What it approves
Installation of the Honeywell GNS-XLS Flight Management 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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)
Number: SA01194WI-D This certificate issued to: Honeywell International Inc.
21111N 19th Ave Phoenix, Arizona 85027 Part 23of the Federal Aviation Regulations.
Original Product – Type Certificate Number: Make: Rytheon Model:
A24CE
A200C, S/N BJ-1 Through BJ-66 B200C, S/N BU-1 Through BU-10 B200C, S/N BV-1 Through BV-10
Installation of the Honeywell GNS-XLSFlight Management System.
REQUIRED DATA:
1. Master Drawing List 159-08299-0001, Revision F, dated 9-17-2003 (See continuation sheet)
1. The installation should not be incorporated in any aircraft unlessit isdetermined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.
2. 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: 6-2-2003 Date Reissued: 4-6-2020
Date of Issuance: 10-3-2003 Date Amended:
Signature
Title Richard B. Sleigh ODA Administrator, ODA-602216-NM
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of 3
(Continuation Sheet) Number: SA01194WI-D
Description of Type Design Change: (continued)
2. Airplane Flight Manual Supplements asfollows:
For A200C: S/N BJ-1-BJ-66: 006-10311-0000, Revision -, dated 10-3-2003 For B200C: S/N BU-1-BU-10: 006-10312-0000, Revision -, dated 10-3-2003 For B200C: S/N BV-1-BV-10: 006-10313-0000, Revision -, dated 10-3-2003 Later FAA approved revisionsto the above listed data are incorporated without further revision to this Supplemental Type Certificate.
Certification Basis:
Based on the 14 CFR§§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basisfor this change isasfollows:
a. The certification basisfor parts not changed or not affected by this change isshown on TCDSA24CE.
b. The certification basisfor partschanged or affected by this change since the date of application isdetermined to be:
Regulationsat the latest amendment
Regulationsat an intermediate amendment none
Regulationsat the amendment level shown on TCDS none ------------------------------------------------------------------------------------END--------------------------------------------------------------------------------
Section Amdt. Section Amdt.
23.301 All 23-48 23.1322 23-43
23.305 23-45 23.1331 (a) 23-0
23.307 23-0 23.1351 (a) 23-49
23.561 (e) 23-48 23.1357 (a), (b), (c), (d) 23-43
23.601 23-0 23.1365 (a), (b), (d), (e) 23-49
23.603 All 23-23 23.1367 All 23-0
23.605 (a) 23-23 23.1381 All 23-0
23.607 23-0 23.1431 (a), (b) 23-49
23.609 All 23-0 23.1501 23-21
23.613 All 23-45 23.1525 23-0
23.1301 All 23-20 23.1529 23-26
23.1309 (a)(1)(3), (b), (c)(1),(e) 23-49 23.1541 (a)(2), (b) 23-21
23.1321 (a) 23-49
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 · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 6, 2020 | Reissued, current | Certificate |
| October 3, 2003 | Issued, earlier issue | Certificate |