Installation of a drag reduction system (including outboard trailing edge extension, leading edge vortilons, and contoured flap) in accordance with Raisbeck Engineering Drawing Number 202L-5700, Revision A, dated August 29, 2004, or later FAA approved revisions.

Please contact modification supplier for further details.

STC Status: Amended
STC Date: 24/03/05
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400

Learjet Inc.

• 35
• 35A (C-21A)
• 36
• 36A