STC SA00541DE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00541DE This certificate issued to: Wescam 7150 Hayvenhurst Avenue Van Nuys, CA 91406-3823 Part 23 of the Federal Aviation Regulations.

Original Product -Type Certificate Number: ЗА13 Make: Cessna Aircraft Company Model: 182Q Serial Numbers: 18266591 through 18267715 Description of Type Design Change:

Installation of an Wescam Gimbled Camera System with Master Data List for Cessna 182 Wing Mounted Camera, Document No. 18201-MDL-1, revision C, dated March 13, 2004, FAA approved March 26, 2004, or later FAA approved revision.

1. STC SA3825SW, "Installation of a Teledyne Continental IO-470F engine equipped with a McCauley 2A34C58/90 AT-2, or 2A34C66/90 AT-8, or a 2A34C50/90A propeller" is required.

2. One or both of the following STC design changes: STC SA1297SO, "Aileron trim system" or STC SA1758WE, "Auxiliary 12 gallon wingtip fuel tanks" is required.

3. This approval is limited to the M12-DS, MX15 and 16SS models manufactured by Wescam. This approval does not extend to Laser pointer, illuminator or rangefinder payload equipment or combinations thereof.

4. a. Maximum Gross Take-off Weight is limited to 2900 Ibs.

b. Maximum Gross Take-off Weight is 2850 Ibs when used in conjunction with STC SA00542DE, "Cessna 182 Skypod Microwave Antenna".

Date of Application: October 11, 2002 Date Reissued:

Date of Issuance: March 30, 2004 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Das 7. Corosama David T. Grossman (Signature) ADMINISTRATION Program Manager Northwest Mountain Region Denver Aircraft Certification Office (Title)

FAA Form 8110.2/10.681 Dana 1 at A Danas

Hutta States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00541DE Date of Issuance: March 30, 2004 Date Amended:

Limitations and Conditions: (Continued):

5. Airspeed Limits (IAS) Never exceed Maximum structural cruising

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

A copy of this certificate, continuation sheet, and FAA approved Airplane Flight Manual Supplement, Document No. 18201-FMS-1, Revision IR, dated March 26, 2004, or later FAA approved revision must be maintained as part of the permanent records of the modified aircraft.

8. Instructions for Continued Airworthiness, Document No. 18202-ICA-1, entitled, Instructions for Continued installation. Airworthiness", Revision B, dated March 13, 2004, or later FAA accepted revision is required for this

9. 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.

•END--- FAA Form 8110-2(10-68) Page 3 of 3 Pages