Hellicopter Association International
Register   ::   Login   ::   Search   ::   Site Map

Featured Pages  
Hellicopter Association International - Rotor.com
 RotorNews
Go to the My Rotor.com page for information on receiving RotorNews by e-mail and contributing news stories including press releases online. To view stories online in a particular category, click one of the following links: Advisory Circulars, Affiliate,  Airworthiness Directives, Government, HAI Happenings, Helicopters Saving Lives, Industry Press Releases, Legislative, Maintenance Update (members only), Operations Update (members only), Preliminary Accident Reports (members only), Safety, and Security.   

 Print   

 Airworthiness Directives
    
Page: 1 2
Robinson Helicopter Company Hot Weather Operation
Tuesday, June 30, 2009 (299 reads)Airworthiness Directives

This Special Airworthiness Information Bulletin (SAIB) alerts owners and operators of the potential for fuel vapor in high ambient temperatures and altitude on Robinson Helicopter Company (RHC) Model R44 II helicopters.

 



Read More      
Carburetor Icing Prevention
Tuesday, June 30, 2009 (131 reads)Airworthiness Directives

This Special Airworthiness Information Bulletin is written to inform pilots of the potential hazards associated with carburetor icing.

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



Read More      
EMERGENCY AIRWORTHINESS DIRECTIVE
Tuesday, March 24, 2009 (826 reads)Airworthiness Directives

March 23, 2009 - This Emergency Airworthiness Directive (AD) is prompted by the failure of 2 main gearbox filter bowl assembly mounting studs (studs) that were found broken during a fatal accident investigation in Canada. Prior to the accident, the manufacturer was investigating a July 2008 incident that also involved broken studs. In both cases, the broken studs resulted in rapid loss of oil. The failures have been tied to fretting and galling of the original titanium studs; therefore, we are requiring the removal of all titanium studs and replacement with steel studs. We are issuing this EmergencyAD to prevent failure of a stud which could result in rapid loss of oil, failure of the main gearbox, and subsequent loss of control of the helicopter.



Read More      
Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters
Friday, September 12, 2008 (1294 reads)Airworthiness Directives

AD 2008-19-02

SUMMARY: We are superseding an existing airworthiness directive (AD) for Bell Helicopter Textron Canada (Bell) Model 222, 222B, 222U, 230, and 430 helicopters. That AD currently requires visually inspecting the main rotor hydraulic actuator support (support) to verify the presence of all dowel pins and sealant between the support and transmission and verifying the proper torque of each attaching nut (nut). This AD requires the same actions as the existing AD and also requires repetitive actions at intervals not to exceed 600 hours time-in-service (TIS) or 12 months, whichever occurs first.



Read More      
Special Airworthiness Information Bulletin: Lycoming Direct-Drive Reciprocating Engines
Wednesday, September 10, 2008 (1242 reads)Airworthiness Directives

This Special Airworthiness Information Bulletin alerts you, owners, operators, and certificated repair facilities that, all Lycoming Engines (Lycoming) direct-drive reciprocating engines, including VO-360 and IVO-360; except O-320-H, O-360-E, LO-360-E, TO-360-E, LTO-360-E, and TIO- 541 series engines, must be in compliance with Airworthiness Directive (AD) 2004-10-14 if they have had a propeller strike.



Read More      
EC135 Emergency Airworthiness Directive
Saturday, December 15, 2007 (1170 reads)Airworthiness Directives

ADMINISTRATOR'S AIRWORTHINESS DIRECTIVE ALERT

SUBJECT:  Eurocopter Deutschland Model EC135 Helicopters.

 

BACKGROUND:  The Rotorcraft Directorate will issue an emergency airworthiness directive (EAD) that is prompted by the failure of a tail rotor control rod which resulted in an accident that occurred in Japan.

 

UNSAFE CONDITION:  The EAD is intended to prevent failure of a tail rotor control rod and subsequent loss of control of the helicopter.  The Civil Aviation Bureau of Japan (JCAB) and European Aviation Safety Agency (EASA) have issued their own Airworthiness Directives.

 

ACTION:  The EAD will require, within the next 5 hours time-in-service, inspecting the control rod and adjoining ball pivot and replacing any unairworthy parts before further flight.

 

IMPACT:   U.S.-registered fleet:  163

                   Worldwide fleet:  2315

Labor Cost per Helicopter:  $80 per work hour.  We estimate 1 work hour to inspect the control rod and ball pivot and 3 work hours to replace a control rod or ball pivot, if necessary. 

                    Parts Cost per Helicopter:  $400 for the control rod and $675 for the ball pivot

                    Total Estimated Cost Impact:  $32,765, assuming 15 helicopters require replacing parts.

 

AFFECTED U.S. OPERATORS:  General Aviation (Air Tour Operators, Powerline/Pipeline Survey), Law Enforcement.

 

NEWS VALUE/MEDIA INTEREST:  General press interest.

 

Regional Duty Officer:  (817) 222-5006 



Read More      
Sikorsky Needs Your Help
Friday, June 01, 2007 (1290 reads)Airworthiness Directives

As a service to our members, HAI would like to make you aware of the following Airworthiness Directive:

Sikorsky Airworthiness Directive

Please review your equipment and contact Sikorsky Aircraft if the AD applies to you.


Read More      
FAA Aircraft Certification Service SPECIAL AIRWORTHINESSINFORMATION BULLETIN
Monday, February 12, 2007 (3919 reads)Airworthiness Directives

http://www.faa.gov/aircraft/safety/alerts/SAIB SAIB:  SW-07-16DATE:  February 9, 2007
This is information only.  Recommendations aren’t mandatory.

Introduction

This Special Airworthiness Information Bulletin (SAIB) alerts owners and operators of Robinson Helicopter Company models R22 and R44 that the rotor blade skin may begin to debond at the skin-to-spar joint on the lower surface at the tip. 



Read More      
Page: 1 2


 Print   


 Translate rotor.com

Click on a language below for a software translation of this Web site.


  


Copyright© 2009 HAI Website    Terms Of Use  Privacy Statement