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Aircraft record

N845X2006 Egolf Mark COMPAIR 8

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply

Registration
Valid
expires Oct 31, 2029
Based in
Bozeman, MT
owner city / state
Engine
M601E-11 · 751 hp
Walter
Owners
1
since 2010
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Central Copters INC
Owner type
Corporation
City, state
Bozeman, MT
Certificate issued
Oct 1, 2010
Expires
Oct 31, 2029
Airworthiness
Experimental · Amateur Built
Airworthiness date
Mar 2, 2006

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 data

Airframe

Manufacturer
Egolf Mark
Model
COMPAIR 8
Year
2006
Serial number
0585206
Aircraft type
Fixed wing single engine
Category
Land
Certification
Not Type Certificated
Seats
8
Engines
1
Max takeoff weight
Up to 12,499 lb
Kit
Aerocomp Inc Compair 8
Mode S code
AB9479

Engine

Make and model
Walter M601e-11
Type
Turbo-prop
Power
751 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2010 – nowCentral Copters INCBozeman, MT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (6)

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.

ADSubjectEffectiveApplies to
2025-18-08GE Aviation Czech s.r.o. (Type Certificate Previously Held by WALTER Engines a.s.…Oct 21, 2025Engine (M601E-11)
2024-03-05Turbine Engine Reduction GearApr 17, 2024Engine (M601E-11)
2024-02-04Turbine Engine Compressor SectionMar 28, 2024Engine (M601E-11)Only with: Centrifugal compressor case P/N M601-154.61 installed.
2022-26-01Turbine Engine Combustion SectionJan 26, 2023Engine (M601E-11)Only with: Engines installed on single-engine airplanes with combustion chamber outer liner P/N M601-229.3, M601-229.3A, M601-229.3B, M601-229.31A, or M601-229.31B installed.
2020-23-01Fuel Control/ Turbine EnginesNov 24, 2020Engine (M601E-11)Serial numbers per Appendix 1 of GE Aviation Czech ASB-H75-73-00-00-0038 [01] et al. (single document), dated September 24, 2020. Only with: Fuel control unit (FCU) with P/N and S/N listed in Appendix 1 of the ASB installed.
Show all 6 ADs
ADSubjectEffectiveApplies to
2020-15-04Engine Collector/Tailpipe/NozzleAug 31, 2020Engine (M601E-11)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (0)

No Service Difficulty Reports found for this airframe since 1995.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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