Attachment 2 FA568225Q8013 Silents Characteristics.pdf
PDF 101 KB Posted
- Attached to
- TowFlexx TF5 or Equal
- Solicitation number
- FA568225Q8013
About this file
The document is a Salient Characteristics specification for a TowFlexx TF5 towbarless aircraft tow tractor or equivalent, targeting the Department of the Air Force. The specification requires an electric-powered tow tractor with a 100,000 lbs maximum aircraft weight capacity, compatible with Sikorsky HH-60W helicopters and preferably with F-16 aircraft. Key requirements include a towbarless design using a lifting cradle system, 8-hour battery operation, 360-degree turning capability, remote or walk-behind operation, compact dimensions for hangar storage, automatic safety features, and compliance with DoD, OSHA, and AFOSH safety standards. The tractor must have intuitive controls, minimal maintenance requirements, and include on-board storage for towing mechanisms.
The associated federal contract opportunity (Solicitation Number FA568225Q8013) is a Request for Quotes (RFQ) for commercial products issued by the United States Air Forces in Europe - Air Forces Africa. Quotes are due by 2:00 PM CST on 5 August 2025, with questions accepted until 1 August 2025. The anticipated contract is a Firm Fixed Price (FFP) with a requested delivery date of 30 September 2025, with performance location at Aviano Air Base in Italy. The solicitation uses Simplified Acquisition Procedures under NAICS Code 488190, with no specific set-aside, and requires submission via email to specified contracting personnel.
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Other files
| File | Type | Posted |
|---|---|---|
| Attachment 1 FA568225Q8013 Clause and Provision Set.pdf | ||
| Combo RFQ FA568225Q8013 TowFlexx.pdf |
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Text version
Salient Characteristics
1 EA TowFlexx TF5 or Equivalent
Type and Functionality Must be a towbarless aircraft tow tractor designed for safe and efficient handling of aircraft in ground movement operations. Capable of towing aircraft without the use of a traditional tow bar, utilizing a lifting cradle system to engage the nose landing gear.
Capacity and Aircraft Compatibility Must support a maximum aircraft weight capacity of at least 100,000 lbs. Must be compatible with Sikorsky HH-60W. Prefer to be compatible with F-16s as well, but not mandatory.
Powertrain Must be electric powered, ensuring minimal emissions and compliance with installation environmental goals. Battery system must allow for minimum 8-hour operational shifts on a single charge.
Maneuverability and Safety Capable of 360-degree turning radius or equivalent for precision maneuvering in tight hangars or on congested ramps. Equipped with automatic braking systems, emergency stop features, and nose gear load sensors to prevent over-torque or over-lifting.
Operator Interface Features intuitive, ergonomic controls that minimize training requirements. Remote control or walk-behind operation is requested instead of a typical driver seat operation to enhance visibility and reduce collision risks.
Dimensions and Storage Must be compact enough to operate within standard hangar doors and storage bays. Include on-board storage cradle for towing forks or lifting mechanism.
Maintenance and Support Designed for low maintenance with accessible service points. OEM must provide training manuals, safety documentation, and optional training support.
Compliance and Safety Must meet all applicable DoD, OSHA, and AFOSH safety standards. Vendor must certify non-use of prohibited components under Section 889 compliance.
| Type and Functionality |
| Capacity and Aircraft Compatibility |
| Powertrain |
| Maneuverability and Safety |
| Operator Interface |
| Dimensions and Storage |
| Maintenance and Support |
| Compliance and Safety |
File details come from the government source that posted it. Updated .