Attachment 1 - Salient Characteristics - Airlift Mobility Ramps Final.docx
DOCX document 21 KB Posted
- Attached to
- Airlift Mobility Ramp Kit Federal contract opportunity
- Solicitation number
- FA286024Q4010
About this file
This document is the Salient Characteristics Sheet for an Airlift Mobility Ramp Kit required by the Department of the Air Force's 89th Airlift Wing, Presidential Airlift Group (PAG). The kit must be comprised of non-wood ramp components to load vehicles into C-17 or C-5 aircraft, and meet requirements in AFI 11-289, AFI 24-605, and have Air Transportability Test Loading Agency (ATTLA) certification. The kit must include aluminum ramps with handles, PVC belting to prevent damage, and aluminum approach shoring. It cannot weigh more than 2,160 lbs and must fit in a box truck. The kit must support loading vehicles up to 429" L x 102" W x 156" H and 30,940 lbs. Specific required components include 4 ramp sections, 2 flat top ramp sections, 2 lead ups, 2 ramp pads, various adjustable stands, and aircraft pedestal shoring of specific dimensions. This is in support of the related federal contract opportunity, Solicitation Number FA286024Q4010 for the Airlift Mobility Ramp Kit, which is a 100% small business set-aside.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Attachment 3 - AFI24-605.pdf | ||
| Attachment 5 - ATTLA certification Ambulift.pdf | ||
| COMBINED SYNOPSISSOLICITATION PAG Airlift Mobility Ramp Kit.docx | DOCX document | |
| Attachment 2 - AFI11-289.pdf | ||
| Attachment 4 - DoD Manual 414065.pdf | ||
| Attachment 6 - ATTLA certification High Lift Catering Truck (Heritage).pdf | ||
| Attachment 7 - ATTLA certification Isuzu.pdf |
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Text version
Salient Characteristics Sheet
Describe the requested item(s) in salient terms:
Airlift Mobility Kit is a ramp kit built to load vehicles into either C-17 or C-5. Items in this product kit should meet all requirements in AFI 11-289, AFI 24-605, and Air Transportability Test Loading Agency (ATTLA) certification. Ramps should be ATTLA certified too this shows they are safe transport in an aircraft and what requirements we would have on securing ramps inside the aircraft.
Physical characteristics Aluminum ramp pieces with built in handles on both sides. Ramps that touch the aircraft ramps have PVC belting to prevent damage to ramps and to aircraft ramps. Approach shoring shall be aluminum. No wood components. Entire ramps and pedestal shoring kit has a total weight of 2,160 lbs. Ramps and shoring shall break down to fit in our box truck to ease transportation. Air Mobility Kit shall hold the weight of vehicles and provide enough approach angle to prevent vehicles scraping against the aircraft ramp, or the aircraft. Ramp kit must be able to support loading our longest vehicle which is 429” L x 102” W x 156” H and the gross weight of this vehicle is 30,940 lbs.
Essential Characteristics of Airlift Mobility Kit
Ramps 4 Each - 30" X 94" X 20K Ramp Section 2 Each - 30" X 94" X 20K Flat Top Ramp Section 2 Each - 30" X 54" X 20K Lead Up 2 Each - 4" tall Ramp Pad 2 Each - Stand Adjustable 13" - 15" (set at 13") 2 Each - Stand Adjustable 20" - 24" (set at 22") 2 Each - Stand Adjustable 28" - 32" (28"/C-5, 32"/C-17)
Aircraft Pedestal shoring 4 Each - 15"x15"x4"tall (C-5) 12 Each - 15"x15"x6"tall (C-5) 4 Each - 15"x18"x4"tall (C-5) 4 Each - 15"x18"x6"tall (C-5/C-17) 1 Each - 18"x30"x2" (C-17)
Functions to be performed Deliver complete Airlift Mobility Kit with non-wood components.
File details come from the government source that posted it. Updated .