N2432B1950 Globe GC-1B
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched1 service difficulty report
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Individual owner
- City, state
- Seattle, WA
- Certificate issued
- Aug 27, 1997
- Expires
- Jan 31, 2028
- Airworthiness
- Standard
- Airworthiness date
- Mar 2, 1956
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
- Globe
- Model
- GC-1B
- Year
- 1950
- Serial number
- 3732
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 2
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A23DC4
Engine
- Make and model
- Cont Motor C125 Series
- Type
- Reciprocating
- Power
- 125 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1997 – nowIndividual ownerSeattle, WA · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (0)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
- Reciprocating engine · cover · failedJun 14, 2001
WHILE AIRCRAFT WAS IN FLIGHT ALL ENGINE OIL WAS PUMPED OVERBOARD CAUSING CATASTROPHIC ENGINE FAILURE. LOSS OF ENGINE OIL WAS DUE TO FAILURE OF THREADS ON MAGNESIUM CRANKCASE COVER ASSEMBLY. THE THREADS FAILED WHERE THE OIL FILTER ADAPTER THREADS INTO THE CRANKCASE COVER ASSEMBLY. TO PREVENT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
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