AD 60-13-04

final rule

Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters

AD Number
60-13-04
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 Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation HRS-1/CH-19 Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters
aircraft Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation HRS-3/H-19B Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters
aircraft Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation S-51 Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters
aircraft Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation S-55 Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters
aircraft Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation S-55B Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters
aircraft Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation S-55C Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters

Unsafe Condition

Fatigue failure of the RE5M7 shank rod end bearing with a hollow shank, which is not an approved part, occurred in the S-55 main rotor upper controls due to improper identification and installation.

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

Required Actions

Remove and inspect rod assemblies for RE5M7 rod end bearings with hollow shanks and S510085 pivots with hollow shanks. Replace hollow shank units with solid shank units.

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

Compliance Time

August 15, 1960

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

Affected Aircraft

Sikorsky Models S-51 and S-55 Helicopters, including variants HRS-1/CH-19, HRS-3/H-19B, S-51, S-55, S-55B, S-55C

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

Federal Register Abstract

Rotor Shank Rod

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_60-13-04.html
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AD Number:
60-13-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters
Subject:
Rotor Shank Rod
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation
Model:
HRS-1/CH-19 | HRS-3/H-19B | S-51 | S-55 | S-55B | S-55C
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: 60-13-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   60-13-04

SUBJECT HEADING:   Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
60-13-04 SIKORSKY: Amdt. 171 Part 507 Federal Register June 24, 1960. Applies to All Models S-51 and S-55 Helicopters.

Compliance required by August 15, 1960.

A fatigue failure of the RE5M7 shank rod end bearing has occurred in the S-55 main rotor upper controls. This rod had a hollow shank rather than a solid shank and is not an approved part. Preliminary investigation indicates that the hollow shank part has been installed in S-51 and S-55 helicopters because of improper identification. To ensure removal of this part from service, the following must be accomplished:

Unless already accomplished, remove the following rod assemblies and inspect for RE5M7 rod end bearings with hollow shanks and S510085 pivots with hollow shanks, as noted (S510085 pivots are altered RE5M7 rod ends.)

(a) Model S-51 main rotor assembly, P/N S510000.

(1) P/N S510333 (Alternate P/N S510140) rod assembly contains one RE5M7 rod end.

(2) P/N S510082 rod assembly contains one RE5M7 rod end and one P/N S510085 pivot.

(b) Model S-51 main rotor assembly, P/N S10-10-1100.

(1) P/N S510333 rod assembly contains one RE5M7 rod end.

(c) Model S-55 servo unit assembly, P/N S14-40-5000.

(1) P/N S14-40-5024 control arm contains one RE5M7 rod end.

Remove all hollow shank units and replace with solid shank units.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_60-13-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
60-13-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters
Subject:
Rotor Shank Rod
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Orlando Helicopter Airways, Inc. | Sikorsky Aircraft Corporation
Model:
HRS-1/CH-19 | HRS-3/H-19B | S-51 | S-55 | S-55B | S-55C
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: 60-13-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   60-13-04

SUBJECT HEADING:   Airworthiness Directives; Sikorsky Models S-51 and S-55 Helicopters

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
60-13-04 SIKORSKY: Amdt. 171 Part 507 Federal Register June 24, 1960. Applies to All Models S-51 and S-55 Helicopters.

Compliance required by August 15, 1960.

A fatigue failure of the RE5M7 shank rod end bearing has occurred in the S-55 main rotor upper controls. This rod had a hollow shank rather than a solid shank and is not an approved part. Preliminary investigation indicates that the hollow shank part has been installed in S-51 and S-55 helicopters because of improper identification. To ensure removal of this part from service, the following must be accomplished:

Unless already accomplished, remove the following rod assemblies and inspect for RE5M7 rod end bearings with hollow shanks and S510085 pivots with hollow shanks, as noted (S510085 pivots are altered RE5M7 rod ends.)

(a) Model S-51 main rotor assembly, P/N S510000.

(1) P/N S510333 (Alternate P/N S510140) rod assembly contains one RE5M7 rod end.

(2) P/N S510082 rod assembly contains one RE5M7 rod end and one P/N S510085 pivot.

(b) Model S-51 main rotor assembly, P/N S10-10-1100.

(1) P/N S510333 rod assembly contains one RE5M7 rod end.

(c) Model S-55 servo unit assembly, P/N S14-40-5000.

(1) P/N S14-40-5024 control arm contains one RE5M7 rod end.

Remove all hollow shank units and replace with solid shank units.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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