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.

FAA-listed holder

Aero-Dyne Repair Services Ltd.

Aircraft configurations

FAA revision date

February 9, 2005

FAA status

Current · Issued

Recorded modification

What the FAA record covers

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.

Bell Helicopter Textron (Canada) 206BH2SW Bell Helicopter Textron (Canada) 206LH2SW Bell Helicopter Textron (Canada) 206L-1H2SW Bell Helicopter Textron (Canada) 206L-3H2SW Bell Helicopter Textron (Canada) 206L-4H2SW

ST01458SEAircraft performanceRevised Sep 23, 2004

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

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ST09848SCAircraft performanceRevised Dec 31, 2003

Installation of side-facing divan certified for take-off and landing use.

FAA holder: Gulfstream Aerospace Corporation

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ST00671ATAircraft performanceRevised Dec 29, 2003

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

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ST00719ATAircraft performanceRevised Dec 29, 2003

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

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FAA record reference

STC number: SR02056NY
Product: Aircraft · Rotorcraft
Country: Canada
Application date: July 14, 2004
Revision date: February 9, 2005
CFR references: Part 21, Part 27

What the FAA record covers

Aircraft named in FAA DRS

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.

Installation of side-facing divan certified for take-off and landing use.

Approval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY).

FAA record reference