AD: Hartzell (Correction) | 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-11.10.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-Unlimited-11.06.25

AirborneUnlimited-11.07.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Wed, Jul 09, 2003

AD: Hartzell (Correction)

AD NUMBER: 97-18-02R1
MANUFACTURER:
Hartzell
SUBJECT: Airworthiness Directive 97-18-02 R1

SUMMARY: CORRECTION - This amendment revises an existing airworthiness directive (AD), that is applicable to Hartzell Propeller Inc. ( )HC-()(2,3)(X,V)( )-( ) series and HA-A2V20-1B series propellers with aluminum blades. That AD currently requires initial and repetitive dye penetrant and eddy current inspections of the blade and an optical comparator inspection of the blade retention area, and, if necessary, replacement with serviceable parts. In addition, that AD currently requires initial and repetitive visual and magnetic particle inspection of the blade clamp, dye penetrant inspection ofthe blade internal bearing bore, and, if necessary, replacement with serviceable parts. Also, for all HC-(1,4,5,8)(2,3)(X,V)( )-( ) steel hub propellers, that AD currently requires an additional initial and repetitive visual and magnetic particle inspection of the hub, and, if necessary, replacement with serviceable parts. This amendment revises that AD by permitting the replacement of affected propellers with Hartzell Propeller Inc. model "MV" series propellers as an optional terminating action for the initial and repetitive inspections of that AD. This amendment is prompted by type certification approval of the Hartzell "MV" series propellers that are direct replacements for the affected propellers, and service bulletin approval to allow modification of affected propellers to the "MV" type design configuration. The actions specified by this AD are intended to prevent blade separation due to cracked blades, hubs, or blade clamps, which can result in loss of control of the airplane.

FMI: www.avantext.com/DailyADIndex.ASP?AD=971802R1

Advertisement

More News

ANN's Daily Aero-Term (11.14.25): Marker Beacon

Marker Beacon An electronic navigation facility transmitting a 75 MHz vertical fan or boneshaped radiation pattern. Marker beacons are identified by their modulation frequency and >[...]

Aero-News: Quote of the Day (11.14.25)

“Aviation is an incredible tool for Samaritan’s Purse. After a disaster strikes, we want people to know why we are bringing life-saving supplies. We want them to know t>[...]

Classic Aero-TV: CiES All-Digital Fuel Senders

From 2024 (YouTube Edition): New Capabilities For Business Aviation CiES Corporation President Scott Philiben walked Aero-News Editor in Chief Jim Campbell through some of what set>[...]

Airborne 11.10.25: Affordable Expo Succeeds, Citation Ascend, Kenai Shuts Down

Also: Duffy Predicts ‘Mass Chaos’, Modern Skies Coalition, More Impacts, Archer Buys Hawthorne With only a few months of preparation—and minimal outside media sup>[...]

NTSB Final Report: Lancair 320

The Experienced Pilot Chose To Operate In Instrument Meteorological Conditions Without An Instrument Flight Rules Clearance Analysis: The airplane was operated on a personal cross->[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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