AD 52-01-07

final rule

Airworthiness Directives; Bell Model 47D1 Helicopters

AD Number
52-01-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Scotts-Bell 47 Inc 47D1 Airworthiness Directives; Bell Model 47D1 Helicopters

Unsafe Condition

The possibility of throwing blades in flight due to the existing 47-661-030-1 hub assembly in the cooling fan.

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

Required Actions

Rework the existing 47-661-030-1 hub, reassemble the fan using parts from the modification kit, and balance the modified fan assembly (P/N 47-661-036-5) according to specified procedures before installation.

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

Compliance Time

At the next 300-hour overhaul, but not later than March 1, 1952.

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

Affected Aircraft

All Model 47D1 Helicopters having 47-661-030-1 Hub Assembly in the Cooling Fan.

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

Federal Register Abstract

Engine Cooling Fan

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
52-01-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47D1 Helicopters
Subject:
Engine Cooling Fan
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47D1
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Superseded AD: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Superseded By: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: 52-01-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   52-01-07

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47D1 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
52-01-07 BELL: Applies to All Model 47D1 Helicopters Having 47-661-030-1 Hub Assembly in the Cooling Fan. Refer to Bell Service Bulletin No. 72.

Compliance required at the next 300-hour overhaul, but not later than March 1, 1952.

To reduce the possibility of throwing blades in flight, rework the existing 47-661-030-1 hub and reassemble the fan using the parts provided in the modification kit. (Note: Do not install old fan blades.) Balance modified fan assembly (assigned P/N 47-661-036-5) in accordance with specified erection and maintenance procedure prior to installation.

(Bell Service Bulletin No. 82 covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_52-01-07.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
52-01-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bell Model 47D1 Helicopters
Subject:
Engine Cooling Fan
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Scotts-Bell 47 Inc
Model:
47D1
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: 52-01-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   52-01-07

SUBJECT HEADING:   Airworthiness Directives; Bell Model 47D1 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
52-01-07 BELL: Applies to All Model 47D1 Helicopters Having 47-661-030-1 Hub Assembly in the Cooling Fan. Refer to Bell Service Bulletin No. 72.

Compliance required at the next 300-hour overhaul, but not later than March 1, 1952.

To reduce the possibility of throwing blades in flight, rework the existing 47-661-030-1 hub and reassemble the fan using the parts provided in the modification kit. (Note: Do not install old fan blades.) Balance modified fan assembly (assigned P/N 47-661-036-5) in accordance with specified erection and maintenance procedure prior to installation.

(Bell Service Bulletin No. 82 covers this same subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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