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Aircraft STC directory

SOCATA TBM 700 STCs

The Jun 30, 2026 FAA DRS snapshot contains 13 selected supplemental type certificates with status Current whose public applicability data names the SOCATA TBM 700. Use it to identify modification scope and recorded holders—not to determine serial-number effectivity, compatibility, installation approval, or commercial availability.

13
listed Current at snapshot
9
holder directories
8
modification categories
Mar 24, 2025
latest recorded revision

Modification demand surface

Other aircraft modifications4
Aircraft connectivity2
Propellers2
Avionics1
Cabin and interiors1
Electrical systems1
Aircraft structures1
Landing gear and brakes1

Recorded holders

Aircraft Systems and Manufacturing Inc1Amphenol Cable and Interconnect Technologies Inc.1Elliott Aviation Technical Products Development, Inc.1Raisbeck Engineering Inc.1Honeywell International Inc1Air Comm Corporation1Textron Aviation Inc1Hartzell Propeller Inc1MT- Propeller Entwicklung GmbH1

Recently revised TBM 700 STCs

Showing the 13 most recently revised records. Each entry links to the FAA source and separates public approval data from private commercial claims.

ST02994NYAircraft structures

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.

FAA holder: Quest Diagnostics

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SA02958NYPropellers

Installation of propeller MTV-27-1-E-C-F-R(P)/CFR225-55f in accordance with MT Propeller Installation Instruction Doc. No. E-1879, Original Issue, dated October 25, 2010. The following MT Propeller documents are required with this installation: EASA Approved Airplane Flight Manual Supplement Doc. No. E-1878, Original Issue, dated October 25, 2010 and Instruction for Continued Airworthiness Doc. No. E-1880, Original Issue, dated October 25, 2010.

FAA holder: MT- Propeller Entwicklung GmbH

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SA11045SCLanding gear and brakes

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.

FAA holder: Down Time Aviation LLC

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