Airworthiness Directives; McCauley Propeller Systems, Inc. Propeller Hub Models B5JFR36C1101, C5JFR36C1102, B5JFR36C1103, and C5JFR36C1104
airworthiness · Rule · Final rule; request for comments. · Published 2003-08-21 · Effective 2003-08-21 · 68 FR 50462
Document
Document number
03-21519
Federal Register citation
68 FR 50462
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
McCauley
Publication date
2003-08-21
Effective date
2003-08-21
FAA docket
Docket No. 2003-NE-32-AD
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.