STC ST02647AT

FAA DRS lists ST02647AT as Current · Reissued, held by HAECO Cabin Solutions LLC, for McDonnell Douglas MD-11. Recorded change: Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. Snapshot dated June 30, 2026.

FAA-listed holder

HAECO Cabin Solutions LLC

Aircraft configurations

FAA revision date

March 11, 2019

FAA status

Current · Reissued

Recorded modification

What the FAA record covers

ST02647AT 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: McDonnell Douglas MD-11. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

McDonnell Douglas MD-11A22WE

SA99CEAircraft structuresRevised Sep 30, 2011

Installation of Hoskins Supplemental Model A or B High Intensity Wing Tip Lights, Model C Tail Light, with or without Model 1 or 2 High Intensity Fuselage Lights.

FAA holder: BF Goodrich Aerospace

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SA1649CEAircraft structuresRevised Sep 28, 2011

Installation of either the tail safe support angles or a stub spar at the 3% chord station on the root rib of horizontal stabilizer.

FAA holder: D'Shannon Products Ltd.

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SA1650CEAircraft structuresRevised Sep 28, 2011

Installation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on the root rib of the horizontal stabilizer per Smith Speed Conversions Drawing List No. 1006 with an FAA approved date of May 8, 1981, or later.

FAA holder: D'Shannon Products Ltd.

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ST00734DEAircraft structuresRevised Sep 28, 2011

Installation of three (3) fuselage optical window assemblies to support atmospheric research and meteorological observations in accordance with National Center for Atmospheric Research Optical Window Project Drawing List DL-100-09, Revision A, dated May 26, 2010 or later FAA approved revision. This installation is complemented by STC No. ST03056AT that provides the fuselage view port locations for the optical window assemblies.

FAA holder: National Science Foundation

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FAA record reference

STC number: ST02647AT
Product: Aircraft · Large Airplane
Country: United States
Application date: March 13, 2003
Revision date: March 11, 2019
CFR references: Part 21, Part 25

What the FAA record covers

Aircraft named in FAA DRS

Related aircraft structures STCs

Installation of Hoskins Supplemental Model A or B High Intensity Wing Tip Lights, Model C Tail Light, with or without Model 1 or 2 High Intensity Fuselage Lights.

Installation of either the tail safe support angles or a stub spar at the 3% chord station on the root rib of horizontal stabilizer.

Installation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on the root rib of the horizontal stabilizer per Smith Speed Conversions Drawing List No. 1006 with an FAA approved date of May 8, 1981, or later.

FAA record reference