STC SA1686CE-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1686CED This certificate issued to: Rockwell Collins. Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Certifies that the change in the type design for the feltowing produrt with the limitutions and senditions therefor as spreifind hereen meets the nirverthiness requirents of durt 3 of the Civil Ait ryufelice effective May 15, 1956. plus amendments and special conditions listed in Type Certificate Data Sheet ASSW (SFAR 41).

Original Product Type Certificate, Number : ASSW Make: Fairchild Swearingen

• Aret: SA227-AT Cescriptics o/ Tyresipe Cange: Installation of Collins FCS-80 Flight Control System with various flight director and air data systems in accordance with the following data or later FAA Approved revisions thereto:

(See Continuation Sheet for data required) Viations and Conditicas: (1) This approval should not be extended to other specific airplanes 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 will introduce no adverse effect upon the airworthiness of that airplane. (2) This STC is applicable to airplanes with takeoff weights up to 16,000 pounds. (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.

Adminisdrater of the Federal Aviation Administration .

Lude of appliration: August August 1981 Late retired: November 7, 1997 Lute n/ inmence : October 22, 1981 Lut amended: December December 1984;

December 12, 1991, October 31, 2008 FEDERAL AVIATION By Direction of the Administrator (Signature) John S. Bohn TOMINSTRATIO Administrator, DAS-500864-CE (hitles

000. or imprisonment not exceeding 3 years, or both.

PAA POR> 8110-2(10-68) PAGE 1 OF / PAGES This corti icate may be transferred in accordance with ran 21.47

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1686CE-D Installation to be accomplished in accordance with the appropriate drawing index listed below:

Collins Airplane Flight Drawing Manual Supplement Index Configuration (AFMS) 992-2778-001, RevE FCS-80 with analog air data and single ACC-08-031, Rev B October 23, 1987 FIS-84 June 27, 2008" 992-2779-001, Rev F FCS-80 with digital air data and single ACC-08-031, Rey B October 23, 1987 FIS-84 June 27, 2008 992-2780-001, Rev E FCS-80 with digital air data and dual. ACC-08-031, Rev B October 23, 1987 FIS-84 June 27, 2008 992-2781-001, RevE PCS-80 with digital air data and ACC-08-031, Rev B October 23, 1987(1} FIS-84/FIS-85 June 27, 2008 992-2782-001, Rev D FCS-80 with analog air data and single ACC-08-031, Rev B October 23, 19871) FIS-85 June 27, 2008 992-2783-001, Rev E FCS-80 with digital air data and single ACC-08-031, Rev B October 23, 1987 FIS-85 June 27, 2008 992-2786-001, Rev C FCS-80 with analog air data and single ACC-08-031, Rev B October 23, 1987 FIS-84 June 27, 2008" .... [1] Or later FAA approved revision or imprisonment not excecding 3 years, or both PAA PORN 8110-2-1 (10-69) PAGE 2 Of