ASTM F3064/F3064M-24 PDF
Standard Specification for Aircraft Powerplant Control, Operation, and Indication
Standard Specification for Aircraft Powerplant Control, Operation, and Indication
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 12
- Дата публикации:
- 1 марта 2024 г.
- Издание:
- F3064/F3064M
- ICS:
- 49.140
ABSTRACT This specification provides minimum requirements for the control, indication, and operational characteristics of propulsion systems. It was developed based on propulsion system installed on aeroplanes, but may be applicable to other applications. The applicant for a design approval must seek the individual guidance to their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan. SCOPE 1.1 This specification covers minimum requirements for the control, indication, and operational characteristics of propulsion systems. It was developed based on propulsion system installed on aeroplanes, but may be applicable to other applications as well. 1.2 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their Aeroplane Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. Annex A1 maps the Means of Compliance described in this specification to EASA CS-23, amendment 5, or later, and FAA 14 CFR Part 23, amendment 64, or later. 1.3 Units—The values stated are SI units followed by imperial units in brackets. The values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined. 1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Abstract
Overview
ASTM F3064/F3064M-24 – Standard Specification for Aircraft Powerplant Control, Operation, and Indication establishes the minimum requirements for the control systems, operational characteristics, and indication of propulsion systems installed on aeroplanes. Developed by ASTM Committee F44, this international standard guides design approval applicants in achieving compliance with civil aviation airworthiness regulations for powerplant systems. While its primary focus is on aeroplanes, the specification’s content may also be relevant for other propulsion system applications. This standard aligns with internationally recognized standardization principles and serves as a valuable reference in aircraft certification plans.
Key Topics
-
Powerplant Control Requirements:
- Ensures controls are properly located, arranged, and secured, minimising inadvertent movement and preventing unsafe operation.
- Details redundancy considerations and fire-resistance requirements for critical controls.
-
Indication Systems:
- Specifies requirements for the reliable measurement and display of essential powerplant parameters (e.g., fuel, oil quantity, temperature, and pressure).
- Covers installation and calibration practices for both analog and digital displays to support clear pilot awareness.
-
Operational Characteristics:
- Requires thorough evaluation of both normal and emergency operating conditions, such as engine starting/stopping, cooling, and response to negative acceleration.
- Addresses operational limitations, fuel type and grade, temperature ranges, and compatibility with auxiliary systems like APR (Automatic Power Reserve).
-
Electronic Engine Control and Safety:
- Outlines expectations for electronic engine control system integrity, high-intensity radiated field (HIRF) and lightning resilience, and prevention of loss-of-thrust/control (LOTC/LOPC) events.
- Calls for comprehensive safety assessments and compliance with applicable regulatory guidance (e.g., FAA and EASA standards).
-
Compliance Mapping:
- Provides correlation tables and annexes mapping requirements to EASA CS-23 and FAA 14 CFR Part 23, facilitating regulatory acceptance and streamlined certification.
Applications
ASTM F3064/F3064M-24 is utilized by:
- Aircraft Designers & Manufacturers: Assisting in the design, validation, and certification of powerplant controls and indication systems for aeroplanes, including engine control levers, mixture controls, and engine status indicators.
- Certification Consultants & Compliance Specialists: Supporting preparation of certification plans that meet regulatory authority (CAA/FAA/EASA) requirements for airworthiness.
- Maintenance, Repair & Overhaul (MRO) Organizations: Referring to operational and indication standards to ensure ongoing compliance in servicing aircraft propulsion systems.
- Avionics Developers: Designing display and alerting systems that meet the standard’s human factors and performance requirements.
- Regulatory Authorities: Benchmarking national airworthiness rules and interoperability with global standards.
Related Standards
The following ASTM and regulatory documents are closely associated with ASTM F3064/F3064M-24:
- ASTM F3060: Terminology for Aircraft
- ASTM F3061/F3061M: Specification for Systems and Equipment in Aircraft
- ASTM F3062/F3062M: Specification for Aircraft Powerplant Installation
- ASTM F3063/F3063M: Specification for Aircraft Fuel Storage and Delivery
- ASTM F3116/F3116M: Specification for Design Loads and Conditions
- ASTM F3117/F3117M: Specification for Crew Interface in Aircraft
- ASTM F3233/F3233M: Specification for Flight and Navigation Instrumentation in Aircraft
- ASTM F3432: Practice for Powerplant Instruments
Referenced regulatory standards include:
- EASA CS-23: Certification Specifications for Normal-Category Aeroplanes
- FAA 14 CFR Part 23: Airworthiness Standards: Normal Category Airplanes
For updated acceptance status and further guidance, consult the ASTM F44 committee webpage and relevant CAA resources.
Keywords: aircraft powerplant control, powerplant operation, powerplant indication, engine control systems, aviation standards, FAA Part 23, EASA CS-23, electronic engine control, LOTC, aircraft certification, ASTM F3064
Технические детали
- Технический комитет
- F44 - General Aviation Aircraft
- SKU
- ASTM F3064/F3064M-24
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