# STC ST11047SC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dassault Aircraft Services - Description: Installation of upgraded hardware to replace Rockwell Collins Pro Line 4 displays with Rockwell Collins Pro Line 21 displays, add an Integrated Flight Information System (IFIS), and enable localizer performance with vertical guidance (LPV) capability - Status date: November 15, 2019 - Data sheets: A50NM, A50NM - Certificate PDF: https://openairdocs.org/files/sha256/a8/72/a8725f4b2b9468f70b38f45b3794c3fd8759614db462e9d1578b58dd8c10e09f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133382971420230302163349.0001 - Page: https://openairdocs.org/stc/ST11047SC ## ADs that name it None. ## Approved models (2) - Dassault Aviation FALCON 2000 (TCDS A50NM) - Dassault Aviation FALCON 2000EX (TCDS A50NM) ## 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. FAA Form 8110-2 (7/19) Page 1 of 3 Number: ST11047SC Parts 25 of the Federal Aviation Regulations. Original Product – Type Certificate Number: A50NM Make: Dassault Aviation Model: Falcon 2000/2000EX Installation of upgraded hardware to replace Rockwell Collins Pro Line 4 displays with Rockwell Collins Pro Line 21 displays, add an Integrated Flight Information System (IFIS), and enable localizer performance with vertical guidance (LPV) capability in accordance with “Master Data List” document no. 365-00-0001, Revision C dated April 01, 2011 or later FAA approved revision; and “Airplane Flight Manual Supplement document” no. 365-00-0056, revision IR dated May 3, 2011 for FMS-6100 version 4.1 or document 365-00-0086 revision IR, dated December 12, 2017 for FMS-6100 version 4.2 or later FAA approved revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. 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. 3. For aircraft with no Flight data recorder (FDR) or FDR with less than 42 parameters, software version 8.0 or later is required. For aircraft with FDR with 42 parameters to 88 parameters, software version 10.4 or later is required. 4. This installation requires the installation of supplemental type certificate ST01833WI AND/OR ST01433WI-D in order to provide global positioning system data enhanced with the wide area augmentation system. Certification Basis: Date of Application: November 30, 2010 Date Reissued: November 15, 2019 Date of Issuance: May 04, 2011 Date Amended: 01/09/18; 08/10/18; 08/28/19 Signature Title Jim Grigg Manager, Fort Worth ACO Branch, Compliance & Airworthiness Division Aircraft Certification Service Dassault Aircraft Services 191 North Dupont Highway New Castle, DE 19720 FAA Form 8110-2 (7/19) Page 3 of 3 FAA Form 8110-2 (7/19) Page 3 of 3 Transfer the ownership of Supplemental Type Certificate Number: ST11047SC To (Name and address of transferee) From (Name and address of grantor) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11047SC FAA Form 8110-2 (7/19) Page 3 of 3 Date of Issuance: May 04, 2011 Date Amended: August 28, 2019 Date of Reissuance: November 15, 2019 Certification Basis (Continued): 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 Dassault Aviation Falcon 2000/2000EX series aircraft modified by for the installation of Pro Line 21 equipment updates with MR 10.4 Adaptive Flight Displays (AFD) that includes both the Primary Flight Displays (PFDs) & the Multifunction Flight Displays (MFDs), Data Concentrator Units (DCUs), Input Output Concentrators (IOCs) and Optional Data Base Unit (DBU) is as follows: a. The type certification basis for Dassault Aviation Falcon 2000/2000EX series airplanes is shown on TCDS A50NM for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, 11/30/2010, include: 14 CFR § Part 25 Regulations at the latest amendment 25-0 through 25-129 14 CFR § 25.1; 25.2; 25.23(b); 25.301; 25.303; 25.305(a)(b); 25.307(a); 25.321; 25.341(a); 25.365; 25.561(a)(b); 25.571(a)(b); 25.581(a)(b); 25.601; 25.603; 25.605(a); 25.609(a); 25.613(a)(b); 25.771(a); 25.773(a); 25.789(a); 25.1303; 25.1307(c); 25.1316; 25.1317(d); 25.1321(a)(b)(e); 25.1322; 25.1329; 25.1331; 25.1333; 25.1351(a); 25.1381; 25.1431; 25.1501; 25.1519; 25.1523; 25.1529; 25.1541; 25.1543; 25.1555(a); 25.1581; 25.1583(h); and 25.1585(a) 14 CFR § Part 25 Regulations at an intermediate amendment 14 CFR §25.981(a)(3) amendment 25-102, 25.1353(a)(b)(d) amendment 25-113 14 CFR regulations at amendment level in TCDS A50NM 14 CFR §25.869(a)(4); 25.1301, 25.1309, 25.1357(a)(c) Exemptions from 14 CFR part 25 – None Equivalent safety findings exist with respect to the following regulations – None Special conditions – None Special Federal Aviation Regulations – None -END- ## Every issue (4) - November 15, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a8/72/a8725f4b2b9468f70b38f45b3794c3fd8759614db462e9d1578b58dd8c10e09f) - August 10, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b6/53/b65329fbbb37ce6fa6950212a0bb06a44d59cd160b01aaceacf862654520c8d2) - January 9, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/60/d0/60d05fee21c9987e92c9f9aeba85fd9cf6a1b114dd0fa9d92f2312e03aef59a9) - May 4, 2011: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/7c/b5/7cb5c722c719516f1e2980f3954f1f3b6773786f13e69451ea50bf915b8e999d) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.