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Installation of a Universal Avionics Inc. UNS- 1B FMS (Dual)....

Airframe Systems (ATA 20-50) Navigation + EFB (ATA 34 + 46 )
Overview Product description

Overview

STC Number
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STC Date
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Contact Details
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Introduction

Installation of a Universal Avionics Inc. UNS- 1B FMS (Dual). Certification Basis Limitations -FAA STC ST00546WI.-Duncan Aviation Inc. Document List No10049800, May 27, 1997, or later FAA-approved revisions.-Duncan Aviation Inc; Document No 40173300, FAA- approved AFMS, June 13, 1997, or later FAA- approved revisions. Conditions 1. For certification basis refer to FAA TCDS A10CE.2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.
Bombardier Learjet 55, 60, 60XR
€ RFQ

Product Description

Installation of a Universal Avionics Inc. UNS-
1B FMS (Dual).

Certification Basis


Limitations
-FAA STC ST00546WI.-Duncan Aviation Inc.
Document List No10049800, May 27, 1997,
or later FAA-approved revisions.-Duncan
Aviation Inc; Document No 40173300, FAA-
approved AFMS, June 13, 1997, or later FAA-
approved revisions.

Conditions
1. For certification basis refer to FAA TCDS
A10CE.2. This STC is approved only for the
product configuration as defined in the
approved design data referred to in the
paragraph "Description". Compatibility with
other aircraft/engine configurations shall be
determined by the installer.

Please contact modification supplier for further details.

STC Status: Revision Level:
STC Date: 11/04/05
Responsible Office: EASA