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Engine and powerplant

STC ST02265CH

FAA DRS lists ST02265CH as Current · Issued, held by Leading Edge Designs LLC, for Learjet 24, Learjet 24A, and Learjet 24B, and 13 more aircraft configurations. Recorded change: Installation of Thrust Reverser Hydraulic System Modifications that were previously installed by STC SA1731SW, SA1669SW or SA1670SW. Snapshot dated June 30, 2026.

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FAA-listed holder
Leading Edge Designs LLC
Aircraft configurations
16
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

ST02265CH 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 24, Learjet 24A, and Learjet 24B, and 13 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Learjet 24A10CELearjet 24AA10CELearjet 24BA10CELearjet 24B-AA10CELearjet 24CA10CELearjet 24DA10CELearjet 24D-AA10CELearjet 24EA10CELearjet 24FA10CELearjet 24F-AA10CELearjet 25A10CELearjet 25AA10CELearjet 25BA10CELearjet 25CA10CELearjet 25DA10CELearjet 25FA10CE

Related engine and powerplant STCs

FAA record reference

STC number
ST02265CH
Product
Aircraft · Large Multi-Engine
Country
United States
Application date
August 26, 2005
Revision date
March 28, 2006
CFR references
Part 21, Part 25