Question_and_Answers_for_Posting_12_through_13.docx

DOCX document 14 KB Posted

Attached to
Trans Sahara Short Take Off & Landing Federal contract opportunity
Solicitation number
HTC711-13-R-C003
Issued by
Department of Defense United States Transportation Command

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Answers to questions 12 13 are hereby posted.

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Text version

Question and Answers Solicitation HTC711-13-R-C003

Question 12 Please define or clarify the meaning of “Internal Aircraft Power Unit capability”. This is not commonly used aircraft terminology that applies to turbo prop STOL aircraft.

Answer 12 The purpose of the requirement is for the aircraft to have the capability to start engines without use of an external cart, which is typically found in larger aircraft. Amendment 0002 changes PWS paragraph 3.5 to read “Ability to start aircraft engines without use of external ground power units.”

Question 13 Please clarify the Aircraft Range Requirement in Paragraph 3.6.7, all available data from STOL Aircraft Manufacturers and STOL Aircraft operators confirms that the Casa 212 or any other turbo prop STOL aircraft cannot meet this requirement legally under FAA 135 operation.

Answer 13 Amendment 0002 changes the requirement within PWS paragraph 3.6.7 from 800 nautical miles to 700 nautical miles.

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