SOW Front End Loader Rental.pdf
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- Attached to
- Front End Loader Rental
- Solicitation number
- FA820125Q0015
About this file
This Statement of Work (SOW) details the requirements for renting a front-end loader for the 75th Civil Engineer Squadron at Hill Air Force Base in Utah. The loader must be suitable for heavy-duty industrial construction projects, with specific technical specifications including an engine power of 322-325 kW, bucket capacity of 4.8-6.25 cubic yards, and a static tipping load of 46,000-49,000 lbs. The equipment must be delivered to the Utah Test and Training Range by May 1, 2025, with delivery including assembly, testing, and personnel training.
Vendor requirements include providing a detailed quotation with itemized costs, warranty information, and delivery timeline. The loader must come with a manufacturer's warranty and technical support. Acceptance criteria will be based on successful delivery, compliance with specified technical requirements, and satisfactory performance during testing. The rental period is from May 1 to October 31, 2025, with the loader to be used at the Thermal Treatment Unit location (UTTR/50037).
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| File | Type | Posted |
|---|---|---|
| Combo Synopsis Solicitation Front End Loader Rental Hill AFB UT-.pdf | ||
| Solicitation - FA820125Q0015.pdf |
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Text version
DEPARTMENT OF THE AIR FORCE
75TH CIVIL ENGINEER SQUADRON (AFMC)
HILL AIR FORCE BASE UTAH
21 Jan 25
Work Task: 13616628 Location: Thermal Treatment Unit/UTTR/50037 Project Title: Front End Loader Rental Period of Performance: 1 May 25 – 31 Oct 25
Statement of Work for Front End Loader Purchase
1. Introduction
This Statement of Work (SOW) outlines the requirements and specifications for the rental of a front-end loader.
2. Scope of Work:
The front-end loader shall be suitable for heavy-duty industrial use in construction projects.
The loader should have a static tipping load of 46000 lbs. at 40 degree turn with tire deflection and static tipping load of 49000 lbs. at 40 degree turn with no tire deflection. It should be equipped with a quick-attach system for easy interchangeability of attachments. The loader must comply with all relevant safety standards and regulations.
3. Specifications
Engine Power: @1700 RPM – ISO 14396:2002/322 KW/432 HP
Gross Power @ 1700 RPM – SAE J1995:2014/325 kW/463 HP
Net Power @ 1700 RPM – ISO 9249:2007, SAE J1349:2011/301KW/404 HP
Engine Torque – 1515 lbs.
Bucket Capacity: 4.8 – 6.25 yds
Breakout Force – 59060 lbf.
Operating Weight: 78000
4. Delivery Requirements
The front-end loader must be delivered to 75 CES/CEOR (Range Support Flight/Utah Test and Training Range) by NLT 1 May 2025.
Delivery includes assembly, testing, and training of personnel on operation and maintenance.
5. Warranty and Support
The loader should come with a manufacturer's warranty. Supplier should provide technical support, maintenance services, and spare parts availability for the duration of the warranty and beyond.
6. Vendor Requirements
Vendors must provide a detailed quotation including itemized costs, warranty information, delivery timeline, and any additional services offered. Vendors must be reputable, experienced, and certified to sell and service the specified brand/model of front-end loader.
7. Acceptance Criteria
Acceptance of the front-end loader will be based on successful delivery, compliance with specifications, and satisfactory performance during testing.
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