AD 74-19-03

final rule

Airworthiness Directives; Bell Model 206A and 206B Helicopters

AD Number
74-19-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bell Helicopter Textron Canada Limited 206A Airworthiness Directives; Bell Model 206A and 206B Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B Airworthiness Directives; Bell Model 206A and 206B Helicopters

Unsafe Condition

Failure of the inboard ribs with possible loss of a stabilizer on Model 206A and 206B helicopters, and excessive movement of the horizontal stabilizer.

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

Required Actions

Replace any cracked inboard ribs, install a doubler specified in Bell Service Bulletin 206-01-73-7, and install Horizontal Stabilizer Stop Kit P/N 206-704-096-3 following applicable service bulletins.

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

Compliance Time

within 100 hours time in service after the effective date of this A.D.

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

Affected Aircraft

Bell Model 206A and 206B helicopters, serial numbers 1 through 913 (for inboard ribs issue) and serial numbers 1 through 1251 (for horizontal stabilizer stop kit), equipped with specific part numbers as noted.

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

Federal Register Abstract

Horizontal Stabilizer Ribs

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_74-19-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-19-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 206A and 206B Helicopters
Subject:
Horizontal Stabilizer Ribs
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/13/1974
Make:
Bell Helicopter Textron Canada Limited
Model:
206A | 206B
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-19-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1954

AD NUMBER:   74-19-03

SUBJECT HEADING:   Airworthiness Directives; Bell Model 206A and 206B Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective October 13, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-19-03 BELL: Amendment 39-1954. Applies to Bell Model 206A and 206B helicopters as noted herein, certificated in all categories.

Compliance required within 100 hours time in service after the effective date of this A.D., unless already accomplished.

To prevent possible failure of the inboard ribs with possible loss of a stabilizer on Model 206A and 206B helicopters, serial numbers 1 through 913 equipped with horizontal stabilizer, P/N 206-020-119, replace any cracked inboard ribs and modify all inboard ribs by installing a doubler specified in and using the applicable procedures described in Items 3 through 24, Bell Helicopter Company Service Bulletin No. 206-01-73-7, Revision A, dated December 11, 1973 or later FAA approved revision.

To prevent excessive movement of the horizontal stabilizer install Horizontal Stabilizer Stop Kit, P/N 206-704-096-3, on Model 206A and 206B helicopters, Serial Numbers 1 through 1251, in accordance with Bell Helicopter Company Service Bulletin No. 206-01-74-1, Revision A, dated May 6, 1974, or later FAA approved revision.

This amendment becomes effective October 13, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-19-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-19-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 206A and 206B Helicopters
Subject:
Horizontal Stabilizer Ribs
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/13/1974
Make:
Bell Helicopter Textron Canada Limited
Model:
206A | 206B
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-19-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1954

AD NUMBER:   74-19-03

SUBJECT HEADING:   Airworthiness Directives; Bell Model 206A and 206B Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective October 13, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-19-03 BELL: Amendment 39-1954. Applies to Bell Model 206A and 206B helicopters as noted herein, certificated in all categories.

Compliance required within 100 hours time in service after the effective date of this A.D., unless already accomplished.

To prevent possible failure of the inboard ribs with possible loss of a stabilizer on Model 206A and 206B helicopters, serial numbers 1 through 913 equipped with horizontal stabilizer, P/N 206-020-119, replace any cracked inboard ribs and modify all inboard ribs by installing a doubler specified in and using the applicable procedures described in Items 3 through 24, Bell Helicopter Company Service Bulletin No. 206-01-73-7, Revision A, dated December 11, 1973 or later FAA approved revision.

To prevent excessive movement of the horizontal stabilizer install Horizontal Stabilizer Stop Kit, P/N 206-704-096-3, on Model 206A and 206B helicopters, Serial Numbers 1 through 1251, in accordance with Bell Helicopter Company Service Bulletin No. 206-01-74-1, Revision A, dated May 6, 1974, or later FAA approved revision.

This amendment becomes effective October 13, 1974.

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.