AD T84-18-51

final rule

Airworthiness Directives; BELL HELICOPTER TEXTRON, INCORPORATED Model 214ST Helicopters

AD Number
T84-18-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
84-ASW-42
FR Citation
This information is not available.
Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

Applicability

TypeManufacturerModelDetails
aircraft Bell Helicopter Textron, Inc. 214ST Airworthiness Directives; BELL HELICOPTER TEXTRON, INCORPORATED Model 214ST Helicopters

Unsafe Condition

Failure of the main rotor spindles P/N 214-010-103-003 due to cracking or fatigue.

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

Required Actions

Remove from service spindles with 1250 or more hours time in service by October 15, 1984, and thereafter every 1250 hours. Perform daily inspections using Bell Alert Service Bulletin 214ST-84-24 or approved procedure. Replace spindles with 1250+ hours within 150 hours or by October 15, 1984, whichever comes first.

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

Compliance Time

Within the next 150 hours time in service or October 15, 1984, whichever occurs first.

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

Affected Aircraft

Bell Helicopter Textron, Inc. Model 214ST helicopters equipped with main rotor spindles P/N 214-010-103-003.

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

Federal Register Abstract

Main Rotor Spindles

Applicability Source Text

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AD Number:
T84-18-51
Document Type:
AD Final Rules
Docket Number:
84-ASW-42
Subject Heading:
Airworthiness Directives; BELL HELICOPTER TEXTRON, INCORPORATED Model 214ST Helicopters
Subject:
Main Rotor Spindles
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Bell Helicopter Textron, Inc.
Model:
214ST
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Superseded AD: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Superseded By: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: T84-18-51
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   84-ASW-42

AMENDMENT:  

AD NUMBER:   T84-18-51

SUBJECT HEADING:   Airworthiness Directives; BELL HELICOPTER TEXTRON, INCORPORATED Model 214ST Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
T84-18-51 BELL HELICOPTER TEXTRON, INCORPORATED: Telegram issued September 7, 1984. Applies to Bell Helicopter Textron, Incorporated, Model 214ST helicopters certified in all categories that are equipped with main rotor spindles P/N 214-010-103-003 (Airworthiness Docket No. 84-ASW-42).

Compliance is required as indicated.

To prevent possible failure of the main rotor spindles, accomplish the following:

A. Remove from service any spindle with 1250 or more hours time in service on October 15, 1984, and thereafter at intervals not to exceed 1250 hours time in service.

B. After the effective date of this AD, for aircraft with spindles which have, or attain, 1250 or more hours time in service, perform a daily inspection of the main rotor spindle as prescribed in Bell Alert Service Bulletin 214ST-84-24 or other FAA approved equivalent procedure. Remove any cracked spindle from service and replace with a serviceable spindle.

C. After the effective date of this AD, replace all spindles having, or attaining 1250 or more hours time in service, within the next 150 hours time in service or October 15, 1984, whichever occurs first.

D. The helicopter may be flown to a repair base for the above inspection under the provisions of FAR 21.197.

E. Any equivalent means of compliance with this AD must be approved by the Manager, Helicopter Certification Branch, Federal Aviation Administration, Southwest Region.

F. Bell Helicopter Textron, Incorporated, Telegraphic Alert Service Bulletin 214ST- 84-23 is an equivalent means of compliance with this AD.

This airworthiness directive becomes effective upon receipt.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_T84-18-51.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
T84-18-51
Document Type:
AD Final Rules
Docket Number:
84-ASW-42
Subject Heading:
Airworthiness Directives; BELL HELICOPTER TEXTRON, INCORPORATED Model 214ST Helicopters
Subject:
Main Rotor Spindles
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Bell Helicopter Textron, Inc.
Model:
214ST
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: T84-18-51
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   84-ASW-42

AMENDMENT:  

AD NUMBER:   T84-18-51

SUBJECT HEADING:   Airworthiness Directives; BELL HELICOPTER TEXTRON, INCORPORATED Model 214ST Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
T84-18-51 BELL HELICOPTER TEXTRON, INCORPORATED: Telegram issued September 7, 1984. Applies to Bell Helicopter Textron, Incorporated, Model 214ST helicopters certified in all categories that are equipped with main rotor spindles P/N 214-010-103-003 (Airworthiness Docket No. 84-ASW-42).

Compliance is required as indicated.

To prevent possible failure of the main rotor spindles, accomplish the following:

A. Remove from service any spindle with 1250 or more hours time in service on October 15, 1984, and thereafter at intervals not to exceed 1250 hours time in service.

B. After the effective date of this AD, for aircraft with spindles which have, or attain, 1250 or more hours time in service, perform a daily inspection of the main rotor spindle as prescribed in Bell Alert Service Bulletin 214ST-84-24 or other FAA approved equivalent procedure. Remove any cracked spindle from service and replace with a serviceable spindle.

C. After the effective date of this AD, replace all spindles having, or attaining 1250 or more hours time in service, within the next 150 hours time in service or October 15, 1984, whichever occurs first.

D. The helicopter may be flown to a repair base for the above inspection under the provisions of FAR 21.197.

E. Any equivalent means of compliance with this AD must be approved by the Manager, Helicopter Certification Branch, Federal Aviation Administration, Southwest Region.

F. Bell Helicopter Textron, Incorporated, Telegraphic Alert Service Bulletin 214ST- 84-23 is an equivalent means of compliance with this AD.

This airworthiness directive becomes effective upon receipt.

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.