What it approves
Installation of Structural Provision for Cabin Completion
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 ST04719NY Lufthansa Technik AG Weg Beim Jager 193 Hamburg, Germany 22335 Part 25 Title 14 Code of Federal Regulations A21EA-1 MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100 & 440)
1. Installation of Structural Provision for Cabin Completion must be in accordance with Lufthansa Technik Supplemental Type Definition Document Doc. No. STDD00-07/05M, Issue 01, Rev. 00, dated January 29, 2008, or later EASA approved revisions.
(See Description of Type Design Change Continued on Page 3 of 3)
1. The installer must determine whether this design change is compatible with previously approved modifications.
(See Limitations and Conditions Continued on Page 3 of 3) February 16, 2022 March 31, 2022 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3
IMPORT ST04719NY ST04719NY 3
IMPORT ST04719NY Date of Issuance: March 31, 2022
Description of Type Design Change (continued):
2. Maintenance must be in accordance with Lufthansa Technik Instructions for Continued Airworthiness Doc. No. A-00-07/6232-ICA, Issue 01, Rev. IR, dated March 4, 2008, or later EASA accepted revisions.
3. Operation must be in accordance with Lufthansa Technik Flight Manual Supplement Doc. No. A-00-07/6232-AFM, Issue 01, Rev. IR, dated March 4, 2008, or later EASA approved revisions.
2. 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.
3. This STC is applicable to all serial numbers for this Make-Model.
4. Maintenance must be in accordance with the "Airworthiness Limitations" section of Lufthansa Technik, Instructions for Continued Airworthiness referenced under the Description of the Type Design section.
5. For all flights with "Green Aircraft" and "Structural Provisions for cabin completion" (293,7 [kg]) installed the installation of Ferry-Kit M/S TC 601R16990 (867 [kg]) is necessary.
6. With the installation of Ferry-Kit M/S TC 601R16990 (867 [kg]) the aircraft will stay in C.G. envelope.
7. This approval is limited to only the installation of structural provision for cabin completion. The FAA has not certified the equipment for which these provisions are intended. You must get additional FAA approval to install this equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards.
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