What it approves
Installation of Special Mission Role Equipment 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 Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 SA01723WI Federal Aviation Regulations.
23 B300 Installation of Special Mission Role Equipment System. Data required includes:
1. Hawker Pacific Technologies, Master Data List (MDL) HP4122-100-MDL, Revision 0, Dated 9/26/2013 or later FAA approved revisions.
2. Hawker Pacific Technologies, Aircraft Flight Manual Supplement (AFMS) HP4122-100-12, Revision 2, Dated: 9/26/2013 or later FAA approved revisions.
(see continuation sheet 3 of 3) Hawker Beechcraft
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
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.
(see continuation sheet 3 of 3) October 22, 2012 September 26, 2013 A24CE December 5, 2013; November 16, 2016 Mark Fuller STC ODA Administrator ODA-100129-CE 4
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
SA01723WI Date of Issuance: September 26, 2013 Date Reissued: November 16, 2016
Description of Type Design Change (continued):
3. Hawker Pacific Technologies, Instructions for Continued Airworthiness (ICA) HP4122-100-13, Revision 2, Dated: 9/13/2013 or later FAA accepted revisions.
3. You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Hawker Beechcraft Corporation Model B300 Serial Nos. FL-680 and FL-683. This STC does not permit manufacturing of parts for multiple installations.
4. A copy of this certificate and the ICA shall be maintained in the airplane permanent records.
5. The modification has not been evaluated to check its proper operations for its intended function.
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 Corporation Model B300 Special Mission Role Equipment System is as follows:
a. The type certification basis for Hawker Beechcraft Corporation B300 is shown on A24CE 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 the application, 10/22/2012, is based upon 14 CFR Part 23 as amended by Amendment 23-62. Based on 14 CFR §21.115 and §21.101, and the FAA policy for significant changes in the FAA Order 8110.48, the certification basis for this modification was determined to be:
Regulations at the latest amendment 23-0 through 23-62
23.3 [Amdt. 23-62], 23.29 [Amdt. 23-21], 23.303 [Amdt. Original], 23.307 [Amdt. Original], 23.365 [Amdt. Original], 23.601 [Amdt.
Original], 23.603 [Amdt. 23-23], 23.605 [Amdt. 23-23], 23.609 [Amdt. Original], 23.619 [Amdt. 23-7], 23.625 [Amdt. 23-7], 23.627 [Amdt. Original], 23.771(a) [Amdt. 23-14], 23.867 [Amdt. 23-49], 23.1367(a)(b)(c)(d) [Amdt. Original], 23.1381 [Amdt. Original],
23.1415(a)(b)(c)(d) [Amdt. Original], 23.1519 [Amdt. Original], 23.1524 [Amdt. 23-10], 23.1529 [Amdt. 23-26], 23.1541(a)(b) [Amdt.
23-21], 23.1561(a)(b) [Amdt. Original], 23.1587 [Amdt. 23-62]
FAA Form 8110-2 (5/14) Page 4 of
Date of Issuance: September 26, 2013 Date Reissued: November 16, 2016
Certification basis (continued):
Regulation at the amendment level in TCDS A24CE
23.251 [Amdt. Original], 23.301 [Amdt. 23-28], 23.305 [Amdt. Original], 23.321 [Amdt. Original], 23.337 [Amdt. 23-34], 23.341 [Amdt. 23-34], 23.561 [Amdt. 23-34], 23.571 [Amdt. 23-34], 23.572 [Amdt. 23-34], 23.607 [Amdt. 23-17], 23.611 [Amdt. 23-7],
23.613 [Amdt. 23-23], 23.773(a)(1) [Amdt. 23-14], 23.777(a)(b) [Amdt. 23-51], 23.785(a)(b)(g)(i)(j)(l) [Amdt. 23-34], 23.787(a)(e)(g) [Amdt. 23-34], 23.807(b)(1)(d)(4) [Amdt. 23-34], 23.815 [Amdt. 23-34], 23.831(a)(b) [Amdt. 23-34], 23.841(a) [Amdt. 23-17],
23.851(a)(b) [Amdt.23-34], 23.853(a)(c)(d)(1)(2)(3)(i)(ii) [Amdt. 23-34], 23.1301(a)(b)(c)(d) [Amdt. 23-20], 23.1309(a)(1)(b)(d) [Amdt.
23-34], 23.1322 [Amdt. 23-17], 23.1351(a)(1)(2)(ii)(b)(1)(i)(2)(3)(5)(i)(iii)(iv)(v) [Amdt. 23-34], 23.1357(a)(b)(c)(d) [Amdt. 23-20],
23.1365(a)(b) [Amdt. 23-14], 23.1411(a)(b) [Amdt. 23-17], 23.1419(b) [Amdt. 23-14], 23.1431 [Amdt. Original], 23.1447(a)(c)(e) [Amdt. 23-30], 23.1557(a)(d) [Amdt. 23-23], 23.1581(a)(b)(1)(3)(d) [Amdt. 23-34], 23.1583(b)(1)(2) [Amdt. 23-34], 23.1585 [Amdt.
23-34].
Regulation at an intermediate amendment
23.811(b) [Amdt. 23-36]
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.
-- END -- SA01723WI 4
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 |
|---|---|---|
| Beechcraft Corporation | B300 | A24CE |
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 |
| December 5, 2013 | Reissued, earlier issue | Certificate |
| September 26, 2013 | Issued, earlier issue | Certificate |