AD 74-23-08

final rule

Airworthiness Directives; GRUMMAN AMERICAN CORPORATION G-159 Airplanes

AD Number
74-23-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Gulfstream Aerospace Corporation G-159 Airworthiness Directives; GRUMMAN AMERICAN CORPORATION G-159 Airplanes

Unsafe Condition

Failure of the fire extinguisher squib circuits due to single point failure of electrical power, which could result in inability to discharge fire extinguishers during an engine fire emergency.

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

Required Actions

Remove existing left and right engine fire extinguisher switches and left hand eyebrow circuit breaker panel nameplate. Install MS24524-21 switches, electrical wiring, 159SB10112-1 nameplate, and check out system in accordance with Grumman Gulfstream I Aircraft Service Change 210.

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

Compliance Time

within the next 200 hours time in service after the effective date of this airworthiness directive unless already accomplished

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

Affected Aircraft

Grumman American Corporation G-159 airplanes certificated in all categories.

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

Federal Register Abstract

Fire Extinguishers

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_74-23-08.html
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Details
AD Number:
74-23-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GRUMMAN AMERICAN CORPORATION G-159 Airplanes
Subject:
Fire Extinguishers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/15/1974
Make:
Gulfstream Aerospace Corporation
Model:
G-159
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Superseded AD: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Superseded By: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: 74-23-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2007

AD NUMBER:   74-23-08

SUBJECT HEADING:   Airworthiness Directives; GRUMMAN AMERICAN CORPORATION G-159 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 15, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   74-23-08 GRUMMAN AMERICAN CORPORATION: Amendment 39-2007. Applies to Grumman G-159 airplanes certificated in all categories.

Compliance required within the next 200 hours time in service after the effective date of this airworthiness directive unless already accomplished.

To provide dual electrical power for the fire extinguisher squib circuits accomplish the following or an equivalent rework approved by the Chief, Engineering and Manufacturing Branch, Southern Region.

Remove the existing left and right engine fire extinguisher switches and left hand eyebrow circuit breaker panel nameplate. Install MS24524-21 switches, electrical wiring, 159SB10112-1 nameplate and check out system in accordance with Grumman Gulfstream I Aircraft Service Change 210.

This amendment becomes effective November 15, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-23-08.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-23-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GRUMMAN AMERICAN CORPORATION G-159 Airplanes
Subject:
Fire Extinguishers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/15/1974
Make:
Gulfstream Aerospace Corporation
Model:
G-159
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: 74-23-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2007

AD NUMBER:   74-23-08

SUBJECT HEADING:   Airworthiness Directives; GRUMMAN AMERICAN CORPORATION G-159 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 15, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   74-23-08 GRUMMAN AMERICAN CORPORATION: Amendment 39-2007. Applies to Grumman G-159 airplanes certificated in all categories.

Compliance required within the next 200 hours time in service after the effective date of this airworthiness directive unless already accomplished.

To provide dual electrical power for the fire extinguisher squib circuits accomplish the following or an equivalent rework approved by the Chief, Engineering and Manufacturing Branch, Southern Region.

Remove the existing left and right engine fire extinguisher switches and left hand eyebrow circuit breaker panel nameplate. Install MS24524-21 switches, electrical wiring, 159SB10112-1 nameplate and check out system in accordance with Grumman Gulfstream I Aircraft Service Change 210.

This amendment becomes effective November 15, 1974.

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.