# STC SA561WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Robertson Lorene E, United States
- Description: 12.7-gallon auxiliary fuel tank.
- Applied: November 15, 1963
- Status date: June 20, 2003
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 5A6](https://openairdocs.org/tcds/5A6)
- Certificate PDF: https://openairdocs.org/files/sha256/bf/69/bf6967cdc3ab68082a67f63472eb5dbcedcaed3f4818df699003afb5b7b981ed
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2282B559217DA8CE86256D8A006C28AC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA561WE

## ADs that name it (0)

None.

## Approved models (14)

- The Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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.

Number SA561WE

This Certificate issued to Lorene E. Robertson 106 Lindbergh Ct.

Dayton, Nevada 89403-8807 Part CAR 3 of the Civil Air Regulations.

See AML #SA561WE See AML #SA561WE See AML #SA561WE Description of Type Design Change: Installation of 12.7-gallon auxiliary fuel tank in accordance with Aircraft Modification and Repair drawings dated February 10, 1963, sheets 1 thru 4, and supplemental drawing for Cessna 182E and F. FAA Approved Airplane Flight Manual Supplement dated December 11, 1963 is required for the Cessna 180, 180A and 180B airplanes Limitations and Conditions: This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. 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. See Page 3 for Operating Limitations.

Date of application : November 15, 1963

Date of issuance : December, 12, 1963

Date reissued : July 1, 1964, June 20, 2003

( Signature) Manager, 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 SA561WE

**OPERATING LIMITATIONS**

Placards Required:

A. The following fuel system placard is required in full view of the pilot:

“AUXILIARY FUEL TRANSFER PROCEDURE:

**1. TRANSFER IS NOT TO BE INITIATED UNTIL RIGHT TANK INDICATES ONE-HALF FULL.**

**2. FUEL TRANSFER IS TO BE CONDUCTED IN LEVEL FLIGHT ONLY. THE**

**FUEL TRANSFER BLUE WARNING LIGHT WILL BE ON DURING TRANSFER.**

**3. THE MAIN FUEL VALVE IS TO BE ON THE LEFT TANK PRIOR TO AND DURING FUEL TRANSFER.**

4. UNUSABLE AUXILIARY FUEL IS 2/3 GALLON (4 POUNDS).”

B. The following placard is required at the baggage compartment (all models except Cessna 182E and F):

“MAXIMUM BAGGAGE ALLOWABLE FOR OPERATION WITH AUXILIARY FUEL ON BOARD 40 POUNDS.”

C. The following placard is required at the baggage compartment, Cessna 182E and F:

“1. MAXIMUM BAGGAGE WITH TANK EMPTY IS 106.5 POUNDS.

2. MAXIMUM BAGGAGE WITH TANK FULL IS 30 POUNDS.”

D. The following placard is required at fuel tank filler cap:

“12.7 GALLONS 80/87 GRADE.”

## Every issue (1)

- June 20, 2003: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/bf/69/bf6967cdc3ab68082a67f63472eb5dbcedcaed3f4818df699003afb5b7b981ed)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.