STC SR02056NY
FAA DRS lists SR02056NY as Current · Issued, held by Aero-Dyne Repair Services Ltd., for Bell Helicopter Textron (Canada) 206B, Bell Helicopter Textron (Canada) 206L, and Bell Helicopter Textron (Canada) 206L-1, and 2 more aircraft configurations. Recorded change: Installation of Helicopter Performance Monitoring System is to be done in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332101, Revision 1, dated July 25, 2003, or later Transport Canada approved revision. Audio option is to be installed in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332102, dated April 2, 2003, or later Transport Canada approved revisions. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of Helicopter Performance Monitoring System is to be done in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332101, Revision 1, dated July 25, 2003, or later Transport Canada approved revision. Audio option is to be installed in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332102, dated April 2, 2003, or later Transport Canada approved revisions.
SR02056NY 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 Helicopter Textron (Canada) 206B, Bell Helicopter Textron (Canada) 206L, and Bell Helicopter Textron (Canada) 206L-1, and 2 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Bell Helicopter Textron (Canada) 206B and Bell Helicopter Textron (Canada) 206L, and 3 more aircraft configurations model, serial range, and configuration?
- 02Which limits, loading assumptions, performance data, and supplements apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related aircraft performance STCs
Incorporation of change in aircraft weight and balance by supplementing the current aircraft weight and balance manual with Newport Aeronautical Development Report No. NAD 2004-101, Revsion A, dated June 16, 2004, or later FAA approved revision.
FAA holder: Newport Aeronautical Development
Installation of side-facing divan certified for take-off and landing use.
FAA holder: Gulfstream Aerospace Corporation
Approval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY).
FAA holder: Structural Integrity Engineering
Approval of increased operating weights as substantiated by the design data listed in Structural Integrity Engineering (SIE) Master Report List or Master Document List No. SIE-28-703, no revision, dated February 24, 1995, or later FAA approved revision. Aircraft with Increase of Maximum Takeoff or Landing Weight must also be modified in accordance with: Drawing SIE-28-901 (taxi weight up to 183,000 lb, landing weight to 164,000 lb), 28-904 (taxi weight up to 178, 500 lbs, landing weight to 164,000 lbs), 28-905 (taxi weight up to 191,000 lb, landing weight to 164,000 lbs), Rev NC or later FAA approved revisions.
FAA holder: Structural Integrity Engineering