STC SA28EA

Supplemental type certificate · D'Shannon Products Ltd.

Holder
D'Shannon Products Ltd. · United States
Status
Current · Reissued
Status date
August 16, 2011
Applied
November 20, 1961
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23

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

What it approves

Installation of 12-gallon fiberglass wing tip fuel tanks.

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

Part 23 / Car 3 of the Regulations.

Configuration 1

Installation of 12 gallon fiberglass wing tip fuel tanks RB1-100, Revision L, (Serial Numbers 5000 and up; 135 to 186), and fuel system in accordance with Flight Extenders Inc. Installation Instructions RB1-201 dated June 15, 1962, and Drawing RB1-201A, (FEI Change Notice No. 1 dated 3-16-63) for Beech Model 35 only.

D’Shannon Products, Ltd.

1309 County Road 134 Buffalo, MN 55313

Original Product --Type Certificate Number: 3A15 Models H35, J35, K35, M35 35-33 A777 Models 35 & A35 thru G35 Incl.

Make: Beech Model : 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, 35-33 Date reissued : August 27, 1968, August 8, 1973, October 3, 1973; February 14, 1975 August 16, 2011 Date amended : December 17, 1962; April 4, 1963

( Signature)

Melvin D. Taylor, Manager Atlanta Aircraft Certification Office

( Title)

Date of application : November 20, 1961

Date of issuance : April 30, 1962

INSTRUCTIONS: Thc transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.

The FAA will reissue the certifi cate in the name of the tran sferee and forward it to him.

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (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)

Signature of grantor (In ink):

FAA FORM 8110-2-1(10-69) PAGE 3 of 5 PAGES

(Continuation Sheet) Number SA28EA Date: August 8, 1973, October 3, 1973, February 14, 1975 August 16, 2011 Supplemental Type Certificate Addendum No. SA28EA Installation of 13.5 gallon fiberglass wing tip fuel tanks RB1-100, Revision L, (Serial Numbers 135 to and including 186) in accordance with Flight Extenders Installation Instructions Manual FEI-35(V) dated April 9, 1962, and (FEI Engineering Change Notice No. 1 dated 3-16-63) for all models as listed herein excluding Beech Model 35.

Configuration 2 FAA Approved “Flight Extenders, Inc. Service Bulletin No. 1” dated March 25, 1963, increases RB1-100 wing tip tanks fuel capacity from 13.5 gallons to 14.7 gallons for Beech Models as listed herein, excluding Beech Model 35, upon which are installed Flight Extenders Inc. RB1-100 wing tip tanks, Serial Numbers 100 to and including 186.

Configuration 3 Beech Models affected: All beech Models listed herein, excluding Beech Model 35.

Installation of 15 gallon fiberglass wing tip fuel tanks RB2-100, Revision B, dated 1-10-63, (FEI Engineering Change Notice No. 1 dated 3-16-63) for tank serial numbers 187 and up, and fuel system in accordance with Extenders, Inc.

Installation Instructions Manual FEI-35(V) – “Tip Tank Installation Type V Kit, “ Revision A, dated March 25, 1963, and Installation Drawing RB1-101, Revision E, dated 3-11-63 (FEI Engineering Change Notice No. 1 dated 3-16-63) and Bill of Materials RB1-101, Revision RB1-101, Revision 3-11-63.

Limitations and Conditions (Continued)

A. Complete installed empty weight increase is 23.7 pounds at 89.1 inches from datum-aft

B. The center of gravity of wing tip fuel is 87 inches from datum-aft

C. The following weight and center of gravity limitations are to be placarded in full view of the pilot as applicable to the particular Model:

Allowable Gross Weight With Empty Fiberglass Tanks. All Weight in Excess of this Amount Must be in Wing Tip Fuel

Model

Rear C.G. at all Weights (Inches Aft of Datum) 2488 A35, B35 84.4 2538 C35 84.4 2563 D35 84.3 2563 E35 84.9 2588 F35 84.9 2613 G35 84.9 2738 H35, J35 84.7 2788 K35, N35 84.7 2738 35-33 84.7 2435 35 Normal 84.8

FAA FORM 8110-2-1(10-69) PAGE 3 of 5 PAGES

2010 35 Utility 84.6

FAA FORM 8110-2(10-68) PAGE 4 of 4 PAGES (Continuation Sheet) Number SA28EA Date: August 8, 1973, October 3, 1973, February 14, 1975 August 16, 2011 Supplemental Type Certificate Addendum No. SA28EA D. Configuration 1 Airplane Flight Manual Supplement dated April 30, 1962 is required for each Model (the 12 and 13.5 gal. wing tip tank installation not eligible with fuselage tanks).

Configuration 2 Airplane Flight Manual Supplement dated March 29, 1963 is required for each Model when the RB1-100 wing tip tanks are modified in accordance with Flight Extenders, Inc. Service Bulletin No. 1” dated March 25, 1963. (The modified 14.7 gal wing tip tank installation not eligible with fuselage tanks). Beech Model 35 not eligible for this configuration.

Configuration 3 Airplane Flight Manual Supplement dated April 2, 1963 is required for each Model (the 15 gal. wing tip tank installation not eligible with fuselage tanks). Beech Model 35 not eligible for this configuration.

-END-

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 13

MakeModelData sheet
Hawker Beechcraft Corporation35A-777
Hawker Beechcraft Corporation35-333A15
Hawker Beechcraft CorporationA35A-777
Hawker Beechcraft CorporationB35A-777
Hawker Beechcraft CorporationC35A-777
Hawker Beechcraft CorporationD35A-777
Hawker Beechcraft CorporationE35A-777
Hawker Beechcraft CorporationF35A-777
Hawker Beechcraft CorporationG35A-777
Hawker Beechcraft CorporationH353A15
Hawker Beechcraft CorporationJ353A15
Hawker Beechcraft CorporationK353A15
Hawker Beechcraft CorporationM353A15