FPS Pedestal Main Bearing SOW_6973GH-21-Q-00054.pdf

FAA

AJW-L910 FPS

Pedestal Main Bearing Statement of Work

Rev - 12-2-2020

AJW-L910 FPS Main Bearings Rev -

Statement of Work (SOW) For

Process Improvement Equipment, Freestanding Bridge Crane and Freestanding Articulating Jib Crane

1.0 Background

This solicitation is for the procurement of the following part:

• ANFPS-20 Pedestal Main Bearings, as per FAA drawing DE-B-2120, Rev G (see attached)

This part is required for continued support of the ANFPS-20 (Air Navigation Fixed Position System) Radar as currently deployed by the FAA.

2.0 Equipment Details

Details for the required part are noted below:

A. Fabricated, constructed and assembled in complete compliance with FAA drawing DE-B-2120, Rev G, including but not limited to:

i. All dimensions as denoted

ii. All heat treatments as denoted

iii. Roller requirements as denoted

iv. Eccentricity and runout as denoted

v. Pre-load as denoted

vi. Material requirements as denoted

vii. Rollers/cages as denoted

viii. Hardness as denoted

ix. Overall configuration as denoted

x. Each bearing shall be permanently stamped or engraved with the following part identification info:

1. P/N DE-B-2120, Rev G

2. Three (3) digit serial number. Serial numbers shall be sequential beginning with serial number for the First Article bearing

3. Date of bearing manufacture (month and year)

4. Manufacturer

B. Vendor shall provide printed documentation of compliance with the following for each bearing manufactured:

i. All dimensions as denoted. Measurement document shall include at a minimum:

1. Required dimension including tolerance

2. Dimension as measured

3. Pass/Fail determination of dimension measured

4. Date of measurement

5. A Coordinate Measuring Machine (CMM) shall be used to verify all dimensions. Proof of current CMM calibration shall be provided

ii. Housing fit as denoted

iii. Eccentricity and runout as denoted

iv. Diametreal pre-load as denoted

v. Magna flux and hardness inspections as denoted

3.0 First Article Inspection/Testing and Bearing Production

Vendor shall provide a First Article (FA) bearing to the FAA for inspection/testing prior to commencing full bearing production. Details associated with the FA bearing and bearing production processes are noted below:

A. FA bearing shall be shipped to the FAA no later than six (6) months

ARO

B. FA bearing will be inspected/tested by the FAA using documents issued with this solicitation

a. In the event issues are found with the bearing, the FAA will provide written notification to the vendor detailing the nature of all deficiencies. FA bearing will then be returned to the vendor and they shall have two (2) weeks to remedy all deficiencies. Repaired FA bearing shall then be return shipped to FAA for Follow-Up inspection.

i. If FA bearing fails Follow-Up inspection, the FAA has the option to return the bearing for further remediation or possibly terminate the contract for cause

C. The FAA will provide written notification to vendor in the event the FA bearing passes all inspections/tests. This will serve as a Notice to Proceed (NTP) with fabrication of all remaining bearings required as per contract.

D. Remaining production bearings shall be delivered in accordance with the following schedule:

i. First production bearing shall be delivered three (3) months following receipt of NTP

ii. Any remaining bearings shall be delivered at a rate of one (1) bearing per month beginning four (4) months following receipt of NTP

iii. All bearings shall be packaged and shipped to be FAA in accordance with Provision 61, Rev D (see attached)

E. All bearings shipped to the FAA or returned to the Vendor for remediation/repair shall be FOB FAA, Freight Prepaid

4.0 Required Documents and Warranty

Vendor shall provide the following documentation and warranty for each bearing supplied:

A. All documentation noted in paragraph 2.0 above B. Certificate of Compliance denoting complete compliance with all requirements detailed in the Statement of Work and all other design documents attached to this solicitation

C. Each bearing shall be fully warranted for one (1) year following date of formal acceptance of each bearing. Formal acceptance shall be provided by the FAA Contracting Officer.