Attachment_3_-_Aircraft_Identification_Table_(Amd_2).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 contains templates for identifying fixed wing and rotary wing aircraft capabilities for the Worldwide Airlift Services Program - 135 (WASP-135) solicitation. The templates require offerors to provide specifications for their aircraft including type, payload capacity, range, fuel efficiency, certifications, and hazardous material transport capabilities. Offerors must input maximum performance data under standard temperature and pressure conditions with no wind. The solicitation seeks comments on the templates by November 28, 2018 to inform the final solicitation, though this synopsis does not constitute a request for proposal. The United States Transportation Command is the issuing agency.
Aircraft Identification Table (Attachment 3) Amendment 2
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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-IX) | 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 calculated at Maximum Payload. | |||||||||||||||||
| 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 .