# N385AC: 2015 Bombardier CL-215-6B11 (CL-415)

- Status: Valid registration
- Airframe: [Bombardier CL-215-6B11 (CL-415)](https://openairdocs.org/model/bombardier-cl-215-6b11-cl-415) (registry code 1390019, 10 seats)
- Engine: [Pratt & Whitney Canada PW123AF](https://openairdocs.org/engine/pratt-whitney-canada-pw123af) (registry code 52224)
- Data sheets: [TCDS A14EA](https://openairdocs.org/tcds/A14EA) (De Havilland Aircraft of Canada Limited), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 2095
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Restricted, forest
- Airworthiness date: January 8, 2016
- Certificate issued: March 16, 2026
- Expires: March 31, 2033
- Mode S code: A46DE0
- 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=385AC
- Page: https://openairdocs.org/aircraft/N385AC

From the FAA registry file of October 20, 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.

## ADs that may apply (OpenAirDocs): 34 in force

### Matched by airframe (Bombardier CL-215-6B11 (CL-415))

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 2025
- [AD 2023-07-10](https://openairdocs.org/ad/2023-07-10): Equipment/furnishings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jun 20, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2019-25-11](https://openairdocs.org/ad/2019-25-11): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Feb 10, 2020
- [AD 2019-08-12](https://openairdocs.org/ad/2019-08-12): Flight controls · Viking Air CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 13, 2019
- [AD 2019-02-05](https://openairdocs.org/ad/2019-02-05): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Mar 22, 2019
- [AD 2017-17-17](https://openairdocs.org/ad/2017-17-17): Hydraulic power · Viking Air CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 11, 2017
- [AD 2017-15-14](https://openairdocs.org/ad/2017-15-14): Equipment/ Furnishings · Viking Air CL-215-6B11 (CL-415 Variant). Effective Sep 5, 2017
- [AD 2015-02-02](https://openairdocs.org/ad/2015-02-02): Flight Controls · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 11, 2015
- [AD 2014-16-08](https://openairdocs.org/ad/2014-16-08): Nacelles/Pylons · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Sep 23, 2014
- [AD 2013-20-09](https://openairdocs.org/ad/2013-20-09): ATA Code 53, Fuselage · Bombardier CL-215-6B11 (CL-415 Variant). Effective Oct 18, 2013
- [AD 2012-11-04](https://openairdocs.org/ad/2012-11-04): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jul 9, 2012
- [AD 2012-05-05](https://openairdocs.org/ad/2012-05-05): Equipment/Furnishings · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Apr 24, 2012
- [AD 2011-22-06](https://openairdocs.org/ad/2011-22-06): Landing Gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 14, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2009-05-04](https://openairdocs.org/ad/2009-05-04): Rudder lower torque tube · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 16, 2009
- [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 2005
- [AD 2004-26-08](https://openairdocs.org/ad/2004-26-08): Mounting Pad Studs of the Auxiliary Feather Pump · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Feb 9, 2005
- [AD 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004
- [AD 2004-10-04](https://openairdocs.org/ad/2004-10-04): Rear engine mount struts · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 21, 2004
- [AD 2004-03-13](https://openairdocs.org/ad/2004-03-13): Main landing gear (MLG) axles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 17, 2004
- [AD 2002-12-12](https://openairdocs.org/ad/2002-12-12): Wing-to-Fuselage Frame Angles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jul 25, 2002
- [AD 98-05-11](https://openairdocs.org/ad/98-05-11): Switching Valve-to-Rear Inlet Case Sealing Air Tube Assembly · Bombardier CL-215-6B11 (CL-215T Variant). Effective Mar 23, 1998
- [AD 97-11-09](https://openairdocs.org/ad/97-11-09): AFM - Limitation Section - Power Levers · Bombardier CL-215-6B11 (CL-215T Variant). Effective Jun 12, 1997
- [AD 97-11-08](https://openairdocs.org/ad/97-11-08): AFM - Limitation Section - Power Levers · Bombardier CL-215-6B11 (CL-415 Variant). Effective Jun 6, 1997
- [AD 93-16-06 R2](https://openairdocs.org/ad/93-16-06-R2): Rudder-Aileron Interconnect Tab · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 25, 1995
- [AD 77-17-13](https://openairdocs.org/ad/77-17-13): Nose Landing Gear Doors · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Aug 30, 1977
- [AD 77-13-05](https://openairdocs.org/ad/77-13-05): Missing Rivets In Bulkhead · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 29, 1977

### Matched by engine (Pratt & Whitney Canada PW123AF)

- [AD 2013-15-08](https://openairdocs.org/ad/2013-15-08): First-stage PT blades · Pratt & Whitney Canada PW118A, PW118B, PW119B and 15 more. Effective Sep 17, 2013
- [AD 2012-26-08](https://openairdocs.org/ad/2012-26-08): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Feb 15, 2013
- [AD 2004-20-01](https://openairdocs.org/ad/2004-20-01): Bypass valve cover · Pratt & Whitney Canada PW123, PW123AF, PW123B and 10 more. Effective Nov 5, 2004
- [AD 2003-16-04](https://openairdocs.org/ad/2003-16-04): Fuel heaters · Pratt & Whitney Canada PW118, PW118A, PW118B and 19 more. Effective Sep 10, 2003

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

- [AD 2013-11-03](https://openairdocs.org/ad/2013-11-03) (historical): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jun 14, 2013
- [AD 2011-03-08](https://openairdocs.org/ad/2011-03-08) (historical): Landing gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 14, 2011
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2005-18-05](https://openairdocs.org/ad/2005-18-05) (historical): Lower caps of the wing front spar and rear spar · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 6, 2005
- [AD 98-04-08](https://openairdocs.org/ad/98-04-08) (historical): Inspect Lower Cap of Wing Front & Rear Spars · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 4, 1998
- [AD 95-22-04](https://openairdocs.org/ad/95-22-04) (historical): Main Landing Gear Axle · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 8, 1995
- [AD 94-04-02](https://openairdocs.org/ad/94-04-02) (historical): Rear Engine Mount Struts · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Apr 4, 1994
- [AD 2012-11-14](https://openairdocs.org/ad/2012-11-14) (historical): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Jul 20, 2012

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

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N385AC.

## FAA accident and incident reports

None matched to N385AC.

## Service difficulty reports (2)

As reported by operators and repair stations. Reports filed since January 6, 2000, when the mark's previous registration was cancelled.

- [SDR DAT2006F00004](https://openairdocs.org/sdr/DAT2006F00004), May 5, 2006: ENGINE. LEAKING. DURING THE FLIGHT, THE FLIGHT CREW SAW A LOW OIL PRESSURE LIGHT. THE FLIGHT CREW CHECKED THE ENGINE GAUGES AND CONFIRMED IT BY THE LOW OIL PRESSURE GAUGE. THE F
- [SDR CED2006F00024](https://openairdocs.org/sdr/CED2006F00024), Sep 1, 2005: UPLOCK SWITCH. INOPERATIVE. ON APPROACH THE LANDING GEAR HAD TO BE LOWERED USING PROCEDURE A (EMERGENCY PROCEDURES). MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR2 LANDING GEAR UPLOC

## Earlier aircraft with N385AC

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N385AC before.

- [Cancelled 2000-01-06](https://openairdocs.org/deregistered/N385AC-2000-01-06): Crum Alan B EVANS VP-1, S/N 01. Triennial form not returned. Owner: [Crum Alan B](https://openairdocs.org/faa-owner/CRUM%20ALAN%20B), [Joplin, MO](https://openairdocs.org/faa-place/MO/Joplin)
- [Cancelled 1974-08-06](https://openairdocs.org/deregistered/N385AC-1974-08-06): Lockheed 188C, S/N 2004, built 1959. Exported to Ecuador. Owner: [Frederick B Ayer & Associates Inc](https://openairdocs.org/faa-owner/FREDERICK%20B%20AYER%20%26%20ASSOCIATES%20INC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

## Related

- Other Bombardier CL-215-6B11 (CL-415) aircraft: https://openairdocs.org/model/bombardier-cl-215-6b11-cl-415/aircraft.md
- STCs for the Bombardier CL-215-6B11 (CL-415): https://openairdocs.org/model/bombardier-cl-215-6b11-cl-415/stcs.md
- The Pratt & Whitney Canada PW123AF engine: https://openairdocs.org/engine/pratt-whitney-canada-pw123af.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.