STC SA1-368

Supplemental type certificate · D'Shannon Products Ltd.

Holder
D'Shannon Products Ltd. · United States
Status
Current · Reissued
Status date
August 16, 2011
Applied
July 15, 1959
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 auxiliary wing tip fuel tanks in accordance with Safe Flight Extenders Company s Manual SFE-35(III) dated July 15, 1959, Tip Tank Installation, Type III Kit, utilizing parts listed on Bamber Wing Tanks Type III Kit Contents dated July 15, 1959. This wing tip tank installation may be used in combination with either the wing auxiliary tanks or a baggage auxiliary tank, but not when both are installed. Complete installed weight empty is 23.7 lb. at 89.1 inches. The CG of the tip fuel is 87.0 inches.

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.

Installation of auxiliary wing tip fuel tanks in accordance with Safe Flight Extenders Company’s Manual SFE-35(III) dated July 15, 1959, “Tip Tank Installation, Type III Kit,” utilizing parts listed on “Bamber Wing Tanks Type III Kit Contents” dated July 15, 1959.

This wing tip tank installation may be used in combination with either the wing auxiliary tanks or a baggage auxiliary tank, but not when both are installed. Complete installed weight empty is 23.7 lb. at 89.1 inches. The CG of the tip fuel is 87.0 inches.

An individual Airplane Flight Manual Supplement dated August 3, 1959 for A35 through G35 and H35 is required.

D’Shannon Products, Ltd.

1309 County Road 134 Buffalo, MN 55313 Original Product --Type Certificate Number: A777 and 3A15 Make: Beech Model : A35 thru G35 and H35 Date reissued : August 27, 1968, August 8, 1973, October 3, 1973; February 14, 1975 August 16, 2011 Date amended :

( Signature)

Melvin D. Taylor, Manager Atlanta Aircraft Certification Office

( Title) Date of application : July 15, 1959

Date of issuance : August 3, 1959

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(10-68) PAGE 3 of 4 PAGES United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA1-368 Date: August 8, 1973, October 3, 1973, February 14, 1975 August 16, 2011 Supplemental Type Certificate Addendum No. SA1-368 The following placards must be displayed in full view of the pilot:

"TRANSFER TIP TANK FUEL IN LEVEL FLIGHT ONLY. TIP TANK QUANTITY 24 GALLONS.”

MODEL A35 and B35

Safe Flight Extenders Airplane Flight Manual Supplement dated August 3, 1959 is required.

Placard in full view of pilot:

“GROSS WEIGHT LIMITED TO 2506 POUNDS WITH WING TIP TANKS EMPTY. ALL ADDITIONAL WEIGHT MUST BE WING TIP FUEL.”

“REAR C.G. AT ALL TIME 84.4 INCHES.”

MODEL C35

Safe Flight Extenders Airplane Flight Manual Supplement dated August 3, 1959 is required.

Placard in full view of pilot:

“GROSS WEIGHT LIMITED TO 2556 POUNDS WITH WING TIP TANKS EMPTY. ALL ADDITIONAL WEIGHT MUST BE WING TIP FUEL.”

“REAR C.G. AT ALL TIME 84.4 INCHES.”

MODEL D35

Safe Flight Extenders Airplane Flight Manual Supplement dated August 3, 1959 is required.

Placard in full view of pilot:

“GROSS WEIGHT LIMITED TO 2581 POUNDS WITH WING TIP TANKS EMPTY. ALL ADDITIONAL WEIGHT MUST BE WING TIP FUEL.”

“REAR C.G. AT ALL TIME 84.3 INCHES.”

MODEL E35

Safe Flight Extenders Airplane Flight Manual Supplement dated August 3, 1959 is required.

Placard in full view of pilot:

“GROSS WEIGHT LIMITED TO 2581 POUNDS WITH WING TIP TANKS EMPTY. ALL ADDITIONAL WEIGHT MUST BE WING TIP FUEL.”

“REAR C.G. AT ALL TIME 84.9 INCHES.”

FAA FORM 8110-2(10-68) PAGE 4 of 4 PAGES United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA1-368 Date: August 8, 1973, October 3, 1973, February 14, 1975 August 16, 2011 Supplemental Type Certificate Addendum No. SA1-368 MODEL F35

Safe Flight Extenders Airplane Flight Manual Supplement dated August 3, 1959 is required.

Placard in full view of pilot:

“GROSS WEIGHT LIMITED TO 2606 POUNDS WITH WING TIP TANKS EMPTY. ALL ADDITIONAL WEIGHT MUST BE WING TIP FUEL.”

“REAR C.G. AT ALL TIME 84.9 INCHES.”

MODEL G35

Safe Flight Extenders Airplane Flight Manual Supplement dated August 3, 1959 is required.

Placard in full view of pilot:

“GROSS WEIGHT LIMITED TO 2631 POUNDS WITH WING TIP TANKS EMPTY. ALL ADDITIONAL WEIGHT MUST BE WING TIP FUEL.”

“REAR C.G. AT ALL TIME 84.9 INCHES.”

MODEL H35

Safe Flight Extenders Airplane Flight Manual Supplement dated August 3, 1959 is required.

Placard in full view of pilot:

“GROSS WEIGHT LIMITED TO 2756 POUNDS WITH WING TIP TANKS EMPTY. ALL ADDITIONAL WEIGHT MUST BE WING TIP FUEL.”

“REAR C.G. AT ALL TIME 84.7 INCHES.”

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 · 8

MakeModelData sheet
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