CASA Urgent AD: Bell Helicopter | 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-06.23.25

Airborne-NextGen-06.24.25

AirborneUnlimited-06.25.25

Airborne-AffordableFlyers-06.26.25

AirborneUnlimited-06.27.25

Thu, Dec 01, 2005

CASA Urgent AD: Bell Helicopter

Applicability: Bell Helicopter Textron Canada (BHTC), Model 206 series helicopters as follows: Model 206A, 206B Serial Numbers (S/N) 004 through 660 and 672 through 715 661 through 671 and 716 through 4586 and 5101 through 5305

Requirement: 1. Inspect the grounding of the fuel pumps and solenoid valve, as per instructions provided in Part I of Alert Service Bulletin (ASB) 206-05-103, dated 11 February 2005, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada.
2. Helicopters which have incorporated the modification consisting of relocation of the purge hose, as per instructions provided in Part II of (ASB) 206-05-103 (Requirement 2 of the initial issue of this Directive), are to restore the purge hose to the previous configuration, which existed prior to the introduction of this Alert Service Bulletin.

Note: Transport Canada AD CF-2005-10R1 refers.

Compliance: For Requirement 1 - Remains unchanged as “Within the next 100 hours time in service, but no later than 10 July 2005”.
For Requirement 2 - Before further flight after 29 December 2005.

This Amendment becomes effective on 2 December 2005.

Background: Transport Canada has advised that inadequate electrical grounding of the fuel boost pump and the fuel drain solenoid valve, combined with fuel hoses contact, could cause arcing in the main fuel cell which may in turn cause an explosion and resultant fire. The original issue of this Directive required a one time inspection to ensure correct grounding and, if necessary the disconnection and stowage of the engine fuel purge hose. Since Canadian Airworthiness Directive CF-2005-10 was issued, Transport Canada has determined that the purge hose relocation as per instructions provided in Part II of ASB 206-05-103, could cause an engine flameout in a low fuel, boost pump off, condition.

Therefore, until further notice, Requirement 2 of the initial issue of this Directive is revoked and this Amendment requires the helicopter fuel purge hose to be returned to its previous configuration.

The original issue of this Directive became effective on 16 June 2005.

FMI: www.casa.gov.au

Advertisement

More News

Airborne 06.30.25: US v ADS-B Misuse, Nat’l STOL Fire, Volocopter Resumes

Also: Netherlands Donates 18 F16s, 2 737s Collide On Ramp, E-7 Wedgetail Cut, AgEagle's 100th In S Korea The Pilot and Aircraft Privacy Act was introduced in the House by Represent>[...]

NTSB Prelim: Piper PA-23

Pilot Also Reported That Due To A Fuel Leak, The Auxiliary Fuel Tanks Were Not Used On June 4, 2025, at 13:41 eastern daylight time, a Piper PA-23, N2109P, was substantially damage>[...]

ANN FAQ: Submit a News Story!

Have A Story That NEEDS To Be Featured On Aero-News? Here’s How To Submit A Story To Our Team Some of the greatest new stories ANN has ever covered have been submitted by our>[...]

Classic Aero-TV: One Man’s Vietnam

From 2023 (YouTube Edition): Reflections on War’s Collective Lessons and Cyclical Nature The exigencies of war ought be colorblind. Inane social-constructs the likes of racis>[...]

Klyde Morris (06.30.25)

What Goes Around, May Yet Come Back Around, Klyde FMI: www.klydemorris.com>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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