FAA PMA/TSO Lookup -

Introduction:
This catalog contains a current listing of "eligible" parts for which Rockwell Collins Commercial and Government Systems has received Federal Aviation Administration (FAA) Technical Standard Order (TSO) Approval, Parts Manufacturing Approval (PMA) or has received Direct Shipment Authorization from the Production Certificate (PC) holder (i.e., OEM). Piece parts and subassemblies that appear on this list are a part of a TSO, PMA or DSA article that was approved at a higher level, such as a top level unit, kit or aircraft.
Parts noted as Standard Parts (SP) are parts manufactured in complete compliance with an established Government or industry-accepted specification that contains design, manufacturing and uniform identification requirements, per FAA Advisory Circular AC 20-62( ).
This catalog has additional listings identified as "not eligible" and "European Technical Standard Order". The "not eligible" description means that the part identified is not used on a Rockwell Collins product that is FAA TSO/PMA approved or a product for which Rockwell Collins has not been granted DSA, and therefore is not eligible for an FAA Form 8130-3 Airworthiness Approval Tag. The "European Technical Standard Order" description means that the part identified only has a European approval and does not have FAA approval. Therefore, it is not eligible for an FAA Form 8130-3 Airworthiness Approval Tag.
Upon request, only products listed as "eligible" may have an FAA Form 8130-3 accompany shipment.

Note:
Installer is responsible for confirming that the product is eligible for installation.

This article meets the minimum performance and quality control standards required by a technical standard order (TSO). Installation of this article requires separate approval.
or
The conditions and tests required for TSO authorization of this hardware element are minimum performance standards. Those installing this hardware element either on or within a specific type or class of aircraft are responsible for determining that the installation conditions are within the TSO standards. This hardware element may be installed only if evaluation by the applicant (i.e., the user/installer) documents an acceptable installation per Title 14 of the Code of Federal Regulations part 43 (or the applicable airworthiness requirements) and is approved by the FAA Administrator.
or
The conditions and tests required for TSO approval of this appliance represent a minimum performance standard. It is the responsibility of those desiring to install the appliance on, or within, a specific, general class or type of aircraft to determine that the aircraft installation conditions are within the TSO standards. If not within the TSO standards, the appliance may be installed only if further evaluation documents an acceptable installation and is approved by the Administrator.
or
The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those desiring to install this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. If not within the TSO standards, the article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the Administrator.
or
The conditions and tests for TSO approval of this article are minimum performance standards. Those installing this article, on or in a specific type or class of aircraft, must determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The article may be installed only according to 14 CFR part 43 or the applicable airworthiness requirements.
or
The conditions and tests required for the TSO approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The article may be installed only if performed under 14 CFR Part 43 or the applicable airworthiness requirements.

Purpose:
To provide an up-to-date listing of Rockwell Collins Commercial and Government Systems FAA TSO/PMA approved and DSA parts.

For the purpose of utilizing this database, consider that Rockwell Collins has two basic Aviation product lines, those being, Avionics and In-Flight Entertainment. Due to acquisitions by Rockwell Collins, in the area of In-Flight Entertainment, some duplication of part numbers has occurred, within products utilizing a ten digit part numbering format (example: xxx-xxxx-xxx part numbers). If the part number, for which you are inquiring is a 10 digit format and is In-Flight Entertainment product, please enter the letters "RV" in front of the part number. The "RV" has been established as an internal alpha site code identifier to prevent you from receiving incorrect information regarding aircraft eligibility.