# STC ST10885SC-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Dassault Falcon Jet Corp., United States
- Description: Avionics and Interior Installations in accordance with Data List Report No. F9EX-01084 Revision B dated August 24, 2010, or later FAA approved revision.
FAA Approved AFM Supplement, Report 37159-F9EX-D260 dated August 24, 2010 or later FAA approved revision is required.
Supplemental Maintenance Manual, Report SMM F900EX - SN 234, revision A, dated July 23, 2010 or later FAA approved revision is required. 
Supplemental Illustrated Part Catalog, Report SPIC F900EX- SN 234, revision A, dated July 23, 2010 or later FAA approved revision is required.
Supplemental Wiring Diagram Manual, Report DGT/DTACF 342128, revision A, dated July 20, 2010 or later FAA approved revision is required.
- Applied: June 1, 2010
- Status date: August 24, 2010
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A46EU](https://openairdocs.org/tcds/A46EU)
- Certificate PDF: https://openairdocs.org/files/sha256/12/e7/12e72b65cae901f5f12e65f8d4258d50037165b05297aa59a5fcdbaa7f4b129b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CB10CD93EC9E23E7862578AE0068B706.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST10885SC-D

## ADs that name it (0)

None.

## Approved models (1)

- Dassault Aviation Falcon 900EX ([TCDS A46EU](https://openairdocs.org/tcds/A46EU))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number ST10885SC-D

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

Part 25 of the Federal Aviation Regulations.

A46EU Dassault Aviation Make:

Model: Falcon 900EX Avionics and Interior Installations in accordance with Data List Report No. F9EX-01084 Revision B dated August 24, 2010, or later FAA approved revision.

FAA Approved AFM Supplement, Report 37159-F9EX-D260 dated August 24, 2010 or later FAA approved revision is required.

Supplemental Maintenance Manual, Report SMM F900EX - SN 234, revision A, dated July 23, 2010 or later FAA approved revision is required.

Supplemental Illustrated Part Catalog, Report SPIC F900EX- SN 234, revision A, dated July 23, 2010 or later FAA approved revision is required.

Supplemental Wiring Diagram Manual, Report DGT/DTACF 342128, revision A, dated July 20, 2010 or later FAA approved revision is required.

You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Dassault Aviation Model 900EX Serial No. 234.

This STC does not permit manufacturing of parts for multiple installations.

Date of application: June 1, 2010

Date of issuance: August 24, 2010

(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 ST10885SC-D Issue Date: August 24, 2010

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

(None)

(None)

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 Falcon 900EX (EASy Definition) aircraft fitted with this STC is as follows.

The certification basis for this STC same as stated in Type Certification Data Sheet (TCDS) A46EU, Revision 15, data March 2, 2010, for Falcon 900EX

**SECT. PARA. AMDT.**

25.1 a,b O

25.29 25-72

25.301 a,b,c 25-23

25.303 - 25-23

25.305 a,b,c 25-77

25.307 a 25-72

25.365 a,b,c,d,e, f,g 25-54

25.561 a,b,c 25-23

25.571 a,b 25-72

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,e 25-72

25.619 a,b,c 25-23

25.623 a,b O

25.625 a,b,c,d 25-23

25.777 a 25-46

25.783 b,e,j 25-54

25.785 a,b,c,d,e, g,i,k 25-51

25.787 a,b,c 25-51

25.789 a,b 25-46 SECT. PARA. AMDT.

25.791 a,b,c,d,e 25-72

25.793 - 25-51

25.803 e,1,2 25-46

25.807 b 25-55

25.809 b,d 25-47

25.811 a,b,c,d,1, 2,e,1,f,1, 2,g 25-46

25.812 a1,2,c,d, h,i,k 25-46

25.813 a,b,c,2,d, e,f 25-46

25.815 - 25-38

25.817 - 25-15

25.831 a,b,c,d,e, f 25-41

25.851 a,1,2,3,5, 7,8 25-74

25.853 a,c,f,g,h 25-83 a,b 25-116

25.855 d,e,f,g 25-93

25.856 a 25-111

25.869 a,1,2,3,4, c 25-72

25.981 a,3 25-102 SECT. PARA. AMDT.

25.1301 a,b,c,d O

25.1307 c 25-72

25.1309 a,b,d,e,f, g 25-41

25.1351 a,1 25-72

25.1353 a,b,c 25-42

25.1355 a 25-38

25.1357 a,c O

25.1411 a,b,d,1,2, 4,e,f,g 25-79

25.1415 a,b,c,d 25-82

25.1431 c O

25.1438 a,b,c 25-41

25.1439 a,b 25-38

25.1447 c,1 25-41

25.1529 - 25-54

25.1541 a,b O

25.1557 a,b,c 25-72

25.1561 a,b,c,d,e 25-46

25.1581 a,b,d 25-72 H25.1 a,b,c 25-54 H25.2 a,b 25-54 H25.3 a,b,c,d,e, f,g 25-54 END

## Every issue (1)

- August 24, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/12/e7/12e72b65cae901f5f12e65f8d4258d50037165b05297aa59a5fcdbaa7f4b129b)

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