# STC ST00301LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rockwell Collins Inc., United States
- Description: Installation of flush/fill line Nipple Valve Assembly P/N 062-0009-( ) {DL 0062-0009 Rev -, dtd 8/29/96 or later FAA Approved Revision}.
- Applied: August 2, 1996
- Status date: November 17, 2011
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/09/fe/09fee2ba2b38a273d7d5301a678207396bee6d69e974468f96b060917de09cfd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0CCA9838981D23F386257989005C0136.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00301LA

## ADs that name it (0)

None.

## Approved models (6)

- The Boeing Company 737-100 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-200 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-200C Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-300 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-400 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-500 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

This Certificate issued to Rockwell Collins, Inc.

2642 Michelle Drive Tustin, CA 92780 Part 25 of the Federal Aviation Regulations.

[For Certification Basis see Type Certificate Data Sheet A16WE.] Original Product Type Certificate Number :

A16WE Boeing 737-100, -200, -200C, -300, -400, -500 Series Description of Type Design Change: Installation of flush/fill line Nipple Valve Assembly P/N 0062- 0009-( ) {DL 0062-0009 Rev. “-“, dated August 29, 1996 or later FAA approved revision}in accordance with Service Bulletin No. 96-132-SB/9030-38-42 dated August 15, 1996 or later FAA approved revisions.

Limitations and Conditions: This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: August 2, 1996

Date of issuance: December 18, 1996

Date reissued: December 7, 2005; November 17, 2011

( Signature)

Manager, Cabin Safety, Mechanical & Environmental Systems Branch Los Angeles Aircraft Certification Office

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

## Every issue (2)

- November 17, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/09/fe/09fee2ba2b38a273d7d5301a678207396bee6d69e974468f96b060917de09cfd)
- December 7, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/84/99/8499cba18b577adc7b96cf6ed16aae781b0cb4191e0d01816d66e4f08bf2c0aa)

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