STC SA8095SW-D

Part 25 of the Federal Aviation R egulations.

Original Product Type Certificate N umber :

Installation of an Automatic Flight Inspection System consisting of a Flight Inspection Operator Console, a Flight Inspection Rack and provisions for interface of Collins Radio Auxiliary Equipment Rack in accordance with (1) Raytheon Company Sealed Drawing List, SDL 5150-1, Rev. J dated 15 December 1999,

(2) FAA/DAS Approved Airplane Flight Manual Supplement 60-01, Rev. 01 dated 28 June 1996, or later DAS approved data.

Flight Inspection Maintenance Division, DAS11SW, AVN-300 6500 S. Mac Arthur Blvd.

Oklahoma City, OK 73169 A10CE M ake : Learjet M odel : 60 Date of application : May 11, 1993

Date of issuance : December 19, 1995

Date reissued : March 21, 2003

Date amended : 1 – August 20, 1996; 2 – June 11, 1997; 3 – December 16, 1999

B y direction of the A dministrator

(Signature) S. Frances Cox, Manager Special Certification Office, Southwest Region

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 3

FAA Form 8110-2-1(10-69) Page 3 of 3

N umber SA8095SW-D Date of Issuance: December 19, 1995 Reissuance Date: March 21, 2003

1. The following STC’s must be installed prior to this installation:

a. ST00280WI, APU/ECS

b. Either ST00140WI or ECR 3797A, FIAS Window Plugs

c. Either ST00142WI or ECR 3796A, Dual Oxygen System

d. ST00331WI, FIAS Interior

e. ST00333WI, ELT

f. ST00225WI-D, Pro-Line 4

g. ST00217WI, Emergency Bus

h. ECR 3802C, Strain Sensor Instl.

i. ECR 3803A, Vert. Stab. Conduit Instl.

j. ECR 3820D, Lucas Starter/Gen.

k. ECR 3867A, Cabin Baggage Mod.

l. Either ST107CH or ECR 3798B, FIAS Radome Instl.

2. Compatibility of this design change with previously approved modifications must be determined by the installer.

3. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

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