AD 57-08-02

final rule

Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters

AD Number
57-08-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Scotts-Bell 47 Inc 47B3 Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters
aircraft Scotts-Bell 47 Inc 47D Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters
aircraft Scotts-Bell 47 Inc 47D1 Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters
aircraft Scotts-Bell 47 Inc 47G Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters
aircraft Scotts-Bell 47 Inc 47H-1 Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters

Unsafe Condition

Failures of the hinge in the oil system Parker check valve (P/N 1111-517703, 1111-517704, or 1111-517744) have occurred, resulting in restriction of oil flow from the pump.

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

Required Actions

Inspect the Parker check valve at next oil change and every 25 hours thereafter for hinge wear/failure and freedom of operation. Replace the valve if defects are found. The 25-hour inspections may be discontinued after installing the approved James Pond Clark check valve (P/N 879A-10TT).

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

Compliance Time

At next oil change and every 25 hours thereafter until replacement is accomplished.

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

Affected Aircraft

Bell Model 47B3, 47D, 47D1, 47G, and 47H1 helicopters equipped with Parker Check Valves in the oil system.

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

Federal Register Abstract

Parker Check Valve

Applicability Source Text

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AD Final Rules - DRS_57-08-02.html
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AD Number:
57-08-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters
Subject:
Parker Check Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47B3 | 47D | 47D1 | 47G | 47H-1
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: 57-08-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   57-08-02

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
57-08-02 BELL: Applies to All Models 47B3, 47D, 47D1, 47G, and 47H1 Helicopters Equipped With Parker Check Valves in the Oil System.

Compliance required at next oil change and every 25 hours thereafter until replacement is accomplished.

Several failures of the hinge in the oil system Parker check valve, P/N 1111-517703, 1111-517704, or 1111-517744, have occurred resulting in restriction of the flow of oil from the pump. To preclude recurrence of such failures, the following must be accomplished:

1. At the next oil change and every 25 hours thereafter, remove, disassemble, and inspect the oil system Parker check valve, P/N 1111-517703, 1111-517704, or 1111-517744, for wear or failure of the hinge and freedom of operation. If defects are found, replace the valve.

2. James Pond Clark check valve, P/N 879A-10TT, has been approved as a replacement valve. The 25-hour inspection outlined above may be discontinued when the valve is installed.

(Bell Service Bulletin No. 119 dated March 15, 1957, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_57-08-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
57-08-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters
Subject:
Parker Check Valve
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47B3 | 47D | 47D1 | 47G | 47H-1
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: 57-08-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   57-08-02

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47B3, 47D, 47D1, 47G, and 47H1 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
57-08-02 BELL: Applies to All Models 47B3, 47D, 47D1, 47G, and 47H1 Helicopters Equipped With Parker Check Valves in the Oil System.

Compliance required at next oil change and every 25 hours thereafter until replacement is accomplished.

Several failures of the hinge in the oil system Parker check valve, P/N 1111-517703, 1111-517704, or 1111-517744, have occurred resulting in restriction of the flow of oil from the pump. To preclude recurrence of such failures, the following must be accomplished:

1. At the next oil change and every 25 hours thereafter, remove, disassemble, and inspect the oil system Parker check valve, P/N 1111-517703, 1111-517704, or 1111-517744, for wear or failure of the hinge and freedom of operation. If defects are found, replace the valve.

2. James Pond Clark check valve, P/N 879A-10TT, has been approved as a replacement valve. The 25-hour inspection outlined above may be discontinued when the valve is installed.

(Bell Service Bulletin No. 119 dated March 15, 1957, covers this same subject.)

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.