AD 81-15-01

final rule

Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes

AD Number
81-15-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft M7 Aerospace LLC SA226-AT Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes
aircraft M7 Aerospace LLC SA226-T Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes
aircraft M7 Aerospace LLC SA226-TC Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes

Unsafe Condition

Structural wear or damage to the lower wing-to-fuselage aerodynamic fairing stiffeners, attached grommets, and lower fuselage pressure vessel skin.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the lower wing-to-fuselage aerodynamic fairing stiffers, attached grommets, and lower fuselage pressure vessel skin for deterioration, wear, or damage. Repair damaged areas and modify the structure in accordance with Swearingen Service Bulletin SB53-006 or equivalent means approved by the FAA.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within the next 200 hours' time in service after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Swearingen Models SA226-T (S/N T201 through T275 and T277 through T291), SA226-AT (S/N AT001 through AT074), and SA226-TC (S/N TC201 through TC407) airplanes certificated in all categories.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Structural Wear or Damage

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
81-15-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes
Subject:
Structural Wear or Damage
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/15/1981
Make:
M7 Aerospace LLC
Model:
SA226-AT | SA226-T | SA226-TC
Product Type:
Aircraft
Product Subtype:
Small/Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 81-15-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4163

AD NUMBER:   81-15-01

SUBJECT HEADING:   Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 15, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-15-01 SWEARINGEN: Amendment 39-4163. Applies to Swearingen Models SA226-T, S/N T201 through T275 and T277 through T291; SA226-AT, S/N AT001 through AT074, and SA226-TC, S/N TC201 through TC407 airplanes certificated in all categories. Compliance required within the next 200 hours' time in service, after the effective date of this AD, unless Swearingen Bulletin SB53-006 issued November 27, 1980, has been accomplished. (Airworthiness Docket No. 80-ASW-54.)

Inspect the lower wing-to-fuselage aerodynamic fairing stiffeners, the attached grommets, and the lower fuselage pressure vessel skin for deterioration, wear, or damage. Repair any damaged areas and modify the structure in accordance with Swearingen Service Bulletin SB53-006 issued November 24, 1980, or equivalent means approved by the Chief, Engineering and Manufacturing Branch, FAA, Southwest Region.

A special flight permit may be issued in accordance with FAR 21.197 to allow flight of the aircraft to a location where this AD can be accomplished.

This amendment becomes effective August 15, 1981.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_81-15-01.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
81-15-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes
Subject:
Structural Wear or Damage
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/15/1981
Make:
M7 Aerospace LLC
Model:
SA226-AT | SA226-T | SA226-TC
Product Type:
Aircraft
Product Subtype:
Small/Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 81-15-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4163

AD NUMBER:   81-15-01

SUBJECT HEADING:   Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 15, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-15-01 SWEARINGEN: Amendment 39-4163. Applies to Swearingen Models SA226-T, S/N T201 through T275 and T277 through T291; SA226-AT, S/N AT001 through AT074, and SA226-TC, S/N TC201 through TC407 airplanes certificated in all categories. Compliance required within the next 200 hours' time in service, after the effective date of this AD, unless Swearingen Bulletin SB53-006 issued November 27, 1980, has been accomplished. (Airworthiness Docket No. 80-ASW-54.)

Inspect the lower wing-to-fuselage aerodynamic fairing stiffeners, the attached grommets, and the lower fuselage pressure vessel skin for deterioration, wear, or damage. Repair any damaged areas and modify the structure in accordance with Swearingen Service Bulletin SB53-006 issued November 24, 1980, or equivalent means approved by the Chief, Engineering and Manufacturing Branch, FAA, Southwest Region.

A special flight permit may be issued in accordance with FAR 21.197 to allow flight of the aircraft to a location where this AD can be accomplished.

This amendment becomes effective August 15, 1981.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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