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SAMDAILY.US - ISSUE OF JUNE 07, 2020 SAM #6765
SOLICITATION NOTICE

66 -- Ball-on-Cylinder Lubricity Evaluator

Notice Date
6/5/2020 9:12:55 AM
 
Notice Type
Combined Synopsis/Solicitation
 
NAICS
334516 — Analytical Laboratory Instrument Manufacturing
 
Contracting Office
FA8601 AFLCMC PZIO WRIGHT PATTERSON AFB OH 45433-5344 USA
 
ZIP Code
45433-5344
 
Solicitation Number
FA860120Q0099
 
Response Due
6/4/2020 10:00:00 AM
 
Archive Date
06/19/2020
 
Point of Contact
Aaron Pitts, Phone: 9375224638, Alanna Medina, Phone: 3125224509
 
E-Mail Address
aaron.pitts.1@us.af.mil, alanna.medina@us.af.mil
(aaron.pitts.1@us.af.mil, alanna.medina@us.af.mil)
 
Small Business Set-Aside
SBA Total Small Business Set-Aside (FAR 19.5)
 
Description
The procurement is for one Ball-on-Cylinder Lubricity Evaluator (BOCLE) instrument that will be used at AFPA laboratories.� Aerospace Fuels Laboratories perform quality control testing for JET A grade aviation fuel. BOCLE instrument must at a minimum: Meet all the requirements in ASTM D5001, �Standard Test Method for Measurement of Lubricity of Aviation Turbine Fuels by the Ball-on-Cylinder Lubricity Evaluator (BOCLE)�. In accordance with T.O. 42B-1-1, �Quality Control Of Fuels and Lubricants�; MIL-DTL-83133K, �Detail Specification: Turbine fuel, Aviation, Kerosene Type, JP-8 (NATO F-34), NATO F-35, and JP-8+100 (NATO F-37)�; DEF STAN 91-091, �Turbine Fuel, Kerosene Type, Jet A- 1; NATO Code: F-35; Joint Service Designation: AVTUR� and ASTM D1655-15 �Standard Specification for Aviation fuels�. Generates a measurable wear scar by friction between a stationary ball and a rotating cylinder. Capable of cylinder rotational speed of 240 � 1 rpm. The temperature of the fuel tank reservoir is controlled. Fluid temperature should be maintained at 25 � 1?. The relative humidity of the compressed air which is circulated into and above the test fluid, also including the air flow rate, is controlled. Conditioned air should be controlled at 10 � 0.2% relative humidity at 25 � 1?. Air flow rate should be maintained at 3.8 L/min for duration of test. No microscope is needed, if sold separately. If attached, microscope should be capable of 100x magnification and suitable of measuring the wear scar to the nearest 0.01nm. No computer is needed, if sold separately. Typical power of 100-240V, 250W. Delivery within 4-8 week lead time after receipt of award.
 
Web Link
SAM.gov Permalink
(https://beta.sam.gov/opp/10f7ad7eeb794b08823fefda25234bda/view)
 
Place of Performance
Address: Kadena Air Base, Okinawa 96368-5161, JPN
Zip Code: 96368-5161
Country: JPN
 
Record
SN05682301-F 20200607/200605230147 (samdaily.us)
 
Source
SAM.gov Link to This Notice
(may not be valid after Archive Date)

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