STC ST00321WI-D

FAA FORM 8110-2(10-68) Number ST00321WI-D This certificate issued to Learjet Inc.

One Learjet Way Wichita, Kansas 67209

Part 25 of the Federal Aviation Regulations. (For Certification Basis see T.C.D.S. A10CE)

Original Product--Type Certificate Number : A10CE

Make : Learjet Model :35/35A/36/36A

Install Rosemount Pitot / Static Probes in accordance with Learjet Master Document List (MDL), M100165ICT, Revision A dated 5/19/95 or later FAA approved revision.

1. Learjet Inc. Airplane Flight Manual Supplement Document No. W1266, Change 1 FAA approved 5/26/95 or later FAA approved revision, is required with this installation.

2. Installation of Century III Wing (AAK 76-04) with Softflite (AMK 83-5) is a prior or concurrent requirement for this STC.

3. This approval should not be extended to aircraft of this model on which other 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.

4. 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.

5. A copy of this certificate must be maintained as part of the permanent record for the modified aircraft.

Date of application : May 12, 1995

Date of issuance : May 26, 1995 Date reissued :

Date amended : January 10, 2003, November 17, 2004

( Signature) Keith Johnston DAS Administrator DAS-501508-CE, Learjet Inc.

Wichita,_Kansas (Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

Number ST00321WI-D Date of Issuance: May 12, 1995 Date Amended: January 10, 2003, November 17, 2004

6. The appropriate Instructions for Continued Airworthiness, M100165ICT-IFCA-4 Revision A, dated November 12, 2004, FAA accepted November 17, 2004 or later FAA accepted revision is required for the M100165ICT-4 installation.