What it approves
Installation of Radome
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 SA04080NY This certificate, issued to: Delta Engineering Corporation 13 DRBA Way New Castle, Delaware 19720 Part 23 of the Federal Aviation Regulations.
Original Product — Type Certificate Number: Make: Textron Aviation Inc.
A24CE Model: B300, B300C Description of Type Design Change:
Installation of Radome in accordance with Delta Engineering Master Data List 0141-10432-2458 Revision I dated May 5, 2021 or later FAA approved revisions to Delta Engineering Master Data List previously listed. The Instructions for Continued Airworthiness and Airplane Flight Manual Supplement as listed on Master Data List is required for this installation.
1. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.
2. Compatibility of this design change with previously approved modifications must be determined by the installer.
(See Continuation Sheets 3 and 4)
Date of Application: March 6, 2018 Date reissued:
Date of issuance: April 15, 2019 Date amended: Ma y 12, 2020, June 2, 2021 By direction of the Administrator Signature:
Title: Jonathan E. Moritz ODA Administrator ODA-800728-NE Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.
FAA Form 8110-2 (5/14) Page 1 of 4 Pages
Transfer Endorsement Transfer the ownership of Supplement Type Certificate Number:
Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.
FAA Form 8110-2 (5/14) Page 2 of 4 Pages
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA04080NY Date June 2, 2021 Limitations and Conditions:
3. This STC is applicable to all serial numbers listed Approved Model List listed under Description of Type Design Change.
4. Reference Delta Engineering Master Data List, which can be found in Description of Type Design Change for additional limitations and conditions.
5. Laser operation is not FAA approved for civil aircraft operations. The laser is disabled.
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, this STC is a significant change. The certi fication basis for un-changed or not affected areas by this STC remains un-changed by this STC and the certification basis for this STC is as follows:
a. The following regulations for CFR Part 23 at later amendment than the TCDS all other regulations at certification basis defined in the TCDS:
Section Title At Amendment 23-
23.177 Static directional and lateral stability 50
23.181 Dynamic stability 45
23.201 Wings level stall 50
23.203 Turning flight and accelerated stalls 50
23.251 Vibration and buffeting 45
23.301 Loads 48
23.305 Strength and deformation 45
23.321 General 45
23.331 Symmetrical flight conditions 42
23.337 Limit maneuvering load factors 48
23.341 Gust load factors 48
23.347 Unsymmetrical flight conditions 48
23.349 Rolling conditions 48
23.421 Balancin g loads 42
23.423 Maneuverin g loads 42
23.425 Gust loads 42
23.427 Unsymmetrical loads 42
23.441 Maneuverin g loads 48
23.443 Gust loads 48
23.479 Level landing conditions 45
23.571 Metallic pressurized cabin structures 48
23.573 Damage tolerance and fatigue evaluation of structure 48
23.574 Metallic damage tolerance and fatigue evaluation of commuter category 48
23.575 Inspections and other procedures 48
23.607 Self-locking nuts 48
23.611 Accessibility 48
23.613 Material strength properties and design values 45 Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.
FAA Form 8110-2 (5/14) Page 3 of 4 Pages
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA04080NY Date June 2, 2021 Section Title At Amendment
23.629 Flutter 48
23.853 Passenger and crew compartment interiors 49
23.867 Lightning protection of structure 49
23.1307 Miscellaneous equipment 49
23.1309 Equipment, systems, and installations 49
23.1359 Electrical system fire protection 49
23.1431 Electronic equipment 49
23.1581 General 50
23.1583 Operating limitations 50
23.1585 Operating procedures 50
23.1587 Performance information 50 -------------------------------------------------END------------------------------------------------- Possession of this Supp lemental Type Certificate (STC) document by persons other than the STC holder does not cons titute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.
FAA Form 8110-2 (5/14) Page 4 of 4 Pages
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 |
|---|---|---|
| June 2, 2021 | Amended, current | Certificate |
| May 12, 2020 | Amended, earlier issue | Certificate |