What it approves
Installation of Collins Pro Line 21 Avionics System
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.
Number SA01268WI-D
This certificate, issued to
Part 23 of the Federal Aviation Regulations.
Original Product--Type Certificate Number : A24CE Make : Hawker Beechcraft Corporation (formerly Raytheon) Model : B200 King Air, S/N BB-1769 B200C King Air, S/N BW-01 through BW-29
Description of Type Design Change: Installation of Rockwell Collins, Inc. Pro Line 21 Avionics System in accordance with:
(1) Master Drawing List RCA-0129, Revision F, dated August 14, 2013;
(2) Maintenance Manual Supplement RCA-0019-001 (B200), Revision -, dated October 15, 2004;
(3) Airplane Flight Manual Supplement RCA-0028-001 (B200), Revision -, dated October 15, 2004;
(4) Maintenance Manual Supplement (B200C) RCA-0109, Revision D, dated June 5, 2013;
(5) Airplane Flight Manual Supplement (B200C) RCA-0110, Revision D, dated May 30, 2013;
or later approved/accepted revisions for items (1), (2), (3), (4) or (5).
(1) Approval of this change in type design applies to the above model aircraft only;
(2) Compatibility of this design change with previously approved modifications must be determined by the installer;
(3) A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft;
(4) 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.
Rockwell Collins, Inc.
400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Date of application : August 26, 2004
Date of issuance : October 15, 2004 Date reissued :
Date amended : February 16, 2006; May 7, 2007, August 14, 2013
(Signature) Steven P. Brune
STC ODA Administrator, ODA-500864-CE
(Title)
Number SA01268WI-D August 14, 2013
Certification Basis:
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 Hawker Beechcraft (formerly Raytheon) B200 is as follows:
(1) The type certification basis for the Hawker Beechcraft (formerly Raytheon) B200 is shown on TCDS A24CE for parts not changed or not affected by the change.
(2) The certification basis for parts changed or affected by this change since the reference date of application, August 26, 2004, is as follows:
Hawker Beechcraft B200 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend.
23.29 (a)(b) Orig. 23.771 (a) Orig. 23.1331 (a)(b) Orig.
23.301 (a) Orig. 23.777 (a)(b) 7 23.1335 All 20
23.303 All Orig. 23.867 (a)(b) 7 23.1351 (a)(c) 7
23.305 (a)(b) Orig. 23.901 (a)(b) 7 23.1357 (a)(b)(c)(d) Orig.
23.307 (a) Orig. 23.1301 (a)(b)(c)(d) 20 23.1367 (a)(b)(c)(d) Orig.
23.365 (a)(b)(c)(d) Orig. 23.1303 (a)(b)(c) Orig. 23.1381 (a)(b)(c) Orig.
23.397 (a)(b) 7 23.1305 (a)(c) 7 23.1431 All Orig.
23.561 (a)(b) 7 23.1309 (a)(b)(c)(e) 41 23.1523 All Orig.
23.601 All Orig. 23.1311 (a)(b) 41 23.1525 All Orig.
23.603 (a)(b) Orig. 23.1321 (a)(b)(c)(d)(e) 41 23.1529 All 8
23.605 All Orig. 23.1322 (a)(b)(c)(d) 17 23.1545 (a) 23
23.607 All Orig. 23.1323 (a) 7 23.1545 (b)(c) 7
23.609 (a)(b) Orig. 23.1323 (b) 49 23.1547 (a)(b)(c)(d) Orig.
23.611 All 7 23.1325 (a)(b) 6 23.1549 (a)(b)(c)(d) Orig.
23.613 (a)(b)(c) Orig. 23.1327 (a)(b) Orig. 23.1583 (h) 10
23.677 (a)(b)(c) 7 23.1329 (a)(b)(d)(e)(f) Orig. 23.1585 (a) 7
Number SA01268WI-D August 14, 2013
Certification Basis:
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 Hawker Beechcraft (formerly Raytheon) B200C is as follows:
(1) The type certification basis for the Hawker Beechcraft (formerly Raytheon) B200C is shown on TCDS A24CE for parts not changed or not affected by the change.
(2) The certification basis for parts changed or affected by this change since the reference date amended, May 7, 2007, is as follows:
Hawker Beechcraft B200C 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend.
23.29 (a)(b) 21 23.672 (a)(b)(c) Orig. 23.1329 (e)(f) Orig.
23.301 (a) 48 23.771 (a) 14 23.1331 (a)(b) Orig.
23.303 All Orig. 23.777 (a)(b) 14 23.1335 All 20
23.305 (a)(b) 45 23.867 (a)(b) 49 23.1351 (a)(c) 49
23.307 (a) Orig. 23.901 (a)(b) 53 23.1357 (a)(b)(c)(d) 51
23.365 (a)(b)(c)(d) Orig. 23.1301 (a)(b)(c)(d) 20 23.1367 (a)(b)(c)(d) Orig.
23.397 (a)(b) 7 23.1303 (a)(b)(c) 49 23.1381 (a)(b)(c) Orig.
23.561 (a)(b) 48 23.1305 (a)(c) 52 23.1431 (a)(b)(c)(e) 49
23.601 All Orig. 23.1309 (a)(b)(c)(e) 49 23.1501 (a)(b) 23
23.603 (a)(b) 23 23.1311 (a)(b) 49 23.1523 All 34
23.605 All Orig. 23.1321 (a)(b)(c)(d)(e) 49 23.1525 All 45
23.607 All 48 23.1322 (a)(b)(c)(d)(e) 43 23.1529 All 26
23.609 (a)(b) Orig. 23.1323 (b) 49 23.1549 (a)(b)(c)(d) Orig.
23.611 All 48 23.1325 (a)(b) 50 23.1581 (a)(b)(c) 50
23.613 (a)(b)(c) 45 23.1327 (a)(b) 20 23.1583 (h) 10
23.671 (a)(b) Orig. 23.1329 (a)(b)(d) 49 23.1585 (a) 7
Number SA01268WI-D August 14, 2013
(3) After the initial certification basis of the Hawker Beechcraft B200C for parts changed or affected by this change since the reference date amended, August 14, 2013, the differences are as follows:
Hawker Beechcraft B200C 14 CFR Part Amend. 14 CFR Part Amend. 14 CFR Part Amend.
23.251 All Orig. 23.615 (a) 7 23.1331 (a)(b)(c) 62
23.301 (a)(b) Orig. 23.619 All 7 23.1335 All 20
23.303 All Orig. 23.625 (a)(b)(c) 7 23.1351 (a)(1)(2)(i)(b)(1) 49
23.305 (a)(b) Orig. 23.627 All Orig. 23.1353 (h) 49
23.307 (a) Orig. 23.867 (a)(b) 49 23.1357 (a)(b)(c) 43
23.321 (a) Orig. 23.1301 (a)(b)(c) 62 23.1359 (c) 49
23.341 All 7 23.1303 (a)(b)(c)(e) 62 23.1365 (a)(b)(d)(e) 49
23.365 (a)(b)(c)(d) Orig. 23.1305 (a)(c)(e) 52 23.1367 (a)(b)(c)(d) Orig.
23.561 (a)(b) 7 23.1306 (a)(b) 61 23.1431 (a)(b)(e) 62
23.571 (a) Orig. 23.1308 (a)(b)(c) 57 23.1501 (a)(b) 21
23.601 All Orig. 23.1309 (a)(1)(2)(b)(c)(d) 62 23.1545 (d) 62
23.603 (a)(b) Orig. 23.1311 (a)(b)(c) 62 23.1547 (a)(b)(c)(d)(e) 20
23.605 All Orig. 23.1321 (a)(b)(c)(d)(e) 49 23.1549 (a)(b)(c)(d) 45
23.607 All Orig. 23.1322 (a)(b)(c)(d)(e) 43 23.1581 (a)(b)(1)(3)(c)(d)(f) 50
23.609 (a) Orig. 23.1323 (a) 62 23.1583 (h)(m) 62
23.611 All 7 23.1327 (a)(1)(2)(b) 20 23.1585 (a)(j) 62
23.613 (a)(b)(c) Orig. 23.1329 (h) 49
----------------------------------------End----------------------------------------
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 4
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 14, 2013 | Amended, current | Certificate |
| May 7, 2007 | Amended, earlier issue | Certificate |
| February 16, 2006 | Amended, earlier issue | Certificate |
| October 15, 2004 | Issued, earlier issue | Certificate |