RFQ_80NSSC18Q0491_-_Left_Wing_Attach_Corrosion_Repair_SOW.pdf
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- Attached to
- Corrosion repair on the GIII 808
- Solicitation number
- 80NSSC18Q0491
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Solicitation# 80NSSC18Q0491 - SOW (Part 1)
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| RFQ_80NSSC18Q0491_-_808_Excel_Due_list.pdf |
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Text version
RFP #
STATEMENT OF WORK
NASA 808 Corrosion Repair and Scheduled Maintenance
Armstrong Flight Research Center
Date: April 29, 2018
National Aeronautics and Space Administration Armstrong Flight Research Center Edwards, California
RFP/Contract No. Sonic Booms in Atmospheric Turbulence (SonicBAT) Date or Version #
Table of Contents
1.0 Background
2.0 Objectives
3.0 Scope
4.0 Requirements
5.0 Deliverables
6.0 Government-Furnished Property (GFP)
7.0 Security Considerations
8.0 Travel
9.0 Special Material Requirements
10.0 Place of performance
11.0 Period of performance
1.0 Background
Armstrong Flight Research Center (AFRC) operates a Gulfstream III aircraft, G-1159A, tail number N808NA (N94FL), serial number 424. During recent non-destructive inspections, corrosion was found in the left aft inboard wing to fuselage attachment referenced in the Gulfstream Computerized Maintenance Program (CMP) task item 575720. Gulfstream Technical Operations has confirmed that the attachment fitting must be repaired according to Airframe Service Change (ASC) 229. The repair involves shoring the aircraft and a significant amount of time to complete. In addition, the contract agency is expected to perform scheduled maintenance tasks as defined in the attachments.
2.0 Objectives
2.1 Complete the corrosion repair specified by Airframe Service Change (ASC) 229
2.2 Complete scheduled maintenance tasks as defined in the attachments
3.0 Scope
The NASA 808 aircraft shall be returned to normal service with a repaired left wing to fuselage attachment fitting and completed maintenance tasks.
4.0 Requirements
4.1 Repair the left aft inboard wing to fuselage attachment according to ASC-229.
4.2 After performing the required repairs and scheduled maintenance tasks the contractor shall restore the aircraft to a flyable state. This includes reinstallation, operational checks and leak checks of removed panels and aircraft systems, log book entries, return to service authorizations, and any other required closeout tasks.
RFP/Contract No. SOW Title
4.3 The work necessary to complete ASC-229 and scheduled maintenance tasks shall be performed at the contractor’s facility. This includes any work necessary to prepare the aircraft for access to the corroded area involving removal and replacement of panels and any aircraft hardware or components blocking necessary access.
4.4 The contractor must allow NASA designated personnel including inspectors, aircraft maintenance personnel, and other technical experts to observe the work at any time. NASA designated personnel may include employees of NASA and employees of NASA Armstrong support contractors.
4.5 The contractor shall allow NASA to maintain the presence of at least one designated person on-site at the contractor facility throughout the course of the work.
4.6 Contractor must notify NASA designated inspector at the following progress points for inspection/witnessing:
4.6.1 After the corroded attachment fitting has been removed
4.6.2 Immediately prior to installing the new attachment fitting
4.6.3 Before & during reinstallation of aircraft hardware or components whose removal was required to access the repair area
4.6.4 During any scheduled maintenance task for which inspection of work is normally required
4.7 The contractor shall immediately notify the on-site NASA designated personnel should any unknown conditions be found requiring repair outside the original scope of this contract.
4.7.1 The on-site NASA designated personnel shall coordinate with the Contractor and relevant NASA Armstrong offices to develop a disposition plan for the additional repair and to secure authorization for any additional required work.
4.7.2 Under no circumstances should the Contractor perform work outside the original scope of this contract without the express authorization of the NASA Contracting Officer.
4.8 Contractor must be an FAA certified 14 CFR PART 145 FAA Repair Station
5.0 Deliverables
5.1 Contractor shall provide an airworthy aircraft with the left aft inboard wing to fuselage attachment free of corrosion
5.2 Contractor shall provide material certification records for any fasteners
5.3 Contractor shall provide the original, corroded left aft inboard wing to fuselage attachment hardware
5.4 Contractor shall provide all records associated with completion of scheduled maintenance tasks as listed by the Gulfstream CMP
5.5 Contractor shall provide all records associated with completion of ASC-229
5.6 Contractor shall provide completed FAA 8100-9 record for a major repair indicating the corroded part was replaced according to ASC-229
6.0 Government-Furnished Property, Material, Equipment, or Information (GFP, GFM, GFE, or
GFI)
The Government shall provide the following to the Contractor:
6.1 The ASC-229 documentation
6.2 List of scheduled maintenance tasks to be performed from the Gulfstream Computerized
Maintenance Program (CMP)
RFP/Contract No. SOW Title
6.3 The GIII aircraft at the contractor location for repair
7.0 Security
All data under this project shall be unclassified and not subject to ITAR or EAR restrictions, as verified by NASA Headquarters Security through the Department of Defense.
8.0 Travel
No contractor travel is expected during the course of this contract.
9.0 Special Material Requirements
There are no special materials required. The contractor is expected to provide all assets necessary to complete the listed tasks in this statement of work.
10.0 Place of Performance
All repair and maintenance work shall be performed at the contractor repair facilities.
11.0 Period of Performance
The provided list of scheduled maintenance tasks come due in late April. The projected period of performance may begin as early as April 23rd to accommodate the calendar maintenance. Beginning work as close as possible to April 23rd is preferred to avoid having the aircraft in an unusable state. All work is expected to be complete within 6 weeks from delivery of aircraft to repair facility.
| 1.0 Background |
| 2.0 Objectives |
| 3.0 Scope |
| 4.0 Requirements |
| 5.0 Deliverables |
| 6.0 Government-Furnished Property, Material, Equipment, or Information (GFP, GFM, GFE, or GFI) |
| 7.0 Security |
| 8.0 Travel |
| 9.0 Special Material Requirements |
| 10.0 Place of Performance |
| 11.0 Period of Performance |
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