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includes but is not limited to:
• Accomplishment of physical inspections
• Witnessing of installation of critical assemblies
• Witnessing of functional tests
• Verification of company conformity through documented evidence (i.e., Material certifications, special process
certifications, shop travelers, work orders).
270.3 Conformity Plan Requirements*
The Supplier shall provide a Conformity Plan that:
• Defines how the company conformity will be completed.
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• Provides a schedule of when parts will be available.
• Identifies where the parts will be FAA conformed.
• Identifies who will perform the conformities. (FAA, FCAA, DAR)
The Conformity Plan shall be approved by the Honeywell Supplier Quality Assurance Manager of the procuring site.
Revisions: Edited for clarity. Approval of the Conformity Plan clarified Para 270.3.
*Revised / **Added
SPOC 273 – NASA Required Notification *
273.1 Scope
NASA required notification in procurement documentation.
273.2 Requirements
Purchase requests, Purchase Orders, contracts, and subcontracts covering the procurement of flight hardware items
for use in manned spacecraft shall contain the two blocks of text shown below either printed, stamped, or added in
boldface type. All Honeywell subcontractors and all of their subcontractors, including their lowest tier subcontractors
shall include these blocks in all of their procurement documentation:
• “NOTE: For use in manned space flight. Materials, manufacturing, and workmanship of highest quality
standards are essential to astronaut safety. If the supplier is able to supply the desired item with a quality which
is higher than that of the items specified or proposed, the Supplier is requested to bring this fact to the
immediate attention of the purchaser."
• "For all Space Station Freedom hardware, random and systematic errors in any article or material measurement
shall not exceed 10 percent of the tolerance of the article or material being measured. Authorization for
exceptions shall be requested from Honeywell Aerospace Equipment Systems. Random and systematic errors
in any calibration measurement shall not exceed 25 percent of the tolerance of the parameter being measured.
Authorization for exceptions shall be requested from Honeywell Aerospace Equipment Systems. Certification of
conformance to these requirements shall be provided with each shipment of product. These requirements shall
be flowed down to all Sub-Tier Suppliers.”
Revisions: Title changed.
SPOC 275 – NASA Source Inspection Required – CANCELLED
Revisions: SPOC cancelled. Content moved to SPOC 179.
Aerospace
Supplemental Purchase Order Conditions (SPOC) Manual
UNCONTROLLED IN HARDCOPY
Revision H Effective Date: 15 January 2009 66
SPOC 276 – NASA Product Requirements
276.1 Scope
NASA product requirements for Manned Space Flight.
276.2 Purchase Order Requirements
For Purchase Orders involving product for Manned Space Flight: materials, manufacturing, processes and
workmanship of the highest quality standards are essential to Manned Space Flight safety. If the Supplier or its Sub-
Tier Suppliers can provide a higher standard of quality than requested in this purchase order and associated SPOCs,
the Supplier must bring this information to the attention of the buyer.
The Supplier and its Sub-Tier Suppliers must be approved by Honeywell.
Supplier’s certifications (i.e., material, controlled process, etc.) including those of Supplier’s Sub-Tier Suppliers, in
support of this order shall provide an auditable trail back to the Honeywell Purchase Order.
Soldering operations for manned space flight applications must conform to NASA's soldering requirements specified in
NHB 5300.4(3A-1), unless otherwise noted in the specification control or source control drawing. Evidence of solder
operation performance must appear on the packing slip and certificate of conformance for products shipped.
There will be no change in the design of the part, in the material and processes, in its construction or in the
manufacturer's part number after the first acceptable unit has been received by Honeywell unless requested and/or
approved by Honeywell in writing.
Parts and materials which have been permanently installed in an assembly using soldering, alloying, or other fusing
techniques, and are then removed from the assembly for any reason shall not be used again in any flight hardware
without specific written approval from Honeywell.
　
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