AD 69-18-02

final rule

ALLISON Models 250-C10 and 250-C18 Series Engines

AD Number
69-18-02
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Corporation 250-C10 (T63-A-5) ALLISON Models 250-C10 and 250-C18 Series Engines
engine Rolls-Royce Corporation 250-C10B (T63-A-5A) ALLISON Models 250-C10 and 250-C18 Series Engines
engine Rolls-Royce Corporation 250-C10D (T63-A-700) ALLISON Models 250-C10 and 250-C18 Series Engines
engine Rolls-Royce Corporation 250-C18 ALLISON Models 250-C10 and 250-C18 Series Engines
engine Rolls-Royce Corporation 250-C18A ALLISON Models 250-C10 and 250-C18 Series Engines
engine Rolls-Royce Corporation 250-C18B ALLISON Models 250-C10 and 250-C18 Series Engines
engine Rolls-Royce Corporation 250-C18C ALLISON Models 250-C10 and 250-C18 Series Engines

Unsafe Condition

Excessive wear of the internal splines on the P/N 6840847 helical power train drive gear.

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

Required Actions

Inspect the internal spline using Allison P/N EX 83339 plug gage. Replace the gear with a new or serviceable part if the gage enters the spline. Modify the engine per Allison CEB-61 to eliminate future inspections.

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 the effective date, for engines with 750+ hours since new/overhaul, or at or before 800 hours' time in service for those with less than 750 hours at effective date.

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

Affected Aircraft

Rolls-Royce Corporation Models 250-C10 (T63-A-5, T63-A-5A, T63-A-700) and 250-C18 (C18, C18A, C18B, C18C) series engines.

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

Federal Register Abstract

Internal Splines

Applicability Source Text

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AD Number:
69-18-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
ALLISON Models 250-C10 and 250-C18 Series Engines
Subject:
Internal Splines
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/03/1969
Make:
Rolls-Royce Corporation
Model:
250-C10 (T63-A-5) | 250-C10B (T63-A-5A) | 250-C10D (T63-A-700) | 250-C18 | 250-C18A | 250-C18B | 250-C18C
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: 69-18-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-831

AD NUMBER:   69-18-02

SUBJECT HEADING:  
ALLISON Models 250-C10 and 250-C18 Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective September 3, 1969.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  

69-18-02 ALLISON: Amdt. 39-831. Applies to Models 250-C10 and 250-C18 Series Engines.


Compliance: Unless already accomplished, within the next 50 hours' time in service after the effective date of this AD, on all engines having 750 or more hours' time in service since new or last overhaul, or at or before 800 hours' time in service on engines that have less than 750 hours' time in service since new or last overhaul at the effective date of this AD, accomplish the following:


To detect excessive wear of the internal splines:


A) Inspect the internal spline on the P/N 6840847 helical power train drive gear using an Allison P/N EX 83339 plug gage. If this gage enters the spline, replace the gear with a new or serviceable part prior to returning the engine to service. Allison Commercial Service Letter No. 250 CSL-35, dated August 15, 1969, pertains to this inspection.


B) When the engine is modified in accordance with Allison Commercial Engine Bulletin No. 250 CEB- 61, dated July 25, 1969, the inspections required by Paragraph A of this AD will no longer be required. Gear boxes having Serial Numbers ending in the suffix "B" incorporate Commercial Engine Bulletin No. 250 CEB-61.


This amendment becomes effective September 3, 1969.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_69-18-02.html
Copy URL
Print/Save as PDF
Document Versions
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Details
AD Number:
69-18-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
ALLISON Models 250-C10 and 250-C18 Series Engines
Subject:
Internal Splines
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/03/1969
Make:
Rolls-Royce Corporation
Model:
250-C10 (T63-A-5) | 250-C10B (T63-A-5A) | 250-C10D (T63-A-700) | 250-C18 | 250-C18A | 250-C18B | 250-C18C
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: 69-18-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-831

AD NUMBER:   69-18-02

SUBJECT HEADING:  
ALLISON Models 250-C10 and 250-C18 Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective September 3, 1969.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  

69-18-02 ALLISON: Amdt. 39-831. Applies to Models 250-C10 and 250-C18 Series Engines.


Compliance: Unless already accomplished, within the next 50 hours' time in service after the effective date of this AD, on all engines having 750 or more hours' time in service since new or last overhaul, or at or before 800 hours' time in service on engines that have less than 750 hours' time in service since new or last overhaul at the effective date of this AD, accomplish the following:


To detect excessive wear of the internal splines:


A) Inspect the internal spline on the P/N 6840847 helical power train drive gear using an Allison P/N EX 83339 plug gage. If this gage enters the spline, replace the gear with a new or serviceable part prior to returning the engine to service. Allison Commercial Service Letter No. 250 CSL-35, dated August 15, 1969, pertains to this inspection.


B) When the engine is modified in accordance with Allison Commercial Engine Bulletin No. 250 CEB- 61, dated July 25, 1969, the inspections required by Paragraph A of this AD will no longer be required. Gear boxes having Serial Numbers ending in the suffix "B" incorporate Commercial Engine Bulletin No. 250 CEB-61.


This amendment becomes effective September 3, 1969.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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