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Textron Aviation, Inc. 700: certification basis

TCDS EASA.IM.A.620 revision 3 (26 Oct 2021) · Transport · EASA · Source TCDS

Export CSV Export JSON All entries: /aircraft/easa/EASA.IM.A.620/700/basis.csv

Basis entries as written on the TCDS

  1. REG

    FAA Type Certificate Data Sheet No. T00015WI

    State of Design Airworthiness Authority Type Certification Data Sheet No.

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

  2. REG

    See FAA Type Certificate Data Sheet No. T00015WI

    State of Design Airworthiness Authority Certification Basis

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

  3. REG

    Certification Specification CS-25 Amendment 15, dated 23 July 2014 amended with the following requirements: CS 25.1316 and CS 25.1317 at CS-25 Amendment 17, dated 16 July 2015.

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

  4. REG

    CS 25.975 at CS-25 Amendment 18, dated 22 June 2016.

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

  5. REG

    CS 25.603(a), 25.788(b), 25.811(e)(2), 25.812(d), Appendix S at CS-25 Amendment 19, dated 12 May 2017

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

  6. REG

    CS 25.853(g) at CS-25 Amendment 23, dated 16 July 2019 CS-ACNS issue 2 dated 26 April 2019 CS-FCD Initial Issue, dated 31 January 2014 CS-MMEL Initial Issue, dated 31 January 2014 CS-SIMD Initial Issue, dated 2 December 2014

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

  7. ◆ SPECIAL

    Flight Instrument External Probes – Qualification in Icing Conditions Control Surface Position Awareness / Electronic Flight Control Systems Airworthiness Standards for aircraft operations under snow both falling and blowing Rudder Control Reversal Load Conditions High Altitude Operation above 41.000 ft / High Cabin Heat Load Personal injury criteria of dynamic testing of side facing sofas Occupant Protection for Side-Facing Seat Installed Forward of Aft-Facing Seat Pilot compartment view – Hydrophobic coatings in lieu of windshield wipers Water / Ice in Fuel Engine Cowling Retention Use of APR for Go-Around Performance Credit Flight Recorders including Data Link Recording Security Protection of Aircraft Systems and Networks Rechargeable Lithium battery installations

  8. ◆ SPECIAL

    Non-rechargeable Lithium Battery Installations MCSD requirements

  9. OTHER

    Deviation to CS 25.981(b)(3), M25.1(a), M25.1(b) and M25.2(b) ofappendix M of CS 25 amdt. 15 for fuel tank flammability reduction means

  10. ELOS

    Pressurisation and Low Pressure Pneumatic System Flight Control System Failure Criteria Cabin Outflow Valve Cabin Entry Door Latching and Locking Independence Ditching Emergency Exits for Passengers Green Arc for Powerplant Instrument Thrust Reverser Testing Powerplant Valves Indication Electronic Standby Direction Indicator (Compass)

  11. OTHER

    N-01 See EASA Noise Type certificate Data Sheet, TCDSN IM.A.620

  12. OTHER

    N-02 Fuel Venting Requirements, ICAO Annex 16, Volume II, Part II, Chapter 2

  13. Exemptions: none recorded.
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