STC ST00063IB

IMPORT ST00063IB FOKKER SERVICES B.V.

HOEKSTEEN 40 2132 MS HOOFDDORP

NETHERLANDS Part 25 Title 14 Code of Federal Regulations A2NM The Boeing Company 757-200, 757-200PF, 757-300 Series

1. Installation of CPDLC (Controller Pilot Data Link Communication) must be in accordance with Fokker Services B.V. Master Document List No. B757-CPDLC-MDL-0001, Issue 2, dated September 22, 2022, or later EASA approved revisions.

(See 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.

(See Limitations and Conditions Continued on Page 3 of 3) August 17, 2022 September 27, 2022 September 8, 2022 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

IMPORT ST00063IB 3

IMPORT ST00063IB Date Reissued: September 27, 2022

Description of Type Design Change (continued):

2. Maintenance must be in accordance with Fokker Services B.V. Instructions for Continued Airworthiness Doc. No. SE-782, Issue 2, dated January 21, 2021, or later EASA accepted revisions.

3. Operation must be in accordance with Fokker Services B.V. Airplane Flight Manual Supplement Doc. No. B752-EXS-AFM-S-001, Rev. 4, dated March 11, 2019, or later equivalent publications issued for different customers under a different reference, as identified in the Master Document List B757-CPDLC-MDL-0001, Issue 2, dated September 22, 2022, or later EASA approved revisions.

2. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. Maintenance must be in accordance with the "Airworthiness Limitations" section of Fokker Services B.V. Instructions for Continued Airworthiness referenced under the Description of the Type Design section.

4. Operation must be in accordance with the "Limitations" section of Fokker Services B.V. Airplane Flight Manual Supplement referenced under the Description of the Type Design section.

5. This STC is applicable to all serial numbers for this Make/Model.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48A, the certification basis for The Boeing Company Model 757-200, 757-200PF, and 757-300 Series aircraft as follows:

a. The type certification basis for the aircraft is shown on TCDS A2NM for parts not changed or not affected by the change.

b. The type certification basis for the aircraft is shown on TCDS A2NM for parts changed or affected by the change.

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