This document discusses the roles and responsibilities of the Military Type Certificate Holder (MTCH) under the European Military Aviation Requirements (EMAR 21). It raises concerns that some member states interpret EMAR 21 to mean the MTCH must be a "servant of the state", rather than requiring a Design Organization Approval (DOA) as stipulated in EMAR 21. This could lead to inefficient practices and safety issues if type design and certification are not consistent across borders. The document advocates aligning the MTCH role with international civil aviation conventions to realize the full benefits of harmonization.
This presentation was given at the AAUS Conference preceding the Avalon Airshow in Melbourne. It combines work being done as part of the Industry Support to the CASA UAS Standards Subcommittee, in conjunction with a brief intro into elements of the JARUS Working Group 6 Specific Operations Risk Assessment Process
The document discusses airworthiness review requirements according to regulations. It distinguishes between carrying out a review and issuing a certificate, and notes the DGCA can always issue certificates based on CAMO recommendations. The DGCA may also conduct reviews when safety is threatened or for small aircraft if requested. Reviews are required for imported aircraft. Privileges and procedures are described for CAMOs conducting reviews and issuing or recommending certificates. Requirements are outlined for airworthiness review staff qualifications and record keeping.
1) FADEC systems use digital controls and computers to precisely regulate factors like fuel flow and engine speed, allowing consistent engine performance. HUMS monitors helicopter components for faults or reduced lifespan.
2) FADEC systems have wiring to sensors, actuators, and the aircraft to allow the electronic engine control unit to compute and relay control signals. HUMS includes onboard and ground equipment to analyze vibration and performance data.
3) FADEC and HUMS provide benefits like reduced maintenance, lower costs, increased safety and reliability compared to older mechanical controls. HUMS requires cooperation across organizations for its maintenance approach.
This document provides an overview of airworthiness directives, service bulletins, and maintenance requirements for aircraft. It defines airworthiness directives as legally enforceable regulations issued by the FAA to correct an unsafe condition. Service bulletins are notices from manufacturers about product improvements. The document outlines required inspections, owner responsibilities, and record keeping duties. It also explains how to find current airworthiness directives and service bulletins on the FAA and manufacturer websites.
A simple fact of the aircraft resale market is that aircraft with missing documents usually sell for significantly less than those with continual chronological history. At best, expensive maintenance procedures may have to be reperformed and properly documented in order to return the aircraft to airworthy status. With a standardized Records Archive Management, you can control, collaborate, and safeguard the value of the aircraft records.
This document discusses the requirements for a Continuing Airworthiness Management Organization (CAMO). It outlines that a CAMO must have a Continuing Airworthiness Management Exposition (CAME) approved by the aviation regulator that defines its procedures. Key roles like the Accountable Manager, Continuing Airworthiness Manager, and Quality Manager are described along with their responsibilities to ensure compliance with regulations and airworthiness standards. The document also discusses the use of Maintenance Programs, Master Minimum Equipment Lists, and Deferred Item Lists by CAMOs.
1. The document discusses regulations regarding airworthiness review certificates (ARCs) in India.
2. It outlines who can issue ARCs for different types of aircraft, including those used in commercial air transport, non-commercial aircraft, and aircraft of different weights.
3. The key requirements for an airworthiness review to be performed in order to issue an ARC are described, including inspecting the aircraft and records to ensure continued airworthiness.
This presentation was given at the AAUS Conference preceding the Avalon Airshow in Melbourne. It combines work being done as part of the Industry Support to the CASA UAS Standards Subcommittee, in conjunction with a brief intro into elements of the JARUS Working Group 6 Specific Operations Risk Assessment Process
The document discusses airworthiness review requirements according to regulations. It distinguishes between carrying out a review and issuing a certificate, and notes the DGCA can always issue certificates based on CAMO recommendations. The DGCA may also conduct reviews when safety is threatened or for small aircraft if requested. Reviews are required for imported aircraft. Privileges and procedures are described for CAMOs conducting reviews and issuing or recommending certificates. Requirements are outlined for airworthiness review staff qualifications and record keeping.
1) FADEC systems use digital controls and computers to precisely regulate factors like fuel flow and engine speed, allowing consistent engine performance. HUMS monitors helicopter components for faults or reduced lifespan.
2) FADEC systems have wiring to sensors, actuators, and the aircraft to allow the electronic engine control unit to compute and relay control signals. HUMS includes onboard and ground equipment to analyze vibration and performance data.
3) FADEC and HUMS provide benefits like reduced maintenance, lower costs, increased safety and reliability compared to older mechanical controls. HUMS requires cooperation across organizations for its maintenance approach.
This document provides an overview of airworthiness directives, service bulletins, and maintenance requirements for aircraft. It defines airworthiness directives as legally enforceable regulations issued by the FAA to correct an unsafe condition. Service bulletins are notices from manufacturers about product improvements. The document outlines required inspections, owner responsibilities, and record keeping duties. It also explains how to find current airworthiness directives and service bulletins on the FAA and manufacturer websites.
A simple fact of the aircraft resale market is that aircraft with missing documents usually sell for significantly less than those with continual chronological history. At best, expensive maintenance procedures may have to be reperformed and properly documented in order to return the aircraft to airworthy status. With a standardized Records Archive Management, you can control, collaborate, and safeguard the value of the aircraft records.
This document discusses the requirements for a Continuing Airworthiness Management Organization (CAMO). It outlines that a CAMO must have a Continuing Airworthiness Management Exposition (CAME) approved by the aviation regulator that defines its procedures. Key roles like the Accountable Manager, Continuing Airworthiness Manager, and Quality Manager are described along with their responsibilities to ensure compliance with regulations and airworthiness standards. The document also discusses the use of Maintenance Programs, Master Minimum Equipment Lists, and Deferred Item Lists by CAMOs.
1. The document discusses regulations regarding airworthiness review certificates (ARCs) in India.
2. It outlines who can issue ARCs for different types of aircraft, including those used in commercial air transport, non-commercial aircraft, and aircraft of different weights.
3. The key requirements for an airworthiness review to be performed in order to issue an ARC are described, including inspecting the aircraft and records to ensure continued airworthiness.
A flight control system (FCS) controls the flight of an aircraft and modern aircraft include automatic flight control systems (AFCS) that aid pilots. An AFCS has three main components: computers to process inputs and determine outputs, sensors to provide data to the computers like aircraft position and speed, and output devices/actuators that convert computer signals into physical control surface movements. There are different types of AFCS including stability augmentation systems that improve stability, autopilots to reduce pilot workload, and navigation aids for tasks like landing. A typical FCS architecture incorporates these elements along with feedback control loops between sensors and actuators.
The document discusses aircraft certification and type certificates provided by the Federal Aviation Administration (FAA). It provides an overview of the FAA's Aircraft Certification Service (AIR) and their role in issuing type certificates and ensuring continued airworthiness. It defines key terms like type design, airworthiness, and the different categories of type certificates (standard, primary, restricted, surplus military, import). It also describes the type certificate data sheet, instructions for continued airworthiness, and how type certificates relate to airworthiness certificates and maintenance regulations.
A320 Flight Deck And Systems Briefing For PilotsFelicia Clark
This document provides an overview of the flight deck and systems for the Airbus A319/A320/A321 aircraft. It describes the general features and layout of the flight deck, including the sidestick controllers, main instrument panels, glareshield, pedestal, overhead panel and pilot visibility. It also summarizes the electrical, hydraulic, flight control, landing gear, fuel, engine control, auxiliary power unit and other systems. The document is intended as a basic briefing for pilots and notes that it should not be used as an official technical reference.
Este documento presenta información sobre la documentación aeronáutica requerida para la planificación y ejecución de vuelos. Explica los diferentes tipos de publicaciones como la AIP, suplementos AIP, NOTAM y PIB que contienen información aeronáutica permanente y temporal. También describe cómo se actualizan estos documentos y dónde pueden consultarse. Por último, brinda detalles sobre las regulaciones argentinas de aviación civil y la documentación reglamentaria y operativa que debe llevarse a bordo según la parte 91 de
The document provides an overview of requirements for airworthiness management as per Part M, including:
1) The scope and extent of approval for a Continuing Airworthiness Management Organisation (CAMO), which includes developing maintenance programs and managing approvals.
2) Requirements for the Continuing Airworthiness Management Exposition (CAME) that specifies the CAMO's procedures and scope.
3) Requirements for facilities, personnel, and contracting maintenance to approved organisations.
4) Requirements for the CAMO's quality system to monitor compliance and ensure airworthy aircraft.
The document outlines the various types of documentation required for an aircraft maintenance program. It discusses preventative maintenance types including servicing, scheduled maintenance, condition-based maintenance, and out-of-phase maintenance. It also lists the regulatory, manufacturer's, airline generated, and ATA documentation standards that maintenance programs must adhere to. Key manufacturer's documentation includes the airplane maintenance manual, component maintenance manual, and illustrated parts catalog.
The document discusses the design and development of quadcopter unmanned aerial vehicles (UAVs). It describes the prototypes created, including improvements made to reduce weight and increase lift. Sensors and controllers are discussed, including sensors for position, proximity, and navigation. The final prototype achieved stable hovering with a weight of 43 grams and incorporated an inertial measurement unit, ultrasonic sensors, GPS, and radio frequency transmission for control and data transmission.
Este documento proporciona información sobre seguridad de la aviación (AVSEC), incluyendo definiciones, amenazas, actividades en el aeropuerto y planes de emergencia. Explica que AVSEC implica medidas para proteger la aviación civil contra actos ilícitos mediante controles de acceso, inspecciones y protección de aeronaves. También destaca la importancia de la coordinación entre AVSEC y planes de emergencia de salud pública para controlar brotes de enfermedades.
The document discusses Air Traffic Control transponders. It describes:
1. Transponders allow air traffic controllers to track aircraft on radar by sending interrogation signals that the transponder responds to with a coded reply signal containing identification and altitude information.
2. There are two main radar systems - primary surveillance radar which detects aircraft but does not identify them, and secondary surveillance radar which interrogates transponders for identification and altitude data.
3. The transponder receives interrogation signals and uses information from the control panel and air data computer to generate and transmit a coded reply on a different frequency, which is displayed on the air traffic controller's radar screen.
The Directorate General of Civil Aviation (DGCA) is India's civil aviation regulatory body. This document outlines requirements and procedures for organizations involved in aircraft manufacturing, maintenance, testing, storage, and training. It discusses approval requirements for these organizations and categories they can seek approval in, such as manufacturer, maintenance, testing, fuel/lubricants, stores/distribution, and training. The document also provides detailed guidelines and safety procedures that must be followed for aircraft fueling operations.
El documento describe los componentes básicos de un aeropuerto, incluyendo las pistas, calles de rodaje, terminales y estacionamientos. Explica los factores que se deben considerar al planificar un nuevo aeropuerto, como la ubicación, funciones previstas, economía local y condiciones meteorológicas. También analiza brevemente el aeropuerto de Bahía Blanca y los desafíos que plantea el crecimiento del tráfico aéreo.
This document discusses the design and fabrication of a fuselage for a radio-controlled model aircraft. It provides guidelines for selecting parameters and dimensions for the fuselage and other components. Key parts of the fuselage like the nose, tail, and stabilizer width are calculated as percentages of the total fuselage length and wingspan. Dimensions for other components like ailerons, elevators, rudders, and stabilizers are then derived based on their recommended areas as percentages of other surfaces. The center of gravity is also calculated based on the wing chord length. Overall, the document provides a step-by-step approach to sizing an RC aircraft based on established best practices and formulas.
CAR-145 was introduced in 2005 and revised in 2008 and 2013 to align with EASA regulations. It applies to maintenance of large aircraft and aircraft used for commercial air transport. Practical training for flight crew was enhanced to include de-icing activities. Personnel conducting non-destructive testing must be qualified according to DGCA standards. Line maintenance includes troubleshooting, defect rectification, component replacement and scheduled maintenance while base maintenance involves larger tasks. A CAR-145 approved organization must have its management located in the certifying country. Guidance material provides alternatives for small single person organizations to be approved for limited maintenance classes.
Servicio de Control de Aeródromo: Funciones de la Torre de Control. Información Suministrada a las Aeronaves (hora, meteorología; pista en uso; autorizaciones). Tránsito Esencial Local. Control de Aeronaves que Salen y que Llegan.Separaciones. Operaciones con escasa visibilidad.
El documento presenta la introducción de un curso sobre control de tránsito aéreo. Explica las reglas de convivencia del curso, el contenido académico de la unidad 1 que incluye una presentación sobre los servicios de tránsito aéreo y la autoridad competente, y finaliza con una sección de preguntas.
A Technical Study and Industrial Report on the various Electrical and Communication Systems used in choppers manufactured and Overhauled by Hindustan Aeronautics Limited.
FAA Safety Requirements for Airfield Constructionoffthewallsafety
The purpose of this presentation is to supplement the
airport specific training for construction personnel
working on or adjacent to runways and taxiways
addressing the Construction Safety Plan and airport
ground vehicle/pedestrian procedures.
Servicio de Control de Tránsito Aéreo (ATC) - Servicios de Tránsito Aéreo (ATS)Lic. Christian Buchanan
Este documento describe los aspectos fundamentales del servicio de control de tránsito aéreo, incluyendo su aplicación a aeronaves que vuelan en espacio aéreo controlado, la provisión del servicio por diferentes dependencias, las responsabilidades involucradas y las autorizaciones emitidas. Explica que el objetivo de las autorizaciones es acelerar y brindar separación adecuada entre aeronaves de forma segura y eficiente.
In this presentation provided to the media in Spain during the Airbus Trade Media Briefing on June 8th and 9th, Eric Isorce, the head of A400M flight tests provides an overview of the test effort and results to date. As the plane has entered service, testing has continued to broaden the use envelope of this very flexible asset.
The document discusses the development of Instructions for Continuing Airworthiness (ICA) and Certification Maintenance Requirements (CMR). It addresses:
- The ICA development process as part of type certification and supplemental type certification according to regulatory standards. ICA include documents like maintenance manuals, service bulletins, and the minimum equipment list.
- The principles and requirements for developing CMRs during certification to ensure compliance with safety regulations and detect safety issues. CMRs result from a system safety analysis and address impending failures.
- The documentation and approval process for CMR changes and their inclusion in the airworthiness limitations section of manuals.
The document discusses a new FAA rule requiring airplane manufacturers to establish limits of validity (LOV) for airline fleets to address widespread fatigue damage. The LOV defines the maximum usage limit for an airplane based on fatigue test data. Boeing must provide LOVs and service bulletins to preclude fatigue damage for its models by certain deadlines. Airlines must incorporate the LOVs and service bulletins into their maintenance programs by subsequent deadlines. The rule aims to prevent structural failures from widespread fatigue cracks developing as older airplanes exceed their original design lives.
A flight control system (FCS) controls the flight of an aircraft and modern aircraft include automatic flight control systems (AFCS) that aid pilots. An AFCS has three main components: computers to process inputs and determine outputs, sensors to provide data to the computers like aircraft position and speed, and output devices/actuators that convert computer signals into physical control surface movements. There are different types of AFCS including stability augmentation systems that improve stability, autopilots to reduce pilot workload, and navigation aids for tasks like landing. A typical FCS architecture incorporates these elements along with feedback control loops between sensors and actuators.
The document discusses aircraft certification and type certificates provided by the Federal Aviation Administration (FAA). It provides an overview of the FAA's Aircraft Certification Service (AIR) and their role in issuing type certificates and ensuring continued airworthiness. It defines key terms like type design, airworthiness, and the different categories of type certificates (standard, primary, restricted, surplus military, import). It also describes the type certificate data sheet, instructions for continued airworthiness, and how type certificates relate to airworthiness certificates and maintenance regulations.
A320 Flight Deck And Systems Briefing For PilotsFelicia Clark
This document provides an overview of the flight deck and systems for the Airbus A319/A320/A321 aircraft. It describes the general features and layout of the flight deck, including the sidestick controllers, main instrument panels, glareshield, pedestal, overhead panel and pilot visibility. It also summarizes the electrical, hydraulic, flight control, landing gear, fuel, engine control, auxiliary power unit and other systems. The document is intended as a basic briefing for pilots and notes that it should not be used as an official technical reference.
Este documento presenta información sobre la documentación aeronáutica requerida para la planificación y ejecución de vuelos. Explica los diferentes tipos de publicaciones como la AIP, suplementos AIP, NOTAM y PIB que contienen información aeronáutica permanente y temporal. También describe cómo se actualizan estos documentos y dónde pueden consultarse. Por último, brinda detalles sobre las regulaciones argentinas de aviación civil y la documentación reglamentaria y operativa que debe llevarse a bordo según la parte 91 de
The document provides an overview of requirements for airworthiness management as per Part M, including:
1) The scope and extent of approval for a Continuing Airworthiness Management Organisation (CAMO), which includes developing maintenance programs and managing approvals.
2) Requirements for the Continuing Airworthiness Management Exposition (CAME) that specifies the CAMO's procedures and scope.
3) Requirements for facilities, personnel, and contracting maintenance to approved organisations.
4) Requirements for the CAMO's quality system to monitor compliance and ensure airworthy aircraft.
The document outlines the various types of documentation required for an aircraft maintenance program. It discusses preventative maintenance types including servicing, scheduled maintenance, condition-based maintenance, and out-of-phase maintenance. It also lists the regulatory, manufacturer's, airline generated, and ATA documentation standards that maintenance programs must adhere to. Key manufacturer's documentation includes the airplane maintenance manual, component maintenance manual, and illustrated parts catalog.
The document discusses the design and development of quadcopter unmanned aerial vehicles (UAVs). It describes the prototypes created, including improvements made to reduce weight and increase lift. Sensors and controllers are discussed, including sensors for position, proximity, and navigation. The final prototype achieved stable hovering with a weight of 43 grams and incorporated an inertial measurement unit, ultrasonic sensors, GPS, and radio frequency transmission for control and data transmission.
Este documento proporciona información sobre seguridad de la aviación (AVSEC), incluyendo definiciones, amenazas, actividades en el aeropuerto y planes de emergencia. Explica que AVSEC implica medidas para proteger la aviación civil contra actos ilícitos mediante controles de acceso, inspecciones y protección de aeronaves. También destaca la importancia de la coordinación entre AVSEC y planes de emergencia de salud pública para controlar brotes de enfermedades.
The document discusses Air Traffic Control transponders. It describes:
1. Transponders allow air traffic controllers to track aircraft on radar by sending interrogation signals that the transponder responds to with a coded reply signal containing identification and altitude information.
2. There are two main radar systems - primary surveillance radar which detects aircraft but does not identify them, and secondary surveillance radar which interrogates transponders for identification and altitude data.
3. The transponder receives interrogation signals and uses information from the control panel and air data computer to generate and transmit a coded reply on a different frequency, which is displayed on the air traffic controller's radar screen.
The Directorate General of Civil Aviation (DGCA) is India's civil aviation regulatory body. This document outlines requirements and procedures for organizations involved in aircraft manufacturing, maintenance, testing, storage, and training. It discusses approval requirements for these organizations and categories they can seek approval in, such as manufacturer, maintenance, testing, fuel/lubricants, stores/distribution, and training. The document also provides detailed guidelines and safety procedures that must be followed for aircraft fueling operations.
El documento describe los componentes básicos de un aeropuerto, incluyendo las pistas, calles de rodaje, terminales y estacionamientos. Explica los factores que se deben considerar al planificar un nuevo aeropuerto, como la ubicación, funciones previstas, economía local y condiciones meteorológicas. También analiza brevemente el aeropuerto de Bahía Blanca y los desafíos que plantea el crecimiento del tráfico aéreo.
This document discusses the design and fabrication of a fuselage for a radio-controlled model aircraft. It provides guidelines for selecting parameters and dimensions for the fuselage and other components. Key parts of the fuselage like the nose, tail, and stabilizer width are calculated as percentages of the total fuselage length and wingspan. Dimensions for other components like ailerons, elevators, rudders, and stabilizers are then derived based on their recommended areas as percentages of other surfaces. The center of gravity is also calculated based on the wing chord length. Overall, the document provides a step-by-step approach to sizing an RC aircraft based on established best practices and formulas.
CAR-145 was introduced in 2005 and revised in 2008 and 2013 to align with EASA regulations. It applies to maintenance of large aircraft and aircraft used for commercial air transport. Practical training for flight crew was enhanced to include de-icing activities. Personnel conducting non-destructive testing must be qualified according to DGCA standards. Line maintenance includes troubleshooting, defect rectification, component replacement and scheduled maintenance while base maintenance involves larger tasks. A CAR-145 approved organization must have its management located in the certifying country. Guidance material provides alternatives for small single person organizations to be approved for limited maintenance classes.
Servicio de Control de Aeródromo: Funciones de la Torre de Control. Información Suministrada a las Aeronaves (hora, meteorología; pista en uso; autorizaciones). Tránsito Esencial Local. Control de Aeronaves que Salen y que Llegan.Separaciones. Operaciones con escasa visibilidad.
El documento presenta la introducción de un curso sobre control de tránsito aéreo. Explica las reglas de convivencia del curso, el contenido académico de la unidad 1 que incluye una presentación sobre los servicios de tránsito aéreo y la autoridad competente, y finaliza con una sección de preguntas.
A Technical Study and Industrial Report on the various Electrical and Communication Systems used in choppers manufactured and Overhauled by Hindustan Aeronautics Limited.
FAA Safety Requirements for Airfield Constructionoffthewallsafety
The purpose of this presentation is to supplement the
airport specific training for construction personnel
working on or adjacent to runways and taxiways
addressing the Construction Safety Plan and airport
ground vehicle/pedestrian procedures.
Servicio de Control de Tránsito Aéreo (ATC) - Servicios de Tránsito Aéreo (ATS)Lic. Christian Buchanan
Este documento describe los aspectos fundamentales del servicio de control de tránsito aéreo, incluyendo su aplicación a aeronaves que vuelan en espacio aéreo controlado, la provisión del servicio por diferentes dependencias, las responsabilidades involucradas y las autorizaciones emitidas. Explica que el objetivo de las autorizaciones es acelerar y brindar separación adecuada entre aeronaves de forma segura y eficiente.
In this presentation provided to the media in Spain during the Airbus Trade Media Briefing on June 8th and 9th, Eric Isorce, the head of A400M flight tests provides an overview of the test effort and results to date. As the plane has entered service, testing has continued to broaden the use envelope of this very flexible asset.
The document discusses the development of Instructions for Continuing Airworthiness (ICA) and Certification Maintenance Requirements (CMR). It addresses:
- The ICA development process as part of type certification and supplemental type certification according to regulatory standards. ICA include documents like maintenance manuals, service bulletins, and the minimum equipment list.
- The principles and requirements for developing CMRs during certification to ensure compliance with safety regulations and detect safety issues. CMRs result from a system safety analysis and address impending failures.
- The documentation and approval process for CMR changes and their inclusion in the airworthiness limitations section of manuals.
The document discusses a new FAA rule requiring airplane manufacturers to establish limits of validity (LOV) for airline fleets to address widespread fatigue damage. The LOV defines the maximum usage limit for an airplane based on fatigue test data. Boeing must provide LOVs and service bulletins to preclude fatigue damage for its models by certain deadlines. Airlines must incorporate the LOVs and service bulletins into their maintenance programs by subsequent deadlines. The rule aims to prevent structural failures from widespread fatigue cracks developing as older airplanes exceed their original design lives.
The Australian Defence Force engaged Baines Simmons to help prepare for the transition to adopting the European Military Airworthiness Requirements (EMARs) within its Defence Aviation Safety Regulations (DASRs) by 2018. Baines Simmons provided training to over 50 Defence staff to aid understanding of EMAR 21 and differences from the European Aviation Safety Agency requirements. They also assisted the Directorate General Technical Airworthiness with customizing EMAR 21 implementation and supported defence organizations to develop documentation required for approval under the new regulations. Initial training phases helped stakeholders better understand principles of the regulations and their application in the military domain.
The document discusses maintenance planning and control for aircraft. It describes the Maintenance Planning Document which lists all maintenance tasks and intervals. It provides guidance for airlines to establish their own maintenance programs. It defines operational and calendar maintenance units and codes used to specify maintenance task intervals. Thresholds and intervals are provided for fatigue damage tasks and environmental/accidental damage tasks. General rules for aircraft maintenance programs are outlined.
The document provides guidance on determining what supplier data is considered part of the instructions for continued airworthiness (ICA) for an aircraft. It outlines several key points:
1) Supplier data related to airworthiness limitations or scheduled maintenance is considered part of the aircraft ICA.
2) Other supplier data may be included directly in the aircraft ICA or referenced for additional/optional information.
3) For supplier data not related to airworthiness limitations or scheduled maintenance, the aircraft ICA can reference it as additional information but it is not formally part of the ICA documentation.
This document discusses recent developments in aging airplane maintenance programs. It provides background on aging concerns as aircraft accumulate flight hours and cycles. Recent regulatory actions include the widespread fatigue damage rule and aging airplane safety rule. Program developments aim to ensure structural airworthiness as fleets age, through supplemental inspections, corrosion prevention, and addressing combined damage from fatigue and corrosion.
The document discusses proposed amendments to the Defence Procurement Procedure (DPP) 2016 in India. Key amendments include:
1. Allowing higher authorities like the Defence Acquisition Council to approve retraction of Request for Proposals in certain cases.
2. Requiring vetting of draft contract documents concurrently with the Contract Negotiation Committee process.
3. Standardizing the composition of Contract Negotiation Committees for delegated procurement cases.
4. No longer mandating a Technical Oversight Committee for cases valued over Rs. 300 crores.
5. Requiring Service Headquarters to approve Technical Evaluation Committee reports.
The amendments are aimed at further refining and simplifying defence
The document summarizes an aerodrome certification workshop that took place in Paris, France from 18-20 December 2018. It discusses the objectives of the workshop which were to provide insight into aerodrome certification requirements and processes, and to develop participants' skills and knowledge in areas like aerodrome certification and safety management. The document also outlines aspects of aerodrome certification requirements in the Chicago Convention and ICAO Annex 14, and guidance on certification procedures from ICAO Document 9774.
The document outlines the procurement process for categories under the 'Buy' and 'Buy and Make' schemes in India's Defence Procurement Procedure. Key steps in the process include issuing a Request for Information to generate requirements, obtaining Acceptance of Necessity approval, issuing a Request for Proposals, technical and field evaluation of bids, negotiations and awarding of contracts. Services Qualitative Requirements are developed to lay out comprehensive user needs and are approved by competent authorities before the Request for Proposal is issued.
This document provides guidelines for the type certification of turbine aircraft engines. It outlines the general type certification process and provides guidance on specific regulations. The document discusses certification of surplus military engines and parts for use in civil aircraft. It also provides compliance methods and references for selected regulations regarding engine design, components, instrumentation, and testing.
This framework, which is aligned with the personnel requirements of Part CAMO, sets out the key knowledge, skills, and experience needed for the effective management of airworthiness.
It has been designed as a guidance tool for individuals and managers to facilitate:
1. the evaluation of role specific competence,
2. identifying gaps, and
3. informing professional development plans.
Running head ACQUISITION STRATEGY PIEZOELECTRIC EMBEDDED TRA.docxSUBHI7
Running head: ACQUISITION STRATEGY: PIEZOELECTRIC EMBEDDED TRANSDUCERS UNDER WALL GEOSTRUCTURE PROGRAM
4
ACQUISITION STRATEGY: PIEZOELECTRIC EMBEDDED TRANSDUCERS UNDER WALL GEOSTRUCTURE PROGRAM
Acquisition Strategy: Piezoelectric Embedded Transducers (PET)
Under the WALL Geostructure Program
XXXXXX
ASCM 628 Section 9040 2172
University of Maryland University College
March 11, 2017
This strategic plan will specify the details relating to the acquisition of Piezoelectric Embedded Transducers (PET) to be utilized to provide enhanced surveillance capabilities for the new Wide Alignment Limited Loading (WALL) Geostructure Program. As referenced by Kim, Roberts & Brown (2016), United States federal policy and regulatory guidance encourage the use of fixed-price contracts in an effort to secure best value for purchasing groups; therefore, the form of contract that shall be utilized shall be a Fixed Price Economic Price Adjustment (FPEPA) contract to account for the uncertainties of future economic conditions that may cause fluctuations in the future costs of supplies and equipment that the contractor might be required to provide under contract and would not at this time be predictable. Contract Type
Pursuant to 41 USC 253 and 10 USC 2305, competition will be full and open and the contract shall be both severable and non-severable. For the procurement of 1,000 Piezoelectric Embedded Transducers, the contract shall be non-severable; however, any elements relating to their maintenance and non-developmental support and data to be reported shall be considered non-severable. Additionally, given the complexity and technical nature of this service, price alone is not sufficient to determine the award and therefore, the contract will be awarded based on a contracting by negotiation bidding process. Furthermore, it is assumed that the U.S. Immigrations and Customs Enforcement (ICE) Acquisitions Division wishes to hold discussions regarding the contract to ensure that its needs are clearly communicated and met to its satisfaction. To allow ICE to have maximum flexibility in awarding the contract, the trade-off process shall also be initiated.
Planning Fundamentals
The subsequent planning fundamentals shall also be incorporated within this strategic plan as they are essential for the PET sourcing and future negotiations: (1) Contractor Performance Requirements, (2) Deliverables, and (3) Assumptions.
Contractor Performance Requirements and Deliverables
The contractor shall be responsible for providing substantial value to ICE in the form of required hardware to ensure the enhancement of the surveillance capability for the WALL program, software to certify the technical monitoring and successful operation of the hardware, and the non-developmental support and data which will be utilized to analyze the stabilization and sustainabili ...
This supplemental agenda provides details for an upcoming ASME BTH Standards Committee meeting on May 26, 2021. The agenda includes a new business item to discuss the NRC's draft regulatory guide 1.244, which proposes to endorse parts of ASME BTH-1 for controlling heavy loads at nuclear facilities. The agenda also includes reviewing a membership application from Jon Alberson. The secretary of the committee, Elijah Dominguez, respectfully submitted the supplemental agenda with these details for committee review and action.
Multi Role Carrier Borne Fighter AircraftAnkur Gupta
The Indian Nay has recently released a very detailed RFI for procuring 57 naval fighter platforms. It is a Buy and Make Global program with 30% offsets. Platforms with CATOBAR and STOBAR can submit their response.
Guidance on guide 62 issue 3 (from greg)youssefpec
A person who accompanies and assists an auditor during an audit but who is not
qualified or approved to perform audits independently or make audit decisions.
G.1.3.2. The term "certification/registration body" is used throughout this document to refer to
bodies operating assessment and certification/registration of quality management systems.
G.1.3.3. The term "accreditation body" refers to a body that performs accreditation of
certification/registration bodies.
The market for defence maintenance, repair, and overhaul (MRO)-air platforms is predicted to expand due to increased demand for efficient MRO operations. AI-powered predictive maintenance will play a significant role in the aircraft health monitoring systems market. More data collection will become possible as aeroplane technology advances. The ultimate goal is to gain a better understanding of the aircraft, anticipate maintenance needs, and add considerable value to operations. This corresponds to the potential for more powerful analytics to emerge. MRO services are highly influenced by both maintenance activities and an ageing aircraft fleet.https://aviationanddefensemarketreports.com/product/global-defense-mro-air-platforms-market/
Transformative Roles Of Global Engineering Partnersgiancarlo
The document discusses the role of Global Engineering Partners (GEPs) in supporting aircraft certification processes for the aerospace and defense industry. It outlines how GEPs can help address challenges related to [1] regulatory compliance, [2] reducing time-to-market pressures, and [3] increasing complexity across globally distributed supply chains. Case studies are provided showing how GEPs have contributed to certification efforts at the component, system, and aircraft levels through activities like testing, documentation, and concurrent engineering. By leveraging their experience and global presence, GEPs can significantly aid certification and help aerospace companies meet business objectives.
1. The document discusses legal aspects of offset obligations in Brazil. It outlines the key authorities and laws governing offsets, requirements and selection criteria.
2. It describes the offset agreement process, including concepts like compensation credits and multipliers. Main clauses of an offset agreement are also outlined.
3. Financial support options from public funding sources for offsets are provided, as well as details on credit insurance and preferential tax regimes for certain sectors.
4. Examples of direct offset contracts involving foreign direct investment and subcontracting or technology transfer are presented.
This document provides guidelines for capital acquisitions and procurement in the Indian defence sector. It outlines the different categories of acquisition as Buy (Indian-IDDM), Buy (Indian), Buy and Make (Indian), Buy and Make, Buy (Global), and Make. Buy (Indian-IDDM) involves procuring indigenously designed, developed, and manufactured products with 40%+ indigenous content. Buy (Indian) requires 40%+ indigenous content. Buy and Make categories involve initial procurement followed by indigenous production through technology transfer. The document provides definitions and priorities for each category and aims to promote indigenous design, development, and manufacturing while ensuring transparency and accountability.
Design of modern aircraft structure and the role of ndiDinesh Kumar C
1) The document discusses the design of modern aircraft structure and the role of non-destructive inspection (NDI).
2) Regulations have increasingly required damage tolerance and inspection programs to prevent fatigue cracks and catastrophic failures.
3) Modern designs use principles like multiple load paths and NDI to detect cracks before they spread, allowing inspection intervals and repair.
Similar to EMAR-who-should-be-the-military-type-certificate-holder-v5 (20)
1. European Military
Aviation Requirements:
Who should be the
Military Type Certificate Holder?
A joint paper by Duane Kritzinger, Principal Consultant at Baines Simmons,
and Lionel Wallace, Consultant at Baines Simmons.
With the promulgation of EMAR 21 in the European Military aviation industry, this paper focuses on
EASA/EMAR 21 Subpart B, which concerns the role and responsibilities of the Type Certificate Holder
(TCH). Specifically the paper strives to stimulate debate on how the participating Member States
(pMS’s) are interpreting the civil requirements when adapting them to the concept of what a Military
Type Certification Holder (MTCH) should be doing.
The concerns identified in this paper have led to some confusion in the industry. If not addressed they
may lead to inefficient practices and result in safety lessons not being disseminated across national
borders. Various scenarios are considered on how to address this issue, with advantages and limitations
of each. Ultimately Baines Simmons has a substantiated preferred option (i.e. Scenario 1) which might
require a fundamental policy shift for many military aviation authorities if they are to realise the full
benefits which the international harmonisation of airworthiness management brings.
July 2016
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12. About Baines Simmons
We are specialists in aviation regulations, compliance and safety management and partner with the
world’s leading civil and defence aviation organisations to improve safety performance.
As trusted advisors to businesses, armed forces, governments and regulators across all sectors of
aviation, we help to advance best practice, shape safety thinking and drive continuous improvement to
safety performance through our consulting, training and outsourced services.
We have a range of white papers available, sharing our expertise in aviation safety issues, from views on
industry news, to more in-depth papers designed to stimulate discussion and debate.
View and download them at www.bainessimmons.com/papers
Baines Simmons is the consulting arm of the LSE-listed global aviation services group, Air Partner PLC
www.airpartner.com
Authors
Duane Kritzinger
Principal Consultant, Baines Simmons
Duane Kritzinger is an experienced Certification and Safety Engineering specialist. His distinguishing safety
expertise lies in the ability to differentiate and integrate the Safety Assessments in the design phase with
the Safety Management activities in the operational phase. His certification skills cover both the military
and civil aviation domains, where he not only provides expertise in the certification of products/parts/
appliance, but also assists with EASA/EMAR Part 21 Design Organisation Approvals (which includes the
establishment of organisation processes and structures to move beyond minimum compliance towards
organisational performance).
Since the publication of EMAR 21, Duane has been assisting both the military regulators (in their adoption
of EMAR 21) and the regulated community (in demonstration compliance in the most efficient manner
with due consideration of other approvals held).
Lionel Wallace
Consultant, Baines Simmons
Lionel is an accomplished Airworthiness, Safety and Certification Consultant who assists clients operating
in the Initial and Continuing Airworthiness sectors with performance enhancing programmes.
With a career background spanning more than 30 years, he is skilled in delivering highly effective
training programmes and provides bespoke advisory services to civil and defence organisations looking
to achieve, maintain and improve compliance with part 21 design approvals. Lionel has previously
represented UK Industry on the ASD Airworthiness Committee and participated in the European
Defence Agency’s work with industry on the establishment of the EMARs through the MAWA forum,
both as a focal point (TF1 - Framework Document) or member of various associated Task Forces
initiated to charter the basis of a EU military airworthiness approach, taking into consideration the civil
aviation regulatory system.
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