Diamond Aircraft Industries GmbH DA 50 C: certification basis

Basis entries as written on the TCDS

1. REG

   CS-23, Amendment 4, issued 15-Jul-2015 CS-ACNS, Initial Issue, issued 17-Dec-2013 For aircraft equipped with the factory installed Anti-icing system the requirements are listed below: CS-23 Amendment 5: 23.2005, 23.2010,

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

2. REG

   23.2165 with AMC1 ASTM F3120/F3120M-15 Section A1.4 and A2.4 (SLD icing conditions for aircraft not approved for operation in SLD icing conditions) for SLD “detect and exit” and AMC2 CS-23 Amdt 4 23.1419 Ice Protection, 23.2415 with AMC2 CS-23 Amdt 4 23.929, 23.975, 23.997, 23.1093, 23.1105, 23.2540 with AMC2 CS-23 Amdt 4 23.1323, 23.1325(b), (g), 23.1419, 23.775(f)

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

3. ◆ SPECIAL

   Fuel Tank Filler Connection Fuel Tank Outlet Fuel Water Absorption Markings and Placards Powerplant Instruments Powerplant Limitations Cyber Security Battery Endurance

4. OTHER

   CRI F-107 -Continuity requirements for ADS-B

5. ELOS

   Liquid Cooling – Tank Volume

6. OTHER

   see TCDSN EASA.A.639

7. Exemptions: none recorded.