Colonel Saunders, sorry but you don't have a clue. Yes, everyone uses parts from Aircaft Spruce but as my post stated they often give the buyer an option buy parts with no 8130-3 form. From their website:
Aircraft Spruce provides you with its own Certificate of Conformance for our products at no charge. This is noted on every invoice. Factory certification and test reports are available on some items and 8130 Forms are available on FAA approved products. A cost of $25-$100 per product is charged to secure these forms.
Please inquire at time of order if test reports/8130 Forms are available for the items you are ordering. If available, the forms must be requested at time of order and the product must be special-ordered from the factory with the forms. These forms cannot be furnished after you receive the product. Anticipate shipping delays if 8130 Forms are requested.
Do not order products using catalog part number if you require 8130 forms, as you will receive standard parts without the form. Simply describe the part and specifically request Form 8130. Due to delays and costs involved in furnishing these forms, we strongly suggest that you check to see if the Aircraft Spruce Certificate of Conformance will be acceptable in lieu of Form 8130.
So that means that unless specifically requested, you will receive parts that may as well have fallen off the back of a truck....on it's way to Walmart.
And for your information and the benefit of others:
571.07 Installation of New Parts
Information Note:
The definitions of ‘commercial part’ and ‘standard part’ set out in Subpart 101 of the CARs apply to this Standard and are reproduced below for convenience only.
(amended 2002/03/01; no previous version)
“commercial part”, in respect of an aircraft, means a part
(amended 2002/03/01; no previous version)
(a) that is not specifically designed or produced for use as an aeronautical product,
(b) that is made to a specification or catalogue description and marked under an identification scheme of the maker, and
(c) whose failure does not adversely affect the continued safe flight and take-off and landing of the aircraft; (pièce commerciale)
“standard part”, in respect of an aircraft, means a part manufactured in conformity with a specification that
(amended 2002/03/01; no previous version)
(a) is established, published and maintained by an organization setting consensus standards or by a government agency, and
(b) includes design, manufacturing, test and acceptance criteria and identification requirements; (pièce standard)
The standards of airworthiness applicable to the installation of new parts are as follows:
(a) The requirements detailed in section 571.13 of this standard are met;
Information Note:
Parts and bulk materials provided under this provision do not require an airworthiness certification, but must be identified or be identifiable, through a part number, shipping document, etc.
(b)Parts that were not originally intended for aeronautical use (e.g. automotive voltage regulators, electronic components, air filters), providing the original manufacturer’s part number is shown in the parts list of the next or subsequent higher assembly. Where the original manufacturer’s part number is not shown in a parts list, other data authorised by type design, such as data approved under a supplemental type certificate are to be consulted.
(amended 2009/12/01; previous version)
Information Note:
(i) The person installing a replacement electronic component is responsible for ensuring that the replacement part meets the correct tolerance required by the type design. This information can usually be obtained from either a colour code or markings on the original part, or the illustrated parts catalogue of a higher assembly.
(ii) The part may be:
(amended 2002/03/01; no previous version)
(a) a standard electrical or electronic part, that requires additional processing before it can be used in the intended application;
(b) produced in conformance with a specification published and maintained by a consensus standards organization, a government agency, a holder of a type certificate or in conformance with the manufacturer's internal specifications and standards.
(amended 2009/12/01; previous version)
(iii) The specification may include manufacturing controls, quality and reliability test methods, acceptance criteria, and identification requirements. It does not include electrical parameters and test methods which are obtained from the supplier's data sheet. The part is used within the manufacturer's published operating characteristics and environmental ranges.
(amended 2002/03/01; no previous version)
(c) Parts produced pursuant to an FAA Parts Manufacturer approval (PMA) are eligible for installation on a Canadian aircraft or on an aeronautical product intended for installation on a Canadian aircraft provided that:
(amended 2009/12/01; previous version)
(i) the parts are marked in accordance with the part marking requirements set out by the FAA; and
(amended 2009/12/01; previous version)
(ii) the parts are accompanied by an authorized release certificate which certifies the parts conform to the applicable design data approved by the FAA or the Minister and indicates the aeronautical product for which they are eligible.
(amended 2009/12/01; previous version)