Supplier Quality (SQ) from Northrop Grumman Aeronautics Systems (NGAS) and the Strategic Space Systems Division (SSSD) and the Strategic Deterrent Systems (SDS) of the Space Sector (SP) maintain an "Approved Special Processor List" (ASPL) for all NGAS, SSSD and SDS programs. This list can be sorted by Supplier Name, Supplier Number, Country, or Process Specifications and Process Categories.

How to use the ASPL and the enclosed information is bulleted below:

  • Users must initially select the specific ASPL they are searching within (i.e. Aeronautics Systems, Strategic Space Systems, or Strategic Deterrent Systems). If you are unsure which ASPL to search please verify with your NG Buyer.
  • All specifications can be selected by selecting Specification (1st button), Category (2nd button), which includes 8 categories and Space Systems Division specifications, or F35 specifications under Program (3rd button).
  • At the Top RH side of the site is a “Helpful Links” button that has 8 links. See Below for 5 specific ones.
    • First two links are to Boeing’s ‘D1-4426’ ASPL and Lockheed’s ‘QCS-001’ ASPL.
    • Third is a “Change Log” that shows when processors are added or removed, or when specifications are added or removed from the processors or the ASPL.
    • The 4th and 5th are listings of NDT technique approvals; by “Processor and by Part Number”.
For any questions, contact:

Warning:    Northrop Grumman process specifications contain technical data whose export is restricted by the Arms Export Act (Title 22, U.S.C., Sec 2751 et seq.) or the Export Administration Act (Title 50, U.S.C., App. 24001-240). Violation of these export laws are subject to severe criminal penalties.

 


 
Applied Composite Technology Aerospace dba ACT Aerospace - NADCAP Approved
90044639
Manufacturer
425 E 400 N
Gunnison, UT 84634 United States
Phone: 435-528-7199
Fax:
Selected sector: AS

Specification
Process Description
Category
Process Specification for Sealing, Integral Fuel Tank and Fuel Cell Cavity
Finishes/Coatings
Limits:
Limits: Type II Faying Surface/ Seam and Joint Fillet Sealing Only. Not Approved or Appendix A (Ref: RC/I R432667 defines Qualification requirements)

Surface Preparation for Structural Adhesive Bonding
Chemical Processing
Limits:
Limited to Type I, Class A only

Surface Preparation for Structural Adhesive Bonding, Composites
Composites
Limits:
Limited to producing Epoxy parts. Ref. RCI 445148

Curing Procedures for Composite Laminates and Sandwich Assemblies
Composites
Limits:
Not approved for Appendix A

Process Specification Fabrication of Out-of-Autoclave, 350°F Cure, Epoxy Laminates
Composites
Limits:
Limits: None NGAS M&P (B. Marino) confirmed that all room temperature qualification testing has been completed.

Machining of Nonmetallic Honeycomb Details
Composites
Limits:
Limits: Not approved for Application of Removable Stabilization Material for Machining (Ref: para. 3.3.5.2) Not approved for Appendix A

Process Specification for Fabrication Of 350°F Curing Out-Of-Autoclave Epoxy Composite Structure, Bonded, Cocured, Or Cobonded
Composites
Limits:
Limits: None NGAS M&P (B. Marino) confirmed that all room temperature qualification testing has been completed Ref RC/I’s R429930, R431982

Process Specification for Fabrication of Secondarily Bonded Structure Using Low Vacuum
Composites
Limits:
None

Installing Inserts, Hardpoints, and Edge Filler in Composite Sandwich Structure
Composites
Limits:
None

Hole Preparation, Drilling, Mach.,Trimming for Composite/Metallic Structure
Composites
Limits:
Not approved for Appendix A,B & C

Process Specification for Contamination Free Hole Preparation, Drilling, Machining and Trimming of Composites and Composite/Metallic Structures
Composites
Limits:
None

Ultrasonic Inspection of Composites and Bonded Assemblies
Non-Destructive Testing
Limits:
Not approved for Appendix A & B

Non-Destructive Inspection of Composite Structures
Non-Destructive Testing
Limits:
None

Area Requirements for Composite Fabrication
Composites
Limits:
Limits: Limited to Areas; C, D and E only Not Approved for Appendix A & B