Airworthiness Directive

AD 2003-17-10 Amendment 39-13285

Federal Aviation Administration · 14 CFR part 39

FR document
03-21519
Amendment
39-13285
Published
2003-08-21
Models covered
1
Last live check
Not yet re-verified
AD

2003-17-10

FR doc 03-21519

AD 2003-17-10Published 2003-08-21Effective 2003-08-21

Requires a one-time fluorescent penetrant inspection (FPI) of propeller blade retention areas for cracks.

Full official abstract

The FAA is superseding an existing airworthiness directive (AD) for McCauley Systems, Inc. propellers that are installed on, but not limited to, BAE Systems (Operations) Limited Jetstream Model 4101 airplanes. That AD currently requires a one-time fluorescent penetrant inspection (FPI) of propeller blade retention areas for cracks. This AD requires initial and repetitive FPI or Ultrasonic Inspection (UT) of propeller blade retention areas for cracks, replacement of high time propeller blades, and a one-time inspection of propeller hubs. This AD is prompted by four reports of significant cracks found in propeller blade shanks since the issuance of AD 2003-15-01. We are issuing this AD to prevent propeller blade failure or hub failure due to cracking, which could result in failure of the propeller and loss of control of the airplane.

Applies to 1 model in our index