Gulfstream Aerospace Corporation GVII-G500: certification basis

Basis entries as written on the TCDS

1. REG

   T000021AT

   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

   14 CFR Part 25, effective February 1, 1965, including Amendments 25-1 through 25-137.

   State of Design Airworthiness Authority Certification Basis

   Includes 14 CFR 25 through 25-137 · current is 25-153, 16 revisions later

   Expands to 414 provision links ! 1 text missing · shown below

3. REG

   Additional voluntary compliance with Amendment 25-143 for 25.975(a)(7) only as it pertains to fuel tank vents, and Amendment 25-144 for 25.773(e) only as it pertains to pilot compartment view with installed vision systems with transparent displays.

   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.

4. REG

   EASA Certification Specification (CS) 25, Amendment 13, effective as of June 14, 2013 and CS AWO effective October 17, 2003, except where identified below. Additional voluntary compliance with CS 25, Amendment 19: 25.603 [completions phase only], 25.788, Appendix S. Compliance against CS-ACNS, Subpart B, Section 2, and Subpart D, section 4. CS-ACNS, Airborne Communications, Navigation and Surveillance, Issue 3 Subpart E Section 3, dated 31 May 2021

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

5. REG

   The following part of the certification basis constitutes the minimum required safety level of CS 25.571 Amdt. Initial Issue. For changes that affect or introduce fatigue critical structures CS

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

6. REG

   25.571 Amdt. Initial Issue applies, plus:

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

7. REG

   a. WFD evaluations must substantiate freedom from WFD up to the limit of validity (LOV);

   Applies to: 1. For structures susceptible to widespread fatigue damage (WFD)

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

8. REG

   b. Inspections and other maintenance actions upon which the LOV is dependent must be established and submitted to EASA for approval;

   Applies to: 1. For structures susceptible to widespread fatigue damage (WFD)

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

9. REG

   2. The baseline corrosion prevention and control programme must be amended or supplemented to address the influence of the change on the effectiveness of the programme, as necessary.

   Applies to: 1. For structures susceptible to widespread fatigue damage (WFD)

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

10. REG

    Note 1: Points 1 and 2 do not apply to changes introduced by STC.

    Applies to: 1. For structures susceptible to widespread fatigue damage (WFD)

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

11. REG

    Note 2: Points 1 and 2 do not apply to repairs.

    Applies to: 1. For structures susceptible to widespread fatigue damage (WFD)

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

12. REG

    Note 3: CS 25.571 Amdt. Initial Issue or later does not include the above exceptions for STC and repair applicants any longer.

    Applies to: 1. For structures susceptible to widespread fatigue damage (WFD)

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

13. REG

    Note 4: This TCDS entry does not invalidate the 21.A.101 process by which a later CS 25.571 amendment may become applicable.

    Applies to: 1. For structures susceptible to widespread fatigue damage (WFD)

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

14. ◆ SPECIAL

    Subject

15. ◆ SPECIAL

    EASA OSD Maintenance Certifying Staff Data Certification Basis for Gulfstream GVII-G500 EASA OSD Simulator Data for Gulfstream GVII-G500 Flight Envelope Protection High Incidence Protection Function; Stall speeds, stall warning High Altitude Operation Single- and multiple-place side facing seats Electronic Flight Control System: Control Surface Position Awareness Leg Flail Falling and blowing snow Fire Extinguishing Plumbing and Wiring Connections HIRF Protection Data Link Recording Security protection of Aircraft systems and networks Flight Instrument External Probes – Qualification in Icing Conditions Pilot Compartment View Requirement with Enhanced Flight Vision System Non-rechargeable Lithium Battery Installations

16. OTHER

    Subject Compliance against CS 25.1322

17. ELOS

    Subject Electronic Flight Control System: Out-of-Trim Characteristics Flight Control System Failure Criteria Emergency Exit Signs Emergency Exits Exits and seat encroachment* Hydrophobic Coating Combined Aircraft Pressurization Outflow and Positive Pressure Differential Relief Valves Use of Reduced Vertical Bunsen Burner Flammability Requirements for Interior Materials Thrust reverse testing Fan Zone Fire classification Green Arc PWP Instrument TRAS compartment absence of fire detect sys APU Subpart J (Cover CRI)

18. ELOS

    Engine Control in Icing Ignition Switches Vertical Acceleration for flight data recorder Use of an Electric-Only Direction Indicator for Standby Instrumentation

19. ELOS

    Steep Approach and Landing Capability – Demonstration of safe operational and flight characteristics

20. ELOS

    FAA ELOS TD-01-2019-0050-F-15 – Vibration/Buffeting Compliance Criteria for External Modifications Installed on Gulfstream GVII-Series Aircraft

21. ELOS

    *FAA ELOS TC-01-2010-0024-C-7-GVI Rev. 1 - Encroachment into Emergency Exits (for 25.813(c)(2)(ii) aspects of CRI D-17)

22. REG

    CS 36 Amendment 4 NPA 2013-07 Chapter IV (CS 25.571) (CRI C-02)

    Elect to Comply

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

23. REG

    CS 25.1316, Amendment 17

    Elect to Comply

    Includes CS-25 §25.1316 through CS25-17 · current is CS25-28, 11 revisions later

    Expands to 1 provision link · Show the expansion

24. REG

    CS 25 Appendix S, Amendment 19

    Elect to Comply

    Includes CS-25 through CS25-19 · current is CS25-28, 9 revisions later

    Expands to 396 provision links ! 1 text missing · Show the expansion

25. REG

    CS 25.603 [for the Completions STC] and CS 25.788, Amendment 19

    Elect to Comply

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

26. REG

    CS 25.1592 Amendment 27 (for Aircraft with ASC 014 Steep Approach Landing installed)

    Elect to Comply

    Includes CS-25 §25.1592 through CS25-27 · current is CS25-28, 1 revision later

    Expands to 1 provision link · Show the expansion

27. REG

    CS 25 Appendix Q Amendment 13 (for Aircraft with ASC 014 Steep Approach Landing installed)

    Elect to Comply

    Includes CS-25 through CS25-13 · current is CS25-28, 15 revisions later

    Expands to 387 provision links ! 1 text missing · Show the expansion

28. OTHER

    Noise: See TCDSN no. EASA.IM.A.595 Fuel Venting: CS-34 amendment 1, ICAO Annex 16, Volume II, Third edition, Amendment 7, Part II, chapter II.

29. Exemptions: none recorded.