AD 84-01-52 R1

final rule

Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters

AD Number
84-01-52 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Westland Helicopters Limited Westland 30 Series 100 Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters

Unsafe Condition

Failure of the tail rotor gearbox input pitch control lever and subsequent loss of control in flight.

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

Required Actions

Comply with Westland Service Bulletins W30-67-26 (Rev. 3) and W30-65-14 or FAA-approved equivalents. Remove and replace tail rotor gearbox input pitch control levers P/N WK 3068-0037-101 with 200 hours time in service. Use equivalent methods of compliance if approved by the Manager, Brussels Aircraft Certification Office.

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

Compliance Time

Prior to further flight

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

Affected Aircraft

Westland Helicopters Limited Model 30 Series 100 helicopters certificated in all categories.

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

Federal Register Abstract

Pitch Control Lever

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
84-01-52 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters
Subject:
Pitch Control Lever
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/16/1984
Make:
Westland Helicopters Limited
Model:
Westland 30 Series 100
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Superseded AD: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Superseded By: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: 84-01-52 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4845

AD NUMBER:   84-01-52 R1

SUBJECT HEADING:   Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective April 16, 1984.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
84-01-52 R1 WESTLAND HELICOPTERS LIMITED: Amendment 39-4845. Applies to Westland Model 30 Series 100 helicopters certificated in all categories.

Compliance is required as indicated (unless already accomplished).

To prevent failure of the tail rotor gearbox input pitch control lever and subsequent loss of control in flight accomplish the following:

(a) Prior to further flight comply with the requirements of Westland Service Bulletins W30-67-26, Revision 3, and W30-65-14 or subsequent FAA approved revisions or FAA approved equivalent.

(b) Remove from service all tail rotor gearbox input pitch control levers P/N WK 3068-0037-101 with 200 hours time in service and replace with a serviceable part.

(c) An equivalent method of compliance with this AD may be used when approved by the Manager, Brussels Aircraft Certification Office, c/o United States Embassy, Brussels, Belgium.

This amendment becomes effective April 16, 1984, as to all persons except those persons to whom it was made immediately effective by priority letter AD T84-01-52, issued December 30, 1983, which contained this amendment.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_84-01-52_R.html
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Print/Save as PDF
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 Feedback
Details
AD Number:
84-01-52 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters
Subject:
Pitch Control Lever
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/16/1984
Make:
Westland Helicopters Limited
Model:
Westland 30 Series 100
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: 84-01-52 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4845

AD NUMBER:   84-01-52 R1

SUBJECT HEADING:   Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective April 16, 1984.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
84-01-52 R1 WESTLAND HELICOPTERS LIMITED: Amendment 39-4845. Applies to Westland Model 30 Series 100 helicopters certificated in all categories.

Compliance is required as indicated (unless already accomplished).

To prevent failure of the tail rotor gearbox input pitch control lever and subsequent loss of control in flight accomplish the following:

(a) Prior to further flight comply with the requirements of Westland Service Bulletins W30-67-26, Revision 3, and W30-65-14 or subsequent FAA approved revisions or FAA approved equivalent.

(b) Remove from service all tail rotor gearbox input pitch control levers P/N WK 3068-0037-101 with 200 hours time in service and replace with a serviceable part.

(c) An equivalent method of compliance with this AD may be used when approved by the Manager, Brussels Aircraft Certification Office, c/o United States Embassy, Brussels, Belgium.

This amendment becomes effective April 16, 1984, as to all persons except those persons to whom it was made immediately effective by priority letter AD T84-01-52, issued December 30, 1983, which contained this amendment.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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