STC SA02410CH-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST02410CH-D This certificate issued to: Duncan Aviation 15745 S. Airport Rd.

Battle Creek, MI 49015 CAR 4b of the Federal Aviation

•Regulations. See page 3 of 3 for complete certification basis.

Original Product - Type Certificate Number: ABEU Abuke: Raytheon Aircraft Company Model: BAe. 125 Series 800A Description of Type Design Change:

Installation of Rockwell Collins Pro Line 21 IDS (Integrated Display System) With IFIS-5000 (Integrated Flight Information System) and Engine Instrument Display in accordance with Duncan Aviation Master Drawing List 060912014, Revision G, dated April 20, 2007 or later FAA approved revision.

1. FAA approved Airplane Flight Manual Supplement for the Collins IDS-3000, 060912018, Revision Ø, dated April 18, 2007, FAA approved April 20, 2007, or later FAA approved revision is required.

2. FAA approved Airplane Flight Manual Supplement for Category II Minimums Operations, 061031009, Revision Ø, dated January 5, 2007, FAA approved April 20, 2007, or later FAA approved revision is required for Category Il operations.

3. FAA approved Airplane Flight Manual Supplement for installation of a dual ADS-85A Air Data Systems, 070118003, Revision Ø, dated January 18, 2007, FAA approved April 20, 2007, or later FAA approved revision is required when dual Collins ADC-85A Air Data Computers are installed.

The installation of Raytheon Aircraft Service Bulletin 34-3166, Revision 1 is required prior to installing this STC.

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

A copy of this Certificate and Flight Manual Supplement must be maintained as part of the permanent records of the modified aircraft.

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.

Date of Application: October October 2006 Date Reissued:

Date of Issuance: April 20, 2007 Date Amended:

By Direction of the Administrator FEDERAL AVIATION 2. Chiller (Signature) Peter G. Phillips DAS Coordinator, DAS-405253-CH TOMNISTRATOT Duncan Aviation Battle Creek, Michigan (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 STO2410CH-D Certification Busis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Raytheon Aircraft Model BAe. 125 Series 800A is as follows:

a. The type certification basis for Raytheon Aircraft Model BAe. 125 Series 800A aircraft is shown on TCDS A3EU for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, October 27, 2006, is as shown on Type Certificate Data Sheet A3EU and amended by Special Condition No. 25-345-SC, dated February 12, 2007, Docket No.

NM369 for complete certification basis. The certification basis for this modification was determined to be 14 CFR Part 25 as amended Regulations at the latest amendment 25-0 through 25-117 14 CFR Part Amendment 14 CFR Part Amendment 14 CFR Part Amendment

25.301 (a)(b) 25-23 25.981 (a)(b) 25-102 25.1355 (c) 25-38

25.303 25-23 25.1301 (a)(b)(c)(d) original 25.1357 (a)(c)(d)e) original

25.305 (a)(b) 25-86 25.1303 (a)(b)(c) 25-90 25.1381 (a)(b) 25.72

25.307 (a) 25-72 25.1305 (a)(c)(d) 25-115 25.1431 (a)(b)(c)(d) 25-113

25.561 (c) 25-91 25.1307 (c) 25-72 25.1501 (a)(b) 25-42

25.581 (a)(b) 25-23 25.1309 (a)(b)(c)(d)(e)(g) 25-41 25.1519 original

25.601 original 25.1316 (a)(b)(c) 25-80 25.1521 (a)(c) 25-72

25.603 25-46 25.1321 (a)(b)(c)(d)(e) 25-41 25.1525 original

25.605 (a) 25-46 25.1322 (a)(b)(c)(d) 25-38 25.1541 (a)(b) original

25.609 (a) original 25.1323 (a)(b)(c)(d)(e)(f)(g) 25-109 25.1543 (b) 25-72

25.611 25-23 25.1325 (e)(t) 25-108 25.1549 (a)(b)(c) 25-40

25.613 (a) 25-112 25.1329 (e)(h) 25-46 25.1555 (a) original

25.771 (a)(e) 25-4 25.1331 (a) 25-41 25.1581 (a)(b)(d) 25-72

25.773 (a) 25-108 25.1333 (a)(b)(c) 25-41 25.1583 (a)(b)(c)(d)(e) (Đ(h)(i) 25-105

25.777 (a)(b) 25-46 25.1335 25-41 25.1585 (a)(b)(c)(d)(e) 25-105

25.869 (a) 25-113 25.1351 (a)(d) 25-72 25.1587 (a)(b) 25-108

25.901 (c) 25-46 25.1353 (a)(b)(c)(d) 25-113 END

FAA FORM 8110-2-1 (10-69) PAGE 3 of 3 PAGES