTION HIGH
- [SDR 2023F00093](https://openairdocs.org/sdr/2023F00093), Mar 18, 2023: FLAP. FAILED. FLAPS TRANSIT LIGHT AMBER WITH TRAILING EDGE FLAPS EXTENDED AND THEY AGREE WITH FLAP HANDLE POSITION 27808001/08
- [SDR 2023F00076](https://openairdocs.org/sdr/2023F00076), Jan 16, 2023: NONE. NONE. FUEL DRIP ENGINE 2 DURING STAR, WAS ACCOMPLISHED TEST IDLE POWER LEACK CHECK IAW AMM. 71-00-00-700-801-F00, ENGINE VENTS AND DRAINS
- [SDR 2022FA0000252](https://openairdocs.org/sdr/2022FA0000252), Mar 1, 2022: ANTI-SKID VALVE. FAILED. LUZ DE SISTEMA DE ANTI-SKID ENCENDIDA / ANTI-SKID SYSTEM LIGHT ON FALLA DE VALVULA DE ANTI-SKID / ANTI-SKID VALVE FAULTE
- [SDR 2022FA0000067](https://openairdocs.org/sdr/2022FA0000067), Dec 14, 2021: TRIM MOTOR. FAILED. DURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW FIM 27-41 TASK 805 PROCE
- [SDR 2022F00041](https://openairdocs.org/sdr/2022F00041), Dec 14, 2021: NONE. DAMAGED. DURING TRANSIT CHECK THE STABILIZER TRIM WITHOUT MOVEMENT, DURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PE
- [SDR ASMF202110019](https://openairdocs.org/sdr/ASMF202110019), Sep 9, 2021: FUEL HEATER. LEAKING. DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION ON RIGHT ENGINE VENTS AND DRAINS, DETECTING LEAK FU
- [SDR 2021F00227](https://openairdocs.org/sdr/2021F00227), Sep 9, 2021: FUEL HEATER. LEAKING. FUEL LEAK IN THE RIGHT ENGINE, DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION ON RIGHT ENGINE VENT
- [SDR ASMF202101020](https://openairdocs.org/sdr/ASMF202101020), Jan 6, 2021: SELECTOR VALVE. FAILED. CAPTAIN REPORTED THAT DURING CLIMB, THE LANDING GEAR WAS MOVED UP AT THE THIRD ATTEMPT. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED BITE
- [SDR ASMF202101008](https://openairdocs.org/sdr/ASMF202101008), Nov 7, 2020: BEARING. EXCESS PLAY. DURING THE OVERNIGHT AT MEX STATION AND IN ACCORDANCE WITH 16A CHECK AND TASK CARD J3727-098-01-01, IT WAS DETECTED FREEPLAY OUT OF LIMITS AT BOTH ELEVATORS. MA
- [SDR ASMF202101005](https://openairdocs.org/sdr/ASMF202101005), Oct 13, 2020: SWITCH. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO TAKEOFF CONFIGURATION ALARM WAS ACTIVE. MAINTENANCE PERSONNEL PERFORMED TAKE OFF WARNING SYSTEM TEST, IAW AMM 31-51-00-730-
- [SDR ASMF202101002](https://openairdocs.org/sdr/ASMF202101002), Oct 4, 2020: ACOUSTIC PANEL. DAMAGED. DURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL SCRATCHES ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DET
- [SDR ASMF202011014](https://openairdocs.org/sdr/ASMF202011014), Oct 1, 2020: ACOUSTIC PANEL. DAMAGED. DURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL NICKS ON RIGHT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECT
- [SDR ASMF202011010](https://openairdocs.org/sdr/ASMF202011010), Sep 27, 2020: ACOUSTIC PANEL. DENTED. DURING TRANSIT CHECK, IT WAS DETECTED SEVERAL NICKS, DENTS AND GOUGE ON BOTH ENGINES INNER BARREL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DE
- [SDR ASMF202011006](https://openairdocs.org/sdr/ASMF202011006), Sep 22, 2020: BLADE. DENTED. DURING THE OVERNIGHT AT MEX STATION AND IN ACCORDANCE WITH EO 3772005 R4 OF LEFT ENGINE FAN DISK PRESSURE FACES INSPECTION, IT WAS DETECTED A DENT IN THE FAN BL
- [SDR ASMF202006019](https://openairdocs.org/sdr/ASMF202006019), Mar 18, 2020: FUEL HEATER. LEAKING. DURING MAINTENANCE PROGRAM CHECK, IT WAS DETECTED A LEFT ENGINE FUEL LEAK. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING FUEL LEAK IN THE FUEL HEATER SERV
- [SDR ASMF20190614012](https://openairdocs.org/sdr/ASMF20190614012), May 23, 2019: WHEEL. FAILED. CAPTAIN REPORTED HIGH VIBRATION DURING TAKEOFF IN MEX ON THE LEFT INBOARD / OUTBOARD MAIN LANDING GEAR. AT CUN, MAINTENANCE PERSONNEL PERFORMED THE TIRE TREAD L
- [SDR ASMF201708001](https://openairdocs.org/sdr/ASMF201708001), Aug 1, 2017: INDICATION SYS. UNKNOWN. CAPTAIN REPORTED THAT DURING APPROACH, TRAILING EDGE FLAP DISAGREE, SO FLIGHT CREW ACCOMPLISHED THE QRH 9.28 PROCEDURE, BEING NECESSARY A MISSED APPROACH. MAINT
- [SDR ASMF201610009](https://openairdocs.org/sdr/ASMF201610009), Aug 20, 2016: SKIN. DAMAGED. CAPTAIN REPORTED A LIGHTNING STRIKE IN THE FUSELAGE SKIN DURING DESCENT. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTIN

## STCs that may be installed (OpenAirDocs) (2)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (CFM International CFM56-7B27/3 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application 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. Delta Air Lines Inc

## Related

- Other Boeing 737-86J aircraft: https://openairdocs.org/model/boeing-737-86j/aircraft.md
- The CFM International CFM56-7B27/3 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b27-3-series.md

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