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2. Air ambulances in Canada - Wikipedia

   en.wikipedia.org/wiki/Air_ambulances_in_Canada

   1.9 Ontario. 1.10 Prince Edward Island. 1.11 Quebec. 1.12 Saskatchewan. 1.13 Yukon. 2 References. ... STARS - Shock Trauma Air Rescue Society - eastern BC only;

3. Shock Trauma Air Rescue Service - Wikipedia

   en.wikipedia.org/wiki/Shock_Trauma_Air_Rescue...

   The first STARS base opened in Calgary in 1985 under the original name of the Lions Air Ambulance Service. [5] The Lions Club provided the first helicopter, a white BK117 with the Lions Club banner on the side. The Lions Air Ambulance Service's first mission was in December 1985, the transport of a critically ill infant to a hospital in Calgary ...

4. Oshkosh TAK-4 Independent Suspension System - Wikipedia

   en.wikipedia.org/wiki/Oshkosh_TAK-4_Independent...

   The double-wishbone suspension can also be referred to as ‘double A-arm,’ though the arms themselves can be A-shaped, L-shaped, or even a single bar linkage. The complete TAK-4 independent suspension system set-up also includes a subframe which contains the axle differential, half shafts, and wheel ends with steering attachments and brakes.

5. AOL Mail

   mail.aol.com

   Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!

6. List of international airports in Canada - Wikipedia

   en.wikipedia.org/wiki/List_of_international...

   As defined by Transport Canada, an international airport: . means any airport designated by the Contracting State, in whose territory it is situated, as an airport of entry and departure for international commercial air traffic, where the formalities incident to customs, immigration, public health, animal and plant quarantine and similar procedures are carried out.

7. Normal shock tables - Wikipedia

   en.wikipedia.org/wiki/Normal_shock_tables

   In aerodynamics, the normal shock tables are a series of tabulated data listing the various properties before and after the occurrence of a normal shock wave. [1] With a given upstream Mach number , the post-shock Mach number can be calculated along with the pressure , density , temperature , and stagnation pressure ratios.