AD: Hélicoptères Guimbal Helicopters | 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-04.28.25

Airborne-NextGen-04.29.25

AirborneUnlimited-04.30.25

Airborne-Unlimited-05.01.25

AirborneUnlimited-05.02.25

Sat, Oct 02, 2021

AD: Hélicoptères Guimbal Helicopters

AD 2021-19-07 Requires Replacing An Affected MR Non-Rotating Scissor Link With A Serviceable Part

The FAA is adopting a new airworthiness directive (AD) for certain Hélicoptères Guimbal Model CABRI G2 helicopters.

This AD was prompted by a report that, during scheduled maintenance on two helicopters, cracks were found on a certain main rotor (MR) non-rotating scissor link. This AD requires replacing an affected MR non-rotating scissor link with a serviceable part. The FAA is issuing this AD to address the unsafe condition on these products. This AD is effective November 4, 2021. The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD as of November 4, 2021.

Supplementary Information: The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Hélicoptères Guimbal Model CABRI G2 helicopters. The NPRM published in the Federal Register on July 23, 2021 (86 FR 38943). In the NPRM, the FAA proposed to require replacing an affected MR non-rotating scissor link with a serviceable part. The NPRM was prompted by EASA AD 2019-0186, dated July 30, 2019 (EASA AD 2019-0186), issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for certain Hélicoptères Guimbal Model CABRI G2 helicopters. EASA advises that, during scheduled maintenance on two helicopters, cracks were found on the MR non-rotating scissor link, part number (P/N) G41-10-200. The suspected root cause for the cracking is corrosion due to stress induced by the mounting of the metal bushings inside the lug hole. To address this issue the manufacturer modified the design of the MR non-rotating scissor link to reinforce the lugs and replace the metal bushings with plastic bushings. Cracking of a MR non-rotating scissor link, if not addressed, could result in failure of that scissor link, resulting in reduced control of the helicopter.

Accordingly, EASA AD 2019-0186 requires replacement of affected MR non-rotating scissor links with serviceable parts.

FMI: www.regulations.gov

Advertisement

More News

NTSB Final Report: Cozy Cub

Witness Reported The Airplane Was Flying Low And Was In A Left Bank When It Struck The Power Line Analysis: The pilot was on final approach to land when the airplane collided with >[...]

ANN FAQ: Contributing To Aero-TV

How To Get A Story On Aero-TV News/Feature Programming How do I submit a story idea or lead to Aero-TV? If you would like to submit a story idea or lead, please contact Jim Campbel>[...]

Classic Aero-TV: Seated On The Edge Of Forever -- A PPC's Bird's Eye View

From 2012 (YouTube Edition): A Segment Of The Sport Aviation World That Truly Lives "Low And Slow" Pity the life of ANN's Chief videographer, Nathan Cremisino... shoot the most exc>[...]

ANN's Daily Aero-Linx (04.29.25)

Aero Linx: International Business Aviation Council (IBAC) IBAC promotes the growth of business aviation, benefiting all sectors of its industry and in all regions of the world. As >[...]

ANN's Daily Aero-Term (04.29.25): Execute Missed Approach

Execute Missed Approach Instructions issued to a pilot making an instrument approach which means continue inbound to the missed approach point and execute the missed approach proce>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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