AD: McCauley | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-10.06.25

AirborneNextGen-
10.07.25

Airborne-Unlimited-10.08.25

Airborne-FlightTraining-10.09.25

AirborneUnlimited-10.10.25

Fri, Aug 22, 2003

AD: McCauley

AD NUMBER: 2003-17-10
MANUFACTURER:
McCauley
SUBJECT: Airworthiness Directive 2003-17-10


SUMMARY: 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.

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.

FMI: www.avantext.com/DailyADIndex.ASP?AD=20031710

Advertisement

More News

Aero-News: Quote of the Day (10.16.25)

“This integration marks a significant step forward in cockpit connectivity and safety. It is one of few solutions offered to business aviation and rotorcraft operators that p>[...]

Airborne 10.15.25: Phantom 3500 Confounds, Citation CJ3 Gen2 TC, True Blue Power

Also: Kodiak 100 Joins USFS, Innovative Solutions & Support Renamed, Gulfstream Selects Honeywell, Special Olympics Airlift The Phantom 3500 mockup made an appearance where the>[...]

ANN's Daily Aero-Term (10.16.25): Enhanced Flight Vision System (EFVS)

Enhanced Flight Vision System (EFVS) An EFVS is an installed aircraft system which uses an electronic means to provide a display of the forward external scene topography (the natur>[...]

True Blue Power and Mid-Continent Instruments and Avionics Power NBAA25 Coverage

Mid-Continent Instruments and Avionics and True Blue Power ANN's NBAA 2025 Coverage... Visit Them At Booth #3436 True Blue Power Unveils 50 Amp-hour Lithium-ion, Main Ship Battery >[...]

NTSB Final Report: Bellanca 17-30A

Shortly After Takeoff, The Engine Completely Lost Power Analysis: The pilot reported that the engine start, run-up, and takeoff were without incident. However, shortly after takeof>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC