AD 75-06-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gulfstream Aerospace Corporation | G-1159 | Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes |
Unsafe Condition
Possible loss of all DC and AC power due to battery switch ground leads not connected to separate studs at the center overhead panel.
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Required Actions
Connect the battery switch ground leads to separate studs at the center overhead panel in accordance with Grumman ASC 188 or an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, Southern Region, Atlanta, Georgia.
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Compliance Time
within the next 150 hours' time in service after the effective date of this AD
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Affected Aircraft
GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 airplanes certificated in all categories.
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Federal Register Abstract
Battery Switch Ground Leads
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_75-06-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-06-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes Subject: Battery Switch Ground Leads Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/18/1975 Make: Gulfstream Aerospace Corporation Model: G-1159 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-06-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2124 AD NUMBER: 75-06-08 SUBJECT HEADING: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes ACTION: SUMMARY: DATES: Effective March 18, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-06-08 GRUMMAN AMERICAN AVIATION CORPORATION: Amendment 39- 2124. Applies to G-1159 airplanes certificated in all categories. Compliance required within the next 150 hours' time in service after the effective date of this AD, unless already accomplished. To prevent possible loss of all DC and AC power, connect the battery switch ground leads to separate studs at the center overhead panel in accordance with Grumman ASC 188 or in an equivalent manner approved by Chief, Engineering and Manufacturing Branch, Southern Region, Atlanta, Georgia. This amendment becomes effective March 18, 1975. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_75-06-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-06-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes Subject: Battery Switch Ground Leads Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/18/1975 Make: Gulfstream Aerospace Corporation Model: G-1159 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-06-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2124 AD NUMBER: 75-06-08 SUBJECT HEADING: Airworthiness Directives; GRUMMAN AMERICAN AVIATION CORPORATION Model G-1159 Airplanes ACTION: SUMMARY: DATES: Effective March 18, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-06-08 GRUMMAN AMERICAN AVIATION CORPORATION: Amendment 39- 2124. Applies to G-1159 airplanes certificated in all categories. Compliance required within the next 150 hours' time in service after the effective date of this AD, unless already accomplished. To prevent possible loss of all DC and AC power, connect the battery switch ground leads to separate studs at the center overhead panel in accordance with Grumman ASC 188 or in an equivalent manner approved by Chief, Engineering and Manufacturing Branch, Southern Region, Atlanta, Georgia. This amendment becomes effective March 18, 1975. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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