Textron Aviation Inc. 525: certification basis
Basis entries as written on the TCDS
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REG
(525-0001 through 525-0599) Code of Federal Regulations Title 14, Part 23, effective February 1, 1965, as amended by Amendments 23-1 thorough 23-38, and 23-40; The EASA Aircraft Type Certification standard includes that of FAA TCDS A1WI, based on individual EU member state acceptance or certification of this standard prior to 28 September 2003; Other standards conforming to TC/TCDS standards certified by individual EU member States prior to 28 September 2003 are also acceptable. (525-0600 through 525-0684 and 525-0686 through 525-0701)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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Code of Federal Regulations Title 14, Part 23, effective February 1, 1965, as amended by Amendments 23-1 through 23-38, and 23-40; except for the following paragraphs applicable for engines and FADEC’s which are CS23.611, 23.777, 23.779, 23.781, 23.865, 23.867, 23.901, 23.903, 23.939, 23.943, 23.951, 23.955, 23.961, 23.973, 23.1011, 23.1013, 23.1019, 23.1021, 23.1041, 23.1043, 23.1045, 23.1091, 23.1093, 23.1103, 23.1111, 23.1121, 23.1123, 23.1141, 23.1143, 23.1145, 23.1163, 23.1181, 23.1182, 23.1183, 23.1189, 23.1191, 23.1193, 23.1195, 23.1203, 23.1301, 23.1305, 23.1309, 23.1337, 23.1521, 23.1549, 23.1583; as amended through Amendment 23-1 through 23-38, and 23-40 through 23-54.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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CS 23.1309(a) as amended through Amendment 3, for Portable Electronic Device (PED) tolerance only.
Includes CS-23 §23.1309(a) through CS23-3 · current is CS23-6, 3 revisions later
Expands to 1 provision link · shown below
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(525-0685 and 525-0800 and On) Code of Federal Regulations Title 14, Part 23, effective February 1, 1965, as amended by Amendments 23-1 through 23-38, and 23-40; except for the following paragraphs applicable for engines and FADEC’s which are CS23.611, 23.777, 23.779, 23.781, 23.865, 23.867, 23.901, 23.903, 23.939, 23.943, 23.951, 23.955, 23.961, 23.973, 23.1011, 23.1013, 23.1019, 23.1021, 23.1041, 23.1043, 23.1045, 23.1091, 23.1093, 23.1103, 23.1111, 23.1121, 23.1123, 23.1141, 23.1143, 23.1145, 23.1163, 23.1181, 23.1182, 23.1183, 23.1189, 23.1191, 23.1193, 23.1195, 23.1203, 23.1301, 23.1305, 23.1309, 23.1337, 23.1521, 23.1549, 23.1583; as amended through Amendment 23-1 through 23-28, and 23-40 through 23-54.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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CS 23.1309(a) as amended through Amendment 3, for Portable Electronic Device (PED) tolerance only.
Includes CS-23 §23.1309(a) through CS23-3 · current is CS23-6, 3 revisions later
Expands to 1 provision link · Show the expansion
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Additions
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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Amendment Title Comments Level Maneuvering Loads CS 23, Amdt 2 Winglets only Gust loads CS 23, Amdt 2 Winglets only Outboard fins CS 23, Amdt 2 Winglets only
Includes CS-23 through CS23-2 · current is CS23-6, 4 revisions later
Expands to 377 provision links ! 1 text missing · Show the expansion
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23.575 Inspections and other procedures CS 23, Amdt 2 Winglets only Casting Factors CS 23, Amdt 2 Entire aircraft
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.613 Material strength properties and CS 23, Amdt 2 Main landing gear design values actuator internal keylock and ramlock only
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.867 Lightning protection of structure CS 23, Amdt 2 Winglets only
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.929 Engine installation ice protection CS 23, Amdt 2 Entire aircraft Fuel system independence CS 23, Amdt 2 Entire aircraft
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.957 Flow between interconnected tanks CS 23, Amdt 2 Entire aircraft Unusable fuel supply CS 23, Amdt 2 Entire aircraft Fuel Tank Sump CS 23, Amdt 2 Entire aircraft
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.975 Fuel tank vents and carburetor vapor CS 23, Amdt 2 Entire aircraft vents Fuel tank outlet CS 23, Amdt 2 Entire aircraft Fuel pumps CS 23, Amdt 2 Entire aircraft
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.993 Fuel system lines and fitting. CS 23, Amdt 2 Entire aircraft Fuel strainer or filter CS 23, Amdt 2 Entire aircraft Fuel system drains CS 23, Amdt 2 Entire aircraft Fuel jettisoning system CS 23, Amdt 2 Entire aircraft Lightning Protection CS 23, Amdt 2 For changed systems only
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.1308 High-Intensity Radiated Fields (HIRF) CS 23, Amdt 2 For changed Protection systems only
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.1543 Instrument markings: general CS 23, Amdt 2 Entire aircraft Fuel quantity indicator CS 23, Amdt 2 Entire aircraft Control markings CS 23, Amdt 2 Entire aircraft
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.1557 Miscellaneous markings and placards CS 23, Amdt 2 Entire aircraft
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.1559 Operating limitations placard CS 23, Amdt 2 Entire aircraft Airspeed placards CS 23, Amdt 2 Entire aircraft Flight maneuver placard CS 23, Amdt 2 Entire aircraft
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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(525-0685, 525-1400 and On)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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EASA Regulation No. EASA Amdt. Level
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CS 23.1309(a)(1) CS 23 Amdt. 3
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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CS 23.1309(a)(3) CS 23 Amdt. 3 (System Safety Aspects)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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CS 23.1309(b)(1) CS 23 Amdt. 3
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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CS 23.1309(b)(3) CS 23 Amdt. 3 (System Safety Aspects)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.2505(a) CS 23 Amdt. 6
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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(AMC2 23.2505, CS-23 Amdt 4)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.2510(a) CS 23 Amdt. 6
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.2605(a)(b)(c) CS 23 Amdt. 6
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.2500(b) CS 23 Amdt. 6
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.2505(a) CS 23 Amdt. 6
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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(AMC2 23.2505, CS-23 Amdt 4)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.2510 CS 23 Amdt. 6
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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23.2500(b) CS 23 Amdt. 6
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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(525-0001 and On)
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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CS-23 regulations 23.2000, 23.2005, 23.2010, 23.2325(a)(2), 23.2410, 23.2510, 23.2525, and 23.2605, Amendment 6 (see note 9) for new or amended lithium battery systems only.
Includes CS-23 §23.2000, §23.2005, §23.2010, §23.2410, §23.2510, §23.2525, §23.2605 through CS23-6
Includes CS-23 §23.2325(a)(2) through CS23-6
Expands to 8 provision links · Show the expansion
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Compliance with ice protection has been demonstrated in accordance with 14 CFR
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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§§23.1416 and 23.1419.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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CS-ACNS, Issue 2 CS-FCD, Issue 2 CS-MMEL Issue 3
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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◆ SPECIAL
23-ACE-55, additional requirements for: Smoke evacuation, protection of electronic systems from lightning and high intensity radiated electromagnetic fields (HIRF) , electronic flight instruments displays, thrust attenuating systems (thrust attenuating systems not applicable 525- 0600 and On), engine fire extinguishing system, performance, including takeoff, takeoff speeds, accelerate-stop, takeoff path, takeoff distance and takeoff run, takeoff flight path, climb one engine inoperative, landing, balked landing, climb, minimum control speed, trim, static longitudinal stability, demonstration of static longitudinal stability, static directional and lateral stability, wings
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level stall, turning flight and accelerated stalls, stall warning, vibration and buffeting, high speed characteristics, airspeed indicating system, static pressure system, maximum operating speed limit, minimum flight crew, operating limitations, operating procedure, performance information, airspeed indicator, effects of contamination on Natural Laminar Flow airfoils, definitions, and AFM approved information.
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◆ SPECIAL
(525-0685 and 525-0800 and On equipped with Garmin G3000)
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◆ SPECIAL
CRI B-52 Human Factors - Integrated Avionics Systems and associated SC-B 23.div-01, Issue 1
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CRI F-93 Flight Recorders including Data Link Recording and associated SC-F23.1457-01, Issue
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SC-F23.2555-01 Lightweight flight recorder
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OTHER
relaxed “Dutch Roll” damping criteria above 18,000 feet in lieu of damping criteria CS23.181(b).
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ELOS
(525-0360 through 525-0701 equipped with Collins Proline 21 electronic displays of engine instruments): ACE-00-01: 14 CFR §§23.1305(c)(2), (c)(5), and 23.1549(a) through (d), direct reading, digital only displays for the high-pressure turbine speed (N2), and fuel flow indications.
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(525-0685 and 525-0800 and On equipped with Garmin G3000)
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(a) Number ACE-13-09: 14 CFR § 23.841(b)(6), Cabin Pressurization – High Altitude Takeoff and Landing Operations.
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(b) Number ACE-00-05C: 14 CFR § 23.841(a), to allow small temporary cabin altitude excursions above 15,000 feet in the event of any probable pressurization system failure.
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(c) Number ACE-13-17: 14 CFR § 23.1549(a) through (c), direct reading, digital only displays for the high-pressure turbine speed (N2), oil pressure, oil temperature and fuel flow indications
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ELOS
(525-0685, 525-1400 and On equipped with Garmin 3D Safetaxi)
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ESF PCRI-0000399-0060092582 Indications Removal from Primary Flight Displays During Ground Phases
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OTHER
ICAO Annex 16, Volume I, ICAO Annex 16, Volume II, Part II (further details refer to TCDSN.IM.078)
- Exemptions: none recorded.
Entry 3 expanded
Subpart F — Equipment CS-23 1 section
| Section | Title | Cut-off | Text version | Changed since | Status |
|---|---|---|---|---|---|
| §23.1309(a) | Equipment, systems and installations | CS23-3 | CS23-0 | 2 | ✓ Text available |