- Registered owner
- Samson Mason H
- Location
- Rives Junction, MI
- Owner type
- Individual
- Serial number
- 11AC-1813
- Year built
- 1947
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Airworthiness date
- November 13, 1955
- Certificate issued
- April 11, 1997
- Expires
- January 31, 2030
- Mode S code
- A40505
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental A&C65 model are included below.
On this page
Airworthiness directives that may apply · 22
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 2 |
| 1993 | 1 |
| 1995 | 1 |
| 1998 | 2 |
| 2001 | 2 |
Airframe · Aeronca 11AC
AD 2000-25-02 R1Wood SparsAD 47-20-01Gascolator Bowl CleaningAD 79-07-02BatteriesInformation bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Aeronca 11AC
SAIB CE-07-45Flight ControlsNTSB investigations
No NTSB investigations matched to N3581EMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Aeronca 11AC aircraft
FAA incident reports
No FAA accident or incident reports matched to N3581EMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Aeronca 11AC aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2007FA0000463Spar · crackedDELAMINATION OCCURRING AT WING STRUT ATTACH LOCATION. CRACK AT BOTTOM EDGE AT ROOT FITTING. POSSIBLE AGE OF SPAR CAUSING DELAMINATION. LONGITUDINAL CRACK AT WING ROOT POSSIBLE EARLIER DAMAGE REPLACE WITH NEW WOOD SPAR (PN 5146L). (K)SDR 2007FA0000417Spar · delaminatedDELAMINATION OCCURRING AT LT FRONT WING SPAR / STRUT LOCATION. CRACK AT BOTTOM EDGE, AT WING ROOT FITTING. POSSIBLE AGE OF SPAR CAUSING DELAMINATION. LONGITUDINAL CRACK AT WING ROOT POSSIBLE EARLIER DAMAGE. REPLACED WITH NEW WOOD SPAR P/N 5146L.
STCs that may be installed · 120
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Aeronca 11AC
STC SA01233SEFabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assemblySTC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lightsSTC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification