What it approves
G1000 Integrated Avionics System Update with options including Synthetic Vision and Pathways and GTS 820 Traffic Advisory 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.
FAA Form 8110-2 (5/14) Page 1 of
Part of the
Signature
Title SA01595WI-D Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 Federal Aviation Regulations.
Hawker Beechcraft G36 G1000 Integrated Avionics System Update with options including Synthetic Vision and Pathways and GTS 820 Traffic Advisory System. Data Requried:
1. Garmin Master Drawing List (MDL) 005-00620-18, Revision 1, Dated July 21, 2010 or later FAA-approved revision.
2. Airplane Flight Manual Supplement (AFMS), 190-01258-00, Revision 1, Dated July 21, 2010 or later FAA-approved revision.
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
2. The modified aircraft must be operated in accordance with the Airplane Flight Manual Supplement (AFMS) identified above.
(see continuation sheet 3 of 3) 3 23* May 17, 2010 July 21, 2010 3A15 May 13, 2013; November 16, 2016 Mark Fuller STC ODA administrator ODA-100129-CE
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of
SA01595WI-D Date of Issuance: July 21, 2010 Date Reissued: November 16, 2016
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. Aircraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) listed in the Master Drawing List (MDL) identified above.
*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 this change is as follows:
a. The certification basis for parts not changed or not affected by this change is shown on TCDS 3A15.
b. The certification basis for parts changed or affected by this change is:
Section Amdt. Section Amdt.
23.251 45 23.1322 43
23.301(a) 48 23.1327(a) 20
23.303 Original 23.1351(a)(1)(2)(i)(g) 49
23.305 45 23.1353(h) 49
23.307(a) Original 23.1537(a)(c) 43
23.561(a)(b)(3)(e) 48 23.1359 49
23.601 Original 23.1365(a)(b)(d)(e) 49
23.603 23 23.1367(c)(d) Original
23.605(a) 23 23.1381(a)(b) Original
23.607 48 23.1431(a)(b)(e) 49
23.609 Original 23.1501 21
23.611 48 23.1525 45
23.613(a)(b) 45 23.1529 26
23.771(a) 14 23.1541(a) 21
23.773(a)(2) 45 23.1555(a)(b) 50
23.777(a)(b) 51 23.1581(a)(b)(1)(3)(c)(f) 50
23.867(a)(b) 49 23.1583(h)(m) 50
23.1301 20 23.1585(a)(1)(j) 50
23.1309(a)(1)(2)(b)(1)(2)(3)(4)(e) 49 23-172-SC
23.1311(a)(b) 49
23.1321(a)(d)(e) 49
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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 |
|---|---|---|
| Hawker Beechcraft Corporation | G36 | 3A15 |
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| November 16, 2016 | Reissued, current | Certificate |
| May 13, 2013 | Reissued, earlier issue | Certificate |
| July 21, 2010 | Issued, earlier issue | Certificate |