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Installation of drag reduction system (including outboard trailing edge extension,...

Airframe Systems (ATA 20-50)
Overview Product description

Overview

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Introduction

Installation of drag reduction system (including outboard trailing edge extension, leading edge vortilons & contoured flap). EASA.IM.A.S.01642 ST01468SE
Bombardier Learjet 35, 36
€ RFQ

Product Description

Installation of drag reduction system (including outboard trailing edge extension, leading edge vortilons & contoured flap).

EASA.IM.A.S.01642
ST01468SE

Please contact modification supplier for further details.

STC Status: Revision Level REV 3
STC Date: 21/08/06
Responsible Office:

LEARJET 36A
LEARJET 36
LEARJET 35A
LEARJET 35