TUPOLEV PSC TUPOLEV TU 204-120CE: certification basis

Basis entries as written on the TCDS

1. REG

   1. NGLS-3 for TU 204, TU 204-120 and TU 204-120C and for TU 204-120CE AP 25; sp

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

2. REG

   2. Recertification of the TU-204-120CE is based on Aviation Regulations, Part 25 "Airworthiness Standards: Transport Category Airplanes" through Amendments 4 and some provisions in Amendment 5;

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

3. REG

   3. Aviation Regulations, Part 36, para 3 and ICAO Annex 16, Chapter 3 Standards on noise, and ICAO Annex 16, v. II "Aircraft Engine Emissions" approved 30.01.2004. su

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

4. REG

   4.1. Mandatory EASA Airworthiness Requirements: 4.1.1. The mandatory EASA airworthiness standards for TU 204-120CE relating to the reference date of February 26, 1993 are the following: JAR 25 Change 13 05 October 1989 JAR AWO Change 1 10 July 1985 4.1.1.2. Reversions: 4.1.1.3. Special Conditions: 4.1.1.3.1. Novel or unusual Features or unconventional use: SC Tupolev TU 204-120/-120C/D-06 Courier Area (CRI D-06) 4.1.1.3.2. General Experience: SC Tupolev TU 204-120/-120C/B-01 Accelerate-Stop Distances and related Performances (CRI B-01), INT/POL/25/5 SC Tupolev TU 204-120/-120C/B-02 Severe Icing Conditions (CRI B-02), INT/POL/25/11 SC Tupolev TU 204-120/-120C/B-07 Human Factors Aspects of Flight Deck Design d (CRI B-07),INT/POL/25/14 de SC Tupolev TU 204-120/-120C/C-01 SC Tupolev TU 204-120/-120C/C-02 Yawing Manoeuvering Conditions (CRI C-01), INT/POL/25/8 Fuel Tank Crashworthiness (CRI C-02), INT/POL/25/9 en SC Tupolev TU-204-120/-120C/D-04 Class E Cargo Compartments Essential Systems Fire protection (CRI D-04), INT/POL/25/15 SC Tupolev TU 204-120/-120C/D-05 Worn Brakes (CRI D-05), INT/POL/25/6 sp SC Tupolev TU 204-120/-120C/E-05 Fuel Tank Safety CRI E-05), INT/POL/25/12 SC Tupolev TU 204-120/-120C/F-01 Protection from Effects of HIRF su (CRI F-01), INT/POL/25/2 SC Tupolev TU 204-120/-120C/F-02 Lightning Protection, Direct Effects (CRI F-02), INT/POL/25/3 SC Tupolev TU 204-120/-120C/F-03 Lightning Protection Indirect Effects (CRI F-03), INT/POL/25/4 4.1.1.4. Equivalent Safety Findings: JAR 25.858(c) Fire Detection Test in Flight, CRI F-21 JAR 25.1461(c) Equipment containing high energy rotors, CRI -20 4.1.1.5 Exemptions: No exemptions have been granted. 4.1.2. Mandatory EASA airworthiness standards for TU 204-120CE relating to reference date of September 15, 1997 are as follows: JAR 25 Change 14 04 May 1994 Orange Paper 25/96/1 19 April 1996 with Reversion to JAR 25 Change 13 for 25.1351 (d)(1); JAR AWO Change 2 01 August 1996 d 4.2. Elect to Comply Requirements: JAR 25 Change 14 de Elect to comply requirement for the TU 204-120CE not affected by the significant design change passenger to freighter conversion. Orange Paper 25/96/1 04 May 1994 19 April 1996 en with Reversion to JAR 25 Change 13 for 25. 1351 (d)(1); JAR 25.335(a)(2) Change 15 01 October 2000, (CRI C-11) JAR AWO Change 2 01 August 1996 sp

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

5. OTHER

   Noise: ICAO Annex 16, Volume I (Third Edition)

6. OTHER

   Fuel: ICAO Annex 16, Volume II (Second Edition) su

7. Special conditions: none recorded.
8. Equivalent level of safety findings: none recorded.
9. Exemptions: none recorded.