N840GH1979 Rockwell International 690C
Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 18, 2026- Registered owner
- Crescent Valley Baling LLC
- Owner type
- LLC
- City, state
- Corvallis, OR
- Certificate issued
- Oct 18, 2021
- Expires
- Oct 31, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jul 16, 2007
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Rockwell International
- Model
- 690C
- Year
- 1979
- Serial number
- 11615
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 11
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AB8077
Engine
- Make and model
- Honeywell Tpe331-10t
- Type
- Turbo-prop
- Power
- 776 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2021 – nowCrescent Valley Baling LLCCorvallis, OR · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (9)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-13-05 | Turbine Engine Reduction Gear | Jul 26, 2018 | Engine (TPE331-10T)Only with: Hydraulic torque sensor gear assemblies P/Ns 3101726-1, -2, or -3 installed. |
| 2018-02-14 | Turbine Engine Combustion Section | Feb 28, 2018 | Engine (TPE331-10T)Only with: Combustion chamber case assemblies P/Ns 869728-x, 893973-x, 3101668-x, or 3102613-x (any dash number) installed. |
| 2016-21-07 | Honeywell International Inc. Turboprop Engines | Nov 28, 2016 | Engine (TPE331-10T)Only with: Woodward fuel control unit (FCU) assemblies with Honeywell P/Ns listed in Table 1 to paragraph (c) of the AD installed. |
| 2016-18-17 | Honeywell International Inc. Turboprop and Turboshaft Engines | Nov 4, 2016 | Engine (TPE331-10T)Only with: With 2nd stage compressor impeller P/N 893482-1 through -5 inclusive, or P/N 3107056-1 or 3107056-2, installed. |
| 2014-12-04 | Honeywell International Inc. Turboprop Engines | Jul 22, 2015 | Engine (TPE331-10T)Only with: Woodward fuel control unit (FCU) assemblies with Honeywell P/Ns listed in Table 1 to paragraph (c) (P/N 869199, 893561, 897770, 897375, 897780 dash numbers) installed. |
Show all 9 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2012-02-06 | Honeywell International Inc. TPE331-10 and TPE331-11 Series Turboprop Engines | Mar 15, 2012 | Engine (TPE331-10T)Serial numbers per Table 2 of Honeywell International Inc. Alert Service Bulletin TPE331-72-A2156, dated December 2, 2008. Only with: First stage turbine disk P/N 3101520-1 or 3107079-1 with S/N listed in the ASB installed. |
| 2009-17-05 | Honeywell International Inc. TPE331-10 and TPE331-11 Series Turboprop Engines | Sep 1, 2009 | Engine (TPE331-10T)Only with: First stage turbine disk P/N 3101520-1 or 3107079-1, S/N 2-03501-2299, 2-03501-2300, 2-03501-2301, 2-03501-2302, or 2-03501-2304 installed. |
| 2002-25-02 | Honeywell International Inc. TPE331-3, -5, -6, -8, -10, and -11 Series Turboprop and… | Jan 21, 2003 | Engine (TPE331-10T) |
| 2002-21-15 | Honeywell International Inc. TPE331 Series Turboprop and TSE331-3U Series Turboshaft… | Nov 26, 2002 | Engine (TPE331-10T)Only with: Engines with second stage turbine stator assemblies P/N 894528-1, -2, -3, -5, -6, -10, or -11 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Engine · scavenge pump · failedMay 17, 2011
PILOT REPORTED THAT THE RT ENGINE RPM ACCELERATED UNCOMMANDED FROM 98 PERCENT TO APPROXIMATELY 103.5 PERCENT MOMENTARILY, A FEW SECONDS LATER IT DID IT AGAIN AND THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND LAND THE ACFT SINGLE ENGINE, HE DID SO WITHOUT INCIDENT. MX CHECKED THE ENGINE AFTER…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026