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Aircraft structures

STC ST04471CH

FAA DRS lists ST04471CH as Current · Issued, held by StandardAero Business Aviation Services LLC, for Boeing 767-200 Series. Recorded change: Installation of a Fuselage Mounted Radome and Antennta Ring Assembly in accordance GoAeroMX Master Data List 20114-MDL-00001 Rev (IR) dated 06/07/2022 or later FM Approved Revision. Snapshot dated June 30, 2026.

FAA-listed holder
StandardAero Business Aviation Services LLC
Aircraft configurations
1
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

Installation of a Fuselage Mounted Radome and Antennta Ring Assembly in accordance GoAeroMX Master Data List 20114-MDL-00001 Rev (IR) dated 06/07/2022 or later FM Approved Revision.

ST04471CH 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: Boeing 767-200 Series. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Boeing 767-200 SeriesA1NM

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Boeing 767-200 Series 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

SA3-111Aircraft structures

Removed 18 from the outboard end of each wing. Removed the first rib inboard of bow, and also the bow. Manufactured from .032 24ST al. Alloy sheet, a full size rib, installed on wing in place of the rib removed. Manufactured skin from .025 24ST and installed on wing, fastened to the first and second rib with #4 sheet metal screws. Three 4 lightning holes were cut in the new rib for inspection purposes and 8-32 nutplates were riveted to inside of rib for attaching of tip plate. The outboard ends of the ailerons were modified to conform to the chord length of the wing. The completed assembly is fabric covered upon covering of wing. The material for the Tip Plate is Prestwood T. and protrudes in a chordwise manner 1-3/4 .

FAA holder: Forrest Alan Frazier

View record