AD 60-24-04

final rule
Data completeness: 70%

Airworthiness Directives; Sikorsky All Model S-58 Helicopters

AD Number
60-24-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sikorsky Aircraft Corporation S-58A Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58B Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58BT Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58C Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58D Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58DT Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58E Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58ET Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58F Airworthiness Directives; Sikorsky All Model S-58 Helicopters
aircraft Sikorsky Aircraft Corporation S-58FT Airworthiness Directives; Sikorsky All Model S-58 Helicopters

Unsafe Condition

Breakage of the cable connected to the L(plus) terminal of Eclipse Pioneer Voltage Regulator P/N 1597-1, resulting in complete loss of electrical power and excessive battery fumes.

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

Required Actions

Remove existing clamp securing voltage regulator cables to the airframe 12 inches from the regulator base; install cable clamp MS 21919DG5 or equivalent to secure cables to regulator base using an existing hole, ensuring cable slack relieves terminal lug tension without altering routing; add additional clamp if unsupported cable length remains beyond the regulator, ensuring regulator shockmount motion is not restricted.

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

Compliance Time

within the next 50 hours' time in service after effective date

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

Affected Aircraft

Sikorsky S-58A, S-58B, S-58BT, S-58C, S-58D, S-58DT, S-58E, S-58ET, S-58F, S-58FT, S-58G, S-58H helicopters

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

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.