What it approves
Remove the existing G5 galley and replace it with a Diehl SKYPAX monument
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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: ST00173IB
This certificate issued to: Lufthansa Technick AG WEG BEIM JAEGER 193 22335 HAMBURG
GERMANY Part 25 of Title 14 Code of Federal Regulations .
A28NM Make: Airbus SAS Model: A320-214/-232/-233 A321-211/-231 Description of Type Design Change:
1. Remove the existing G5 galley and replace it with a Diehl SKYPAX monument as defined in acccordance with Master Document List L00120-MDL-001 issue G dated May 17, 2020, or later EASA approved revision, ARINC Specification 677 guidane and the DK180 Technical Manual, 03-TM-0064.
(See Description of Type Design Change Continued on Page 3 of 3)
1. Maintenance must be in accordance with Maintenance Planning Document Supplement L00120-MPD-0002 Revision A dated May 13, 2019 or later EASA accepted revision.
(See Limitations and Conditions Continued on Page 3 of 3)
Date of Application: November 4, 2019 Date Reissued:
Date of Issuance: February 6, 2024 Date Amended:
Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: ST00173IB
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT
(Continuation Sheet) Number: ST00173IB Date Issued: February 6, 2024 Limitations and Conditions (continued):
2. Weight and Balance Manual - Supplement L00120-WBR-0002/4/5/6 used in conjunction with the Original Equipment Manufactruer's (OEM) Weight and Balance Manuel.
3. The installer must determine whether this design change is compatible with previously approved modifications.
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 change excludes the installation of the new floor panels from Euro Compsite.
6. On aircraft affected by this change a yearly inspection must be performed throughout the life of the aircraft in accordance with MPD Supplement L00120-MPD-0002 Revision A dated May 13, 2019 or later EASA accepted revision.. This inspection cannot be changed or modified without prior acceptance from the FAA.
Certification Basis:
Based on 14 CFR §21.115 and §21.101 and FAA Order 8110.48A the certification basis for this modification to the Airbus A320-214, -232, -233 and A321-211, -231 aircraft is TCDS A28NM Revision 43. [ Reference: Report Number E-2104-012-003A dated 12-04-2021, Subject: Validation program and compliance Checklist.]
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