AD 74-24-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed Martin Corporation | 382 | LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes |
| aircraft | Lockheed Martin Corporation | 382B | LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes |
| aircraft | Lockheed Martin Corporation | 382E | LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes |
| aircraft | Lockheed Martin Corporation | 382F | LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes |
| aircraft | Lockheed Martin Corporation | 382G | LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes |
Unsafe Condition
The engine throttle cables may become frayed or broken at the F.S. 245 upper and lower pulleys and at all engine horsecollar pulleys on the front wing beam, which could result in loss of engine control.
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Required Actions
Inspect and replace as required the engine throttle cables at specified locations per Lockheed Service Bulletin A382-175 or an equivalent approved procedure.
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Compliance Time
For aircraft with 2000 hours or more time in service: accomplished at the first convenient maintenance period, but not to exceed 200 hours time in service after the effective date. For aircraft with less than 2000 hours time in service: prior to the accumulation of 2000 hours or 200 hours time in service after the effective date, whichever is greater.
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Affected Aircraft
Lockheed-Georgia Company Models 382, 382B, 382E, 382F, and 382G airplanes with serial numbers below 4559.
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Federal Register Abstract
Engine Throttle Cables
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_74-24-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 74-24-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes Subject: Engine Throttle Cables Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/27/1974 Make: Lockheed Martin Corporation Model: 382 | 382B | 382E | 382F | 382G Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 74-24-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2020 AD NUMBER: 74-24-08 SUBJECT HEADING: LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes ACTION: SUMMARY: DATES: Effective November 27, 1974. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 74-24-08 LOCKHEED-GEORGIA COMPANY: Amendment 39-2020. Applies to all Lockheed Models 382, 382B, 382E, 382F, and 382G airplanes certificated in all categories. Compliance required as indicated below for aircraft with serial numbers below 4559 unless already accomplished. A. For aircraft with 2000 hours or more time in service: This inspection is to be accomplished at the first convenient maintenance period, but not to exceed 200 hours time in service after the effective date of this airworthiness directive. B. On aircraft with less than 2000 hours time in service, this inspection is to be accomplished prior to the accumulation of 2000 hours or 200 hours time in service after the effective date of this airworthiness directive, whichever is greater. Accomplish the following: Inspect and replace as required the engine throttle cables located at F.S. 245 upper and lower pulleys and at all engine horsecollar pulleys on the front wing beam as defined and in accordance with Lockheed Service Bulletin A382-175 or later approved revision or an equivalent inspection procedure approved by the Chief, Engineering and Manufacturing Branch, Southern Region. This amendment is effective November 27, 1974. FOOTER:
Document Text
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AD Final Rules - DRS_74-24-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 74-24-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes Subject: Engine Throttle Cables Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/27/1974 Make: Lockheed Martin Corporation Model: 382 | 382B | 382E | 382F | 382G 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: 74-24-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2020 AD NUMBER: 74-24-08 SUBJECT HEADING: LOCKHEED-GEORGIA COMPANY Models 382, 382B, 382E, 382F, and 382G Airplanes ACTION: SUMMARY: DATES: Effective November 27, 1974. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 74-24-08 LOCKHEED-GEORGIA COMPANY: Amendment 39-2020. Applies to all Lockheed Models 382, 382B, 382E, 382F, and 382G airplanes certificated in all categories. Compliance required as indicated below for aircraft with serial numbers below 4559 unless already accomplished. A. For aircraft with 2000 hours or more time in service: This inspection is to be accomplished at the first convenient maintenance period, but not to exceed 200 hours time in service after the effective date of this airworthiness directive. B. On aircraft with less than 2000 hours time in service, this inspection is to be accomplished prior to the accumulation of 2000 hours or 200 hours time in service after the effective date of this airworthiness directive, whichever is greater. Accomplish the following: Inspect and replace as required the engine throttle cables located at F.S. 245 upper and lower pulleys and at all engine horsecollar pulleys on the front wing beam as defined and in accordance with Lockheed Service Bulletin A382-175 or later approved revision or an equivalent inspection procedure approved by the Chief, Engineering and Manufacturing Branch, Southern Region. This amendment is effective November 27, 1974. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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