SOCATA TBM-700A — Primary-Source Maintenance & Technical Documentation
The SOCATA TBM-700A is a pressurized single-engine turboprop built to the highest standards of French aerospace engineering — combining PT6A-64 turbine performance with a fully pressurized cabin, retractable gear, and a capable avionics suite. With approximately 800–900 TBM 700-series aircraft delivered worldwide, this platform has one of the strongest owner/operator communities in business turboprop aviation.=
This collection delivers the original EADS SOCATA factory documentation for the TBM-700A in the native SOCATA Interactive Technical Publications format — the structured, ATA-chapter-navigable system developed and issued by SOCATA's own technical publications department. Issue 2, April 2001. This is the original interactive HTML archive as distributed by EADS SOCATA on DVD — not a PDF scan, not a reformatted document.
Not endorsed by, affiliated with, or authorized by SOCATA, DAHER, EADS, or any manufacturer or regulatory authority. These are archival, static-copy documents.
Document Manifest — EADS SOCATA Interactive Technical Publications, Issue 2 · April 2001
- Maintenance Manual (MM) — ATA chapters 04–57, full airframe systems coverage
- Tool & Equipment Manual — specialized tooling and ground support equipment
- Illustrated Parts Catalog (IPC) — exploded views, part numbers, effectivity codes
- Wiring Manual — electrical schematics, wire routing, connector data
- Service Bulletins — manufacturer-issued SB archive
- Service Letters — SOCATA/EADS service correspondence archive
Navigation: Table of Contents · List of Effective Pages · List of Service Bulletins · List of Effective Pages Index · List of Revision Recording · List of Revised Pages · List of Effective Temporary Revisions · Introduction · List of Publications
Technical Profile — TBM-700A
- Powerplant: Pratt & Whitney Canada PT6A-64, flat-rated to 700 SHP
- Maximum Speed: 330 KTAS at FL280
- Service Ceiling: 31,000 ft (pressurized)
- Range: ~1,730 nm (standard fuel)
- Cabin Pressurization: 6.0 psi differential
- Landing Gear: Electrically actuated retractable tricycle
- Original Manufacturer: SOCATA / EADS SOCATA, Tarbes, France
- Type Certificate Holder: DAHER (successor to SOCATA/EADS SOCATA)
- Publication: Issue 2, April 2001 — EADS SOCATA Interactive Technical Publications
⚠️ Regulatory Notice: Under FAA 14 CFR § 43.13 and EASA Part-M, any mechanic performing maintenance on an active aircraft must use current, manufacturer-approved revision-controlled data. This archival document does not satisfy that requirement.
This is an archival, static-copy edition fixed at its original publication date. Intended for historical reference, flight simulation, museum restoration, and educational use only. Not approved for active airworthiness maintenance under FAA 14 CFR § 43.13, EASA Part-M, or equivalent international regulations. Operators of active aircraft must use current, revision-controlled publications from the Type Certificate holder or an authorized distributor.
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