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ACRO E-mail Archive Thread: 2-Blade Propeller Hub Inspections [International Aerobatic Club] [Communications] [Aerobatics Images] Disclaimer: These aerobatics pages are developed by individual IAC members and do not represent official IAC policy or opinion. |
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Thread: 2-Blade Propeller Hub Inspections
Message: 2-Blade Propeller Hub Inspections
Follow-Up To: ACRO Email list (for List Members only)
From: Skrud at aol.com
Date: Thu, 04 Jan 1996 13:39:56 UTC
>From the previous request about information concerning propeller hub inspections: Hartzell Propeller Service Bulletin 164C dated September 11, 1992 briefly states: Subject: Inspection for Cracks in Certain Two Blade "Y" Shank Aluminum Hubs Effectivity: HC-C2YK -( )( )( ) or HC-C2YR-( )( )( ) type propeller hubs installed on: - aerobatic aircraft regardless of engine model or propeller serial number - all other aircraft with Lycoming (T,I)O-540 series engine rated at 260 HP and 2700 RPM or higher and propeller serial number range CH19835 through CH26050 "There have been incidents of hub cracks in Hartzell two blade "compact" aluminum hub propellers. In nearly every case, blade separation did not occur due to timely inspection (sometimes associated with reports of abnormal vibration or grease leakage). Cracks typically initiate at the same point on the hub. The cracks are external and are observable with careful examination. the cracks originate at a point adjacent to the blade called the "fillet radius". As cracks propagate toward the center of the hub, their progression accelerates and results in failure of one hub half which can then, potentially, progress to blade separation. WARNING: UNEXPLAINED VIBRATION OR GREASE LEAKAGE INCIDENTS, WHERE THE CONDITION INITIATED SUDDENLY, DEMAND IMMEDIATE INSPECTION FOR POSSIBLE CRACKED HUB." Compliance: Hartzell has developed a new hub which has a different contour in the fillet radius and different shot peening. These hubs are exempt from repetitive inspections. These hubs are identified by the suffix letter "A" at the end of the hub serial number and propeller serial numbers. Inspection is required within the next 25 hours of operation [ ], and thereafter at intervals not to exceed 50 hours, or 50 flights whichever occurs first, of operation from the last inspection. The procedure for inspection, line drawings of the affected area, and additional information are included in the SB. Anyone wishing a mailed or faxed copy of the SB can contact me with the appropriate information, I'll be happy to get it right out to you... Scott H. Rodriguez, IAC# 18601 Test Engineer Hartzell Propeller Inc. One Propeller Place Piqua, OH 45356 Skrud at aol.com 513-778-4370 (voice) 513-7784365 (fax)