ST02994NY
a. Fuselage and wing Fatigue Life Expended (FLE) based on Quest s usage profile and recorded flight data. b. Fabrication and installation of the fuselage and wing identification placards in accordance with Quest Diagnostics document No.QDTBM-2010-007, Rev.A. c. The aircraft must be maintained in accordance with Section 6 (Instructions for Continued Airworthiness) of the Maintenance Plan for Continued Airworthiness, QDTBM-2010-006, Rev.A and dated June 13, 2011. Held by Quest Diagnostics. Last revised June 23, 2011. System: airframe structure.
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 22, 2026.