What it approves
Installation of Litef s LCR-100N attitude and heading reference system (AHRS) on Rockwell Collins Fusion (EDS) on a Textron Aviation B200GT/B200CGT aircraft
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.
SA11223DS Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 Part 23 Federal Aviation Regulations A24CE Textron Aviation, Inc.
B200GT, B200CGT Installation of Litef’s LCR-100N attitude and heading reference system (AHRS) on Rockwell Collins Fusion (EDS) on a Textron Aviation B200GT/B200CGT aircraft in accordance with “Master Data List,” document no.
606-00-0001, revision IR, dated 7/25/2018 or later FAA approved revision; “Instructions for Continued Airworthiness,” document no. 606-00-0028, revision A, dated 5/18/2018 or later FAA accepted revision; and “Airplane Flight Manual Supplement,” document no. 606-00-0027, revision C, dated 7/23/2018 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. The STC assumes Rockwell Collins Pro Line Fusion Phase 2 or 3 is already installed on each airplane eligible for the proposed modification.
November 20, 2017 August 22, 2018, April 19, 2023 July 25, 2018 October 15, 2018 Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3
SA11223DS 3
SA11223DS Date Reissued: April 19, 2023
New 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 Textron Aviation, Inc. B200GT, B200CGT series aircraft modified by installing Litef’s LCR-100N attitude and heading reference system (AHRS) is as follows:
a. The type certification basis for Textron Aviation, Inc. B200GT, B200CGT series airplanes is shown on TCDS A24CE 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, November 20, 2017, include:
Regulations at the latest amendment 23-0 through 23-63 14 CFR§ 23.1(a)(b), 23.23(b), 23.771(a), 23.777(a)(b), 23.853(a), 23.1431(a)(b),
23.1525, 23.1555(a)
Regulations at an intermediate amendment None
Exemptions from 14CFR part 23 - None
Equivalent safety findings exist with respect to the following regulations - None
Special conditions – None
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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 · 5
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 19, 2023 | Reissued, current | Certificate |
| October 15, 2018 | Amended, earlier issue | Certificate |
| August 22, 2018 | Reissued, earlier issue | Certificate |
| July 26, 2018 | Issued, earlier issue | Certificate |
| July 25, 2018 | Issued, earlier issue | Certificate |