AD 52-01-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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
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Effective Date: Make: Scotts-Bell 47 Inc Model: 47D1 Product Type: Aircraft Product Subtype: Rotorcraft Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 52-01-07 CITATION: This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:
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.