AD 72-21-02

final rule

Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters

AD Number
72-21-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Brantly International, Inc. B-2 Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters
aircraft Brantly International, Inc. B-2A Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters
aircraft Brantly International, Inc. B-2B Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters

Unsafe Condition

Fatigue failure of the pylon outboard bearing shaft, Part Number 280-5 or 280-6.

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

Required Actions

Replace the pylon outboard bearing shaft parts (three per helicopter) with serviceable parts having Part Number 280-6. Torque the replacement shafts to 2500 ± 100 inch-pounds and secure with an AN435-4-9 rivet or equivalent.

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

Compliance Time

Within the next 10 hours time in service after the effective date of this AD, or upon the accumulation of 500 hours total time in service, whichever occurs later.

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

Affected Aircraft

Brantly International, Inc. Models B-2, B-2A, and B-2B Helicopters certificated in all categories.

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

Federal Register Abstract

Pylon Bearing Shaft

Applicability Source Text

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AD Number:
72-21-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters
Subject:
Pylon Bearing Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/08/1972
Make:
Brantly International, Inc.
Model:
B-2 | B-2A | B-2B
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Superseded AD: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Superseded By: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: 72-21-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1569

AD NUMBER:   72-21-02

SUBJECT HEADING:   Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective December 8, 1972.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
72-21-02 BRANTLY: Amdt. 39-1534 as amended by Amendment 39-1569. Applies to Model B-2, B-2A and B-2B Helicopters certificated in all categories.

Compliance required as indicated, unless already accomplished:

To prevent fatigue failure of the pylon outboard bearing shaft, Part Number 280-5 or 280- 6, replace these parts (three per helicopter) with serviceable parts having Part Number 280-6 within the next 10 hours time in service after the effective date of this AD, or upon the accumulation of 500 hours total time in service, whichever occurs later. The replacement pylon outboard bearing shafts must be torqued to 2500 plus or minus 100 inch-pounds and secured with an AN435-4-9 rivet or equivalent.

This AD effectively revises the service life limits published in Type Certificate Data Sheet No. 2H2 for Part Numbers 280-5 and 280-6, which are a part of the hub and inboard blade assembly Part Number 305-1. Part Numbers 280-5 and 280-6 pylon outboard bearing shafts, will now have a service life limit of 500 hours time in service.

Type Certificate Holder, Mr. M. K. Hynes, 1241 Lake Horney Drive, Lakeland, Florida, 33801, may be contacted for information regarding installation tools, replacement parts, etc.

Amendment 39-1534 became effective October 14, 1972, for all persons except those to whom it was made effective upon receipt of the air mail letter dated October 3, 1972, which contained this amendment.

This Amendment 39-1569 becomes effective on December 8, 1972

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_72-21-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
72-21-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters
Subject:
Pylon Bearing Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/08/1972
Make:
Brantly International, Inc.
Model:
B-2 | B-2A | B-2B
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: 72-21-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1569

AD NUMBER:   72-21-02

SUBJECT HEADING:   Airworthiness Directives; BRANTLY Models B-2, B-2A and B-2B Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective December 8, 1972.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
72-21-02 BRANTLY: Amdt. 39-1534 as amended by Amendment 39-1569. Applies to Model B-2, B-2A and B-2B Helicopters certificated in all categories.

Compliance required as indicated, unless already accomplished:

To prevent fatigue failure of the pylon outboard bearing shaft, Part Number 280-5 or 280- 6, replace these parts (three per helicopter) with serviceable parts having Part Number 280-6 within the next 10 hours time in service after the effective date of this AD, or upon the accumulation of 500 hours total time in service, whichever occurs later. The replacement pylon outboard bearing shafts must be torqued to 2500 plus or minus 100 inch-pounds and secured with an AN435-4-9 rivet or equivalent.

This AD effectively revises the service life limits published in Type Certificate Data Sheet No. 2H2 for Part Numbers 280-5 and 280-6, which are a part of the hub and inboard blade assembly Part Number 305-1. Part Numbers 280-5 and 280-6 pylon outboard bearing shafts, will now have a service life limit of 500 hours time in service.

Type Certificate Holder, Mr. M. K. Hynes, 1241 Lake Horney Drive, Lakeland, Florida, 33801, may be contacted for information regarding installation tools, replacement parts, etc.

Amendment 39-1534 became effective October 14, 1972, for all persons except those to whom it was made effective upon receipt of the air mail letter dated October 3, 1972, which contained this amendment.

This Amendment 39-1569 becomes effective on December 8, 1972

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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