AD 75-07-06

Active

Second Stage Turbine Blades

Key Information
75-07-06
Active
April 07, 1975
Not specified
Unknown
39-2141
Applicability
["Engine"]
Not specified
Rolls-Royce Corporation
501-D22A
Regulatory Text

75-07-06 DETROIT DIESEL ALLISON: Amendment 39-2141. Applies to Detroit Diesel Allison Model 501-D22A engines with turbine assemblies having the following serial numbers:

750137, 750138, 750139, 750140, 750142, 750143, 750145, 750146A, 750147A, 750149, 750150, 750151, 750154, 750158, 750160, 750166, 750176, 750177, 750179, 750181, 750182A, 750184, 750194, 750195, 750201A, 750204, 750205, 750208, 750212, 750213, 750214, 750229, 750230, 750231, 750235, 750241A, 750263A, 750266, 750272, 750301, 750305, 750309, 750312

Within the next 300 hours' time in service after the effective date of this Airworthiness Directive, unless already accomplished, remove the part number 6852228 second stage turbine blades and replace with part number 6890508 second stage turbine blades. Detroit Diesel Allison Commercial Overhaul Information Letter Number COIL-1019 pertains to this subject.

This amendment is effective April 7, 1975.

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