- Registered owner
- Brandt Terry R
- Location
- Hood River, OR
- Owner type
- Individual
- Serial number
- 906
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- November 25, 1985
- Expires
- October 31, 2028
- Mode S code
- A12398
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.
| 1993 | 1 |
|---|---|
| 2000 | 1 |
| 2014 | 1 |
Airframe · Taylor J-2
AD 99-26-19 R1WingsSuperseded and historical ADs · 2
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Taylor J-2
SAIB ACE-99-01NTSB investigations
No NTSB investigations matched to N17240Matched 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 Taylor J-2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N17240Matched 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 Taylor J-2 aircraft
Reports on N17240 not matched to an aircraft · 1
They name N17240, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports
No reports matched to N17240General 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 Taylor J-2 aircraft
STCs that may be installed · 19
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Taylor J-2
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SA00780SEInstallation of the True Lock Safety Retention Axle Lock Nut System