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Aircraft record

N4446T1983 Burkhart Grob G 103 TWIN II

Registration validUnclaimedSource: FAA, updated Oct 18, 2026

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

Registration
Valid
expires Dec 31, 2028
Based in
Hummelstown, PA
owner city / state
Engine
NONE
None
Owners
1
since 2018
NTSB events
1
substantial, 1998
ADs may apply
0
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Registered owner
Individual owner
City, state
Hummelstown, PA
Certificate issued
Dec 28, 2018
Expires
Dec 31, 2028
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
3824
Aircraft type
Glider
Category
Land
Certification
Type Certificated
Seats
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A55CB5

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. 2018 – nowIndividual ownerHummelstown, PA · current
  2. 1972International Aircraft Deliveries INCMiami, FL · different airframe: Piper Pa-32-300 S/N 32-7240060

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

Oct 24, 1998 · Saratoga Spring, NY

The pilot's failure to maintain control of the glider while landing.

Damage
Substantial
Injuries
None
Report
NYC99LA017

From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC99LA017)

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 · rudder pedal · crackedMay 11, 2006

    SIGNIFICANT CORROSION NOTED AT HORIZONTAL BASE OF LEFT RUDDER PEDAL. RUDDER PEDAL CRACKED AND STARTED TO DEFORM SLIGHTLY IN THE VICINITY OF THE CRACK. THE RUDDER PEDAL IS PLATED AND THE CORROSION APPEARED TO HAVE STARTED FROM THE INSIDE BUT THE EXACT CAUSE HAS YET TO BE DETERMINED. THESE PEDALS…

    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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