Supplemental type certificate · Dassault Falcon Jet Corp.

Holder
Dassault Falcon Jet Corp. · United States
Status
Current · Reissued
Status date
October 31, 2011
Applied
March 28, 2011
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA50NM

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Aft RH Divan Installations in accordance with Data List Report No. F2EX-01038 Revision AG dated 14-Apr-2011, or later FAA approved revision. FAA Approved AFM Supplement, Report 40709-1 dated April 14, 2011 or later FAA approved revision is required. Instructions for Continue Airworthiness, Report ICA-F2EX-01038-501, revision Original, dated 21-Jan-2011 or later FAA approved revision is required.

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 ST10890SC-D

3801 East 10 th Street Little Rock, Arkansas 72202-3366

Part 25 of the Federal Aviation Regulations.

A50NM Dassault Aviation Make:

Model: Falcon 2000EX Aft RH Divan Installations in accordance with Data List Report No. F2EX-01038 Revision AJ dated 31-Oct-2011, or later FAA approved revision.

FAA Approved AFM Supplement, Report 40709-1 dated April 14, 2011 or later FAA approved revision is required.

Instructions for Continue Airworthiness, Report ICA-F2EX-01038-501, revision Original, dated 21-Jan-2011 or later FAA approved revision is required.

The installer is required to consider the following items for regulatory compliance. Aft RH Divan Installation Requirements use Report 40577, revision B, dated 4-Apr-2011, or later FAA approved revision which includes the following:

– Installation of Oxygen System per ST10262SC-D (503 installation) that includes 14CFR 25.1447(c)(1) – Variations of the cabin floor plan requires structural substantiation of the floor beam strength – Installation of FAA approved rail system per report 40632 – Storage compartment weight is the maximum limit for this STC – It is the installer’s responsibility to approve the electrical system modification for the emergency exit sign, fabricate burn testing coupons (14CFR 25.853), and cabin interior arrangement separately approved.

Date of application: March 28, 2011

Date of issuance: April 14, 2011

Date reissued: October 31, 2011

(Signature)

Robert J. Feazell ODA-700141-SW STC ODA administrator (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP code)

Signature of grantor (in ink):

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST10890SC-D Issue Date: October 31, 2011

FAA Form 8110-2-1 (10-68) PAGE 3 of 3 PAGES Description of Type Design Change (Continued):

(None)

Compatibility of this modification with other previously approved modifications must be determined by the installer.

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.

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 STC same as stated in Type Certification Data Sheet (TCDS) A50NM, Revision 7, data January 3, for Falcon 2000EX

SECT. PARA. AMDT.

25.1 (a),(b) O

25.29 - 25-72

25.301 (a),(b) 25-23

25.303 - 25-23

25.305 (a),(b) 25-86

25.307 (a) 25-72

25.337 (a) 25-23

25.341 (a) 25-86

25.561 (a),(b),

(c),(d) 25-64

25.562 (c)(5) 25-64 *(c)(7),(8)

25.601 - O

25.603 (a),(b),(c) 25-46

25.605 (a) 25-46

25.609 (a),(b) O

25.611 - 25-23

25.613 (a),(b),(c),

(d) 25-72 SECT. PARA. AMDT.

25.625 (a),(b),

(c),(d) 25-72

25.785 (c),(d),

(i) 25-88 * (b)

25.787 (a),(b) 25-51

25.789 (a) 25-46

25.807 (b) 25-67

25.812 (a)(1),

(e)(2) 25-58

25.813 (c)(2) 25-46

25.815 - 25-38

25.831 (a) 25-41

25.853 (a),(c) 25-83

25.981 (a)(3),(b) 25-102

25.1301 (a),(b),

25.1353 (a) 25-42

25.1411 (a),(b), 25-79 SECT. PARA. AMDT.

25.1431 (c) O

25.1529 - 25-54

25.1541 (a),(b) O

25.1561 (b),(c) 25-46

25.1581 (a),(b),(d) 25-72 H25.1 (a),(b),(c) 25-54 H25.2 (a),(b) 25-54 H25.3

(g) 25-54

*Exemption No 8007A – Side Facing Sofa Exemption: to 25.562 (c) and 25.785 (b); See Exemption 8007A Collector Report, 40889; (Previous TC Substantiation)

END

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
Dassault AviationFALCON 2000EXA50NM

Every issue · 2

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

DateStatusFiles
October 31, 2011Reissued, currentCertificate
April 14, 2011Issued, earlier issueCertificate