STC ST11851IB

Supplemental type certificate · ELBE FLUGZEUGWERKE GmbH

Holder
ELBE FLUGZEUGWERKE GmbH · Germany
Status
Current · Issued
Status date
November 25, 2024
Applied
September 3, 2024
Product
Aircraft · Large Airplane
Certification basis
Part 25
Data sheet
TCDSA46NM
Foreign approvals
EASA 10077950 Rev. 1

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Removal and Maintenance of Panasonic GCS Antenna

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 ST11851IB ELBE FLUGZEUGWERKE GmbH GRENZSTRASSE 1 01109 DRESDEN

GERMANY Part 25 Title 14 Code of Federal Regulations A46NM Airbus SAS A330-200 Series, A330-300 Series

1. Removal and Maintenance of Panasonic GCS Antenna must be in accordance with Elbe Flugzeugwerke GmbH Engineering Order Number EFW-EO-0171-001, Rev. C, dated June 3, 2024, or later EASA approved revisions.

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

(See Limitations and Conditions Continued on Page 3 of 4) September 3, 2024 November 25, 2024 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4

IMPORT ST11851IB 4

IMPORT ST11851IB Date of Issuance: November 25, 2024

2. Maintenance must be in accordance with Airworthiness Limitations Section Part 2 Supplement Number A330P2F-ALS-ALI-CLC-ENV, Rev. 00, dated December 1, 2021, or later EASA approved revisions.

3. Current STC shall be only applied to aircraft that have the following STCs embodied:

-FAA STC ST02884NY - Installation or Removal of a Panasonic Global Communication Suite (GCS) Antenna -FAA STC ST02923NY - Installation of a Panasonic GCS

4. Current STC shall be applied in conjunction with:

-FAA STC ST04038NY - Conversion of Passenger to Freighter Configuration

5. This STC is applicable to serial numbers as listed on Elbe Flugzeugwerke GmbH Engineering Order referenced in the description of type design change section of this STC.

6. 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.

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 Airbus SAS Model A330-200 and A330-300 Series aircraft as follows:

a. The type certification basis is shown on TCDS A46NM for parts not changed or not affected by the change.

b. The type certification basis is shown on TCDS A46NM for parts changed or affected by the change plus the following exceptions:

14 CFR Part 25 Amendment 25-0: §§ 25.601, 25.609 (a), 25.1301 (a)(b), 25.1519 Amendment 25-23: §§ 25.301, 25.303, 25.607, 25.619 Amendment 25-38: § 25.101 (c)(1)(2) Amendment 25-42: § 25.1353 (a) (Certification Basis Continued on Page 4 of 4) 3 4

IMPORT ST11851IB Date of Issuance: November 25, 2024

Certification Basis (continued):

Amendment 25-46: §§ 25.603, 25.605, 25.613 (a)(b) Amendment 25-54: §§ 25.571 (a)(e), 25.1529 Amendment 25-72: §§ 25.307 (a), 25.571 (b), 25.625, 25.1581 (a)(b) Amendment 25-77: § 25.305 (a)(b)(c) Amendment 25-113: § 25.1353 (d)

14 CFR Part 26: Amendment 26-1 ----------END---------- 4 4

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 14

MakeModelData sheet
Airbus SASA330-201A46NM
Airbus SASA330-202A46NM
Airbus SASA330-203A46NM
Airbus SASA330-223A46NM
Airbus SASA330-243A46NM
Airbus SASA330-301A46NM
Airbus SASA330-302A46NM
Airbus SASA330-303A46NM
Airbus SASA330-321A46NM
Airbus SASA330-322A46NM
Airbus SASA330-323A46NM
Airbus SASA330-341A46NM
Airbus SASA330-342A46NM
Airbus SASA330-343A46NM