# STC ST04739NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Space Exploration Technologies Corp./Starlink Aviation, United States
- Description: Installation of Dual SpaceX Starlink Aviation System
- Applied: July 3, 2024
- Status date: July 30, 2026
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS T00001SE](https://openairdocs.org/tcds/T00001SE)
- Certificate PDF: https://openairdocs.org/files/sha256/e1/e0/e1e02a675d8c01a5c60f8ca95e7e0082698bcdcd71ddab8c27a3cd20949c9b12
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198380237020260807142037.0001
- DRS record last changed: August 7, 2026
- Page: https://openairdocs.org/stc/ST04739NY

## ADs that name it (0)

None.

## Approved models (3)

- The Boeing Company 777-200 Series ([TCDS T00001SE](https://openairdocs.org/tcds/T00001SE))
- The Boeing Company 777-200LR Series ([TCDS T00001SE](https://openairdocs.org/tcds/T00001SE))
- The Boeing Company 777-300ER Series ([TCDS T00001SE](https://openairdocs.org/tcds/T00001SE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 

BB__ BB_.

Original Product 7\SH&HUWLILFDWH1XPEHU Make:

VHHFRQWLQXDWLRQVKHHW IRUDGGLWLRQDOGDWHV By Direction of the Administrator Signature:

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(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 the certificate to alter the product, the holder must give the other person written evidence of that permission.

(Limitations and Conditions Continued on Page 3 of 3) 7/3/24 10/17/24 6/9/26 10/10/24 4/30/25 8/26/25 11/7/25 ✔ ODA administrator, ODA-834634-NE 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number  (IIHFWLYH'DWH I Transferr Endorsementt Transfer the ownership of Supplemental Type Certificate Number:

Too (Name and address of transferee):

Date oI transfer:

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(Continuation Sheet) Number  (IIHFWLYH'DWH  $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOH E\D ILQH RIQRW H[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ \HDUVRUERWK7KLVFHUWLILFDWH PD\ EHWUDQVIHUUHGRUPDGH DYDLODEOHWR WKLUGSHUVRQVE\OLFHQVLQJDJ UHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQ RIWKLV6XSSOHPHQWDO7\SH &HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH 67&KROGHUGR HVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWD QRUWRDOWHUDQ DLUFU DIW DLUFUDIWHQJLQH KROGHU$Q 67&KROGHUZKRDOORZVDSHUVRQWRXVHWKH67&WRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHUPXVWSURYLGH WKDWSHUVRQZLWKZULWWHQ SHUPLVVLRQ DFFHSWDEOHWR WKH)$$ 5HI &)5  )$$  3DJH BBBRI BBB ST04739NY Date Amended (continued from Page 1 of 3): 6/06/2026, 7/30/2026.

Limitations and Conditions (continued from Page 1 of 3):

(3) This STC is applicable to all serial numbers for the Make: The Boeing Company Models:

777-200LR Series, 777-300ER Series & 777-200 Series.

(4) Separate approval for Title 14 CFR Part 25 Subparts B & C (Flight & Structure) is required for the SpaceX Starlink Antenna Assembly installation. SpaceX STC ST04738NY meets this approval requirement.

(5) The SpaceX Starlink Aviation System may not interface with any aircraft system other than power and ground.

(6) Operational approval to permit use of Portable Electronic Devices (PED) is not part of this STC.

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 8110.48, the certification basis for The Boeing Company Models: 777-200LR Series, 777-300ER Series & 777-200 Series is as follows:

(1) The type certification basis for parts not changed or not affected by the change is shown on TCDS T00001SE.

(2) The modification certification basis for parts changed or affected by the change since the reference application date, July 3, 2024, is based upon 14 CFR part 25 (dated 01Feb1965) as amended by Amendments 25-1 through 25-100, with the exception of those above 25-100 as follows:

25.613(a)(b)(c) amdt 25-112, 25.853(a) amdt 25-116, 25.869(a)(1)(4) amdt 25-113,

25.1353(a)(d) amdt 25-113, 25.1431(c) amdt 25-113.

(3) Compliance has been demonstrated to 14 CFR Part 26.11(c) amdt 26-7.

For Model 777-200 Series & 777-300ER Series only, additionally 14 CFR part 26.47(c) amdt

26-1.

--- END --- 33 07/30/26

## Every issue (4)

- July 30, 2026: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e1/e0/e1e02a675d8c01a5c60f8ca95e7e0082698bcdcd71ddab8c27a3cd20949c9b12)
- August 26, 2025: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/dc/af/dcaf70b75a68e0049174239cd828924e4bab2985215be703a944bf71a6e1a61b)
- April 30, 2025: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/6f/4e/6f4ec085804984d3e9af725f02cde75917f8d73b5551627395e8fc043e62cf7a)
- October 17, 2024: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/46/b9/46b9c0bb126285a33a3181eab6ac1e8a0985b733bffa2b9665ce6266ce94c90c)

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