# STC SA03012CE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Diamond Aircraft Industries GmbH - Description: Installation of Multi-Purpose Platform (MPP) Basic Options - Status date: August 28, 2025 - Data sheets: A00012NY - Certificate PDF: https://openairdocs.org/files/sha256/e2/b6/e2b6e2962c6510a0a1a63c147800ca0ed6581f1af9ef294fde387f9f90d38030 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161392578020250828182939.0001 - Page: https://openairdocs.org/stc/SA03012CE ## ADs that name it None. ## Approved models (1) - Diamond Aircraft Industries Inc DA 62 (TCDS A00012NY) ## 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. FAA 8110-2 (10/24) Page 1 of ___ IMPORT SA03012CE Diamond Aircraft Industries GmbH Nikolaus-August-Otto-Strasse 5 2700 Wiener Neustadt Austria Part 23 Title 14 Code of Federal Regulations A00012NY Diamond Aircraft Industries Inc. DA 62 1. This approval is limited to only the installation of provisions. The FAA has not certified the equipment for which these provisions are intended. You must get an FAA approval to install the equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards. (See Continuation Sheets 4 and 5) 03/08/2021 11/29/2021 08/28/2025 John Yoo Manager, International Validation Branch, AIR-730 Compliance & Airworthiness Division Aircraft Certification Service 5 1. Installation of Multi-Purpose Platform (MPP) Basic Options in accordance with Master Drawing List, document number STC 62-001, revision f, dated November 13, 2020, or later EASA approved revision. (See Continuation Sheets 3 and 4) FAA 8110-2 (10/24) Page ___ of ___ IMPORT SA03012CE 08/28/2025 Date Amended: August 28, 2025 Description of Type Design Change (continued): 2. Aircraft is to be maintained in accordance with Diamond Aircraft Industries Instructions for Continued Airworthiness (ICA): Supplemental AMM Doc. No. 7.02.25-M00, dated March 15, 2018, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M20, dated March 15, 2018, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M30, dated March 15, 2018, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M50, dated August 25, 2020, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M70, dated March 15 2018, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M80, dated March 15, 2018, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M90, dated March 15, 2018, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M130, dated November 15, 2018, or later EASA accepted revision. Supplemental AMM Doc. No. 7.02.25-M180, dated September 15, 2021, or later EASA accepted revision. 3. Aircraft is to be operated in accordance with Diamond Aircraft Industries Airplane Flight Manual (AFM) Supplements: (see Description of Type Design Change Continued on Page 4 of 4) 3 5 Add Page FAA 8110-2 (10/24) Page ___ of ___ IMPORT SA03012CE 08/28/2025 Date Amended: August 28, 2025 Description of Type Design Change (continued): AFM Supplement STC-62-001-M00 to Doc. No. 7.01.25-E, revision 2, dated August 25, 2021, or later EASA approved revision. AFM Supplement STC-62-001-M20 to Doc. No. 7.01.25-E, dated March 15, 2018, or later EASA approved revision. AFM Supplement STC-62-001-M30 to Doc. No. 7.01.25-E, dated March 15, 2018, or later EASA approved revision. AFM Supplement STC-62-001-M50 to Doc. No. 7.01.25-E, dated August 25, 2020, or later EASA approved revision. AFM Supplement STC-62-001-M70 to Doc. No. 7.01.25-E, dated March 15, 2018, or later EASA approved revision. AFM Supplement STC-62-001-M80 to Doc. No. 7.01.25-E, dated March 15, 2018, or later EASA approved revision. AFM Supplement STC-62-001-M90 to Doc. No. 7.01.25-E, dated March 15, 2018, or later EASA approved revision. AFM Supplement STC-62-001-M130 to Doc. No. 7.01.25-E, dated November 15, 2018, or later EASA approved revision. AFM Supplement STC-62-001-M180 to Doc. No. 7.01.25-E, dated September 15, 2021, or later EASA approved revision. 2. The aircraft must be operated in accordance with the limitations section of the flight manual supplements referenced in the Description section. 3. The aircraft must be maintained in accordance with the airworthiness limitations section of the ICAs referenced in the Description section. 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. FAA 8110-2 (10/24) Page ___ of ___ IMPORT SA03012CE 08/28/2025 Date Amended: August 28, 2025 Limitations and Conditions (continued): 5. The installer must determine whether this design change is compatible with previously approved modifications. 6. A copy of this certificate, issued November 29, 2021 or later FAA approved revisions, must be maintained as part of the permanent records for the modified aircraft. 7. This STC is applicable to serial numbers 62.007 and subsequent. Certification Basis: The Type Certification Basis for the original product remains applicable to this certificate. This certificate involves a change with an impact on noise. The noise standards are amended as follows: 14 CFR part 36, as amended by Amendments 36-1 through 36-31. ----------END---------- 5 5 Add Page ## Every issue (2) - August 28, 2025: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e2/b6/e2b6e2962c6510a0a1a63c147800ca0ed6581f1af9ef294fde387f9f90d38030) - November 29, 2021: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/73/e0/73e0b7f28bdb021a6858f6d5aff489782c51d0513a4375bd6f60de8b96a7baf5) --- 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.