- Registered owner
- Western Antique Aeroplane & Automobile Museum
- Location
- Hood River, OR
- Owner type
- Corporation
- Serial number
- G-11
- Year built
- 1938
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, exhibition
- Airworthiness date
- November 19, 2006
- Certificate issued
- March 5, 2024
- Expires
- March 31, 2031
- Mode S code
- A1B721
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 1
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1986 | 1 |
|---|---|
| 1995 | 1 |
| 2022 | 1 |
Airframe · Dart G
AD 2022-03-15Fuel Quantity IndicatorSuperseded and historical ADs · 3
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Dart G
SAIB CE-14-03Wing Spar DamageNTSB investigations
No NTSB investigations matched to N20993Matched 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 Dart G aircraft
FAA incident reports
No FAA accident or incident reports matched to N20993Matched 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 Dart G aircraft
Service difficulty reports
No reports matched to N20993General aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Dart G aircraft
STCs that may be installed · 2
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Dart G
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01959SEInstallation of a Lycoming O-320-A2B engine and Sensenich M74DM-58 propeller; installed in accordance with FW-TAL385-04, Revision IR, dated July 3, 2008, and maintained in accordance with Instructions for Continued Airworthiness Document Number FW-TAL385-13, Revision IR, dated 9/25/08.