AD 79-25-03

Active

Second, Third, And Fourth Stage Turbine Wheels

Key Information
79-25-03
Active
December 13, 1979
Not specified
Unknown
39-3625
Applicability
["Engine"]
Not specified
Rolls-Royce Corporation
501-D13 501-D13A 501-D13D 501-D13E 501-D13H
Regulatory Text

79-25-03 DETROIT DIESEL ALLISON: Amendment 39-3625. Applies to Model 501-D13, 501-D13A, 501-D13D, 501-D13E, and 501-D13H engines equipped with second, third, and fourth stage turbine wheels P/N's 6829072, 6847112, 6788833, 6842143, 6841223, 6846553, 6738424, and 6843014.

Compliance required as follows unless previously accomplished:

(a) For second stage turbine wheels, remove from service in accordance with FAA approved revision of 501-D13 CSL-235 dated December 13, 1979.

(b) For third and fourth stage turbine wheels, remove from service in accordance with FAA approved revision of 501-D13 CSL-253 dated December 13, 1979.

Detroit Diesel Allison Commercial Service Letters 501-D13 CSL-235, 501-D13 CSL-253, and Commercial Overhaul Information Letter 501-D13 COIL-349 revised as of December 13, 1979 are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). The incorporated service documents may be obtained from Detroit Diesel Allison, Division ofGeneral Motors Corporation, Indianapolis, Indiana 46206.

This amendment becomes effective on December 13, 1979.

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References
This information is not available.
--- - Part 39
FAA Documents