STC SA1585CE
FAA DRS lists SA1585CE as Current · Reissued, held by D'Shannon Products Ltd., for Hawker Beechcraft M35, Hawker Beechcraft N35, and Hawker Beechcraft P35, and 3 more aircraft configurations. Recorded change: Installation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later.
SA1585CE 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 M35, Hawker Beechcraft N35, and Hawker Beechcraft P35, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Hawker Beechcraft M35 and Hawker Beechcraft N35, and 4 more aircraft configurations model, serial range, and configuration?
- 02Which control configuration, rigging, limitations, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related flight controls STCs
Recertification under subparts B &G of CAR 3 and installation of SA4-120 airspeed system, SA4-21, fuel system, and SA-2-523, stabilizer angle of incidence change and elevator seal strips.
FAA holder: Staggerwing Museum Foundation Inc.
Raise horizontal stabilizer and installation of elevator seal assembly.
FAA holder: Staggerwing Museum Foundation Inc.
Delete righthand rudder tab and system; install rudder control system bungee and shut-off valve.
FAA holder: Staggerwing Museum Foundation Inc.
Relocate battery to forward of fire wall, add cowl flap extensions and relocate cylinder head temperature probe to cylinder number 3.
FAA holder: Advanced Instrument Incorporated