What it approves
Installation of the AFIRS (Automated Flight Information Reporting System) Edge 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.
500, 1212 – 31st Avenue N.E.
Calgary, Alberta Canada T2E 7S8 Part 25 Title 14, Code of Federal Regulations A16WE The Boeing Company 737-700 Series, 737-800 Series, 737-8
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) 7/10/24 2/12/25 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4 Boeing 737-700 Series, Boeing 737-800 Series:
1. Installation of the AFIRS (Automated Flight Information Reporting System) Edge system must be in accordance with FLYHT Aerospace Solutions Ltd. Installation Instructions 151-0072, Rev. D, dated October 23, 2024, or later Transport Canada Civil Aviation (TCCA) approved revisions.
2. Operation must be in accordance with FLYHT Aerospace Solutions Ltd. Airplane Flight Manual Supplement 155-0027, Rev. --, dated March 28, 2024, or later TCCA approved revisions.
3. Maintenance must be in accordance with FLYHT Aerospace Solutions Ltd. Instructions for Continued Airworthiness 153-0097, Rev. C, dated October 23, 2024, or later TCCA accepted revisions.
4. Definition of Type Design change per FLYHT Aerospace Solutions Ltd. Master Document List 121-0091, Rev. D, dated October 23, 2024, or later TCCA approved revisions.
Boeing 737-8:
1. Installation of the AFIRS Edge system (provisions) must be in accordance with FLYHT Aerospace Solutions Ltd. Installation Instructions 151-0075, Rev. B, dated October 23, 2024, or later TCCA approved revisions.
2. Maintenance must be in accordance with FLYHT Aerospace Solutions Ltd. Instructions for Continued Airworthiness 153-0102, Rev. A, dated October 24, 2024, or later TCCA accepted revisions.
3. Definition of Type Design change per FLYHT Aerospace Solutions Ltd. Master Document List 121-0095, Rev. B, dated October 23, 2024, or later TCCA approved revisions.
4. For the 737-8 AFIRS Edge system (provisions) installation, activation is not approved.
Note: This STC does not require a revised Electrical Wiring Interconnection System (EWIS) Instructions for Continued Airworthiness (ICA).
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 737-700 Series, 737-800 Series, 737-8 is as follows:
a. The type certification basis for the Boeing 737-700 Series, 737-800 Series, 737-8 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 737-700 Series, 737-800 Series for parts changed changed or affected by the change is per the 737-900ER Series certification basis shown on TCDS A16WE with the following 14 CFR exceptions:
25.899 at Amendment 25-123
25.981 at Amendment 25-125
25.1353(a)(b) at Amendment 25-113
26.11 at Amendment 26-7
26.35 at Amendment 26-7
c. The type certification basis for the Boeing 737-8 for parts changed or affected by the change is shown on TCDS A16WE with the following 14 CFR exception:
26.35 at Amendment 26-7
----------END---------- 4 4
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.