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Aircraft record

N4446Y1983 Burkhart Grob G 103 TWIN II

Registration validUnclaimedSource: FAA, updated Oct 18, 2026

Safety record in brief:1 NTSB accident (substantial damage, Jul 2021)No ADs since 1998 matched1 service difficulty report

Registration
Valid
expires Apr 30, 2027
Based in
Mapleton, UT
owner city / state
Engine
NONE
None
Owners
1
since 2002
NTSB events
1
substantial, 2021
ADs may apply
0
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Registered owner
Utah Soaring Association
Owner type
Corporation
City, state
Mapleton, UT
Certificate issued
May 9, 2002
Expires
Apr 30, 2027
Airworthiness
Standard · Glider
Airworthiness date
Sep 13, 1983

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
Burkhart Grob
Model
G 103 TWIN II
Year
1983
Serial number
3825
Aircraft type
Glider
Category
Land
Certification
Type Certificated
Seats
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A55CBA

Engine

Make and model
None None
Type
None

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

Ownership history

Ownership history from FAA records
  1. 2002 – nowUtah Soaring AssociationMapleton, UT · current
  2. 1966 – 1967Piper Aircraft CorpLock Haven, PA · different airframe: Piper Pa-25-235 S/N 25-4085

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Jul 25, 2021 · Levan, UT

The glider’s encounter with atmospheric conditions where the lift was not sufficient to maintain flight which resulted in an off-airport landing and a collision with a fence.

Damage
Substantial
Injuries
Minor
Report
WPR21LA290

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR21LA290)

Accident history for this model

ADs 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.

  • Flight controls · control column · fracturedJun 16, 2007

    ON SECOND FLT OF DAY, & WHILE STILL ON AERO-TOW, PILOT WHO WAS FLYING FROM THE REAR SEAT WITH A NON-PILOT PASSENGER IN FRONT, NOTICED THAT IT REQUIRED APPROXIMATELY 20 DEGREES OF RT-STICK CORRECTION TO MAINTAIN LEVEL FLT. PILOT ALSO OBSERVED AILERONS TO BE IN A NEUTRAL POSITION WITH THIS RT-STICK…

    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

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