AD 49-40-02

Active

Thrust Plate

Key Information
49-40-02
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Engine"]
Not specified
Pratt & Whitney Division
Double Wasp CA15 Double Wasp CA18 Double Wasp CA3 Double Wasp CA5 Military R-2800 Series
Regulatory Text

49-40-02 PRATT & WHITNEY: Applies to Double Wasp CA Series (-3, -5, -15, -18) and Military R-2800-C Series (-22, -22W, -34, -34W, -57, -73, -77, -81, -83, -85) Engines.

To be accomplished at next overhaul but in no case later than March 1, 1950.

To preclude the possibility of complete loss of power as a result of failure of the supercharger impeller thrust bearing, the engine must be modified to incorporate a new thrust plate P/N 127770 with larger (No. 51) oil feed holes. Also P/N 84012 thrust spacer must be reworked to incorporate circumferential oil skates. Details off this modification and rework are given in Pratt & Whitney Service Bulletin No. 892, Revision B.

As a precautionary measure, it is recommended that the engine be operated with minimum use of high ratio supercharger and that particular attention be directed toward keeping oil sludge to a minimum until the above modification has been accomplished.

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References
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--- - Part 39
FAA Documents