# STC ST11835AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: B/E Aerospace, Inc. - Aftermarket Services, United States
- Description: Removal of floating panel from cabin interior partition and installation of vases and magazine racks
- Applied: July 15, 2024
- Status date: July 6, 2026
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS T00001SE](https://openairdocs.org/tcds/T00001SE)
- Certificate PDF: https://openairdocs.org/files/sha256/40/d2/40d28e72101a7b2204f861dba16f22ed21921f5ded31685d1f0301c7ff456432
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127051456020260710165400.0001
- DRS record last changed: July 10, 2026
- Page: https://openairdocs.org/stc/ST11835AT

## ADs that name it (0)

None.

## Approved models (1)

- 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.

ST11835AT B/E Aerospace, Inc. - Aftermarket Services 1455 Fairchild Road Winston-Salem, NC 27105 Part 25 Federal Aviation Regulations T00001SE Boeing 777-300ER Series Removal of floating panel from cabin interior partition and installation of vases and magazine racks in accordance with FAA approved B/E Aerospace, Inc.'s Master Drawing List MDL-AM80098, Revision C, dated November 12, 2024; or later FAA approved revision.

The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. (Limitations and Conditions continued on page 3 of 4) July 15, 2024 July 6, 2026 November 15, 2024

(for) Michael Linegang Manager, East Certification Branch 4

ST11835AT 4

ST11835AT

Limitations and Conditions: (continued)

The installer must determine whether this design change is compatible with previously approved modifications.

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.

A copy of this STC must be included in the permanent record of the modified aircraft.

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 models listed on page 1 of this certificate is as follows:

a. The type certification basis for parts not changed or not affected by the change, for the models listed on page 1 of this certificate, is shown on TCDS T00001SE.

b. The certification basis for parts changed or affected by the change since the reference date of application, July 15, 2024, is based upon Part 25 as amended by Amendment 25-150. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for non-significant changes in FAA Order 8110.48A, the certification basis for this modification was determined to be: (Certification Basis Continued on Page 4 of 4) 3 4

ST11835AT

(Certification Basis Continued)

Regulations at the latest amendment 25-1 through 25-150:

None

Regulations at an intermediate amendment:

None

Regulations at the amendment level in TCDS T00001SE for the Model 777-300ER Series:

25.301(b)(c), 25.303, 25.305(a)(b)(c), 25.307(a)(d), 25.561, 25.601, 25.603(a)(b)(c),

25.605(a), 25.607(a)(b), 25.609(a)(b), 25.611(a)(b), 25.613(a), 25.785(d)(2)(k),

25.789(a), 25.853(a)(d), 25.1529, and 25.1541(a)(b).

--------------------END-------------------- 4 4

## Every issue (1)

- July 6, 2026: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/40/d2/40d28e72101a7b2204f861dba16f22ed21921f5ded31685d1f0301c7ff456432)

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