AD 71-25-08

final rule

Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters

AD Number
71-25-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

Applicability

TypeManufacturerModelDetails
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12 Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12A Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12B Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12C Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12D Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12L Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12L4 Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E-L Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters

Unsafe Condition

Cracks in main rotor blade part number 53100 could result in blade failure.

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

Required Actions

Inspect main rotor blade P/N 53100 for cracks using dye penetrant within 10 hours time in service after the effective date. Remove defective blades from service prior to further flight and report serial numbers to the specified FAA office.

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

Compliance Time

within 10 hours time in service after the effective date

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

Affected Aircraft

Fairchild Hiller Model UH-12 helicopters certificated in all categories, including models UH-12, UH-12A, UH-12B, UH-12C, UH-12D, UH-12L, UH-12L4, UH-12E, and UH-12E-L.

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

Federal Register Abstract

Inspect Main Rotor Blades

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_71-25-08.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
71-25-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
Subject:
Inspect Main Rotor Blades
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/14/1971
Make:
Hiller Aviation | Siam Hiller Holdings, Inc.
Model:
UH-12 | UH-12A | UH-12B | UH-12C | 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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 71-25-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1356

AD NUMBER:   71-25-08

SUBJECT HEADING:   Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective December 14, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-25-08 FAIRCHILD HILLER ROTORCRAFT: Amdt. 39-1356. Applies to Fairchild Hiller UH-12 helicopters certificated in all categories.

Compliance required as indicated.

Following an immediate visual inspection and within 10 hours time in service after the effective date of this airworthiness directive inspect main rotor blade P/N 53100 for cracks, using dye penetrant. Any blades found defective are to be removed from service prior to further flight and S/Ns reported to Engineering and Manufacturing Branch, Federal Aviation Administration, Eastern Region, JFK International Airport, Jamaica, New York 11430. Approval of this reporting procedure has been obtained from the Bureau of Budget in accordance with Federal Reports Act. Reporting approved by Bureau of Budget under BOB Number 04-R0174.

This amendment is effective December 14, 1971 and was effective upon receipt by owners and operators of the letter dated November 9, 1971 which contained this amendment.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_71-25-08.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
71-25-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters
Subject:
Inspect Main Rotor Blades
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/14/1971
Make:
Hiller Aviation | Siam Hiller Holdings, Inc.
Model:
UH-12 | UH-12A | UH-12B | UH-12C | 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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 71-25-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1356

AD NUMBER:   71-25-08

SUBJECT HEADING:   Airworthiness Directives; Fairchild Hiller Model UH-12 Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective December 14, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-25-08 FAIRCHILD HILLER ROTORCRAFT: Amdt. 39-1356. Applies to Fairchild Hiller UH-12 helicopters certificated in all categories.

Compliance required as indicated.

Following an immediate visual inspection and within 10 hours time in service after the effective date of this airworthiness directive inspect main rotor blade P/N 53100 for cracks, using dye penetrant. Any blades found defective are to be removed from service prior to further flight and S/Ns reported to Engineering and Manufacturing Branch, Federal Aviation Administration, Eastern Region, JFK International Airport, Jamaica, New York 11430. Approval of this reporting procedure has been obtained from the Bureau of Budget in accordance with Federal Reports Act. Reporting approved by Bureau of Budget under BOB Number 04-R0174.

This amendment is effective December 14, 1971 and was effective upon receipt by owners and operators of the letter dated November 9, 1971 which contained this amendment.

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 ↗