Attachment_3_-_Aircraft_Identification_Table.xlsx
XLSX spreadsheet 15 KB Posted
- Attached to
- Worldwide Airlift Services Program - 135 (WASP-135) Federal contract opportunity
- Solicitation number
- HTC71119RR003
About this file
This document includes two attachments related to a solicitation for worldwide airlift services. The first attachment is an aircraft identification table spreadsheet template for offerors to provide details on their fixed wing and rotary wing aircraft fleets. Information required includes aircraft type, capabilities, passenger and cargo capacity, medical evacuation functions, night vision compatibility, and hazardous material transport approvals. The second attachment provides additional context, with the solicitation seeking to establish contracts under the Worldwide Airlift Services Program - 135 (WASP-135) to transport passengers and cargo for the Department of Defense United States Transportation Command on a global basis. Industry feedback on the aircraft template was requested to be submitted by November 28, 2018, though no specific proposal due date or award date were mentioned.
Updated Attachment 3, Aircraft Identification Table
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Text version
Fixed Wing
| Air Carrier Name | Aircraft Type | Tail Number | IFR Capable (Y/N) | Maximum Payload (Lbs) | # of Pax | Cargo (Lbs) | Combi (Y/N) | Medical Evacuation (Y/N) | Air Amb (Y/N) | Pressurized (Y/N) | NVG Capable (Y/N) | Short Take-Off and Landing (Y/N) | Runway Length (Feet) | Unimproved Runway (Y/N) | Range (NM) at Optimal Cruising Speed | HAZMAT Capable (Y/N; if Y, identify Levels I-IX) |
| Instructions: Offerors shall input maximum aircraft capabilities at Standard Day conditions with no wind. Range shall be at Maximum Payload, and runway length required should be at Maximum Gross Takeoff Weight (MGTW). | ||||||||||||||||
| NOTE: Any service marked "Y" must be described in Catalog of Services. "Pressurized" description to be included in Cell 3E under "Fixed Wing." |
| TOTALS |
| Definitions: |
| Standard Day: Temperature of 15 degrees Celsius; altitude of mean sea level; pressure of 29.92 inches of mercury. |
HTC711-19-R-R003, Attachment 3
Rotary Wing
| INTERNAL PAYLOAD | EXTERNAL SLINGLOAD | ||||||||||||||||
| Air Carrier Name | Aircraft Type | Tail Number | IFR Capable (Y/N) | Maximum Payload - HOGE internal (lbs) | Range (NM) at Optimal Cruising Speed | # of Pax | Cargo (Lbs) | Combi (Y/N) | Medical Evacuation (Y/N) | Air Amb (Y/N) | NVG Capable (Y/N) | Number of Engines | HAZMAT Capable (Y/N; if Y, identify Levels I-X) | PART 133 (Y/N) | Slingload (Y/N) | Maximum Payload - HOGE external (lbs) | Range (NM) at Optimal Cruising Speed |
| Instructions: Offerors shall input maximum aircraft capabilities at Standard Day conditions with no wind. Range shall be at Maximum Payload, and runway length required should be at Maximum Gross Takeoff Weight (MGTW). | |||||||||||||||||
| NOTE: Any service marked "Y" must be described in Catalog of Services. |
| TOTALS |
| Definitions: |
| Standard Day: Temperature of 15 degrees Celsius; altitude of mean sea level; pressure of 29.92 inches of mercury. |
| HOGE: Hover Out of Ground Effect. |
File details come from the government source that posted it. Updated .