Airworthiness Directive

AD 2003-04-23 68 FR 9508

Federal Aviation Administration · 14 CFR part 39

FR document
03-4484
Amendment
39-13072
Published
2003-02-28
Models covered
1
Last live check
2026-08-17
AD

2003-04-23

FR doc 03-4484 · 68 FR 9508

AD 2003-04-23Published 2003-02-28Effective 2003-04-04

Requires replacement of those blades with blades of the latest design.

Full official abstract

This amendment adopts a new airworthiness directive (AD), that is applicable to Hartzell Propeller Inc. model HC-B3TN-5( ) propellers, with blades part number (P/N) T10176H(B,K)-5 or T10178H(B)-11(R) that are installed on Mitsubishi Heavy Industries, Ltd, MU-2 series airplanes. This amendment requires replacement of those blades with blades of the latest design. This amendment is prompted by a report of in-flight propeller blade separation that caused a severe out-of- balance condition, damage to the airplane, and resulted in engine shutdown and a safe landing. The actions specified by this AD are intended to prevent propeller blade separation, damage to the airplane, and possible loss of the airplane.

Applies to 1 model in our index