# STC SA2687WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: ROBERTSON FUEL SYSTEMS LLC, United States
- Description: Installation of protective device on fuel tank vent line.
- Applied: April 10, 1973
- Status date: July 19, 2011
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19)
- Certificate PDF: https://openairdocs.org/files/sha256/b3/db/b3db069595693c691d825964b6cc7cd777cab5741bf13f54fee8f4c253940c3b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/94F60CC9823C506A862578E2004B4506.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2687WE

## ADs that name it (0)

None.

## Approved models (9)

- Cessna Aircraft Company 150C ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150D ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150E ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150F ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150G ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150H ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150J ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150K ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150L ([TCDS 3A19](https://openairdocs.org/tcds/3A19))

## 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 ROBERTSON FUEL SYSTEMS LLC 800 West Carver Road, Suite 101 Tempe, Arizona 85284 Part 3 of the Civil Air Regulations.

3A19

Cessna

150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L Description of Type Design Change: Installation of protective device on fuel tank vent line in accordance with FAA approved drawings RE 000 102 and RE 000 103, or later approved revisions.

Limitations and Conditions: The approval of this change should not be extended to other aircraft on this model on which other previously approved modificati on are incorporated in any aircraft unless it is determined that the interrelationship between this inst allation 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, th e holder shall give the other person written evidence of that permission.

Date of application : April 10, 1973

Date of issuance : May 17, 1973

Date reissued : June 28, 2006, July 19, 2011

( Signature) Haifa Haj-Eid Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- July 19, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b3/db/b3db069595693c691d825964b6cc7cd777cab5741bf13f54fee8f4c253940c3b)

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