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-10.27.25

AirborneNextGen-
10.28.25

Airborne-Unlimited-10.29.25

Airborne-Unlimited-10.30.25

AirborneUnlimited-10.17.25

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

A ‘Crazy’ Tesla Flying Car is Coming

Musk Claims the Tech Could Be Unveiled Within a Couple of Months Elon Musk is once again promising the impossible…this time, in the form of a Tesla that flies. Speaking on T>[...]

ANN's Daily Aero-Term (11.xx.25): NonApproach Control Tower

NonApproach Control Tower Authorizes aircraft to land or takeoff at the airport controlled by the tower or to transit the Class D airspace. The primary function of a nonapproach co>[...]

Aero-News: Quote of the Day (11.01.25)

"It was pretty dang cool to be in a tube-and-fabric bush plane that high, and it was surreal hearing airline pilots over ATC wondering what a Cub was doing up there. The UL is trul>[...]

ANN's Daily Aero-Linx (11.01.25)

Aero Linx: Lake Amphibian Club Over the years the cost of a new Skimmer or Lake went from about $16,000 to over $500,000 for many reasons. Sales of Renegades have been very sparse >[...]

Classic Aero-TV: EAA Introduces Angle of Attack Training

From 2024 (YouTube Edition): Clinic Aimed to Promote Safe Aircraft Control The EAA Pilot Proficiency Center hosted an angle of attack (AOA) training clinic during the 2024 Oshkosh >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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