AD 2007-03-17 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA | TBM 700 | Airworthiness Directives; SOCATA Model TBM 700 Airplanes |
Unsafe Condition
Corrosion on the fuselage skin between frames 12 and 13 could lead to reduced structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the fuselage skin between frames 12 and 13 for corrosion. Repair or replace affected areas as necessary. Perform subsequent inspections at specified intervals.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the completion of 50 flight hours after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
SOCATA Model TBM 700 airplanes, all serial numbers.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuselage
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - 2007-03-17R1.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 2007-03-17 R1 Document Type: AD Final Rules Docket Number: FAA-2006-26234 Subject Heading: Airworthiness Directives; SOCATA Model TBM 700 Airplanes Subject: Fuselage Status: Current Citation: Federal Register: August 5, 2009 Citation Publish Date: 08/05/2009 Effective Date: 09/09/2009 Make: SOCATA Model: TBM 700 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: 2007-03-17 Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 0
Document Text
Show stored source text (verify against official source)
AD Final Rules - 2007-03-17R1.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 2007-03-17 R1 Document Type: AD Final Rules Docket Number: FAA-2006-26234 Subject Heading: Airworthiness Directives; SOCATA Model TBM 700 Airplanes Subject: Fuselage Status: Current Citation: Federal Register: August 5, 2009 Citation Publish Date: 08/05/2009 Effective Date: 09/09/2009 Make: SOCATA Model: TBM 700 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: 2007-03-17 Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 0
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.
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