What it approves
Modification of an existing APX-119 ADS-B Out (DO-260A) transponder installation, CDUA-7000F software upgrade, and GPS-4000S upgrade
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00178MC This certificate issued to: Rockwell Collins, Inc.
400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Part 25 of the Federal Aviation Regulations.
Original Product Make: Boeing Type Certificate Number: A22WE Model: DC-10-30F (KC-10A) Description of Type Design Change: Modification of an existing APX-1 19 ADS-B Out (DO-260A) transponder installation, CDUA-7000F software upgrade, and GPS-4000S upgrade in accordance with:
(1) Master Drawing List RCA-0615, Revision (-), dated March 11, 2020
(2) Airplane Flight Manual Supplement RCA-0613, Revision (-), dated January 10, 2020
(3) Instructions for Continued Airworthiness RCA-0614, Revision (-), dated January 9, 2020 or later FAA approved/accepted revision for items (1), (2) and (3).
(1) Prior installation and approval of an APX-119 Transponder, and installation of FAA STC ST00112MC, are prerequisites to this STC;
(2) Approval of this change in type design applies to the above model aircraft serial numbers 48200-48211, 48213- 48251, 48303-48310 only;
(3) The installer must determine whether this design change is compatible with previously approved modifications;
(Limitations and Conditions continued on page 3 of 4)
Date of Application: February 12, 2018 Date Reissued: March 16, 2020 Date of Issuance: March 11, 2020 Date Amended: September 23, 2021 By Direction of the Administrator Signature:
Jeremy L. Crittenden Title: STC ODA Assistant Administrator, ODA-500864-CE
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00178MC
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00178MC September 23, 2021 Limitations and Conditions (continued):
(4) A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft;
(5) 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.
Note: The FAA has reviewed the impact assessment and found that no additional chang es to the EWIS ICA are required.
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are not significant in FAA Order 8110.48, the certification basis for the Boeing DC-10-30F (KC-10A) is as follows:
a. The type certification basis for all Boeing DC-10-30F (KC-10A) is shown on TCDS A22WE for parts not changed or not affected by the change;
b. The certification basis for parts changed or affected by this change since the reference date of application, February 12, 2018 is based upon 14 CFR Part 25 as amended by Amendment 25-134 and 14 CFR Part 26 as amended by Amendment 26-0, and for this modification is:
14 CFR Part Amend. 14 CFR Part Amend.
25.301 (a) Orig. 25.1301 (a)(b)(c)(d) Orig.
25.303 Orig. 25.1309 (a)(b)(c)(d)(e) Orig.
25.305 (a)(b)(c) Orig. 25.1316 (b) 134
25.307 (a) Orig. 25.1317 (b)(c) 122
25.561 (a)(b)(c) Orig. 25.1322 (a)(b)(c)(d) 38
25.581 (a)(b) 23 25.1351 (a)(1)(2) Orig.
25.601 Orig. 25.1353 (a)(b) Orig.
25.603 (a)(b) Orig. 25.1355 (c) 23
25.605 Orig. 25.1360 (b) 123
25.609 (a)(b) Orig. 25.1431 (a)(b)(c) Orig.
25.611 Orig. 25.1501 (b) 42
25.613 (a)(b)(d) Orig. 25.1523 (b) 3
25.615 (a)(b) Orig. 25.1529 54
25.625 (a)(b)(c) Orig. 25.1541 (a) Orig.
25.771 (a)(c)(e) 4 25.1555 (a) Orig.
25.773 (a)(1)(2) Orig. 25.1581 (a)(2) 42
25.777 (a)(b)(c) Orig. 25.1585 (a) 105
25.853 (a)(b) 17 26.11 (c) Orig.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00178MC September 23, 2021 The certification basis also includes Special Conditions No. 25-18-WE-7 dated January 7, 1970; and Special Conditions No. 25-18-WE-7, Amendment 1 dated July 9, 1971.
c. For any future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| The Boeing Company | DC-10-30F (KC-10A KDC-10) | A22WE |