- Registered owner
- Crooks James R
- Location
- Carpinteria, CA
- Owner type
- Individual
- Serial number
- XT-912-008
- Type
- Weight-shift-control
- Engine
- 4 cycle
- Airworthiness
- Experimental, registered before 01/31/08
- Airworthiness date
- March 20, 2008
- Certificate issued
- March 15, 2019
- Expires
- March 31, 2029
- Mode S code
- A880F6
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Rotax 912 model are included below.
On this page
Airworthiness directives that may apply · 17
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1998 | 1 |
|---|---|
| 2002 | 4 |
| 2005 | 1 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2013 | 2 |
| 2016 | 2 |
| 2019 | 1 |
| 2023 | 1 |
| 2025 | 2 |
| 2026 | 1 |
See all 21 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N647TSMatched 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 Airborne XT-912 aircraft
FAA incident reports
No FAA accident or incident reports matched to N647TSMatched 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 Airborne XT-912 aircraft
Service difficulty reports
No reports matched to N647TSGeneral 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 Airborne XT-912 aircraft
Reports on N647TS not matched to an aircraft · 2
They name N647TS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2006FA0000259Casting · bentINCOMING INSPECTION FOUND AILERON DRIVE YOKE ATTACH CASTING BENT. UPON FURTHER INSPECTION IT WAS DISCOVERED THE DRIVE YOKE UPPER OR LOWER SHIMS WERE NOT INSTALLED. DRIVE YOKE ATTACH BOLT WAS INSTALLED CAUSING THE CASTING TO BE BENT AND REQUIRES REPLACEMENT BSDR 2006FA0000329Boot · damagedINADVERRTENT ACTIVATION OF ANTI-ICE SYSTEM ON GROUND, RESULTING IN DAMAGE TO ANTI-ICE BOOTS WAS CAUSED BY AN INTERMITTENT GROUND OF CIRCUIT THAT IS NORMALLY OPEN. THE WIRE NR H255A20 RUNS FROM THE CONTROLLER TO THE REMOTE CIRCUIT BREAKER. (K)
STCs that may be installed · 1
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.