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Aircraft performance

STC ST01817LA

FAA DRS lists ST01817LA as Current · Reissued, held by Long Beach Avionics, for Avions Marcel Dassault - Breguet Aviation Falcon 10. Recorded change: Installation of Dual Collins ADC-87A Air Data Computers, Collins ALI-80A altimeter, Collins MSI-80C Mach Airspeed Indicator, Thommen Standby Altimeter, and Horizon Aerospace Standby Airspeed Indicator. Snapshot dated June 30, 2026.

FAA-listed holder
Long Beach Avionics
Aircraft configurations
1
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

Installation of Dual Collins ADC-87A Air Data Computers, Collins ALI-80A altimeter, Collins MSI-80C Mach Airspeed Indicator, Thommen Standby Altimeter, and Horizon Aerospace Standby Airspeed Indicator.

ST01817LA 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: Avions Marcel Dassault - Breguet Aviation Falcon 10. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Avions Marcel Dassault - Breguet Aviation Falcon 10A33EU

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Avions Marcel Dassault - Breguet Aviation Falcon 10 model, serial range, and configuration?
  2. 02Which limits, loading assumptions, performance data, and supplements 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 performance STCs

ST00779LAAircraft performance

Installation of side vertical restraints in accordance with approved Master Drawing List SIE 37-703, Revision A, dated May 25, 1999, or later FAA approved revisions. Structural Integrity Engineering FAA Approved Airplane Flight Manual Supplement, SIE 37-607 dated May 26, 1999, or later FAA approved revisions and Weight and Balance Supplement, SIE 37-608, dated February 9, 1999, or later FAA approved revisions, are required as part of this modification.

FAA holder: Structural Integrity Engineering

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