SOW.pdf
PDF 589 KB Posted
- Attached to
- Bobtail Aircraft/GSE Tug
- Solicitation number
- 80NSSC24856518Q
About this file
This statement of work outlines requirements for procuring an aircraft and ground support equipment tug vehicle to support NASA's Global Hawk project. Key details include:
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The vehicle must be new or used, have an enclosed cab with climate control, four rear drive wheels, and front and rear tow connections. Specifications cover payload capacity, service weight, dimensions, transmission, braking, and engine options.
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Delivery of the vehicle is required to NASA's Armstrong Flight Research Center at Edwards Air Force Base in California by June 30, 2024. The period of performance on any resulting award or order is six months from the effective date.
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Market research included proposals from TronAir Eagle Tugs and Advanced Ground Support Equipment. The North American Industry Classification System code is 336999 and Procurement Commercial Specification code is FSG17. Broad proposals addressing the specifications are requested with no brand name justification required.
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The related federal contract opportunity is a solicitation issued by NASA's Shared Services Center for the procurement of the bobtail aircraft and ground support equipment tug, as outlined in the attached request for quotation and statement of work.
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Other files
| File | Type | Posted |
|---|---|---|
| Questions and Answers.pdf | ||
| RFQ.pdf |
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Text version
1 Each Aircraft/GSE Tug Vehicle Procurement SOW
Statement of Work Statement of Work and Description for
Procurement of 1 Each Aircraft/Ground Support Equipment Tug Vehicle
1. Objective/Requirements Procure one each Aircraft/Ground Support Equipment Tug Vehicle to support NASA Global Hawk project.
2. Characteristics, Scope, and Specs Condition: New preferred/used considered Cab: Enclosed with air conditioning and heat Drive Wheels: 4 Rear Tow connections: Single pintle in the front and 3 pintle combo in the rear Drawbar Pull Gas/Diesel: 7,500 lbf (33.36 kN) *Max Tow (Dry - 1%Grade): 104,000 lbs (47,174 kgs) *Max Tow (Wet - 1%Grade): 76,000 lbs (34,473 kgs) *Max Tow (Snow - 1%Grade): 55,000 lbs (24,948 kgs) Service Weight:11,200 lbs (5,080 kgs) Turn Radius (outside): 250 in (6350 mm) Bumper (front/rear): 0.5” plate steel / 1-3 in (25-76
mm) A36 steel with pintle hook Suspension: Springs and shock absorbers over each axle Transmission: Automatic,6 forward / 1 reverse, backup alarm Max Speed Governed: 25 mph (40 kph) Steering: Hydraulic power-boosted mechanical, self-centering Brakes: Hydraulic, self-adjusting split type with accumulator
Front/Rear Brakes: Disc
Parking Brake: Foot operated, hard release ENGINE OPTIONS: Gas or Tier 4 diesel Fuel Tank: 40 gal Air Cleaner: Severe environment, heavy duty, dry replacement element Electrical System: 12 volt, Alternator 200 amp diesel, 175 amp gasoline Lights: Halogen headlights / combination brake, tail and back-up, amber beacon Instruments: Oil pressure, water temperature and fuel gauges / hour meter, voltmeter and electric horn, rear camera system
3. Place of Performance Deliver to NASA Armstrong Flight research Center, Edwards AFB, CA 93523
4. Period of Performance
ARO from the order effective date of 6 months. Delivery is requested no later than June 30, 2024
Market Research See included proposals from TronAir Eagle Tugs and Advanced Ground Support Equipment
What is the PSC Code and NAICS Code?
PCS Code: FSG17
NAICS Code: 336999
RDSS or Brand Name Justification
N/A. Submit specifications for broad proposal.
File details come from the government source that posted it. Updated .