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Aircraft structures

STC SR00532SE

FAA DRS lists SR00532SE as Current · Amended, held by Certified Technology, for Bell Textron Canada 206, Bell Textron Canada 206A, and Bell Textron Canada 206A-1 (OH-58A), and 8 more aircraft configurations. Recorded change: Installation of Certified Technology quick release door pins. Snapshot dated June 30, 2026.

FAA-listed holder
Certified Technology
Aircraft configurations
11
FAA revision date
FAA status
Current · Amended

Recorded modification

What the FAA record covers

Installation of Certified Technology quick release door pins.

SR00532SE 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: Bell Textron Canada 206, Bell Textron Canada 206A, and Bell Textron Canada 206A-1 (OH-58A), and 8 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Bell Textron Canada 206H2SWBell Textron Canada 206AH2SWBell Textron Canada 206A-1 (OH-58A)H2SWBell Textron Canada 206BH2SWBell Textron Canada 206B-1H2SWBell Textron Canada 206LH2SWBell Textron Canada 206L-1H2SWBell Textron Canada 206L-3H2SWBell Textron Canada 206L-4H2SWBell Textron Canada 407H2SWBell Textron Canada 429R00003RD

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Bell Textron Canada 206 and Bell Textron Canada 206A, and 9 more aircraft configurations model, serial range, and configuration?
  2. 02Which configuration, loads, materials, inspections, and damage limits 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 aircraft structures STCs

ST02815ATAircraft structures

Installation of a cockpit door and modification of the forward bulkhead in accordance with U. S. Technical Master Drawing List Document No. 4099-25-000, revision G, dated March 4, 2004, or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement (AFMS), U.S. Technical Document No. U10-0127, dated March 8, 2004, or later FAA approved revision, is a required part of this modification. Instructions for Continued Airworthiness can be found in U. S. Technical Document No. U10-0129, release 1, dated March 4, 2004, U. S. Technical Document U10-0128, release 1, dated March 4, 2004, and U. S. Technical Document U10-0130, release 1, dated March 4, 2004.

FAA holder: U.S. Technical

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SA1813NMAircraft structures

Installation of Lompoc Aero Specialties inner Plexiglass pane in swing out window frames presently employing a single window in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacture of the windows is controlled by Lompoc Aero Specialties Drawing LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

FAA holder: G & D Aero Products Inc.

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