What it approves
Installation of a BAE Systems Bifurcated Exhaust Suppressor 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 SR00183BO
FAA Form 8110-2 (5/14) Page 1 of 3 This certificate issued to:
BAE Systems Information and Electronic Systems Integration Inc.
65 Split Brook Road Nashua, NH 03061 Part 27 of the Federal; Aviation Regulations.
Original Product - Type Certificate Number: H2SW Make: Bell Helicopter Textron Canada Limited Model: 407
Installation of a BAE Systems Bifurcated Exhaust Suppressor System in accordance with BAE Systems Master Document List (MDL) 94117-8463088, Revision F, dated September 18, 2019, or later FAA approved revision.
1. Operation must be in accordance with Pro Star Aviation Rotorcraft Flight Manual Supplement (RFMS), Document Number A245-023, Revision IR, dated November 19, 2003, or later FAA approved revision.
The RFMS must be carried in th e rotorcraft during all flights.
(continued on Page 3 of 3)
Date of Application: April 23, 2003 Date reissued: March 02, 20 04; March 22, 2012
Date of Issuance: November 19, 2003 D ate amended: September 07, 2010;
February 10, 2011;
February 16, 2011;
September 23, 2019
Anthony Pigott for Signature Nicholas Faust Acting Manager, Boston ACO Branch Title
FAA Form 8110-2 (5/14) Page 2 of 3
To (Name and address of transferee) Name:
Address (Number and Street, City, State, and ZIP Code):
From (Name and address of grantor) Name:
Address (Number and Street, City, State, and ZIP Code):
(Continuation Sheet) Number SR00183BO
FAA Form 8110-2 (5/14) Page 3 of 3
Limitations and Conditions: (continued from Page 1 of 3)
2. Maintenance must be in accordance with BAE Systems Instructions for Continued Airworthiness (ICA) Document Number A245-022, Revision 3, dated September 07, 2010, or later FAA accepted revision.
The ICA must be made available to the operator at the time of installation.
3. Compatibility of this design with previously approved modifications must be determined by the installer.
Certification Basis:
Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Bell Helicopter Textron Canada Limited Model 407 is as follows:
a. The type certification basis for parts not changed or not affected by the change is shown on TCDS H2SW.
b. The modification certification basis for parts changed or affected by the change since the reference application date, April 23, 2003, is based upon part 27 amended by Amendment 27-45 as follows:
Regulations at the latest amendment 27-0 through 27-45
27.301, 27.303, 27.305(a)(b)(1)(2), 27.307(a), 27.321(a), 27.337(a), 27.561(b)(3),
27.603(a)(b)(c), 27.605(a)(b), 27.609(a)(b), 27.611(a), 27.613(a)(b)(1)(2)(c)(d), 27.623,
27.625 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS H2SW None ------------------------------------------------------------END-------------------------------------------------------
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 |
|---|---|---|
| Bell Helicopter Textron Canada Limited | 407 | H2SW |
Every issue · 4
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| September 23, 2019 | Amended, current | Certificate |
| March 22, 2012 | Reissued, earlier issue | Certificate |
| February 10, 2011 | Amended, earlier issue | Certificate |
| September 7, 2010 | Amended, earlier issue | Certificate |