AD 66-22-04

final rule

Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters

AD Number
66-22-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12D Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12L Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12L4 Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E-L Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters

Unsafe Condition

Failures of the mercury clutch due to cracking at the inner corners of driver lug slots in the side plates.

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

Required Actions

Visually inspect the side plates for cracks using at least 8-power magnification. If cracks are found, replace clutch before further flight with a clutch of the same part number that has been inspected and found free of cracks.

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

Compliance Time

within the next 100 hours' time in service after the effective date of this AD

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

Affected Aircraft

Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters equipped with Mercury Clutch Corporation P/N's 4578-6 and 4692-6, Clutch Serial Numbers 8584 through 9317.

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

Federal Register Abstract

Mercury Clutches

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
66-22-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters
Subject:
Mercury Clutches
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/02/1966
Make:
Hiller Aviation | Siam Hiller Holdings, Inc.
Model:
UH-12D | UH-12L | UH-12L4 | UH-12E | UH-12E-L
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: 66-22-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-280

AD NUMBER:   66-22-04

SUBJECT HEADING:   Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective September 2, 1966.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
66-22-04 HILLER: Amdt. 39-280 Part 39 Federal Register September 2, 1966. Applies to Model UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters Equipped With Clutches, Mercury Clutch Corporation P/N's 4578-6 and 4692-6, Clutch Serial Numbers 8584 through 9317.

Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent failures of the mercury clutch due to cracking at the inner corners of driver lug slots in the side plates, accomplish the following:

(a) Visually inspect the side plates for cracks using at least 8-power magnification.

(b) If cracks are found, replace clutch before further flight with a clutch of the same part number that has been inspected in accordance with this AD and found free of cracks.

(Fairchild Hiller Service Information Letters Nos. 3052 and 5009, dated July 20, 1966, pertain to this subject).

This directive effective September 2, 1966.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_66-22-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
66-22-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters
Subject:
Mercury Clutches
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/02/1966
Make:
Hiller Aviation | Siam Hiller Holdings, Inc.
Model:
UH-12D | UH-12L | UH-12L4 | UH-12E | UH-12E-L
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: 66-22-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-280

AD NUMBER:   66-22-04

SUBJECT HEADING:   Airworthiness Directives; Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective September 2, 1966.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
66-22-04 HILLER: Amdt. 39-280 Part 39 Federal Register September 2, 1966. Applies to Model UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters Equipped With Clutches, Mercury Clutch Corporation P/N's 4578-6 and 4692-6, Clutch Serial Numbers 8584 through 9317.

Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent failures of the mercury clutch due to cracking at the inner corners of driver lug slots in the side plates, accomplish the following:

(a) Visually inspect the side plates for cracks using at least 8-power magnification.

(b) If cracks are found, replace clutch before further flight with a clutch of the same part number that has been inspected in accordance with this AD and found free of cracks.

(Fairchild Hiller Service Information Letters Nos. 3052 and 5009, dated July 20, 1966, pertain to this subject).

This directive effective September 2, 1966.

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.

View Official Source ↗