- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 208B2335
- Year built
- 2012
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 10, 2012
- Certificate issued
- July 12, 2019
- Expires
- July 31, 2029
- Mode S code
- AB6C01
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 26
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 |
|---|---|
| 1990 | 2 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 2 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
See all 32 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Cessna 208B
SAIB CE-18-32Engine Oil System (Airframe Furnished): Flapper Check Valve FailureSAIB CE-17-25ELEVATOR TORQUE TUBE Inspections for cracks and corrosion in elevator torque tubesSAIB CE-09-42Lights - Landing Light, Beacon Light and Taxi Light Switch ApplicationsEngine · Pratt & Whitney Canada PT6A-114A
SAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxSAIB NE-10-47Turbine Engine Compressor SectionNTSB investigations
No NTSB investigations matched to N835MAMatched 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 Cessna 208B aircraft
FAA incident reports
No FAA accident or incident reports matched to N835MAMatched 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 Cessna 208B aircraft
Reports on N835MA not matched to an aircraft · 2
They name N835MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 20070404005349ICessna 441 · West Mifflin, PA(-23) On April 4, 2007 at 0900 local time, Cessna 441, N835MA, landed at kagc with the left engine feathered and CFR standing by. I interviewed the pilot [privacy data omitted] on 4-5-2007. He stated that they were enroute from bmg to agc and was descending…Incident 20031001027219ICessna 441 · Pittsburgh, PA(-23) Allegheny County Airport, PA, October 1, 2003, at 0810E, aircraft N835MA, a C441, landed on runway 28 after reporting communication problems. The pilot of the aircraft mistakenly transmitted the "hijack" code on the transponder while inbound. The local…
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 141A2026081500002Wing · damagedLEFT WING SUFFERED MAJOR DAMAGE FROM WINDS. WILL REMOVE AND REPLACE WINGSDR MK9A20150423001Unknown · malfunctionedAIRCRAFT WAS BEING FLOWN BY PIC & SIC AT APPROX 400 FT, PILOT FELT A JOLT & OBSERVED ITT AT 720 THEN JUMPED TO 805. THE PILOT REPORTED THE POWER LEVER & EMER POWER LEVER WAS UNRESPONSIVE & UNABLE TO REGULATE FUEL FLOW TO ENG.SDR MK9A2014040901Fuel Control · faultyWHILE FLYING, POWER LEVER WAS MOVED TO IDLE POSITION BUT THERE WAS NO CHANGE IN ENG POWER. TORQUE STAYED BETWEEN 1250 & 1400 FLB.
Reports on N835MA not matched to an aircraft · 4
They name N835MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2007FA0000343Scavenge Pump · fluctuatesCOMMANDED IN-FLIGHT SHUTDOWN OF LT ENGINE DUE TO FLUCTUATING OIL PRESSURE. UNEVENTFUL SINGLE ENGINE LANDING. ENGINE LOST OIL. OIL EXITED ENGINE FROM TURBINE AIR/OIL SEAL AS A RESULT OF TURBINE SCAVENGE PUMP FAILURE. RECOMMEND COMPLIANCE WITH SB 72-2074R1. SDR 20010410AP005Skin · corrodedFOUND FUEL LEAK COMING FROM BEHIND THE RT WING DE-ICE BOOT. AFTER PEELING BACK BOOT TO LOCATE LEAK, NOTED SEVERAL AREAS OF HEAVY CORROSION ON LEADING EDGE. FERRIED AIRCRAFT TO FACILITY FOR LEADING EDGE REPLACEMENT. SUSPECT DE-ICE BOOT WAS INSTALLED USING IMSDR 20010410AP003Boot · leakingNOTED FUEL LEAK FROM BEHIND RT WING DE-ICE BOOT. AFTER PEELING BOOT BACK TO RESEARCH LEAK, NOTED NUMEROUS AREAS OF HEAVY CORROSION. AIRCRAFT WAS FERRIED TO FACILITY FOR REPLACEMENT OF LEADING EDGE ASSEMBLY.
STCs that may be installed · 306
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.