STC SA3207NM

Supplemental type certificate · ROBERTSON FUEL SYSTEMS LLC

Holder
ROBERTSON FUEL SYSTEMS LLC · United States
Status
Current · Reissued
Status date
July 19, 2011
Applied
July 29, 1981
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDSA4CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of an automatic fuel spillage valve to improve crashworthiness.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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.

A4CE Cessna

See Page 3 Description of Type Design Change : Installation of an automatic fuel spillage valve to improve crashworthiness in accordance with Robertson Avia tion FAA approved Master Drawing List No. MDL- C206 dated September 23, 1985, or later FAA approve d revisions. For airplane flight manual (AFM) requirements see continuation on page 3.

Limitations and Conditions : The approval of this change in type design applies to the basic aircraft of the specified model that is otherwise unmodified. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder sh all give the other person written evidence of that permission.

Date of application : July 29, 1981

Date of issuance : November 27, 1985

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

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

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.

Number SA3207NM

MODEL: 206, P206, P206A, P206B, P206C, P206D, P 206E, U206, U206A, U 206B, U206C, U206D, U206E, U206F, U206G, TP206A, TP206B, TP206C , TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G

Description of Type Design Change: continued:

For Cessna Models 206, P206, P206A, P206B, P 206C, P206D, P206E, U206, U206A, U206B, U206C, TU206D, TU206E, TU206F, TU206G (S/N 676, 206-0012 through 206-0275, U206-0276 through U20604649, except U20602589, P206-0001 through P20600647), Robertson Aviation, Inc. Supplement AFM No. 1 dated November 27, 1985, or later FAA approved revisions is required.

For Cessna Models U206G and TU206G (S/N U20602589 and U20604650 and up), Robertson Aviation Inc.

Pilots Operating Handbook and FAA Approved Flight Manual Supplement No. 1 to Cessna Models U206G or TU206G Airplane OPH-AM, November 27, 1985, or later FAA approved revisions are required.

-END-

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Approved models · 26

MakeModelData sheet
Cessna Aircraft Company206A4CE
Cessna Aircraft CompanyP206A4CE
Cessna Aircraft CompanyP206AA4CE
See all 26 models