# STC ST00111IB

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Airbus STC Solutions
- Description: Installation of fittings and VIASAT OAE
- Status date: May 10, 2023
- Data sheets: T00063IB
- Certificate PDF: https://openairdocs.org/files/sha256/db/a2/dba2b011e437aeab1b05adc08d409804127cbecc676dd914521bee2340b29e7b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161049297820230518131805.0001
- Page: https://openairdocs.org/stc/ST00111IB

## ADs that name it

None.

## Approved models (1)

- Airbus SAS A350-941 (TCDS T00063IB)

## 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.

IMPORT ST00111IB Airbus STC Solutions 2 Rond Point Emile Dewoitine F-31700, Blagnac France 25 Title 14 Code of Federal Aviation Regulations T00063IB AIRBUS S.A.S.

A350-941

1. Installation of fittings and VIASAT OAE in accordance with Master Data List, Doc. MDL AI0253 dated, March 8, 2023 or later EASA approved revisions.

(Description of Type Design Change continued on page 3 of 4)

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

(Limitations and Conditions continued on page 3 of 4) January 31, 2023 May 10, 2023 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4

**IMPORT ST00111IB 4**

IMPORT ST00111IB Description of Type Design Change: (continued from page 1 of 4)

2. Operation must be in accordance with Airbus Airplane Flight Manual, dated May 4, 2023 or later EASA approved revisions.

3. Maintenance must be accordance with Instructions for Continued Airworthiness, ICA MOD AI0253, dated January 27, 2023 or later EASA approved revisions.

Limitations and Conditions: (continued from page 1 of 4)

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 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 A350-941 series.

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 A350-941 series is shown on TCDS T00063IB for parts not changed or not affected by the change.

(certification basis continued on page 4 of 4) 3 4

IMPORT ST00111IB Certification Basis: Continued from page 3 of 4

b. The Type Certification basis for the A350-941 series is shown on TCDS T00063IB for parts changed or affected by the change in addition to the following:

Equivalent Level of Safety (ELOS) Finding has been made for the following regulation: §25.251 Vibration/Buffeting Compliance Criteria (documented in ELOS Memorandum ST11630IB-T-F-1 dated April 17, 2023.

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## Every issue (1)

- May 10, 2023: Issued, Current. [certificate](https://openairdocs.org/files/sha256/db/a2/dba2b011e437aeab1b05adc08d409804127cbecc676dd914521bee2340b29e7b)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.