Textron Aviation Inc. 680: certification basis
Basis entries as written on the TCDS
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REG
T00012WI
FAA Type Certification Data Sheet No.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
See FAA Type Certificate Data Sheet No. T00012WI
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.
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REG
4.1 EASA Airworthiness Requirements for Citation Sovereign
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
JAR 25, Change 15, effective 01 August 2000, CS 25 amendment 1 for the Aft Openable (Foul Weather) Cockpit Window JAR AWO Change 2, effective 01 August 1996, JAA IL-23 RVSM, effective April 1994.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
4.2 EASA Airworthiness Requirements for Citation Sovereign+
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
JAR 25, Change 15, effective 01 August 2000 with the following additions: a) Certification Specification CS 25 Amendment 9, dated 05 August 2010 CS 25 paragraphs Applicability §§ 25.20, 25.21, 25.23, 25.25, 25.27, 25.29, For entire airplane. 25.31, 25.101, 25.103, 25.105, 25.107, 25.109, 25.111, 25.113, 25.115, 25.117, 25.121(a)(b)(c), 25.123(a), 25.145, 25.147, 25.149, 25.161, 25.171, 25.173, 25.175, 25.177, 25.181, 25.201, 25.203, 25.231, 25.233, 25.235, 25.251, 25.253, 25.255 §§ 25.301, 25.303, 25.305(a)(b)(c)(e), 25.307, For the wing modification and winglet 25.321, installation aspect. §§ 25.331(a)(b)(c1), 25.333, 25.335, 25.337, For entire airplane. 25.341, 25.343, § 25.345(a)(b) For the wing modification and winglet installation aspect. CS 25 paragraphs Applicability §§ 25.349, 25.351, 25.361, 25.365(a)(c)(d), For entire airplane. 25.367 §§ 25.373(a), 25.391(a)(e), 25.393, 25.395, For the wing modification and winglet 25.397(a)(c) installation aspect. § 25.399 For entire airplane. § 25.405 For the wing modification and winglet installation aspect. § 25.427 For entire airplane. §§ 25.445, 25.457, 25.459, 25.571 For the wing modification and winglet installation aspect. § 25.581 For winglet installation and all aircraft installations requiring electrical bonding and p-static protection. §§ 25.601, 25.603, 25.605, 25.609, 25.611(a), For the wing modification and winglet 25.613(a)(b)(d)(e), 25.623, 25.625(a)(b)(c) installation aspect. § 25.629 For entire airplane. §§ 25.631, 25.651, 25.657, 25.671, 25.681, For the wing modification and winglet 25.683, 25.693, 25.697(d), installation aspect. 25.863(a)(b)(1)(2)(3)(5)(d), 25.865 § 25.899 For winglet installation and all aircraft installations requiring electrical bonding and p-static protection. §§ 25.951(c), 25.954(a)(b), 25.965(a), 25.967(b) For the wing modification and winglet installation aspect. § 25.981 For winglet installation. § 25.1001 For entire airplane. § 25.1316 Applies to all electrical/electronic systems installed that have system failures classified as Major, Hazardous (Severe-Major), and Catastrophic. §§ 25.1323, 25.1325 For entire airplane. §§ 25.1385, 25.1387, 25.1389, 25.1391, For exterior position and anti-collision 25.1393, 25.1395, 25.1397, 25.1401 lights. § 25.1419 For entire airplane. (Additionally, ref. Reversion B-05.) § 25.1431 For winglet installation, powerplant improvements, and avionics systems CS 25 paragraphs Applicability § 25.1457(d)(5) When the optional flight data recorder is also required. § 25.1459 For when the optional flight data recorder is installed. CS 25 Subpart G For entire airplane. b) CS 25 subpart B paragraphs amended by Reversion CRI B-05 CS 25 paragraphs Applicability §§ 25.119, 25.121(d), 25.123(b), 25.125, 25.143, For entire airplane. 25.207, 25.237 c) CS 25 at amendment 4 CS 25 paragraphs Applicability § 25.1329 For autothrottle aspects only. All Weather Operations: JAR AWO change 2
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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◆ SPECIAL
5.1 Special Conditions for Citation Sovereign
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SC B-01 Human Factors
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SC B-04 Uncontrolled Thrust Increase
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SC C-01 Interaction of Systems & Structures
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SC C-09 Aeroelasticity / Flutter
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SC C-13 Ground Gust Effects
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SC C-16 Sustained Engine Imbalance
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SC D-06 Single Place Sidefacing Seat/Sidefacing Divans
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SC D-07 Interpretation of Halon Concentration Levels in Class C Compartments
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SC D-08 Improved Flammability Standards for Thermal Acoustic Insulation Materials
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SC D-10 System Operation to 51,000 ft
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SC E-02 Location of the Engine Fire Extinguishing System
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SC E-03 Fuel Tank Safety
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SC F-01 Protection from Effect of HIRF
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5.2 Special Conditions for Citation Sovereign+
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SC B-01 Human Factors
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◆ SPECIAL
SC B-04 Uncontrolled Thrust Increase
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◆ SPECIAL
SC C-01 Interaction of Systems & Structures
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◆ SPECIAL
SC C-09 Aeroelasticity / Flutter
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◆ SPECIAL
SC C-13 Ground Gust Effects
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◆ SPECIAL
SC C-16 Sustained Engine Imbalance
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◆ SPECIAL
SC D-06 Single Place Sidefacing Seat/Sidefacing Divans
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◆ SPECIAL
SC D-07 Interpretation of Halon Concentration Levels in Class C Compartments
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◆ SPECIAL
SC D-08 Improved Flammability Standards for Thermal Acoustic Insulation Materials
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SC D-10 System Operation to 51,000 ft
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SC D-16 Towbarless Towing
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SC E-02 Location of the Engine Fire Extinguishing System
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SC E-03 Fuel Tank Safety
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SC F-01 Protection from Effect of HIRF
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SC F-33 Data Link Services for the Single European Sky
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SC F-34 Data Link Recording
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SC F-43 Compliance to Single European Sky mandate for Mode S & ADS-B Out
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SC F-48 Security Protection of Aircraft Systems and Networks
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SC F-50 Flight Guidance Systems
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OTHER
Flight in Icing Conditions
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ELOS
8.1 Equivalent Safety Findings for Citation Sovereign
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ELOS
ESF C-12 Continuous Turbulence
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ELOS
ESF D-03 Ditching Emergency Exits for Passengers
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ELOS
ESF D-04 Door Between Passenger Compartments
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ELOS
ESF D-05 Width of Aisle
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ELOS
ESF D-09 Emergency Exit Locator Signs/Marking Signs
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ELOS
ESF F-04 Brakes and Braking Systems
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ELOS
ESF F-05 Equipment, Systems & Installation Requirements
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ELOS
ESF F-21 Draft Harmonized 25.1438 for the Pressurization and Pneumantic Systems
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ELOS
ESF F-22 Honeywell EPIC Integrated Modular Avionics System
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ELOS
8.2 Equivalent Safety Findings for Citation Sovereign+
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ELOS
ESF C-12 Continuous Turbulence
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ELOS
ESF D-03 Ditching Emergency Exits for Passengers
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ELOS
ESF D-04 Door Between Passenger Compartments
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ELOS
ESF D-05 Width of Aisle
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ELOS
ESF D-09 Emergency Exit Locator Signs/Marking Signs
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ELOS
ESF D-17 Use of Single Fire Suppression Bottle for Protection of APU and Baggage Compartment
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ELOS
ESF D-19 Flap Control Handle
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ELOS
ESF E-04 Thrust Reversers
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ELOS
ESF F-04 Brakes and Braking Systems
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ELOS
ESF F-05 Equipment, Systems & Installation Requirements
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ELOS
ESF F-21 Draft Harmonized 25.1438 for the Pressurization and Pneumantic Systems
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ESF F-44 APU Instrumentation
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ESF F-45 Digital Display of Engine Instruments
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OTHER
9.1 Environmental Protection Requirements for Citation Sovereign
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OTHER
A-03 Noise requirements: ICAO Annex 16, Volume I, 3rd edition Amendment 6 Refer to the EASA Noise Type Certificate Data Sheet, TCDSN IM.A.033
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OTHER
A-03 Emission requirements: ICAO Annex 16, Volume II, 2nd edition, Amendment 4
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OTHER
9.2 Environmental Protection Requirements for Citation Sovereign+
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OTHER
N-01 Noise requirements: ICAO Annex 16, Volume I, 5th edition, Amendment 9 Refer to the EASA Noise Type Certificate Data Sheet, TCDSN IM.A.033
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OTHER
N-02 Emission requirements: ICAO Annex 16, Volume II, 3rd edition, Amendment 6
- Exemptions: none recorded.