Skip to content
Fuel systems

STC SA808SO

FAA DRS lists SA808SO as Current · Reissued, held by D'Shannon Products Ltd., for Hawker Beechcraft 35-C33, Hawker Beechcraft 36, and Hawker Beechcraft A36, and 18 more aircraft configurations. Recorded change: Installation of Beryl D Shannon Aviation Specialists, Inc., Fiberglass tip tanks (15 gallons each) and fuel transfer system in accordance with Beryl D Shannon Aviation Specialists, Inc., Installation Kit Drawing KB1401, Rev E, dated May 19, 1977, or later FAA approved revisions. Drawing KB1401 Revision F, dated April 12, 1979, includes optional wing-tip anti-collision light installation. This STC requires operation in the Normal Category. Snapshot dated June 30, 2026.

FAA-listed holder
D'Shannon Products Ltd.
Aircraft configurations
21
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

SA808SO identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.

Applicability

Aircraft named in FAA DRS

Named aircraft: Hawker Beechcraft 35-C33, Hawker Beechcraft 36, and Hawker Beechcraft A36, and 18 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Hawker Beechcraft 35-C333A15Hawker Beechcraft 363A15Hawker Beechcraft A363A15Hawker Beechcraft A36TC3A15Hawker Beechcraft E333A15Hawker Beechcraft F333A15Hawker Beechcraft F33A3A15Hawker Beechcraft F33C3A15Hawker Beechcraft G333A15Hawker Beechcraft V353A15Hawker Beechcraft V35A3A15Hawker Beechcraft V35B3A15Hawker Beechcraft 35A-777Hawker Beechcraft 35RA-777Hawker Beechcraft A35A-777Hawker Beechcraft B35A-777Hawker Beechcraft C35A-777Hawker Beechcraft D35A-777Hawker Beechcraft E35A-777Hawker Beechcraft F35A-777Hawker Beechcraft G35A-777

Buyer checks

Confirm before sourcing

Related fuel systems STCs

SA876EAFuel systems

1. Models LA-4-200, LA-4, LA-4A, LA-4P: Installation of Auxiliary Fuel System in accordance with Aerofab Drawings No. 180004, Rev. G, dated June 8, 1971, and 180009, Rev. D, dated February 10, 1971. 2. Model LA-4-200: Increase of Gross Weight to 2690 pounds. Limitations and Conditions (Continued): (b) Aerofab Inc. Airplane Flight Manual Supplement: (i) No. 5, FAA approved June 24, 1971, revised July 18, 1975, for Lake LA-4, LA-4A, LA-4P, LA-4-200 Flight Manual Dated July 11, 1960, revised April 11, 1973, or: (ii) No. 4, FAA approved December 28, 1973, revised July 18, 1975, for Lake LA-4-200 Flight Manual reissued December 28, 1973. is required for operations at 2690 lb. Gross Weight.

FAA holder: Revo Inc

View record