This document discusses Airworthiness Directives (ADs) from Transport Canada's Civil Aviation (TCCA) perspective. It outlines when TCCA issues ADs, the differences between TCCA and EASA AD processes, how Alternative Means of Compliance (AMOC) work, the Continuing Airworthiness Information System (CAWIS) database, and how to address questions about ADs. Key points include:
- TCCA issues ADs when an unsafe condition is identified or may exist in an aircraft product. It may accept a manufacturer's campaign instead of an AD.
- Differences from EASA include wording used, TCCA approves service bulletins, and AD corrections require revisions.
- A
This document provides information on supplemental inspections for Cessna 152 aircraft as part of an aging aircraft program. It outlines key terms, inspection requirements and intervals for different operating environments and usage. The inspection documents cover areas like wings, empennage, fuselage and other structural components. The program also includes corrosion prevention and control.
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 is a presentation by Mark L. Laughridge on pilot's airworthiness responsibilities. It defines an airworthy aircraft as one that conforms to its type design and is safe to operate. It discusses the requirements for an aircraft to be considered airworthy, including having a valid airworthiness certificate and registration, complying with all applicable airworthiness directives and maintenance records, ensuring the aircraft is properly weighed and balanced, and that the pilot in command determines the aircraft is in a condition for safe flight before each flight. It also covers topics like inoperative equipment, preventative maintenance, inspections and other responsibilities of aircraft owners and operators to maintain an aircraft in an airworthy condition.
Mark Howell is an experienced aerospace engineer with 18 years of experience in the industry and 12 years working for the UK Ministry of Defence. He currently holds the position of Airborne Forces Equipment Engineering Manager, where he manages a £13M budget and provides safety and airworthiness advice. Some of his key achievements include introducing a new parachute system and implementing an improved parachute deployment system following an accident. He has extensive experience managing projects from concept through deployment and supporting equipment throughout its lifecycle.
504314483-Fuel-Tank-Safety-Level-I-Presentation.pdfmram r
The document discusses efforts by the FAA and EASA to harmonize their fuel tank safety programs. It provides:
1) An overview of lessons learned from SFAR 88 reviews which revealed unexpected ignition sources and the difficulty of eliminating all risks, leading both agencies to adopt a balanced approach of continued ignition prevention efforts alongside reducing tank flammability.
2) Details on the status of ignition prevention reviews and corrective actions being implemented, as well as progress harmonizing flammability reduction standards and a plan to work towards agreement on retrofit requirements.
3) A summary that the combined ignition prevention and flammability reduction strategies should virtually eliminate the risk of future fuel tank explosions, and that FAA and E
This curriculum vitae summarizes Clayton King's experience as an avionics technician and instructor over 30 years working for various companies. He has extensive experience maintaining electrical, instrument, and radio systems on many aircraft types. He also has qualifications in avionics instruction, assessment, safety coordination, and management. His roles have included maintenance engineering, supervision, training, and quality assurance. Employers have provided positive feedback on his skills, work ethic, and ability to lead teams.
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.
This document provides information on supplemental inspections for Cessna 152 aircraft as part of an aging aircraft program. It outlines key terms, inspection requirements and intervals for different operating environments and usage. The inspection documents cover areas like wings, empennage, fuselage and other structural components. The program also includes corrosion prevention and control.
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 is a presentation by Mark L. Laughridge on pilot's airworthiness responsibilities. It defines an airworthy aircraft as one that conforms to its type design and is safe to operate. It discusses the requirements for an aircraft to be considered airworthy, including having a valid airworthiness certificate and registration, complying with all applicable airworthiness directives and maintenance records, ensuring the aircraft is properly weighed and balanced, and that the pilot in command determines the aircraft is in a condition for safe flight before each flight. It also covers topics like inoperative equipment, preventative maintenance, inspections and other responsibilities of aircraft owners and operators to maintain an aircraft in an airworthy condition.
Mark Howell is an experienced aerospace engineer with 18 years of experience in the industry and 12 years working for the UK Ministry of Defence. He currently holds the position of Airborne Forces Equipment Engineering Manager, where he manages a £13M budget and provides safety and airworthiness advice. Some of his key achievements include introducing a new parachute system and implementing an improved parachute deployment system following an accident. He has extensive experience managing projects from concept through deployment and supporting equipment throughout its lifecycle.
504314483-Fuel-Tank-Safety-Level-I-Presentation.pdfmram r
The document discusses efforts by the FAA and EASA to harmonize their fuel tank safety programs. It provides:
1) An overview of lessons learned from SFAR 88 reviews which revealed unexpected ignition sources and the difficulty of eliminating all risks, leading both agencies to adopt a balanced approach of continued ignition prevention efforts alongside reducing tank flammability.
2) Details on the status of ignition prevention reviews and corrective actions being implemented, as well as progress harmonizing flammability reduction standards and a plan to work towards agreement on retrofit requirements.
3) A summary that the combined ignition prevention and flammability reduction strategies should virtually eliminate the risk of future fuel tank explosions, and that FAA and E
This curriculum vitae summarizes Clayton King's experience as an avionics technician and instructor over 30 years working for various companies. He has extensive experience maintaining electrical, instrument, and radio systems on many aircraft types. He also has qualifications in avionics instruction, assessment, safety coordination, and management. His roles have included maintenance engineering, supervision, training, and quality assurance. Employers have provided positive feedback on his skills, work ethic, and ability to lead teams.
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 summarizes the Goddard Space Flight Center (GSFC) Recertification Program (RECERT) which provides scheduled testing, inspection, certification and recertification of lifting devices and equipment (LDE) and ground-based pressure vessels and pressurized systems (PV/S). It outlines the roles and responsibilities of the RECERT Manager and equipment owners to ensure safety compliance. Key aspects of the program include certification of equipment and operators, conducting inspections, and maintaining certification records and tags.
The document is a report from the Portable Electronic Devices Aviation Rulemaking Committee to the Federal Aviation Administration. The report provides recommendations on expanding the use of portable electronic devices during flight. It defines portable electronic devices, describes the committee's methodology and constituencies involved. The report also outlines the current regulatory framework and provides threshold, technical, operational and safety communications recommendations.
This document provides recommendations for de-icing and anti-icing aircraft on the ground. It was prepared by the AEA's De-icing/Anti-icing Working Group and consists of procedures, definitions, references, and guidelines. The document aims to promote safe practices for aircraft ground operations in winter conditions to ensure safety for passengers, crew, and ground personnel.
This document provides recommendations for de-icing and anti-icing aircraft on the ground. It was prepared by the AEA's De-icing/Anti-icing Working Group and consists of procedures, definitions, references, and guidelines. The document aims to promote safe practices for aircraft ground operations in winter conditions to ensure safety for passengers, crew, and ground personnel.
The document discusses reliability data analysis and sharing practices in the aviation industry. It covers regulatory requirements for reporting failures and collecting reliability data. New technologies allow more data to be collected from onboard systems compared to traditional manual collection. Data mining and machine learning techniques can be used to analyze historical reliability event data and more easily identify problems. The document questions if some of the reliability data analysis and sharing practices could be replicated for flight safety or flight data monitoring data.
This document summarizes the requirements for type and production testing of mechanical equipment as outlined in Naval Engineering Standard 362 Issue 3 (Reformatted). It provides details on general requirements, type tests, production tests, and ancillary drives for auxiliary equipment. The standard establishes procedures for testing equipment prior to installation to demonstrate suitability, establish performance characteristics, and set baseline values for production testing. Requirements addressed include test sites, facilities, instrumentation, and documentation of test plans, procedures, and results.
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.
This document discusses aircraft maintenance records and requirements. It emphasizes the importance of accurate documentation and identifies common documentation problems. It outlines requirements for maintenance record content, including descriptions of work performed, completion dates, and signatures. It also discusses issues like poor shift turnovers, non-compliance with airworthiness directives, and the importance of following regulations and procedures for aircraft maintenance.
We are pleased to update to you OCS Training for the 2019 calendar year.
We would be most grateful if you could distribute these invitations to your colleagues and CC me as well.
OCS Training are attended by candidates from many countries like Malaysia, Indonesia, Vietnam, Thailand, Qatar, Australia, China, Singapore, India, Philippines, Brunei, Saudi Arabia, Japan, Korea, Nigeria, and various countries worldwide.
We run Public, Hybrid and In-house Training.
The rate includes training venue in 4/5 stars hotel, participant's manual, Hand-outs, certificate, Buffet Lunch, Coffee/Tea on arrival, morning & afternoon on each day.
For registration and further information you may reply back this email.
We are looking forward to your participation.
---Get 10% discount by registering before 2019---
For further information and registration please feel free to contact us.
Thank you & have a great day ahead!
For more information on how to enroll contact us at muanisa@ocsgroup.com or phone at +6221 2555 5772 / +6281617851607
#training #piping #preparationcourse #inform #howto #masterclass #bestcourse #pipingengineering #inspectiontraining #certification #downstream
Optimizing Fire3 and Gas System Design Using the ISA Technical Report ISA TR8...Kenexis
Fire and Gas Detection and Suppression Systems (FGS) have long been successfully employed as a safeguard in the process industries. Unfortunately, design methods for determining the quantity and placement of detectors have historically been less than satisfactory. Design practices based on rules of thumb and experiences have often resulted in design inconsistencies, and achievement of tolerable risk cannot be ascertained. Rule-based methods often place detectors where they are not needed and leave high risk areas unnecessarily exposed. ISA released technical report TR 84.00.07 to address this problem. This technical report explains the metrics, such as detector coverage, and techniques that can be applied to the design of FGS which results in optimal designs that are safer and more repeatable. This paper will provide an overview of the contents of the technical report, and also provide some case study examples that show how these performance-based methods result in superior designs to currently used techniques such as grid-based approaches.
Routine of helicopter maintenance activitiesBai Haqi
This document provides information on routine helicopter maintenance activities from the Malaysian Institute of Aviation Technology. It discusses the different types of scheduled and unscheduled inspections, including pre-flight, turn-around, post-flight, minor and major inspections. The document outlines the manufacturer's maintenance program and provides examples of inspection procedures for specific helicopter models. It emphasizes the importance of safety precautions for maintenance personnel.
Emergency Airworthiness Directive (AD) 2014-25-52 is sent to owners and operators of Airbus Model A330-200 Freighter, -200, and -300 series airplanes and Model A340-200, -300, -500, and -600 series airplanes.
This document provides information on the Chassis II course which focuses on electric power steering. The course aims to teach students how to setup a scan tool, perform electric power steering diagnosis using the scan tool, and replace electric power steering components. The course contains 3 competency units - setup scan tool, operate scan tool for electric power steering diagnosis, and replace the electric power steering motor and control module. It outlines the learning standards, assessment criteria, and references for each competency unit.
livro dedicado aos amantes de voo com aeronaves leves, principalmente as de asas rotativas. Excelente manual publicado pela FAA e que serve de referencia para muitas escolas de aviação no mundo todo.
Keith Costall has extensive experience in airport management, airfield lighting, and training for the aviation industry worldwide. He is currently Director of Technical Services and Training at Perfect Airport Solutions, which provides professional support to airport authorities. Keith has a background in both aircraft and airfield engineering and has been involved in developing airfield ground lighting training packages. He has worked with major airports and organizations around the world, including in South Africa, Israel, Malaysia, Afghanistan, and Singapore.
GEPAM uuuuuuuuuuuuuuuuuuuuuuUNIT IV V.pptssuser856cc8
This document discusses general aircraft inspection procedures and techniques. It covers topics such as visual inspections, checklists, publications used for inspections like manuals and airworthiness directives, non-destructive testing methods, and special inspections required after events like hard landings, turbulence, or lightning strikes. The goal of inspections is to determine an aircraft's airworthiness and identify any defects or needed maintenance through systematic examination of its components and systems.
UAV Certification - extract for AUVSI 2015 Mike Roberts
The document discusses regulation and certification of unmanned aerial vehicles (UAVs) from an Australian perspective. It outlines how UAV certification differs from manned aircraft certification due to different risk profiles and inability to meet all manned criteria. While regulation of manned aviation is consistent globally, UAV regulation varies widely. The document evaluates existing certification standards like MIL-HDBK-516B and STANAG 4671 that can be used as bases for UAV certification and notes they provide a solid baseline but lack widely accepted standards. Risk assessment is a key part of UAV certification and operations.
An improved modulation technique suitable for a three level flying capacitor ...IJECEIAES
This research paper introduces an innovative modulation technique for controlling a 3-level flying capacitor multilevel inverter (FCMLI), aiming to streamline the modulation process in contrast to conventional methods. The proposed
simplified modulation technique paves the way for more straightforward and
efficient control of multilevel inverters, enabling their widespread adoption and
integration into modern power electronic systems. Through the amalgamation of
sinusoidal pulse width modulation (SPWM) with a high-frequency square wave
pulse, this controlling technique attains energy equilibrium across the coupling
capacitor. The modulation scheme incorporates a simplified switching pattern
and a decreased count of voltage references, thereby simplifying the control
algorithm.
The document summarizes the Goddard Space Flight Center (GSFC) Recertification Program (RECERT) which provides scheduled testing, inspection, certification and recertification of lifting devices and equipment (LDE) and ground-based pressure vessels and pressurized systems (PV/S). It outlines the roles and responsibilities of the RECERT Manager and equipment owners to ensure safety compliance. Key aspects of the program include certification of equipment and operators, conducting inspections, and maintaining certification records and tags.
The document is a report from the Portable Electronic Devices Aviation Rulemaking Committee to the Federal Aviation Administration. The report provides recommendations on expanding the use of portable electronic devices during flight. It defines portable electronic devices, describes the committee's methodology and constituencies involved. The report also outlines the current regulatory framework and provides threshold, technical, operational and safety communications recommendations.
This document provides recommendations for de-icing and anti-icing aircraft on the ground. It was prepared by the AEA's De-icing/Anti-icing Working Group and consists of procedures, definitions, references, and guidelines. The document aims to promote safe practices for aircraft ground operations in winter conditions to ensure safety for passengers, crew, and ground personnel.
This document provides recommendations for de-icing and anti-icing aircraft on the ground. It was prepared by the AEA's De-icing/Anti-icing Working Group and consists of procedures, definitions, references, and guidelines. The document aims to promote safe practices for aircraft ground operations in winter conditions to ensure safety for passengers, crew, and ground personnel.
The document discusses reliability data analysis and sharing practices in the aviation industry. It covers regulatory requirements for reporting failures and collecting reliability data. New technologies allow more data to be collected from onboard systems compared to traditional manual collection. Data mining and machine learning techniques can be used to analyze historical reliability event data and more easily identify problems. The document questions if some of the reliability data analysis and sharing practices could be replicated for flight safety or flight data monitoring data.
This document summarizes the requirements for type and production testing of mechanical equipment as outlined in Naval Engineering Standard 362 Issue 3 (Reformatted). It provides details on general requirements, type tests, production tests, and ancillary drives for auxiliary equipment. The standard establishes procedures for testing equipment prior to installation to demonstrate suitability, establish performance characteristics, and set baseline values for production testing. Requirements addressed include test sites, facilities, instrumentation, and documentation of test plans, procedures, and results.
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.
This document discusses aircraft maintenance records and requirements. It emphasizes the importance of accurate documentation and identifies common documentation problems. It outlines requirements for maintenance record content, including descriptions of work performed, completion dates, and signatures. It also discusses issues like poor shift turnovers, non-compliance with airworthiness directives, and the importance of following regulations and procedures for aircraft maintenance.
We are pleased to update to you OCS Training for the 2019 calendar year.
We would be most grateful if you could distribute these invitations to your colleagues and CC me as well.
OCS Training are attended by candidates from many countries like Malaysia, Indonesia, Vietnam, Thailand, Qatar, Australia, China, Singapore, India, Philippines, Brunei, Saudi Arabia, Japan, Korea, Nigeria, and various countries worldwide.
We run Public, Hybrid and In-house Training.
The rate includes training venue in 4/5 stars hotel, participant's manual, Hand-outs, certificate, Buffet Lunch, Coffee/Tea on arrival, morning & afternoon on each day.
For registration and further information you may reply back this email.
We are looking forward to your participation.
---Get 10% discount by registering before 2019---
For further information and registration please feel free to contact us.
Thank you & have a great day ahead!
For more information on how to enroll contact us at muanisa@ocsgroup.com or phone at +6221 2555 5772 / +6281617851607
#training #piping #preparationcourse #inform #howto #masterclass #bestcourse #pipingengineering #inspectiontraining #certification #downstream
Optimizing Fire3 and Gas System Design Using the ISA Technical Report ISA TR8...Kenexis
Fire and Gas Detection and Suppression Systems (FGS) have long been successfully employed as a safeguard in the process industries. Unfortunately, design methods for determining the quantity and placement of detectors have historically been less than satisfactory. Design practices based on rules of thumb and experiences have often resulted in design inconsistencies, and achievement of tolerable risk cannot be ascertained. Rule-based methods often place detectors where they are not needed and leave high risk areas unnecessarily exposed. ISA released technical report TR 84.00.07 to address this problem. This technical report explains the metrics, such as detector coverage, and techniques that can be applied to the design of FGS which results in optimal designs that are safer and more repeatable. This paper will provide an overview of the contents of the technical report, and also provide some case study examples that show how these performance-based methods result in superior designs to currently used techniques such as grid-based approaches.
Routine of helicopter maintenance activitiesBai Haqi
This document provides information on routine helicopter maintenance activities from the Malaysian Institute of Aviation Technology. It discusses the different types of scheduled and unscheduled inspections, including pre-flight, turn-around, post-flight, minor and major inspections. The document outlines the manufacturer's maintenance program and provides examples of inspection procedures for specific helicopter models. It emphasizes the importance of safety precautions for maintenance personnel.
Emergency Airworthiness Directive (AD) 2014-25-52 is sent to owners and operators of Airbus Model A330-200 Freighter, -200, and -300 series airplanes and Model A340-200, -300, -500, and -600 series airplanes.
This document provides information on the Chassis II course which focuses on electric power steering. The course aims to teach students how to setup a scan tool, perform electric power steering diagnosis using the scan tool, and replace electric power steering components. The course contains 3 competency units - setup scan tool, operate scan tool for electric power steering diagnosis, and replace the electric power steering motor and control module. It outlines the learning standards, assessment criteria, and references for each competency unit.
livro dedicado aos amantes de voo com aeronaves leves, principalmente as de asas rotativas. Excelente manual publicado pela FAA e que serve de referencia para muitas escolas de aviação no mundo todo.
Keith Costall has extensive experience in airport management, airfield lighting, and training for the aviation industry worldwide. He is currently Director of Technical Services and Training at Perfect Airport Solutions, which provides professional support to airport authorities. Keith has a background in both aircraft and airfield engineering and has been involved in developing airfield ground lighting training packages. He has worked with major airports and organizations around the world, including in South Africa, Israel, Malaysia, Afghanistan, and Singapore.
GEPAM uuuuuuuuuuuuuuuuuuuuuuUNIT IV V.pptssuser856cc8
This document discusses general aircraft inspection procedures and techniques. It covers topics such as visual inspections, checklists, publications used for inspections like manuals and airworthiness directives, non-destructive testing methods, and special inspections required after events like hard landings, turbulence, or lightning strikes. The goal of inspections is to determine an aircraft's airworthiness and identify any defects or needed maintenance through systematic examination of its components and systems.
UAV Certification - extract for AUVSI 2015 Mike Roberts
The document discusses regulation and certification of unmanned aerial vehicles (UAVs) from an Australian perspective. It outlines how UAV certification differs from manned aircraft certification due to different risk profiles and inability to meet all manned criteria. While regulation of manned aviation is consistent globally, UAV regulation varies widely. The document evaluates existing certification standards like MIL-HDBK-516B and STANAG 4671 that can be used as bases for UAV certification and notes they provide a solid baseline but lack widely accepted standards. Risk assessment is a key part of UAV certification and operations.
Similar to EASA AD Workshop 2014 - 06_TCCA AD presentation.pdf (20)
An improved modulation technique suitable for a three level flying capacitor ...IJECEIAES
This research paper introduces an innovative modulation technique for controlling a 3-level flying capacitor multilevel inverter (FCMLI), aiming to streamline the modulation process in contrast to conventional methods. The proposed
simplified modulation technique paves the way for more straightforward and
efficient control of multilevel inverters, enabling their widespread adoption and
integration into modern power electronic systems. Through the amalgamation of
sinusoidal pulse width modulation (SPWM) with a high-frequency square wave
pulse, this controlling technique attains energy equilibrium across the coupling
capacitor. The modulation scheme incorporates a simplified switching pattern
and a decreased count of voltage references, thereby simplifying the control
algorithm.
Rainfall intensity duration frequency curve statistical analysis and modeling...bijceesjournal
Using data from 41 years in Patna’ India’ the study’s goal is to analyze the trends of how often it rains on a weekly, seasonal, and annual basis (1981−2020). First, utilizing the intensity-duration-frequency (IDF) curve and the relationship by statistically analyzing rainfall’ the historical rainfall data set for Patna’ India’ during a 41 year period (1981−2020), was evaluated for its quality. Changes in the hydrologic cycle as a result of increased greenhouse gas emissions are expected to induce variations in the intensity, length, and frequency of precipitation events. One strategy to lessen vulnerability is to quantify probable changes and adapt to them. Techniques such as log-normal, normal, and Gumbel are used (EV-I). Distributions were created with durations of 1, 2, 3, 6, and 24 h and return times of 2, 5, 10, 25, and 100 years. There were also mathematical correlations discovered between rainfall and recurrence interval.
Findings: Based on findings, the Gumbel approach produced the highest intensity values, whereas the other approaches produced values that were close to each other. The data indicates that 461.9 mm of rain fell during the monsoon season’s 301st week. However, it was found that the 29th week had the greatest average rainfall, 92.6 mm. With 952.6 mm on average, the monsoon season saw the highest rainfall. Calculations revealed that the yearly rainfall averaged 1171.1 mm. Using Weibull’s method, the study was subsequently expanded to examine rainfall distribution at different recurrence intervals of 2, 5, 10, and 25 years. Rainfall and recurrence interval mathematical correlations were also developed. Further regression analysis revealed that short wave irrigation, wind direction, wind speed, pressure, relative humidity, and temperature all had a substantial influence on rainfall.
Originality and value: The results of the rainfall IDF curves can provide useful information to policymakers in making appropriate decisions in managing and minimizing floods in the study area.
Electric vehicle and photovoltaic advanced roles in enhancing the financial p...IJECEIAES
Climate change's impact on the planet forced the United Nations and governments to promote green energies and electric transportation. The deployments of photovoltaic (PV) and electric vehicle (EV) systems gained stronger momentum due to their numerous advantages over fossil fuel types. The advantages go beyond sustainability to reach financial support and stability. The work in this paper introduces the hybrid system between PV and EV to support industrial and commercial plants. This paper covers the theoretical framework of the proposed hybrid system including the required equation to complete the cost analysis when PV and EV are present. In addition, the proposed design diagram which sets the priorities and requirements of the system is presented. The proposed approach allows setup to advance their power stability, especially during power outages. The presented information supports researchers and plant owners to complete the necessary analysis while promoting the deployment of clean energy. The result of a case study that represents a dairy milk farmer supports the theoretical works and highlights its advanced benefits to existing plants. The short return on investment of the proposed approach supports the paper's novelty approach for the sustainable electrical system. In addition, the proposed system allows for an isolated power setup without the need for a transmission line which enhances the safety of the electrical network
Embedded machine learning-based road conditions and driving behavior monitoringIJECEIAES
Car accident rates have increased in recent years, resulting in losses in human lives, properties, and other financial costs. An embedded machine learning-based system is developed to address this critical issue. The system can monitor road conditions, detect driving patterns, and identify aggressive driving behaviors. The system is based on neural networks trained on a comprehensive dataset of driving events, driving styles, and road conditions. The system effectively detects potential risks and helps mitigate the frequency and impact of accidents. The primary goal is to ensure the safety of drivers and vehicles. Collecting data involved gathering information on three key road events: normal street and normal drive, speed bumps, circular yellow speed bumps, and three aggressive driving actions: sudden start, sudden stop, and sudden entry. The gathered data is processed and analyzed using a machine learning system designed for limited power and memory devices. The developed system resulted in 91.9% accuracy, 93.6% precision, and 92% recall. The achieved inference time on an Arduino Nano 33 BLE Sense with a 32-bit CPU running at 64 MHz is 34 ms and requires 2.6 kB peak RAM and 139.9 kB program flash memory, making it suitable for resource-constrained embedded systems.
Null Bangalore | Pentesters Approach to AWS IAMDivyanshu
#Abstract:
- Learn more about the real-world methods for auditing AWS IAM (Identity and Access Management) as a pentester. So let us proceed with a brief discussion of IAM as well as some typical misconfigurations and their potential exploits in order to reinforce the understanding of IAM security best practices.
- Gain actionable insights into AWS IAM policies and roles, using hands on approach.
#Prerequisites:
- Basic understanding of AWS services and architecture
- Familiarity with cloud security concepts
- Experience using the AWS Management Console or AWS CLI.
- For hands on lab create account on [killercoda.com](https://killercoda.com/cloudsecurity-scenario/)
# Scenario Covered:
- Basics of IAM in AWS
- Implementing IAM Policies with Least Privilege to Manage S3 Bucket
- Objective: Create an S3 bucket with least privilege IAM policy and validate access.
- Steps:
- Create S3 bucket.
- Attach least privilege policy to IAM user.
- Validate access.
- Exploiting IAM PassRole Misconfiguration
-Allows a user to pass a specific IAM role to an AWS service (ec2), typically used for service access delegation. Then exploit PassRole Misconfiguration granting unauthorized access to sensitive resources.
- Objective: Demonstrate how a PassRole misconfiguration can grant unauthorized access.
- Steps:
- Allow user to pass IAM role to EC2.
- Exploit misconfiguration for unauthorized access.
- Access sensitive resources.
- Exploiting IAM AssumeRole Misconfiguration with Overly Permissive Role
- An overly permissive IAM role configuration can lead to privilege escalation by creating a role with administrative privileges and allow a user to assume this role.
- Objective: Show how overly permissive IAM roles can lead to privilege escalation.
- Steps:
- Create role with administrative privileges.
- Allow user to assume the role.
- Perform administrative actions.
- Differentiation between PassRole vs AssumeRole
Try at [killercoda.com](https://killercoda.com/cloudsecurity-scenario/)
Software Engineering and Project Management - Introduction, Modeling Concepts...Prakhyath Rai
Introduction, Modeling Concepts and Class Modeling: What is Object orientation? What is OO development? OO Themes; Evidence for usefulness of OO development; OO modeling history. Modeling
as Design technique: Modeling, abstraction, The Three models. Class Modeling: Object and Class Concept, Link and associations concepts, Generalization and Inheritance, A sample class model, Navigation of class models, and UML diagrams
Building the Analysis Models: Requirement Analysis, Analysis Model Approaches, Data modeling Concepts, Object Oriented Analysis, Scenario-Based Modeling, Flow-Oriented Modeling, class Based Modeling, Creating a Behavioral Model.
Applications of artificial Intelligence in Mechanical Engineering.pdfAtif Razi
Historically, mechanical engineering has relied heavily on human expertise and empirical methods to solve complex problems. With the introduction of computer-aided design (CAD) and finite element analysis (FEA), the field took its first steps towards digitization. These tools allowed engineers to simulate and analyze mechanical systems with greater accuracy and efficiency. However, the sheer volume of data generated by modern engineering systems and the increasing complexity of these systems have necessitated more advanced analytical tools, paving the way for AI.
AI offers the capability to process vast amounts of data, identify patterns, and make predictions with a level of speed and accuracy unattainable by traditional methods. This has profound implications for mechanical engineering, enabling more efficient design processes, predictive maintenance strategies, and optimized manufacturing operations. AI-driven tools can learn from historical data, adapt to new information, and continuously improve their performance, making them invaluable in tackling the multifaceted challenges of modern mechanical engineering.
Optimizing Gradle Builds - Gradle DPE Tour Berlin 2024Sinan KOZAK
Sinan from the Delivery Hero mobile infrastructure engineering team shares a deep dive into performance acceleration with Gradle build cache optimizations. Sinan shares their journey into solving complex build-cache problems that affect Gradle builds. By understanding the challenges and solutions found in our journey, we aim to demonstrate the possibilities for faster builds. The case study reveals how overlapping outputs and cache misconfigurations led to significant increases in build times, especially as the project scaled up with numerous modules using Paparazzi tests. The journey from diagnosing to defeating cache issues offers invaluable lessons on maintaining cache integrity without sacrificing functionality.
2. Outline
• Issuing ADs – Why, When, What?
• Differences from EASA
• AMOCs
• Continuing Airworthiness Information
System (CAWIS)
• When questions arise
• How can TCCA ADs be improved?
EASAAD Workshop, 2-3 December 2014 2
3. What
Canadian Aviation Regulation (CAR) 101.01:
“an instruction issued by the Minister or by a civil
aviation authority responsible for an aeronautical
product type design that mandates a maintenance or
operation action to ensure that an aeronautical
product conforms to its type design and is in a
condition for safe operation”
EASAAD Workshop, 2-3 December 2014 3
4. What
Mandatory Continuing Airworthiness
Instruction (MCAI) in accordance with ICAO
Annex 8
Issued in English and French, except for
Emergency AD which can be issued in
English only
EASAAD Workshop, 2-3 December 2014 4
5. What
Number of ADs issued:
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Year No. of ADs
2012 33
2013 41
2014 42
6. Why
An unsafe condition has been identified on
an aeronautical product
“aeronautical product” means any aircraft, aircraft
engine, aircraft propeller or aircraft appliance or part or
the component parts of any of those things, including
any computer system and software
Aeronautics Act
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7. Why
CAR compels the Minister of Transport to
issue AD when there is unsafe condition
521.427 (1) The Minister shall issue an airworthiness
directive in respect of an aeronautical product if
(a) an unsafe condition exists in the aeronautical
product and the condition is likely to exist or develop in
other aeronautical products
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8. Why
However, TC can accept a campaign from
the DADH instead of issuing an AD
“Note:
TCCA does not necessarily automatically issue an
airworthiness directive. It may allow the manufacturer to
campaign the replacement of defective parts. Where
that campaign is not successful, then TCCA will issue
an airworthiness directive.”
TCCA/EASA Technical Implementation Procedures for
Airworthiness and Environmental Certification
EASAAD Workshop, 2-3 December 2014 8
9. Why
An unsafe condition has not been verified,
but there is reason to believe that it exists or
is likely to come into existence in an
aeronautical product
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11. Why
An existing AD (foreign or Canadian) needs to be
cancelled or amended
CAR 521.427 (1) The Minister shall issue an airworthiness directive in
respect of an aeronautical product if
(b) it is necessary to modify or cancel the requirements of an airworthiness
directive issued by the foreign airworthiness authority having jurisdiction
over the type design of the aeronautical product because the Minister
considers the airworthiness directive inappropriate for reasons related to
the environment, safety, the delayed receipt of an instruction issued by the
foreign airworthiness authority or reliance on foreign legislation; or
(c) it is necessary to modify or cancel a Canadian airworthiness directive
that is in force, because a condition for issuance referred to in paragraph
(a) or (b) has changed or ceased to exist.
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14. Why
Need to override a global Alternative Means
of Compliance (AMOC) granted by the state
of design
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15. Why
Emergency equipment intended to minimize
the effects of survivable accidents is not
performing its intended function
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17. Why
Hazard of collateral damage/injuries on
ground/personnel caused by components
that have detached from the aircraft
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MLG door landed in Maryland park Engine part damaged car in Toronto
19. Why
Deficiency in components which are
involved in fire protection or are intended to
minimize/retard the effects of fire/smoke in a
survivable crash (e.g. non-compliance with
the applicable flammability requirements)
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21. Why
Design features used to assist in the enquiry
following an accident (e.g. CVR, FDR, ELT
are not performing their intended function
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23. When – Types of AD
•Normal AD
•Emergency AD
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24. When – Compliance Time
Establishing compliance time based on:
•Urgency of the Unsafe Condition
•Parts Availability
•Practicality of Performing the Required Tasks
•Impact of Required Actions on Existing Maintenance
and Overhaul Schedules
•Need for a “Phase-In Period”
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25. What – Equipment AD
•For items with approval certificate such as
TSO, STC, Part Design Approval (PDA)
•AD applicability section identifies affected
components/installed modifications using
words “Installed on, but not limited to, [list
known affected aeronautical products].”
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27. What – AD on Airworthiness
Limitations
AD is required when:
•New or more restrictive Airworthiness Limitations
(AWL), Fuel System Limitations, Flight Manual
Limitations, Certification Maintenance Requirements
(CMR) are introduced post-certification.
Except if:
•Non-compliance with new or more restrictive
limitations/requirements will not result in unsafe
condition
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28. What – AD on Airworthiness
Limitations
Example of “more restrictive”:
•Reduction of inspection interval
•Reduction in Safe Life Limit/mandatory replacement
time
•Reduction in operational limitations (e.g. Never Exceed
Speed)
•Change of inspection method from visual to NDI
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29. What – AD on Airworthiness
Limitations
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30. What – AD on Airworthiness
Limitations
Typical wording:
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31. What – Unilateral AD
State of design authority may disagree with
TCCA on the unsafe condition and decide
not to issue AD
This type of AD issued by TCCA is generally
not of concern to EU operators
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33. What – Supersede vs. Cancel
Supersedure
•ADs are superseded if a different Canadian AD is
issued
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34. What – Supersede vs. Cancel
Cancellation
•ADs are cancelled if the requirements are completely
cancelled, with no other requirements, or if a foreign AD
is applicable
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35. What – Supersede vs. Cancel
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36. Differences from EASA
Wording used
“air time” is defined in CAR 101.01 and operators
are required to track that
EASAAD Workshop, 2-3 December 2014 36
EASA TCCA
Flight hours Hours Air Time
Does not approve
SBs
Approves SB
37. Differences from EASA
Approval of SB
CAR 521.356 If the Minister determines that a
corrective action is required to rectify an unsafe
condition in an aeronautical product, the holder of the
design approval document in respect of the
aeronautical product shall
(a) submit to the Minister for approval the corrective
action required to rectify the unsafe condition
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38. Differences from EASA
Types of AD
EASAAD Workshop, 2-3 December 2014 38
EASA TCCA
AD Correction without AD
revision
Correction to AD requires
AD revision
41. EASAAD Workshop, 2-3 December 2014 41
What to do when caught in a difficult
situation?
AMOC
42. AMOC
3.5(2) “The State of Design shall, upon
request, assist in determining the
acceptability of a specific AMOC request
submitted to the Importing Party on an
airworthiness directive that has been issued
by the State of Design for its own civil
aeronautical products.”
TCCA/EASA Technical Implementation Procedures for
Airworthiness and Environmental Certification
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44. AMOC
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“The State of Design shall, upon request,
assist in determining the acceptability...”
45. AMOC
3.5(1) “An AMOC of general applicability that
is issued by either Competent Authority for
its own State of Design civil aeronautical
products is considered automatically
accepted by the other Competent
Authority.”
TCCA/EASA Technical Implementation Procedures for
Airworthiness and Environmental Certification
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46. AMOC
“general applicability” would mean “Global
AMOCs” issued by TCCA
“Global AMOC” applies to multiple
owners/operators of affected Canadian state
of design aeronautical products
Issued to a DADH
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47. Global AMOC
A letter issued by Chief of Continuing
Airworthiness with AMOC number (e.g
AARDG 2014/A23)
DADH distribute and communicate to
owner/operators (e.g. AOM)
Not published in TCCA website
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