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Avionics

STC SA7837SW

FAA DRS lists SA7837SW as Current · Reissued, held by Hill, Stephen M., for Twin Commander Aircraft 690D, Twin Commander Aircraft 695A, and Twin Commander Aircraft 695B. Recorded change: Structural provisions for camera and navigation sight. Snapshot dated June 30, 2026.

FAA-listed holder
Hill, Stephen M.
Aircraft configurations
3
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

Structural provisions for camera and navigation sight.

SA7837SW 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: Twin Commander Aircraft 690D, Twin Commander Aircraft 695A, and Twin Commander Aircraft 695B. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Twin Commander Aircraft 690D2A4Twin Commander Aircraft 695A2A4Twin Commander Aircraft 695B2A4

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Twin Commander Aircraft 690D and Twin Commander Aircraft 695A, and 1 more aircraft configuration model, serial range, and configuration?
  2. 02Which part numbers, software versions, interfaces, and manual changes apply?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?

Related avionics STCs

SA01057SEAvionics

Install IFR Panel instruments, primary/alternate static system, and heated pitot tube in accordance with the Equipment List below. This installation applies to one aircraft only, Serial Number 9930CC, current registration N117RB. The Sandel Avionics SN3308 Navigation Display shall be maintained in accordance with Sandel Document No. 90106-IM, Revision G(2), dated April 3, 2001, Section 6, Instructions for Continued Airworthiness, or later Federal Aviation Administration accepted revision. (Bulb replacement interval of 225 hours or 1 year, whichever comes first). Title 14 Code of Federal Regulations part 43 is considered adequate for the remainder of the installation.

FAA holder: Cub Crafters Inc

View record