What it approves
Installation of upgraded hardware to the Rockwell Collins Pro Line IV FMS-6100 to provide Localizer Performance with Vertical Guidance (LPV)
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.
ST10978SC BHE and Associates 8627 Cinnamon Creek Dr Suite 301 San Antonio, TX 78240 Part 25 the Title 14, Code of Federal Regulations A50NM Dassault Aviation Falcon 2000, 2000EX 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.
(See Continuation Sheet 3 of 3) 03/01/2010 08/06/2025 08/03/2010 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3 Installation of upgraded hardware to the Rockwell Collins Pro Line IV FMS-6100 to provide Localizer Performance with Vertical Guidance (LPV) in accordance with master drawing list 347-00-0001, revision B, dated June 21, 2010, or later approved FAA revision. Airplane flight manual supplement, document 347-00-0014, revision IR, dated June 30, 2010, or later approved FAA revision, is required.
FAA 8110-2 ( 10/24) Page 2 of __
ST10978SC 08/06/2025 3
ST10978SC 08/06/2025 Certification Basis:
Based on 14 CFR §§21.115 and 21.101, and FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Dassault Falcon 2000 and Falcon 2000EX modified by upgrading the FMS-6100 with Localizer Performance with Vertical Guidance (LPV) is as follows:
a. The type certification basis for Dassault Falcon 2000 and Falcon 2000EX 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 applications, March 3, 2010, is based upon part 25 as amended by Amendment 25-129.
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 modification is determined to be:
Regulations at the latest amendment 25-0 through 25-129 14 CFR §25.1, 25.2, 25.23, 25.29, 25.581(a)(b), 25.601, 25.981(a), 25.1316(b)(c), 25.1317
(d), 25.1321(a)(e), 25.1322(b)(c)(d), 25.1351(a), 25.1381, 25.1431, 25.1529, 25.1541,
25.1555(a), 25.1581, 25.1583(h), and 25.1585(a).
Regulations at an intermediate amendment None
Regulations at the amendment level in TCDS A50NM 14 CFR §25.869(a)(4), 25.1301, 25.1309, 25.1353(a)(c) and 25.1357(a)(c)
-END- 3 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 6, 2025 | Reissued, current | Certificate |
| August 3, 2010 | Issued, earlier issue | Certificate |