STC SA01039WI-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA0103W1-D This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Purt 23 of the Federal Aviation Poryulutions.

Original Product Type Certificute Number : A24CE Abate: Raytheon (Beech) Model: A200CT (C-12F or C-12D), B200C (C-12F) Description of Type Design Change: Installation of Allied Signal EGPWS System. See TABLE 1 or TABLE 2 or TABLE 3 on Sheet 2, or TABLE 4 on Sheet 3.

Limitations and Conditions: (1) Compatibility of this design change with previously approved modifications must be determined by the installer. (2) This STC must be installed concurrently with SCs SA00232WI-D (Drawing Index AAC-0251-001), SA00234WI-D (Drawing Index AAC-0250-001), SA01037WI-D and SA01038WI-D. (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. (4) Prior FAA approved installation of Shadin Air Data Computer, Part Number 962830AR-3-S-1, shall be determined by the installer; it is a prerequisite to this STC installation.

Date of Application: December December 2000 Date Reissued:

Lute of isance: December 20, 2001 Date Amended: September 24, 2003, April 18, 2005 March 20, 2006, April 3, 2006 FEDERAL AVIATION By Direction of the Administrator Here Harene * (Signature) TOMNISTRATIO John S. Bohn Administrator, DAS-500864-CE (Title)

FAA FORM B110-2 (10-68) PAGE 1 of 3 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01039W-D (Continued) TABLE 1 C-12F(F3 OR T3) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplement Index Configuration (AFMS) (MMS) AAC-0194-001, Allied Signal EGPWS AAC-0218, AAC-0219, No revision, System in Beech B200C No revision, No revision, dated 10/23/01 dated 12/20/01 dated 12/20/01 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

TABLE 2 C-12F(F1 OR TI) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplement Index Configuration (AFMS) (MMS) AAC-0320-001, Allied Signal EGPWS AAC-8087, AAC-8092, No revision, System in Beech A200CT No revision, No revision, dated 02/26/03 dated 09/24/03 dated 09/24/03 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

TABLE 3 C-12D(D2) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplement Index Configuration (AFMS) (MMS) RCA-0089-001, Allied Signal EGPWS AAC-0402, AAC-8112, No revision, System in Beech A200CT No revision, No revision, dated 03/21/05 dated 04/04/05 dated 04/18/05 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

FAA FORM 8110-2-1/10-69) PAGE 2 OF 3 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01039W1D (Continued) TABLE 4 C-12F(F2 OR T2) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplement Index Configuration (AFMS) (MMS) AAC-0340-001, Allied Signal EGPWS AAC-8102, AAC-8097, Revision A, System in Beech B200C No revision, No revision, dated 04/03/06 dated 03/20/06 dated 03/20/06 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

FAA FORM 9110-2-1 (10-69) PAGE 3 Of 3 PAGES