AD 78-26-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric Company | CT58-100-2 | GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. |
| engine | General Electric Company | CT58-110-1 | GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. |
| engine | General Electric Company | CT58-110-2 | GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. |
| engine | General Electric Company | CT58-140-1 | GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. |
| engine | General Electric Company | CT58-140-2 | GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. |
Unsafe Condition
Failure of the lube pump drive shaft and resultant loss of oil pressure.
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Required Actions
Perform actions per General Electric Alert Service Bulletin CEB-253 (CT58 A72-157). Remove and replace pumps based on time in service: those with ≤50 hours within 4 hours, and 50-500 hours within 50 hours after AD effective date. Inspect removed and spare pumps, replace Viton seals with Sirvene seals, and check for damage.
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Compliance Time
Within the specified hours operating time after the effective date of this AD (December 19, 1978).
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Affected Aircraft
General Electric Company models CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 series A&L, CT58-140-1, and CT58-140-2 engines. Includes pumps with specific part numbers and serial ranges, and engines with serial numbers 295218 through 295233, 295235 through 295241, 295243 through 295249, and 295255.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Lube Pump Drive Shaft
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_78-26-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 78-26-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. Subject: Lube Pump Drive Shaft Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/19/1978 Make: General Electric Company Model: CT58-100-2 | CT58-110-1 | CT58-110-2 | CT58-140-1 | CT58-140-2 Product Type: Engine Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 78-26-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3376 AD NUMBER: 78-26-08 SUBJECT HEADING: GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. ACTION: SUMMARY: DATES: Effective December 19, 1978. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 78-26-08 GENERAL ELECTRIC COMPANY: Amendment 39-3376. Applies to all model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 series A&L, CT58-140-1 and CT58-140-2 turboshaft engines. Compliance required as indicated, unless already accomplished. To prevent failure of the lube pump drive shaft and resultant loss of oil pressure, perform the following in accordance with General Electric Alert Service Bulletin CEB-253 ((CT58) A72-157) dated October 6, 1978, or later FAA approved revision. 1. Engines with new lube and scavenge pumps P/N 4000T98P02, Serial Number NMA-05635, 5724, 5729, 5736, and 5938 through 06151, or with any lube and scavenge pump P/Ns 37D400035P101, 4000T98P01, or 4000T98P02 overhauled after March 1976. (A) Remove from service pumps with 50 hours or less time in service since new or since overhaul within 4 hours operating time after the effective date of this AD. Replace with serviceable pump. (B) Remove from service pumps with over 50 but less than 500 hours time in service since new or since overhaul within 50 hours operating time after the effective date of this AD. Replace with serviceable pump. 2. Inspect removed pumps, spare pumps overhauled after March 1976 and new spare pumps in the above serial number range, prior to installation on an engine, in accordance with Section 2B of the bulletin. Remove lip seals marked Viton and replace with new unmarked Sirvene seals and inspect adjacent parts for damage in accordance with the instructions in Section 2B(7) of the bulletin. NOTE: New pumps in the affected serial number range were shipped on new production CT58-140-1 engines, S/Ns 295218 through 295233, 295235 through 295241, 295243 through 295249, and 295255. The manufacturer's service bulletin identified and described in this directive is incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received this document from the manufacturer may obtain copies upon request to Customer Service and Support Manager, General Electric Company, 1000 Western Avenue, Lynn, Massachusetts 01910. This document may also be examined at Federal Aviation Administration, New England Region, 12 New England Executive Park, Burlington, Massachusetts 01803, and FAA Headquarters, 800 Independence Avenue, S.W., Washington, D.C. This amendment becomes effective December 19, 1978. FOOTER:
Document Text
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AD Final Rules - DRS_78-26-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 78-26-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. Subject: Lube Pump Drive Shaft Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/19/1978 Make: General Electric Company Model: CT58-100-2 | CT58-110-1 | CT58-110-2 | CT58-140-1 | CT58-140-2 Product Type: Engine Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 78-26-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3376 AD NUMBER: 78-26-08 SUBJECT HEADING: GENERAL ELECTRIC COMPANY Model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 and CT58-140-2 engines. ACTION: SUMMARY: DATES: Effective December 19, 1978. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 78-26-08 GENERAL ELECTRIC COMPANY: Amendment 39-3376. Applies to all model CT58-100-2, CT58-110-1, CT58-110-2, CT58-140-1 series A&L, CT58-140-1 and CT58-140-2 turboshaft engines. Compliance required as indicated, unless already accomplished. To prevent failure of the lube pump drive shaft and resultant loss of oil pressure, perform the following in accordance with General Electric Alert Service Bulletin CEB-253 ((CT58) A72-157) dated October 6, 1978, or later FAA approved revision. 1. Engines with new lube and scavenge pumps P/N 4000T98P02, Serial Number NMA-05635, 5724, 5729, 5736, and 5938 through 06151, or with any lube and scavenge pump P/Ns 37D400035P101, 4000T98P01, or 4000T98P02 overhauled after March 1976. (A) Remove from service pumps with 50 hours or less time in service since new or since overhaul within 4 hours operating time after the effective date of this AD. Replace with serviceable pump. (B) Remove from service pumps with over 50 but less than 500 hours time in service since new or since overhaul within 50 hours operating time after the effective date of this AD. Replace with serviceable pump. 2. Inspect removed pumps, spare pumps overhauled after March 1976 and new spare pumps in the above serial number range, prior to installation on an engine, in accordance with Section 2B of the bulletin. Remove lip seals marked Viton and replace with new unmarked Sirvene seals and inspect adjacent parts for damage in accordance with the instructions in Section 2B(7) of the bulletin. NOTE: New pumps in the affected serial number range were shipped on new production CT58-140-1 engines, S/Ns 295218 through 295233, 295235 through 295241, 295243 through 295249, and 295255. The manufacturer's service bulletin identified and described in this directive is incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received this document from the manufacturer may obtain copies upon request to Customer Service and Support Manager, General Electric Company, 1000 Western Avenue, Lynn, Massachusetts 01910. This document may also be examined at Federal Aviation Administration, New England Region, 12 New England Executive Park, Burlington, Massachusetts 01803, and FAA Headquarters, 800 Independence Avenue, S.W., Washington, D.C. This amendment becomes effective December 19, 1978. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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