RFQ Wheel Assembly Torque System.pdf

REQUEST FOR QUOTE (RFQ)

C-17A Wheel Torquing Assembly System Solicitation # FA441820Q0018

The 628th Contracting Squadron is soliciting quotations on the item(s) listed below. Please complete this form and submit your offer to:

Attn: Anthony L. Lawston Tel No: (843) 963-5163

E-mail: anthony.lawston.1@us.af.mil

RFP Responses Due: 16 June 2020 at 2:00 P.M. EST Set-aside: 100% SB-Set Aside

NAICS: 336413 Size Standard: 1,250 Employees

Vendor Name: _____________________________________________________________________________

Address: _________________________________________________________________________________

Phone_____________________________________ Fax: ____________________________________

Quoted by: ________________________________ Title: ____________________________________

Delivery Date: ______________________________ Warranty: _________________________________

Cage Code: _________________________________ Duns: _____________________________________

Tax ID: ____________________________________ E-mail: ____________________________________

Business Size: ___________________ __________ Discount Terms: _____________________________

FOB: Destination __________ Delivery: ___________________________________

GSA Schedule #:_____________________________ Date Quoted: ________________________________

ITEM # SUPPLIES/SERVICES

ITEM

(Y/N)

QTY U/I Unit Price Extended Amount

Aircraft Wheel Assembly Torquing System (Low) Torque (Range 22-265 ft. lbs) Brand Name or Equal Bauer Wheel Assembly Torquing System (Ref: FAR 52.211-6) (IAW Specification Sheet)

1 EA $___________ $___________

Secondary Gantry Torquing System Option Brand Name or Equal Bauer Secondary Gantry Torquing System (Ref: FAR 52.211-6) (IAW Specification Sheet)

1 EA $___________ $___________

Wheel Lifting Fixture Torquing System Option Brand Name or Equal Bauer Secondary Gantry Torquing System (Ref: FAR 52.211-6) (IAW Specification Sheet)

1 EA $___________ $___________

TOTAL COST- Including Shipping

(FOB DESTINATION) $_____________________

mailto:anthony.lawston.1@us.af.mil

Specifications

• Ease of Operation: Design shall allow for operation by one mechanic with, or without, the aid of an overhead hoist

• Maximum Productivity: Must provide a simple, efficient, and reliable means of assembling aircraft main or nose wheels

• Ease of Calibration and Maintenance: Design practices shall include component selection and detailed instruction manuals that ensure the easiest and most reliable procedures for calibration and maintenance.

• Expandability: The ability to easily add unlimited wheel PINs in the machine at any time

• Mandatory Dimensions: 152”W x 90”Dx124”H

• Touch-screen interface for selecting wheel part numbers

• Operator controls for torqueing start/stop located on the nut runner handle bar

• Dual spindle shall allow for simultaneous torqueing of two fasteners

• Nut runners mounted on positioning fixture shall be adjustable to match bolt diameter

• Scale shall be provided on fixture to indicate distance between nut runners

• Nut runner assembly shall be suspended from air-balanced cable on post-mounted overhead swing boom

• Must include Nut Runner application and controller configuration software

• Must be programmed for torque control, angle control or a combination of both

• Must include BS3096G Secondary Gantry (pneumatic lift hoist for lifting wheel halves) with a weight capacity of 250 pounds and accompanying Lifting Fixture BS3085

• one (1) year warranty

The Torquing system shall provide a convenient, efficient, and reliable means of torqueing aircraft main or nose tire bolts. The unit shall be designed for operation by one mechanic. Nut Runner software shall allow the operator to select wheel, loading all applicable parameters. Electric nut runners shall quickly and accurately tighten fasteners to the appropriate torque and angle.

Secondary Gantry pneumatic hoist shall lift and place wheel halves onto the complementing Wheel Build-up Stand. The Torque System shall be delivered fully programmed with wheel torque and angle parameters corresponding to each customer wheel part numbers. The nut runner spindles shall accept customer supplied standard ¾” drive sockets.