AD 60-13-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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 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:
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.