N76PKExtra-Flugzeugbau Gmbh 300/S
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 16, 2026- Registered owner
- Individual owner
- City, state
- Rockingham, VT
- Certificate issued
- Mar 20, 2018
- Expires
- Mar 31, 2028
- Airworthiness
- Experimental · Exhibition
- Airworthiness date
- Feb 18, 1998
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
- Extra-Flugzeugbau Gmbh
- Model
- 300/S
- Serial number
- 15
- 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
- AA407E
Engine
- Make and model
- None None
- Type
- Reciprocating
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2018 – nowIndividual ownerRockingham, VT · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 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 (2)
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.
- Fuselage · longeron · crackedFeb 2, 1998
DURING A MAINTENANCE PROCEDURE INVOLVING THE REMOVAL OF HORIZONTAL STABILIZER AND FUSELAGE FABRIC, FOUND A CRACK IN THE UPPER LONGERON AT THE HORIZONTAL STABILIZER FORWARD ATTACH POINT. THIS LOCATION CANNOT BE SEEN DURING NORMAL INSPECTION PROCEDURES. SB 300-2-95 INSPECTION OF UPPER LONGERON IN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · wire · bentJun 27, 1996
ELEVATOR TRIM FORWARD SPRING STEEL WIRE WAS FOUND BENT CLOSE TO THE TRIM CONTROL LEVER. THIS RENDERED THE SYSTEM UNUSABLE AND UNAIRWORTHY DUE TO THE POSITION IT WAS IN WHEN IT WAS BENT REMAINS. THE PILOT COULD POSSIBLY NOT KNOW IT WAS BENT AS IT FEELS FREE WHEN OPERATED IN THE COCKPIT. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 16, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 16, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026