What it approves
Activation of SBAS 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.
IMPORT ST00165IB FOKKER SERVICES B.V.
HOEKSTEEN 40 2132 MS HOOFDDORP
NETHERLANDS 25 Title 14 Code of Federal Aviation Regulations A16WE The Boeing Company B737-600/-700/-800/-900/-900ER
1. Activation of SBAS system in accordance with Master Data List, Doc. MDL-0473, dated August 28, 2023 or later EASA approved revisions.
(Description of Type Design Change continued on page 3 of 3)
1. The installer must determine whether this design change is compatible with previously approved modifications.
August 29, 2023 December 29, 2023 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3
IMPORT ST00165IB 3
IMPORT ST00165IB Description of Type Design Change: (continued from page 1 of 3)
2. Operation must be in accordance with Airplane Flight Manual Supplement, doc.
B737-SBAS-AFM-S-001, dated August 18, 2023 or later EASA approved revisions.
3. Maintenance must be accordance with Instructions for Continued Airworthiness, doc.
B737-SBAS-AMM-S-002, B737-SBAS-IPC-S-002 and B737-SBAS-WDM-S-002 as detailed in doc. TE-2788 dated November 3, 2023 or later EASA approved revisions.
Limitations and Conditions: (continued from page 1 of 3)
2. The EASA approved Airworthiness Limitations section of the Instructions for Continued Airworthiness referenced in the Description of the Type Design Section of this STC is mandatory.
3. The aircraft must be operated in accordance with the operations limitations section of the Airplane Flight Manual supplement referenced in the Description of Type Design Section of this STC.
4. 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.
5. This STC is applicable to all make and model of the Boeing 737-600/-700-/-800/-900/-900ER.
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA order 8110.48A, the certification basis for this modification are as follows:
a. The Type Certification basis for the Boeing 737 series is shown on TCDS A16WE for parts not changed or not affected by the change.
b. The Type Certification basis for the Boeing 737 series is shown on TCDS A16WE for parts changed or affected by the change.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.