AD 75-13-01

final rule

Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters

AD Number
75-13-01
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 Sikorsky Aircraft Corporation S-58A Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58B Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58BT Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58C Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58D Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58DT Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58E Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58ET Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58F Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58FT Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58G Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58H Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58HT Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58J Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters
aircraft Sikorsky Aircraft Corporation S-58JT Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters

Unsafe Condition

Fatigue cracks in the main rotor magnesium stationary stars, part numbers S1610-24013-0, S1610-24013-1, and S1610-24013-2, around the recesses and edges surrounding the recesses inboard of all trunnion lugs.

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

Required Actions

Conduct daily pre-flight visual inspections of the stationary star for cracks in specified areas. For stationary stars with over 250 hours time in service, perform dye penetrant inspections within 5 hours after AD effective date and every 50 hours thereafter. Replace cracked stationary stars with inspected and crack-free units before flight.

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

Compliance Time

Prior to further flight and within 5 hours time in service after the effective date of this AD, and at 50 hour intervals thereafter.

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

Affected Aircraft

Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT helicopters, including military types HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C, and VH-34D helicopters.

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

Federal Register Abstract

Main Rotor Assembly

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-13-01.html
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AD Number:
75-13-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-...Show more
Subject:
Main Rotor Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/20/1977
Make:
Sikorsky Aircraft Corporation
Model:
S-58A | S-58B | S-58BT | S-58C | S-58D | S-58DT | S-58E | S-58ET | S-58F | S-58FT | S-58G | S-58H | ...Show more
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: 75-13-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2879

AD NUMBER:   75-13-01

SUBJECT HEADING:   Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective May 20, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   75-13-01 SIKORSKY AIRCRAFT: Amendment 39-2238 as amended by Amendment 39-2879. Applies to S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S- 58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT helicopters certificated in all categories, including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS- 1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D helicopters. To prevent operation with fatigue cracks in the main rotor magnesium stationary stars, P/Ns S1610-24013-0, S1610-24013- 1, and S1610-24013-2, accomplish the following:

(a) Prior to the first flight of each day, conduct visual inspections of stationary star for cracks in the areas around the recesses and edges surrounding the recesses, inboard of all of the trunnion lugs.

(b) For stationary stars with more than 250 hours time in service: Within 5 hours time in service after the effective date of this AD, unless already accomplished, and at 50 hour intervals thereafter, conduct dye penetrant inspections of the areas described in paragraph (a) for cracks.

(c) If a crack is found during the above inspections, replace the cracked stationary star with a star that has been inspected in accordance with paragraph (b) above and found to be free of cracks, prior to flight.

Sikorsky Alert Service Bulletin 58B10-10 covers this inspection.

Amendment 39-2238 became effective upon publication in the FEDERAL REGISTER for all persons except those to whom it was made effective immediately by telegram dated May 16, 1975.

This amendment 39-2879 becomes effective May 20, 1977.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-13-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-13-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-...Show more
Subject:
Main Rotor Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/20/1977
Make:
Sikorsky Aircraft Corporation
Model:
S-58A | S-58B | S-58BT | S-58C | S-58D | S-58DT | S-58E | S-58ET | S-58F | S-58FT | S-58G | S-58H | ...Show more
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: 75-13-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2879

AD NUMBER:   75-13-01

SUBJECT HEADING:   Airworthiness Directives; Sikorsky Models S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S-58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT Helicopters, Including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS-1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective May 20, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   75-13-01 SIKORSKY AIRCRAFT: Amendment 39-2238 as amended by Amendment 39-2879. Applies to S-58A, S-58B, S-58C, S-58D, S-58E, S-58F, S-58G, S-58H, S-58J, S- 58BT, S-58DT, S-58ET, S-58FT, S-58HT, S-58JT helicopters certificated in all categories, including Military Type HSS-1, HSS-1F, HSS-1N, HUS-1, HUS-1A, HUS-1AN, HUS-1G, HUS- 1Z, H-34A, H-34C, H-34J, CH-34A, CH-34C, HH-34F, SH-34G, SH-34H, SH-34J, UH-34D, UH-34E, UH-34G, UH-34J, VH-34C and VH-34D helicopters. To prevent operation with fatigue cracks in the main rotor magnesium stationary stars, P/Ns S1610-24013-0, S1610-24013- 1, and S1610-24013-2, accomplish the following:

(a) Prior to the first flight of each day, conduct visual inspections of stationary star for cracks in the areas around the recesses and edges surrounding the recesses, inboard of all of the trunnion lugs.

(b) For stationary stars with more than 250 hours time in service: Within 5 hours time in service after the effective date of this AD, unless already accomplished, and at 50 hour intervals thereafter, conduct dye penetrant inspections of the areas described in paragraph (a) for cracks.

(c) If a crack is found during the above inspections, replace the cracked stationary star with a star that has been inspected in accordance with paragraph (b) above and found to be free of cracks, prior to flight.

Sikorsky Alert Service Bulletin 58B10-10 covers this inspection.

Amendment 39-2238 became effective upon publication in the FEDERAL REGISTER for all persons except those to whom it was made effective immediately by telegram dated May 16, 1975.

This amendment 39-2879 becomes effective May 20, 1977.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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