STC ST01302WI

FAA DRS lists ST01302WI as Current · Issued, held by JetCorp, for Learjet 60. Recorded change: Revise the environmental control system ducting to add two outlets on the cockpit center pedestal for improved crew comfort in accordance with STC Drawing list No. 67-269L001, Rev. C, dated November 18, 2004, stamped FAA Approved January 20, 2005, or later approved revision. Snapshot dated June 30, 2026.

FAA-listed holder

JetCorp

Aircraft configurations

FAA revision date

January 20, 2005

FAA status

Current · Issued

Recorded modification

What the FAA record covers

ST01302WI 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: Learjet 60. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Learjet 60A10CE

Buyer checks

Confirm before sourcing

ST00899ATOther aircraft modificationsRevised Dec 17, 2021

Installation of a CAS-81 TCAS.

FAA holder: Honeywell International Inc

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ST00903ATOther aircraft modificationsRevised Dec 17, 2021

Installation of a CAS-81 TCAS II and TRA-67 ATC System.

FAA holder: Honeywell International Inc

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ST00904SEOther aircraft modificationsRevised Dec 17, 2021

Rewiring of Flight Data Acquisition Unit (FDAU)/Management Control Unit (MCU) in accordance with Honeywell drawing 755-3030-001 Revision A, dated March 22, 2001 or later FAA approved revision.

FAA holder: Honeywell International Inc

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ST00939SEOther aircraft modificationsRevised Dec 17, 2021

Installation of a the Solid State Flight Data Recorder and Honeywell Flight Data Acquisition Management System in accordance with Master Drawing List 756-0134-001, Revision B, dated June 15, 2001, or later FAA approved revisions.

FAA holder: Honeywell International Inc

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What the FAA record covers

Aircraft named in FAA DRS

Confirm before sourcing

Related other aircraft modifications STCs

Installation of a CAS-81 TCAS.

Installation of a CAS-81 TCAS II and TRA-67 ATC System.

Rewiring of Flight Data Acquisition Unit (FDAU)/Management Control Unit (MCU) in accordance with Honeywell drawing 755-3030-001 Revision A, dated March 22, 2001 or later FAA approved revision.

Installation of a the Solid State Flight Data Recorder and Honeywell Flight Data Acquisition Management System in accordance with Master Drawing List 756-0134-001, Revision B, dated June 15, 2001, or later FAA approved revisions.