SA11045SC
Modification of the nose wheel shimmy damper in accordance with Down Time Aviation, LLC, drawing number DTA-TBM700-3252 (sheets 1-7); sheets 1-3 and 5-6 Revision A; sheet 4 Revision B; and sheet 7 Revision IR, all dated 12/7/2010 or later FAA approved revision. The aircraft is to be maintained per the Modification Instructions and Instructions for Continued Airworthiness, Document Number 32-52-01, Revision IR, dated January, 2011, or later FAA accepted revision. Held by Down Time Aviation LLC. Last revised April 25, 2011. System: landing gear.
What it applies to
- Kind of product
- Aircraft
- Design holder
- SOCATA
- Models
- TBM 700
- Type certificate
- A60EU
- On this site
- Daher (Socata) TBM-700 TBM 700 through TBM 960 1,011 registered
- The FAA's record
- On the FAA's site
What an approved modification is
A supplemental type certificate is the FAA's approval of a change to a certified design: a new engine or propeller, avionics, an autopilot, floats, a parachute, a larger fuel tank, an ice-protection kit. The company holding it may sell the kit and the paperwork to owners of the listed models; the modification then becomes part of that aircraft's record. The FAA's list says what was approved and for which models, not how many aircraft carry it.
Source: FAA supplemental type certificates (Dynamic Regulatory System). Register counts from the FAA register of October 21, 2026.