ATA Spec 100 provides industry-wide standards for aircraft maintenance documentation, including systems numbering and guidelines for technical manual content and format. It was originally released in 1999 but has since been combined with other specifications into a consolidated standard called ATA iSpec 2200, which provides guidelines for electronic aircraft information exchange. ATA Spec 100 defined a widely used numbering scheme for aircraft parts and systems and is used by airlines for maintenance.
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.
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.
The document discusses aircraft maintenance programmes and their importance in airworthiness management. It defines a maintenance programme as a schedule of maintenance tasks with documented management procedures. It notes key information sources for maintenance programmes include the MPD, CMM, SBs, and STCs. Approval of maintenance programmes may be issued to Sub Part G organisations. Effective maintenance programme management requires qualified specialists, applicable procedures, and oversight functions. Programmes aim to optimize maintenance tasks through reliability monitoring and review.
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.
EASA (European Aviation Safety Agency) regulates aviation safety and sets standards across Europe. EASA Part 66 specifies requirements for aircraft maintenance licenses. It establishes license categories based on an individual's knowledge and experience with different aircraft and engine types. Gold Air Training Center is an EASA-approved organization that provides training and examinations to help individuals obtain their EASA Part 66 aircraft maintenance license. Their experienced instructors offer flexible courses both in Turkey and other locations worldwide.
EASA Part 66 Module 5.13 : Software Management Controlsoulstalker
Software management in order the prevent catastrophic failure on aircraft.
Slide for student who want to take EASA part 66 exam.
Other presentation you can get at :
http://part66.blogspot.com/
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.
The responsibilities of EASA include to:
Giving advice for the drafting of EU legislation, implementing and monitoring safety rules (including inspections in the member states),
Giving type-certification of aircraft and components as well as the approval of organizations involved in the design,
Authorizing foreign operators,
Manufacture and maintenance of aeronautical products.
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.
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.
The document discusses aircraft maintenance programmes and their importance in airworthiness management. It defines a maintenance programme as a schedule of maintenance tasks with documented management procedures. It notes key information sources for maintenance programmes include the MPD, CMM, SBs, and STCs. Approval of maintenance programmes may be issued to Sub Part G organisations. Effective maintenance programme management requires qualified specialists, applicable procedures, and oversight functions. Programmes aim to optimize maintenance tasks through reliability monitoring and review.
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.
EASA (European Aviation Safety Agency) regulates aviation safety and sets standards across Europe. EASA Part 66 specifies requirements for aircraft maintenance licenses. It establishes license categories based on an individual's knowledge and experience with different aircraft and engine types. Gold Air Training Center is an EASA-approved organization that provides training and examinations to help individuals obtain their EASA Part 66 aircraft maintenance license. Their experienced instructors offer flexible courses both in Turkey and other locations worldwide.
EASA Part 66 Module 5.13 : Software Management Controlsoulstalker
Software management in order the prevent catastrophic failure on aircraft.
Slide for student who want to take EASA part 66 exam.
Other presentation you can get at :
http://part66.blogspot.com/
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.
The responsibilities of EASA include to:
Giving advice for the drafting of EU legislation, implementing and monitoring safety rules (including inspections in the member states),
Giving type-certification of aircraft and components as well as the approval of organizations involved in the design,
Authorizing foreign operators,
Manufacture and maintenance of aeronautical products.
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 is a presentation by Barry G. Byrd of the Federal Aviation Administration given on March 28, 2012 about failure to follow procedures. It discusses FAA regulations regarding maintenance procedures and performance standards. It provides an overview of causal factors for maintenance errors and uses an accident example where failure to follow procedures led to loss of control during takeoff. The presentation aims to increase awareness of risks from failing to follow procedures and how following preventative measures and safety nets can reduce maintenance errors.
The document provides an overview of changes between the new AC 43.13-1B advisory circular and the old AC 43.13-1A version. Key changes include expanded sections on welding, nondestructive testing, corrosion protection, hardware, and electrical systems. Additional topics such as fiberglass/plastics repair and avionics were also added. The new version aims to provide more detailed guidance and safety information to help aircraft technicians in their inspection and repair tasks.
The document discusses various types of documentation used for aircraft maintenance, including manufacturer's documentation, regulatory documentation, and airline generated documentation. It describes documentation such as the maintenance manual, fault isolation manual, illustrated parts catalogue, wiring diagram manual, minimum equipment list, and more. It explains that proper documentation is essential for safely performing maintenance and troubleshooting aircraft systems.
Aircraft Maintenance Manuals for Engineer's by Engr. Malay Kanti BalaMalay Kanti Bala
Aircraft Maintenance Manual is an important document for the Aircraft Maintenance Personnel. For the airworthiness of any flight, we do an inspection, servicing, repair, removal, installation, etc activities by following the approved documents which in manual or AMM. Here the presentation will disclose and familiarise with different manuals
This document discusses S1000D data modules, which are reusable blocks of information that can be shared and reused across technical publications. It describes the components of a data module, including the metadata ID status section and content section. It provides examples of different types of data modules, such as those for fault isolation, maintenance planning, parts information, and wiring data. The document is presented by Absolute Data Group, a provider of S1000D and technical documentation products and services.
The document provides guidance for maintenance technicians and inspection authorization holders on performing aircraft inspections. It discusses the importance of inspections, building relationships with aircraft owners, explaining inspection requirements to owners, and ensuring discrepancies found are properly addressed. It also reviews sample inspection requirements for specific aircraft, including reviewing registration, manuals, records, the type certificate data sheet, and completing a full inspection to verify airworthiness.
This slide is prepared by me for the students studying in 1st Semester of Aircraft Maintenance Engineering. This is only the the introduction of Maintenance Practices involved in Aircraft Maintenance. Reference is taken from various aviation books and websites. Suggestions are welcome. Pls leave a like
PS- after downloading please don't change the name of author as you will be disregarding all the hard work done by me.
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.
The document discusses India's CAR 66, which establishes requirements for aircraft maintenance engineer licensing. It consolidates separate airframe, engine, electrical and instrument licenses into one license. CAR 66 licenses will be available through converting existing licenses or obtaining new licenses after passing modules. It covers technical requirements, applications, basic knowledge modules, experience requirements, and type ratings. CAR 66 aims to align India's licensing with international standards while allowing for transition from previous licensing rules.
This document outlines the requirements for certifying staff authorisation for aircraft maintenance organisations according to CAR 145. Key points include:
- Initial training and assessment of certifying staff including human factors, procedures, technology and experience requirements.
- Certification authorisations must be issued by the organisation once certifying staff meet competence and experience criteria. Authorisations clearly define the certifier's privileges and limitations.
- Certifying staff must complete continuation training every two years covering technology, procedures, human factors and quality findings to maintain authorisation.
- Certifying staff are required to have six months maintenance experience in relevant aircraft systems over a two-year period.
5.15 Typical electronic digital aircraft systemslpapadop
This document provides an overview of typical electronic and digital aircraft systems. It discusses computer maintenance systems, ACARS, EFIS, EICAS/ECAM, fly-by-wire, flight management systems, GPS, inertial navigation systems, traffic collision avoidance systems, and flight data recorders. It also describes built-in test equipment, on-board maintenance facilities, and how various systems monitor aircraft data and perform tests. Finally, it provides details on electronic flight instrument systems, cockpit displays, and how fly-by-wire replaces manual flight controls with electronic signaling.
The document defines preventive maintenance and outlines who is authorized to perform it according to FAA regulations. It specifies that holders of pilot certificates can perform preventive maintenance on aircraft they own or operate, including private pilots. The document lists the specific preventive maintenance tasks allowed by FAA regulations and provides guidance on maintenance records, required performance standards, and additional FAA resources.
Aircraft maintenance program enhancement badawood mamdoohbmamdooh
This document discusses aircraft maintenance programs and enhancing them for specific operators. It describes developing a customized maintenance program (CMP) by analyzing control elements like utilization and reliability reports. A CMP case study for SVA B747-400s is presented, showing a CMP reduced costs by 23% while improving availability. The document also describes supplementing structural inspection documents into maintenance programs, noting SVA achieved a 64% integration rate and $1.85 million in savings for its B747 fleet.
This document outlines the technical requirements for Maintenance Training Organizations (MTOs) seeking approval under CAR 147. It discusses requirements for facilities, personnel, training procedures and materials, record keeping, examinations and oversight. Key requirements include having adequate facilities, qualified instructors, appropriate training equipment and materials, a quality system for monitoring standards, secure storage of records and examinations, and procedures for handling changes, continued validity and oversight findings.
Aircraft wheels are an important component of the landing gear system that support the weight of the aircraft during taxi, takeoff, and landing. Modern aircraft wheels are typically constructed of two lightweight yet strong aluminum alloy halves bolted together, with the inboard half fitted with keyways to engage the brake discs. The two-piece wheel construction allows for tubeless tires, which are sealed between the wheel halves. Aircraft tires experience tremendous loads and temperatures compared to automobile tires, requiring specialized construction and nitrogen inflation for optimal performance.
This document provides an overview and introduction to the information objects stored in a Common Source Database (CSDB) according to the S1000D specification. It describes the three major types of information objects as data modules, graphical objects, and publication modules. Data modules include different types like crew/operator, descriptive, fault isolation, etc. each with their own SGML document type definitions (DTDs). Other information objects include publication modules, comment modules, data dispatch notes, and data module lists, which have XML DTDs. Graphical objects like illustrations are also stored in the CSDB.
This presentation is an examination of structural repair of aircraft. It details the goals, regulations and classification of repairs for different types of aircraft damage.
The paper that this presentation is based on was presented by Dr. Kishore Brahma of the AXISCADES Engineering Core Group at the International Conference & Exhibition on Fatigue, Durability & Fracture Mechanics (FatigueDurabilityIndia2015) in Bangalore from 28-30th May 2015.
Este documento resume el contenido de varias circulares de asesoramiento emitidas por la Autoridad Aeronáutica Civil de México. Las circulares proveen orientación e instrucciones a operadores aéreos sobre procedimientos para cumplir con normas de aeronavegabilidad. Las circulares cubren temas como aeronaves, aeropuertos, personal técnico, y requisitos para concesionarios y operadores. Todas las circulares buscan mejorar la seguridad operacional de acuerdo con la legislación y normatividad aeronáuticas mexicanas
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 is a presentation by Barry G. Byrd of the Federal Aviation Administration given on March 28, 2012 about failure to follow procedures. It discusses FAA regulations regarding maintenance procedures and performance standards. It provides an overview of causal factors for maintenance errors and uses an accident example where failure to follow procedures led to loss of control during takeoff. The presentation aims to increase awareness of risks from failing to follow procedures and how following preventative measures and safety nets can reduce maintenance errors.
The document provides an overview of changes between the new AC 43.13-1B advisory circular and the old AC 43.13-1A version. Key changes include expanded sections on welding, nondestructive testing, corrosion protection, hardware, and electrical systems. Additional topics such as fiberglass/plastics repair and avionics were also added. The new version aims to provide more detailed guidance and safety information to help aircraft technicians in their inspection and repair tasks.
The document discusses various types of documentation used for aircraft maintenance, including manufacturer's documentation, regulatory documentation, and airline generated documentation. It describes documentation such as the maintenance manual, fault isolation manual, illustrated parts catalogue, wiring diagram manual, minimum equipment list, and more. It explains that proper documentation is essential for safely performing maintenance and troubleshooting aircraft systems.
Aircraft Maintenance Manuals for Engineer's by Engr. Malay Kanti BalaMalay Kanti Bala
Aircraft Maintenance Manual is an important document for the Aircraft Maintenance Personnel. For the airworthiness of any flight, we do an inspection, servicing, repair, removal, installation, etc activities by following the approved documents which in manual or AMM. Here the presentation will disclose and familiarise with different manuals
This document discusses S1000D data modules, which are reusable blocks of information that can be shared and reused across technical publications. It describes the components of a data module, including the metadata ID status section and content section. It provides examples of different types of data modules, such as those for fault isolation, maintenance planning, parts information, and wiring data. The document is presented by Absolute Data Group, a provider of S1000D and technical documentation products and services.
The document provides guidance for maintenance technicians and inspection authorization holders on performing aircraft inspections. It discusses the importance of inspections, building relationships with aircraft owners, explaining inspection requirements to owners, and ensuring discrepancies found are properly addressed. It also reviews sample inspection requirements for specific aircraft, including reviewing registration, manuals, records, the type certificate data sheet, and completing a full inspection to verify airworthiness.
This slide is prepared by me for the students studying in 1st Semester of Aircraft Maintenance Engineering. This is only the the introduction of Maintenance Practices involved in Aircraft Maintenance. Reference is taken from various aviation books and websites. Suggestions are welcome. Pls leave a like
PS- after downloading please don't change the name of author as you will be disregarding all the hard work done by me.
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.
The document discusses India's CAR 66, which establishes requirements for aircraft maintenance engineer licensing. It consolidates separate airframe, engine, electrical and instrument licenses into one license. CAR 66 licenses will be available through converting existing licenses or obtaining new licenses after passing modules. It covers technical requirements, applications, basic knowledge modules, experience requirements, and type ratings. CAR 66 aims to align India's licensing with international standards while allowing for transition from previous licensing rules.
This document outlines the requirements for certifying staff authorisation for aircraft maintenance organisations according to CAR 145. Key points include:
- Initial training and assessment of certifying staff including human factors, procedures, technology and experience requirements.
- Certification authorisations must be issued by the organisation once certifying staff meet competence and experience criteria. Authorisations clearly define the certifier's privileges and limitations.
- Certifying staff must complete continuation training every two years covering technology, procedures, human factors and quality findings to maintain authorisation.
- Certifying staff are required to have six months maintenance experience in relevant aircraft systems over a two-year period.
5.15 Typical electronic digital aircraft systemslpapadop
This document provides an overview of typical electronic and digital aircraft systems. It discusses computer maintenance systems, ACARS, EFIS, EICAS/ECAM, fly-by-wire, flight management systems, GPS, inertial navigation systems, traffic collision avoidance systems, and flight data recorders. It also describes built-in test equipment, on-board maintenance facilities, and how various systems monitor aircraft data and perform tests. Finally, it provides details on electronic flight instrument systems, cockpit displays, and how fly-by-wire replaces manual flight controls with electronic signaling.
The document defines preventive maintenance and outlines who is authorized to perform it according to FAA regulations. It specifies that holders of pilot certificates can perform preventive maintenance on aircraft they own or operate, including private pilots. The document lists the specific preventive maintenance tasks allowed by FAA regulations and provides guidance on maintenance records, required performance standards, and additional FAA resources.
Aircraft maintenance program enhancement badawood mamdoohbmamdooh
This document discusses aircraft maintenance programs and enhancing them for specific operators. It describes developing a customized maintenance program (CMP) by analyzing control elements like utilization and reliability reports. A CMP case study for SVA B747-400s is presented, showing a CMP reduced costs by 23% while improving availability. The document also describes supplementing structural inspection documents into maintenance programs, noting SVA achieved a 64% integration rate and $1.85 million in savings for its B747 fleet.
This document outlines the technical requirements for Maintenance Training Organizations (MTOs) seeking approval under CAR 147. It discusses requirements for facilities, personnel, training procedures and materials, record keeping, examinations and oversight. Key requirements include having adequate facilities, qualified instructors, appropriate training equipment and materials, a quality system for monitoring standards, secure storage of records and examinations, and procedures for handling changes, continued validity and oversight findings.
Aircraft wheels are an important component of the landing gear system that support the weight of the aircraft during taxi, takeoff, and landing. Modern aircraft wheels are typically constructed of two lightweight yet strong aluminum alloy halves bolted together, with the inboard half fitted with keyways to engage the brake discs. The two-piece wheel construction allows for tubeless tires, which are sealed between the wheel halves. Aircraft tires experience tremendous loads and temperatures compared to automobile tires, requiring specialized construction and nitrogen inflation for optimal performance.
This document provides an overview and introduction to the information objects stored in a Common Source Database (CSDB) according to the S1000D specification. It describes the three major types of information objects as data modules, graphical objects, and publication modules. Data modules include different types like crew/operator, descriptive, fault isolation, etc. each with their own SGML document type definitions (DTDs). Other information objects include publication modules, comment modules, data dispatch notes, and data module lists, which have XML DTDs. Graphical objects like illustrations are also stored in the CSDB.
This presentation is an examination of structural repair of aircraft. It details the goals, regulations and classification of repairs for different types of aircraft damage.
The paper that this presentation is based on was presented by Dr. Kishore Brahma of the AXISCADES Engineering Core Group at the International Conference & Exhibition on Fatigue, Durability & Fracture Mechanics (FatigueDurabilityIndia2015) in Bangalore from 28-30th May 2015.
Este documento resume el contenido de varias circulares de asesoramiento emitidas por la Autoridad Aeronáutica Civil de México. Las circulares proveen orientación e instrucciones a operadores aéreos sobre procedimientos para cumplir con normas de aeronavegabilidad. Las circulares cubren temas como aeronaves, aeropuertos, personal técnico, y requisitos para concesionarios y operadores. Todas las circulares buscan mejorar la seguridad operacional de acuerdo con la legislación y normatividad aeronáuticas mexicanas
1) Un Certificado de Tipo es emitido por autoridades de aviación y certifica que el diseño de una aeronave ha cumplido con los requisitos reglamentarios. 2) Un Boletín de Información de Seguridad Operacional alerta a la comunidad de aviación sobre posibles problemas de seguridad sin ser obligatorios. 3) Un Certificado de Aeronavegabilidad certifica que una aeronave específica está en condiciones seguras de vuelo de acuerdo a su Certificado de Tipo.
Procedures for Safe Ground Handling PracticesMike Joseph
This document outlines procedures for safe ground handling practices at an airport. It details requirements for personnel protective equipment, safe loading and unloading of aircraft, handling of ground support equipment, and other operational safety practices like speed limits and fire prevention. Personnel must follow outlined safety protocols to protect themselves, aircraft, and equipment during all ground handling operations.
Este manual general de mantenimiento describe los procedimientos y políticas de mantenimiento de aeronaves de una empresa de aviación boliviana. Explica la organización del departamento de mantenimiento, los procesos de revisión y distribución del manual, y las definiciones y siglas utilizadas.
Dokumen tersebut membahas tentang stres dan konflik di tempat kerja. Ia mendefinisikan stres dan konflik, menjelaskan penyebab dan akibat dari keduanya, serta strategi untuk mengelola stres dan menyelesaikan konflik secara efektif seperti negosiasi. Dokumen ini bertujuan untuk memberikan pemahaman tentang hubungan antara stres dan konflik dengan kinerja karyawan.
This short document promotes creating presentations using Haiku Deck, a tool for making slideshows. It encourages the reader to get started making their own Haiku Deck presentation and sharing it on SlideShare. In just one sentence, it pitches the idea of using Haiku Deck to easily design slideshows.
David Arnold has nearly 10 years of experience as an aircraft structural mechanic and quality assurance representative in the United States Marine Corps. He possesses extensive experience with structural repair for various materials like aluminum, stainless steel, titanium, fiberglass and carbon fiber. Arnold is proficient with riveting, drilling, precision measuring tools, and solving structural problems. He has additional experience with aviation hydraulics systems and has a background in management, leadership, and quality assurance.
El ciclo Brayton consiste en una etapa de compresión adiabática, calentamiento isobárico y expansión adiabática de un fluido compresible. Es la base del motor de turbina de gas y se usa ampliamente para generar energía eléctrica, trabajo mecánico y empuje en aerorreactores. Fue descrito por primera vez en la patente de 1791 del inventor inglés John Barbar para una máquina de gas, aunque su diseño primitivo no tuvo éxito frente a la máquina de vapor de James Watt
Dokumen tersebut membahas tentang keselamatan dan kesehatan kerja, dimana jika program keselamatan dan kesehatan kerja tidak dilaksanakan dengan baik akan meningkatkan risiko kecelakaan kerja dan penyakit akibat kerja seperti silikosis dan tuli akibat bising. Dokumen tersebut juga menjelaskan pentingnya identifikasi bahaya lingkungan kerja dan penerapan program pencegahan.
Ergonomi perkantoran bertujuan untuk merancang tempat kerja agar sesuai dengan kapasitas manusia sehingga dapat mengurangi risiko cidera dan meningkatkan produktivitas. Faktor-faktor yang perlu diperhatikan meliputi postur tubuh, pergerakan berulang, peralatan kerja, dan lingkungan fisik seperti pencahayaan dan kebisingan. Penerapan ergonomi yang tepat dapat mencegah berbagai gangguan kesehatan akibat
The K8-E aircraft has a length of 11.6 meters, width of 9.63 meters, and height of 4.21 meters. It has a maximum takeoff weight of 3,846 kg and can fly at a maximum speed of 800 km/h for up to 4.2 hours with a range of 2,140 km. The aircraft has a low wing layout with two tandem seats and a tricycle landing gear. It uses rigid controls for surfaces like the aileron, rudder and elevator.
This document provides information on recent program developments to ensure the continuing structural airworthiness of aging airplanes. It discusses regulations and programs related to widespread fatigue damage, aging airplane safety rules, corrosion prevention and control programs, and damage tolerance-based inspection programs. The goal is to address fatigue and corrosion issues as airplanes operate longer than originally anticipated through supplemental inspections, corrosion prevention, and other mandated structural maintenance activities.
New holland cs640 combine harvesters service repair manualfjsjekksemm
This document is a repair manual for New Holland agricultural equipment models CS520, CS540, CS640, CS660, and CL560. It contains sections covering the distribution systems, power production, power train, travelling, body and structure, tool positioning, and crop processing systems of the equipment. The manual provides technical data, descriptions of how systems work, diagnostic information, and procedures for removing, installing, and adjusting components. It is designed to help technicians and mechanics resolve customer issues by providing detailed technical information categorized by component, function, and machine model using an ICE coding system.
New holland cs520 combine harvesters service repair manualfjskekmsemmwe
This document is a repair manual for New Holland agricultural equipment models CS520, CS540, CS640, CS660, and CL560. It contains sections on various systems of the equipment like distribution systems, power production, power train, travelling, body and structure, tool positioning, and crop processing. The introduction provides information on how the manual is organized and how to use the integrated ICE coding system to search for specific technical information by function and type within the manual.
New holland cs660 combine harvesters service repair manualjjskefkskemik
This document is a repair manual for New Holland agricultural equipment models CS520, CS540, CS640, CS660, and CL560. It contains sections covering the distribution systems, power production, power train, travelling, body and structure, tool positioning, and crop processing systems of the equipment. The manual provides technical data, descriptions of how systems work, diagnostic information, and procedures for removal and installation of components. It is intended to support maintenance and troubleshooting of issues on the customer's machine.
Case 445 skid steer loader service repair manualujjsfjkkekmem
This repair manual provides instructions for repairing various components of construction equipment, including 435, 445, and 445CT models. It details maintenance tasks like testing hydraulic pump flow rates and removing hydraulic pumps. The manual is divided into sections covering different machine systems, and each section contains chapters relevant to that system. Chapters provide technical specifications, operational descriptions, troubleshooting information, and service procedures.
Case 445 skid steer loader service repair manualfujjsefkskemm
This repair manual provides technical information to support maintenance and service of equipment functions and systems. Information is classified by location, type, and product model. The manual is divided into sections for different machine systems, with chapters covering technical data, operation descriptions, service instructions, and diagnostics for components. Technicians can search for specific information using codes that identify the component, data type, and applicable machine model. The document provides instructions for performing a flow test of a hydraulic pump to check its performance.
Case 435 skid steer loader service repair manualfudjjkskemee
This repair manual provides instructions for repairing various components of construction equipment, including 435, 445, and 445CT models. It details maintenance tasks like testing hydraulic pump flow rates and removing hydraulic pumps. The manual is divided into sections covering different machine systems, and each section contains chapters relevant to that system. Chapters provide technical specifications, operational descriptions, troubleshooting information, and service procedures for repairing components.
Case 445 ct compact track loader service repair manualfusjjjsekkekm
This repair manual provides technical information to support maintenance and service of equipment functions and systems. Information is classified by location, type, and product model. The manual is divided into sections for different machine systems, with chapters covering technical data, operation descriptions, service instructions, and diagnostics for components. Technicians can search for specific information using codes that identify the component, data type, and applicable machine model. The document provides instructions for performing a flow test of a hydraulic pump.
Case 445 ct compact track loader service repair manualusjfjkememe
This repair manual provides instructions for repairing various components of construction equipment, including 435, 445, and 445CT models. It details maintenance tasks like testing hydraulic pump flow rates and removing hydraulic pumps. The manual is divided into sections covering different machine systems, and each section contains chapters relevant to that system. Chapters provide technical specifications, operational descriptions, troubleshooting information, and service procedures.
Case 435 skid steer loader service repair manualfujsjefkksekmm
This repair manual provides instructions for repairing various components of construction equipment, including 435, 445, and 445CT models. It details maintenance tasks like testing hydraulic pumps and removing them for repair. The manual is divided into sections covering different machine systems, and each section contains chapters relevant to that system. Technical information is coded and indexed to allow technicians to quickly find instructions for their needed repair tasks.
Case 435 skid steer loader service repair manualfusjfjskekmsme
This repair manual provides instructions for repairing various components of construction equipment, including 435, 445, and 445CT models. It details maintenance tasks like testing hydraulic pump flow rates and removing hydraulic pumps. The manual is divided into sections covering different machine systems, and each section contains chapters relevant to that system. Chapters provide technical specifications, operational descriptions, troubleshooting information, and service procedures.
Case 445 ct compact track loader service repair manualfujsjefjskekemm
This repair manual provides technical information to support maintenance and service of equipment functions and systems. The manual is divided into sections for different machine systems. Each section contains chapters which provide technical specifications, descriptions of how systems work, diagnostic information, and service instructions. Technical information is indexed and searchable using location, type, and applicable product codes. The document provides instructions for performing a flow test of the hydraulic pump.
Case 445 skid steer loader service repair manualufjjsjfkememe
This repair manual provides instructions for repairing various components of construction equipment, including 435, 445, and 445CT models. It details maintenance tasks like testing hydraulic pump flow rates and removing hydraulic pumps. The manual is divided into sections covering different machine systems, and each section contains chapters relevant to that system. Chapters provide technical specifications, operational descriptions, troubleshooting information, and service procedures.
Case 445 skid steer loader service repair manualfujsejfksekkme
This repair manual provides technical information to support maintenance and service of equipment functions and systems. Information is classified by location, type, and product model. The manual is divided into sections for different machine systems, with chapters covering technical data, operation descriptions, service instructions, and diagnostics for components. Technicians can search for specific information using codes that identify the component, data type, and applicable machine model. The document provides instructions for performing a flow test of a hydraulic pump.
CASE IH AFX8010 COMBINE HARVEST SALVAGE Service Repair Manual Instant Downloa...yan77xunhao
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2 manuales de_mantenimiento
1.
2. ATA Spec 100: Manufacturers' Technical Data
The Air Transport Association released the newest
version of ATA Spec 100 in 1999.
According to the A4A website, this information will
not be revised and has been combined with ATA
Spec 2100 to produce the ATA iSpec 2200:
Information Standards for Aviation Maintenance
manual.
3. This specification defines a widely used numbering scheme
for aircraft parts and the appearance of printed aircraft
maintenance information.
The Federal Aviation Administration's JASC (Joint Aircraft
System/Component) code table provides a modified
version of ATA Spec 100.
4. ATA Spec 100 contains format and content guidelines for
technical manuals written by aviation manufacturers and
suppliers, and is used by airlines and other segments of the
industry in the maintenance of their respective products.
5. This document provides the industry wide standard for
aircraft systems numbering, often referred to as the ATA
system or ATA chapter numbers.
The format and content guidelines define the data
prepared as conventional printed documentation.
In 2000 ATA Spec 100 and ATA Spec 2100 were
incorporated into ATA iSpec 2200: Information Standards
for Aviation Maintenance.
6. Developed by the Air Transport Association, ATA iSpec
2200 is recognized as the global industry standard in
aviation, providing guidelines for the content, structure,
and electronic exchange of information related to aircraft
engineering, maintenance, and flight operations.
7. The data specifications are a collected suite of data
specifications related to maintenance requirements and
procedures, aircraft configuration control, and flight
operations.
The iSpec 2200 was developed as a consolidation between
ATA Spec 100 and Spec 2100, and provides guidance for
preparation of technical documentation related to aircraft
maintenance.
8. ATA Spec 100 contains format and content guidelines for technical
manuals written by aviation manufacturers and suppliers and is used
by airlines and other segments of the industry in the maintenance of
their respective products.
This document provides the industry-wide standard for aircraft
systems numbering, often referred to as ATA system or chapter
numbers.
The format and content guidelines define the data prepared as
conventional printed documentation.
9. CLASIFICACIÓN ATA.
El sistema ATA es un sistema de clasificación de capítulos
que regula y ordena la información aeronáutica en los
manuales de ingeniería y mantenimiento respectivos.
En general la clasificación en los manuales e información
técnica consta de una secuencia de números con
significado específico XX-YY-ZZ.
10. Los dos primeros dígitos (XX) indican el capítulo en donde
se encuentra la información relativa a un sistema
específico.
Los siguientes dos dígitos (YY), indican el subsistema de
ese sistema.
Los últimos dos dígitos (ZZ) señalan el componente o
conjunto específico en ese sistema.
11. Maintenance documents
GENERAL
The maintenance documents for the aircrafts supply help for
all maintenance activities.
Many different documents work together to permit you to
maintain the airplane.
The maintenance documents will help you do scheduled and
unscheduled maintenance work.
12. Scheduled Maintenance
These are examples of scheduled maintenance work:
Through stop checks
Airplane turn around
Daily checks
Planned checks.
13. You use these documents to do scheduled maintenance:
Maintenance Planning Document (MPD)
Airplane Maintenance ManuaL (AMM).
14. These documents supply supporting data to do
scheduled maintenance:
System Schematics Manual (SSM)
Wiring Diagram Manual (WDM)
Structural Repair Manual (SRM)
Illustrated Parts Catalog (IPC).
15. Unscheduled maintenance
These are examples of unscheduled maintenance
work:
Flight faults
Ground faults
Service problems
Structural damage.
16. You use these documents to do unscheduled
maintenance:
Fault Reporting Manual (FRM)
Fault Isolation Manual (FIM)
Built-In Test Equipment Manual (BITE)
Structural Repair Manual (SRM)
Dispatch Deviations Guide (DDG)
Airplane Maintenance Manual (AMM).
17. MAINTENANCE MANUALS
Maintenance planning Document
The Maintenance Planning Document (MPD)
defines the tasks for each type of scheduled
maintenance check.
Airlines use the MPD to make task cards that the
technician uses during the maintenance checks.
18. Airplane Maintenance Manual
The Airplane Maintenance Manual (AMM) has two parts.
Part I is the Systems Description Section (SDS).
This section replaces the description and operation (D and
O) section of the older airplane models.
19. Part II is Practices and Procedures.
It has data related to these functions:
Removal / installation of components.
Component Location.
Maintenance practices.
Servicing.
Adjustment/test.
Inspection/check.
CLeaning/painting.
Repair.
20. System Schematic Manual.
The System Schematic Manual (SSM) gives the user an understanding
of system operation and helps in the fault isolation process.
It supplies the interconnection of all LRU’s of a system or subsystem.
It also supplies a general knowledge about system operation.
Wiring Diagram Manual.
The Wiring Diagram Manual (WDM) supplies details of the point-to-
point wiring on the airplane
21. The Illustrated Parts Catalog.
The Illustrated Parts Catalog supplies part replacement data.
This data includes:
Replacement part number.
Part illustrations.
Supplier data.
Specification numbers.
Recomended spares.
Service Bulletin activity.
22. Standard Wiring Practices Manual.
The Standard Wiring Practices Manual has instructions for
maintenance and repair of the wiring of all Boeing airplanes.
It is not customized.
23. Fault Reporting Manual.
The flight crew uses the Fault Reporting Manual
(FRM) to improve communication with maintenance
personneL.
The flight crew uses the FRM to get fault codes for
airplane faults.
These faults can be flight deck effects or other faults.
24. The FRM has standard log book write-ups for each fault
code.
The fault code permits faster maintenance when the
airplane lands.
FRM fault codes refer you to the FIM.
25. Fault Isolation Manual.
You use the Fault Isolation Manual (FIM) to repair airplane
faults.
You start the fault isolation process with FRM fault codes
or a fault description.
The FIM wiII identify the maintenance action(s) to correct
the fault.
26. BITE Manual.
You use the BITE manual to get fault data from the
airplane built in test equipment.
If you start the fault isolation process with observed
faults, the BITE manual will identify which observed
faults need data from the built in test equipment.
The BITE manual has the BITE procedures from the
FIM.
27. Structural Repair Manual
The Structural Repair Manual (SRM) supplies descriptive
information and specific instructions to help in field repair
of airplane structure.
The SRM is not customized.
28. It has data relative to these areas:
Allowable damage evaluation.
Typical repairs.
Material identification.
Material substitution.
Fastener installation.
Alignment check.
Planning.
29. Dispatch Deviation Guide.
The Dispatch Deviation Guide (DDG) supplies
Boeing’s recommended minimum equipment
required for dispatch in the Master Mínimum
Equipment List (MMEL).
It also supplies the procedures for dispatch with a
fault if permitted.
30. Training information point.
Each maintenance document has an introduction to show
you how to use that document
31.
32. AMM PART I - INTRODUCTION
The Airplane Maintenance Manual (AMM) Part 1 is the
first of the two parts of the AMM.
It is called the Systems Description Section (SDS).
Both Part I and Part II of the AMM show the
configuration of the airplanes in an operator's fleet.
They have frequent revisions for improvements and for
configuration changes.
33. Purpose.
The SDS gives descriptions of the interfaces, function, and
operation of the airplane systems and subsystems.
You use these descriptions to become familiar with the
airplane systems so that you can do fault isolation and
system maintenance.
The SDS content can be used as a training manual.
34. Organization.
The SDS uses text/graphic paravisuals (page
sets).
Each graphic has one or more pages of text
that describe the information on the
graphic.
35. The graphic has the primary information and the
associated text page(s) have the support information or
explanations.
The SDS uses a horizontal (sometimes called landscape)
format.
36. Divisions.
The SDS organization is by ATA chapter (system) or
chapter/section (subsystem).
Each ATA chapter/section usually defines an airplane
system or subsystem.
37. Each subject of the SDS has this information:
Purpose/introduction.
General description.
Component location.
Interface.
Operation.
Functional description.
Training information points (TIPs).
38. AMM PART II - INTRODUCTION
Part II of the AMM contains the maintenances
practices and procedures to do maintenance on
the airplane.
39. Chapter Numbering System.
The manual has a tab section for each ATA chapter.
Within each tab section, the manual has more divisions
that use the assigned subject number (ASN) list number
XX-VV-ZZ, where:
XX is the ATA chapter
YY is the subsystem or sub-subsystem
ZZ is the unit (component).
40. The table of contents for each chapter lists the
maintenance procedures in numerical order for each
subsystem and sub-subsystem.
For each subsystem or sub-subsystem, the maintenance
tasks are in alphabetical order based on the page numbers
described below.
41. Page Numbering System
Each page has two numbers in the Lower right
corner: the ASN and a topic page number.
Each topics is made up of a page block.
Each page block is for a special type of information.
42. These are the page blocks:
Page Type Page Block
MAINTENANCE PRACTICES (MP) 201-299
SERVICING (SRV) 301 399
REMOVAL / INSTALLATION (R/I) 401-499
ADJUSTMENT / TEST (A/T) 501-599
INSPECTION / CHECK (l/C) 601-699
CLEANING / PAINTING (C/P) 701-799
REPAIRS (AR) 801-899
DISPATCH DEVIATIONS GUIDE
(DDG)
901-999
43. Dispatch Deviation Guide.
If all the topics for an ATA chapter, subsystem, or sub-
subsystem are brief, all the topics are in a single
MAINTENANCE PRACTICES page block.
The dispatch deviations guide page block has
procedures with maintenance tasks that prepare the
airplane for flight with certain systems / components
inoperative.
It also has tasks that put the airplane back to its usual
condition.
44. Training Information Point.
Each chapter of part II of the AMM has a List of effective
pages at the beginning of each chapter .
45. Training Information Point.
Chapter 12 of the AMM has the title SERVICING.
This chapter has procedures to fill and drain items
such as:
Fuel.
Oil.
Hydraulic fluid.
Water.
Tire pressure.
46. MAINTENANCE DOCUMENTS
PARTS CATALOG INTRODUCTION
The Boeing Company makes, sends out and revises the
parts catalog for customer use.
Only customers can use it to provision, requisition, store,
and send out line replaceable aircraft parts.
It identifies parts for the airplanes that Boeing delivers to
its customers.
47. The parts catalog has these sections:
Table of Contents.
Introduction.
Explanation of Parts List Data.
General System of Assembly Order-Detailed Parts List.
Instructions To Locate Part.
A/L code to Name List.
48. The parts catalog has these sections (cont):
Zone Diagrams.
Sect / Sta Diagrams.
Major Dwg Index.
Filter Kits.
Suppliers Name And Address Index.
Service Bulletin And Modification List.
49. To quickly know the parts catalog, review these sections in
the front of the catalog:
General System of Assembly Order-Detailed Parts List.
Explanation of Parts List Data.
Instructions To Locate A Part.
50. General System Of Assembly Order - Detailed Parts
List
This catalog uses indentation to show the
relationship of one part to another.
For all items, the indented number shows the
relationship to the installation, next higher assembly,
or components above it.
51. These are the levels and their relationship:
1
Installation
2
.Detailed parts for installation
.Assembly
.Attaching parts for assembly
52. 3
.. Detail parts for assembly
.. Sub-Assembly
.. Attaching parts for Sub-Assembly
4
... Detail parts for Sub-Assembly
... Sub-Sub Assembly
... Attaching parts for Sub-Sub-Assembly
5
.... Detail parts for Sub-Sub-Assembly.
53. MAINTENANCE DOCUMENTS PARTS CATALOG
HOW TO LOCATE A PART
General.
Sample pages in the introduction show how the find a part
number entry.
The instructions are in these sections:
When the part number is known
When the part number is unknown.
54. When The part Number Is Known.
When you know the part number (reference 1), you find the
part number in the numerical index.
Then you can write down the chapter, section, unit, figure,
and item number.
55. When the Part Number is unknown.
When you do not know the number, do these steps:
Go to the table of contents in the chapter where the part is
(reference 2)
Refer to the main group in which the part should be listed
(reference 3)
56. Figures are listed in alphabetical order by a main noun.
You find the title of the figure in which the part is shown
(reference 4).
Write down the section, unit, and figure number.
Go to the chapter and figure and find the part on the
illustration or in the parts list by the item number
(reference 5).