What it approves
Installation of Dual Universal Avionics EFI-890R Advanced Flight Display System
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.
FAA 8110-2 (10/24) Page 1 of ___ IMPORT ST11887IB Mid Canada Mod Center 2450 Derry Road East, Hangar #9 Mississauga, Ontario Canada L5S 1B2 Part 25 Title 14, Code of Federal Regulations A16WE The Boeing Company 737-200 Series, 737-200C Series
1. 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.
2. The installer must determine whether this design change is compatible with previously approved modifications.
3. This STC is applicable to all serial numbers for these Make-Models.
(See continuation sheet 3) 2/5/21 1/28/25 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4
1. Installation of Dual Universal Avionics EFI-890R Advanced Flight Display System must be in accordance with Avionics Design Services Ltd. Master Drawing List MDL17056 Revision D, Transport Canada Civil Aviation (TCCA) approved January 15, 2025, or later TCCA approved revision.
2. Operation must be in accordance with Mid Canada Mod Center Flight Manual Supplement FMS17056-1 Revision C, TCCA approved January 15, 2025, or later TCCA approved revision.
3. Maintenance must be in accordance with Mid Canada Mod Center Instructions for Continued Airworthiness ICA17056-1 Revision B, dated November 28, 2020, or later TCCA accepted revision.
4. The aircraft must be operated in accordance with the Certificate Limitations section of the flight manual supplement identified in the Description of Type Design Change section.
5. The aircraft must be maintained in accordance with Airworthiness Limitations AWL17056-1 Revision N/C, TCCA approved January 17, 2020 or later TCCA approved revision.
Note: This STC does not require a revised Electrical Wiring Interconnection System (EWIS) Instructions for Continued Airworthiness (ICA).
Certification Basis:
Based on Title 14 Code of Federal Regulations (14 CFR) § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the type certification basis for modified Boeing 737-200 Series, 737-200C Series is as follows:
a. The type certification basis for the Boeing 737-200 Series, 737-200C Series is shown on Type Certificate Data Sheet (TCDS) A16WE for parts not changed or not affected by the change.
b. The type certification basis for the Boeing 737-200 Series, 737-200C Series for parts changed or affected by the change is shown on TCDS A16WE with the following additional 14 CFR requirements:
25.771 at Amendment 25-4
25.1322 at Amendment 25-38
25.1321, 25.1331, 25.1333 at Amendment 25-41
25.571 at Amendment 25-45
25.777(a)(b)(c) at Amendment 25-46
25.1529 at Amendment 25-54
25.1381 at Amendment 25-72
25.1303 at Amendment 25-90
25.1431 at Amendment 25-113
25.1317(a)(b)(c) at Amendment 25-122
25.1301(a), 25.1309(a)(b)(c)(d)(e), 25.1310, 25.1353, 25.1357 at Amendment 25-123
25.1316 at Amendment 25-134
25.773(a) at Amendment 25-144
26.11 at Amendment 26-0
26.47 at Amendment 26-1
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