AD 70-25-05

final rule

Airworthiness Directives; American Aviation Model AA-1 Airplanes

AD Number
70-25-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft True Flight Holdings LLC AA-1 Airworthiness Directives; American Aviation Model AA-1 Airplanes

Unsafe Condition

Binding of the trim actuator and elevator centering bungee in the existing bearing.

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

Required Actions

Comply with Item 1, 'Bungee Mounting Plate Replacement,' of American Aviation Service Letter No. 69-1A or later revision or equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA - Eastern Region.

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

Compliance Time

within the next 25 hours in service or within three (3) weeks from the effective date of this AD, whichever occurs first

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

Affected Aircraft

American Aviation Model AA-1, Serial Number AA1-0001 through AA1-0125 airplanes certificated in all categories.

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

Federal Register Abstract

Bungee Mounting Plate

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_70-25-05.html
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Details
AD Number:
70-25-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; American Aviation Model AA-1 Airplanes
Subject:
Bungee Mounting Plate
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/08/1970
Make:
True Flight Holdings LLC
Model:
AA-1
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 70-25-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1118

AD NUMBER:   70-25-05

SUBJECT HEADING:   Airworthiness Directives; American Aviation Model AA-1 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 8, 1970.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-25-05 AMERICAN AVIATION: Model AA-1. Amdt. 39-1118. Applies to American Aviation Model AA-1, Serial Number AA1-0001 through AA1-0125 airplanes certificated in all categories.

Unless already accomplished, compliance required within the next 25 hours in service or within three (3) weeks from the effective date of this AD, whichever occurs first.

To preclude binding of the trim actuator and elevator centering bungee in the existing bearing, comply with Item 1, "Bungee Mounting Plate Replacement," of American Aviation Service Letter No. 69-1A, dated July 10, 1969, or later revision or equivalent modification, either of which must be approved by the Chief, Engineering and Manufacturing Branch, FAA - Eastern Region.

This amendment is effective December 8, 1970.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_70-25-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
70-25-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; American Aviation Model AA-1 Airplanes
Subject:
Bungee Mounting Plate
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/08/1970
Make:
True Flight Holdings LLC
Model:
AA-1
Product Type:
Aircraft
Product Subtype:
Small 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: 70-25-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1118

AD NUMBER:   70-25-05

SUBJECT HEADING:   Airworthiness Directives; American Aviation Model AA-1 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 8, 1970.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
70-25-05 AMERICAN AVIATION: Model AA-1. Amdt. 39-1118. Applies to American Aviation Model AA-1, Serial Number AA1-0001 through AA1-0125 airplanes certificated in all categories.

Unless already accomplished, compliance required within the next 25 hours in service or within three (3) weeks from the effective date of this AD, whichever occurs first.

To preclude binding of the trim actuator and elevator centering bungee in the existing bearing, comply with Item 1, "Bungee Mounting Plate Replacement," of American Aviation Service Letter No. 69-1A, dated July 10, 1969, or later revision or equivalent modification, either of which must be approved by the Chief, Engineering and Manufacturing Branch, FAA - Eastern Region.

This amendment is effective December 8, 1970.

FOOTER:

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.