FAA Issues SAIB For Robinson R44 Main Rotor Blades | 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-04.29.24

Airborne-NextGen-04.30.24

Airborne-Unlimited-05.01.24 Airborne-AffordableFlyers--05.02.24

Airborne-Unlimited-05.03.24

Wed, Feb 25, 2015

FAA Issues SAIB For Robinson R44 Main Rotor Blades

Aircraft Grounded In Australia After Fatal Accident In New Zealand

The FAA has issues a Special Airworthiness Information Bulletin (SAIB SW-15-08) directed towards owners and operators of Robinson Helicopter Company model R44 and R44 II helicopters which have installed main rotor blades with part number C016-7 of a fatigue crack occurrence, and suggests a preflight check for signs of a fatigue crack on the trailing edge of the blade.

The FAA has received a report from New Zealand of an in-flight failure of the main rotor blade on a Robinson R44 II helicopter which resulted in severe main rotor vibration. The aircraft was difficult to control during the subsequent emergency landing. The New Zealand CAA released Continuing Airworthiness Notice – 62-003 on January 26, 2015 recommending a pre-flight inspection of this area. Robinson Helicopter Company subsequently released R44 Safety Alert C016-7 Main Rotor Blade Crack on February 23, 2015 recommending a preflight visual inspection of the trailing edge of the main rotor blade for any evidence of a fatigue crack initiation.

Australia's Civil Aviation Safety Authority (CASA) issued an emergency airworthiness directive grounding certain Robinson R44 helicopters operating in that country following the New Zealand accident.

The FAA says that at this time, the airworthiness concern is not an unsafe condition that would warrant airworthiness directive (AD) action under Title 14 of the Code of Federal Regulations (14 CFR) part 39.

The FAA says that as part of the daily preflight inspection, the trailing edge of the main rotor blade on the upper and lower surfaces of the blade (a stepladder may be necessary) should be visually checked for any damage which may initiate a fatigue crack. Check in the area shown on the Robinson Safety Alert C016-7 Main Rotor Blade Crack, dated February 23, 2015. If any damage is detected, the blade should be thoroughly examined by a qualified technician prior to further flight. If unusual rotor system vibration is detected in flight, land immediately and have blades examined by a qualified technician.

It is recommended that any positive findings be reported to the Robinson Helicopter Company.

(Image from file)

FMI: SAIB

Advertisement

More News

ANN's Daily Aero-Linx (05.02.24)

Aero Linx: Model Aeronautical Association of Australia MAAA clubs are about fun flying, camaraderie and community. For over 75 years, the MAAA has been Australia’s largest fl>[...]

ANN's Daily Aero-Term (05.02.24): Touchdown Zone Lighting

Touchdown Zone Lighting Two rows of transverse light bars located symmetrically about the runway centerline normally at 100 foot intervals. The basic system extends 3,000 feet alon>[...]

Aero-News: Quote of the Day (05.02.24)

“Discovery and innovation are central to our mission at Virgin Galactic. We’re excited to build on our successful record of facilitating scientific experiments in subor>[...]

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>[...]

NTSB Final Report: Cirrus Design Corp SR20

Student Pilot Reported That During Rotation, “All Of A Sudden The Back Of The Plane Kicked To The Right..." Analysis: The student pilot reported that during rotation, “>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC