STC SR09450RC

Supplemental type certificate · Safran Electronics & Defense Avionics USA, LLC

Holder
Safran Electronics & Defense Avionics USA, LLC · United States
Status
Current · Reissued
Status date
July 15, 2024
Applied
May 10, 2005
Product
Aircraft · Rotorcraft
Certification basis
Part 27
Data sheet
TCDSR0001RD

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of SAGEM ICDS-8 Integrated Cockpit Display System that includes a display for the pilot position and a second optional display for the copilot position.

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.

SR09450RC Safran Electronics & Defense, Avionics USA, LLC 2802 Safran Drive Grand Prairie, TX 75052 Part 27 the Federal Aviation Regulations R0001RD Airbus Helicopters EC120B

(See Continuation Sheet 3 of 4) The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

May 10, 2005 May 10, 2007; July 15, 2024 October 28, 2005 June 13, 2007; May 11, 2009; May 12, 2010; December 8, 2016 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4

SR09450RC 4

SR09450RC Date of Issuance: October 28, 2005 Date Amended: December 8, 2016 Date of Reissuance: July 15, 2024

Description of Type Design Change (continued):

1. Installation of SAGEM ICDS-8 Integrated Cockpit Display System (ICDS) that includes a display for the pilot position and second optional display for the copilot position in accordance with Heritage Master Drawing List (MDL) L00-14000, Revision IR, dated 10/10/05, for the -01 configuration of drawing L82-14000, Revision C, dated 06/05/07, or later FAA approved revision. Rotorcraft Flight Manual Supplement (RFMS) Heritage Document L09-64003, dated October 28, 2005, or later FAA approved revision is required. Instructions for Continued Airworthiness (ICA), Heritage Document L04-74000, Revision IR, dated 9/12/05, or later FAA accepted revision is required.

2. The ICDS-8A dual display installation when installed with SAGEM AHRS for the -02 configuration of drawing L82-14000, Revision C, dated 06/05/07, or later FAA approved revision. RFMS Document SA-07R-E-010RFMS, Revision A, dated 08/09/07, or later FAA approved revision is required. ICA SAGEM Document SA-07R-E-005, Revision -, dated 06/06/07, or later FAA accepted revision is required.

3. Installation of SAGEM ICDS-8A Dual ICDS displays coupled to SAGEM Autopilot per STC SR09263RC-D in accordance with SAGEM MDL 120-0002, Revision D, dated 04/01/09, or later FAA approved revision. This installation is for the configuration defined in SAGEM Installation drawing 120-1003-01, Revision F, dated 03/29/09, or later FAA approved revision. RFMS SAGEM Document SA-07R-E-010RFMS, Revision B, dated May 11, 2009, or later FAA approved revision is required. ICA SAGEM Document SA-08R-E-004, Revision A, dated 04/06/09, or later FAA accepted revision is required.

SR09450RC Date of Issuance: October 28, 2005 Date Amended: December 8, 2016 Date of Reissuance: July 15, 2024

Description of Type Design Change (continued):

4. Installation of SAGEM ICDS-8A Dual ICDS displays coupled to SAGEM Autopilot per STC SR09263RC-D in accordance with SAGEM MDL 120-0002, Revision D, dated 04/01/09, or later FAA approved revision. This installation is for the configuration defined in SAGEM Installation drawing 120-1003-03, Revision F, dated 03/29/09, or later FAA approved revision. RFMS SAGEM Document SA-09R-E-001RFMS, Revision -, dated May 11, 2009, or later FAA approved revision is required. ICA SAGEM Document SA-08R-E-004, Revision A, dated 04/06/09, or later FAA accepted revision is required.

5. Installation of SAGEM ICDS-8A Single ICDS Display, not coupled with SAGEM Autopilot STC SR09263RC-D; with Texas Aviation Services Instrument Panel in accordance with SAGEM MDL 120-0002, Revision G, dated 02/26/10, or later FAA approved revision. This configuration is defined in SAGEM Installation drawing 120-1003-04, Revision K dated 02/23/10, or later FAA approved revision. RFMS SAGEM Document SA-10R-E-001RFMS, Revision IR, dated May 12, 2010, or later FAA approved revision is required. ICA SAGEM Document SA-08R-E-004 Revision B dated 09/21/09, or later FAA accepted revision is required.

6. Installation of SAGEM ICDS-8A Dual ICDS displays coupled to SAGEM Autopilot per STC SR09263RC-D in accordance with SAGEM MDL 120-0002, Revision K, dated 08/08/16, or later FAA approved revision. This installation is for the configuration defined in SAGEM Installation drawing 120-1003-05, Revision N, dated 08/08/16, or later FAA approved revision. RFMS SAGEM Document SA-ER-050722-01, Revision 00, dated November 04, 2016, or later FAA approved revision is required. ICA SAGEM Document SA-08R-E-004, Revision C, dated 11/09/16, or later FAA accepted revision is required.

-END- 4 4

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Airbus HelicoptersEC120BR0001RD

Every issue · 4

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
July 15, 2024Reissued, currentCertificate
November 1, 2016Reissued, earlier issueCertificate
June 13, 2007Amended, earlier issueCertificate
May 10, 2007Reissued, earlier issueCertificate