STC SA561WE

Supplemental type certificate · Robertson Lorene E

Holder
Robertson Lorene E · United States
Status
Current · Reissued
Status date
June 20, 2003
Applied
November 15, 1963
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheets
TCDS3A13TCDS5A6

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

What it approves

12.7-gallon auxiliary fuel tank.

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.

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.”

ADs that name this STC · 0

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No AD in this release names this STC

Approved models · 14

MakeModelData sheet
The Cessna Aircraft Company1805A6
The Cessna Aircraft Company180A5A6
The Cessna Aircraft Company180B5A6
The Cessna Aircraft Company180C5A6
The Cessna Aircraft Company180D5A6
The Cessna Aircraft Company180E5A6
The Cessna Aircraft Company180F5A6
The Cessna Aircraft Company1823A13
The Cessna Aircraft Company182A3A13
The Cessna Aircraft Company182B3A13
The Cessna Aircraft Company182C3A13
The Cessna Aircraft Company182D3A13
The Cessna Aircraft Company182E3A13
The Cessna Aircraft Company182F3A13