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Aircraft structures

STC SH5861SW

FAA DRS lists SH5861SW as Current · Reissued, held by The NORDAM Group LLC, for Bell Textron Canada 206A, Bell Textron Canada 206B, and Bell Textron Canada 206L, and 3 more aircraft configurations. Recorded change: Installation of 'Pop-Out' wedge window assembly. Snapshot dated June 30, 2026.

FAA-listed holder
The NORDAM Group LLC
Aircraft configurations
6
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

SH5861SW 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 206A, Bell Textron Canada 206B, and Bell Textron Canada 206L, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Bell Textron Canada 206AH2SWBell Textron Canada 206BH2SWBell Textron Canada 206LH2SWBell Textron Canada 206L-1H2SWBell Textron Canada 206L-3H2SWBell Textron Canada 206L-4H2SW

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Related aircraft structures STCs

SA6073NMAircraft structures

Installation of fatigue sensor and structural life extension of wing spar in accordance with FAA approved SIE Master Drawing List 91000, Revision A, dated September 23, 1993, or later FAA approved revision, and FAA approved Airplane Flight Manual Supplement Report No. SIE-12-601, Revision N/C, dated October 19, 1993 or later FAA approved Airplane Flight Manual Supplement, and Report No. SIE-12-602, Revision N/C, dated December 21, 1993, or later FAA approved Revision. (SIE-12-601 is for model C99 only, and SIE-12-602 is for the remaining models, 99, 99A, A99A, and B99.).

FAA holder: Structural Integrity Engineering

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