STC SA964GL

Part 3 of the Civil Air Regulations.

(See Type Certificate Data Sheet No. 3A13 for complete certification basis.)

1. Installation of a Shadin Company Fuel Flow Indicator in accordance with Shadin Company Number 4091, revised July 15, 1986 or other FAA approved revision (for Cessna 182 Models with pump-fed fuel systems).

2. Installation of a Shadin Company Fuel Flow Indicator and Fuel Flow Transducer in accordance with Shadin Report Number 4091 revised July 15, 1986 or other FAA Approved revision (for Cessna 182 Models with gravity-fed fuel systems).

1) This approval should not be extended to other airlanes of this model that incorporate any other previously approved modification, unless it is determined that the interrelationship between this change and any other previously approved modification will introduce no adverse effect on the airworthiness of these airplanes.

2) 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.

Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 3A13 Make : Cessna Model : 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, R182, T182, TR182 Date of application : October 12, 1985

Date of issuance : January 10, 1986

Date reissued : June 8, 2006

Date amended : August 19, 1986

( Signature) Charles L. Smalley Manager, Systems & Flight Test Branch Chicago Aircraft Certification Office

( Title)