STC SA00122DE-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00122DE-D This certificate issued to:

Learjet Inc.

One Learjet Way Wichita, Kansas 67209 Part 23 of the Federal Aviation Regulations. Plus Special Condition No. 23-ACE-68, dated 1/03/92.

Original Product --Type Certificate Number: A24CE Make: Beech Aircraft Corporation Model: 200 Description of Type Design Change:

Installation of Collins Model EFIS-84 Electronic Flight Instrument System in accordance with AMR Combs, Inc. Certification Drawing List 7501374, revision N/C, dated August 26, 1994, FAA approved August 30, 1994, or later approved revision.

1. FAA approved Airplane Flight Manual Supplement, 01374-1, dated August 30, 1994 or later approved revision is required.

2. The equipment and wiring installed by this STC are in compliance with FAA High Intensity Radiated Fields (HIRF) protection requirements for systems which perform critical functions. To maintain the HIRF integrity, repairs and/or future interfaces to the wiring installation must be in accordance with the Continued Airworthiness Procedures as outlined in AMR Combs Report 01374-80, dated 8/10/94 or later approved revision.

Date of Application: July 12, 1994 Date Reissued: January 4, 1995 May 7, 2002 Date of Issuance: August 30, 1994 Date Amended:

By Direction of the Administrator a . ou (Signature) David T. Grossman Project Manager TOMINISTRATIO Denver Aircraft Certification Office. Northwest Mountain Region, Denver, Colorado (Title)

FAA FORM 8110-2 (10-68) This certificate may be tra red in accordance with FAR 21.47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00122DE-D

3. This approval should not be extended to aircraft of this model on which previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this Certificate, Continuation Sheet, Instructions for Continued Airworthiness and Flight Manual Supplement dated August 30, 1994 or later approved revision, must be maintained as part of the permanent records for the modified aircraft.

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