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Get In Touch Media Contact. Diligent record keeping is an essential element of this critical program. Our personnel managed and performed these tasks on some of the most complex sections of the KC aircraft, including the cockpit, tail cone, and center-wing sections. More than 38 teardown sections were processed, comprising over 2, individual parts. By examining the structural health of sample aircraft and verifying existing analysis predictions, current inspection intervals can be validated and modified as necessary.

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IMDAS support aircraft accident investigation by acquiring flight data from flight data recorder of F, FK aircraft to reproduce actual flight situation at aircraft accident time and provide data for analysis of cause of accident.

Manages various data generated during operation of the FGE engine, and perform predicts engine maintenance time, serial information analysis of engine, TCTO, technical communication analysis, maintenance mil-std-1530cc analysis to improve the efficiency of engine maintenance and lifetime management.

More than 38 teardown sections were processed, comprising over 2, individual parts. The database was developed to record all significant damage findings, such as cracks, corrosion, delaminations, etc. Diligent record keeping is an essential element of this critical program. Get In Touch Media Contact. Ignatius, MT Primary Phone: The SMIMS database mil-std--1530c detailed mi-lstd-1530c on the aging processes which occur in the aircraft, and thus supports the ongoing evaluation mils-td-1530c structural integrity during sustainment.

The Joint Council on Aging Aircraft also suggested that improvements be made to data collection processes to enable trend analysis. FLSG generate operational load spectrum for aircraft structural fatigue analysis and verifies the generated spectrum, and issues a summary report of the result. These protocols identified critical work instructions in documentation, technical procedures, and other guidelines to ensure validity of the data collected during the teardown.

SMIMS provided the A Engineering and Analysis group at Hill Air Force Base in Ogden, Utah, with a data collection and data mining tool that would allow statistical analysis of the data collected and vastly improve their ability to manage the structural health of the A fleet.

Our rapid and flexible response to CSTOs includes reviewing engineering data and USAF TCTOs for applicability to foreign F counterparts, while ensuring that updated documentation is formatted with the same standards as the original data, and incorporating all outstanding supplements into the appropriate manuals and checklists. MDAS support aircraft accident investigation by acquiring flight data from flight data recorder of T series aircraft to reproduce actual flight situation at aircraft accident time and provide data for analysis of cause of accident.

Manages various data generated during operation of the PT6A engine, and perform predicts engine maintenance time, serial information analysis of engine, TCTO, technical communication analysis, maintenance history analysis to improve the efficiency of engine maintenance and lifetime management.

The reports and findings are easily reviewed through an interactive, web-accessible database for ease of accurate reporting of findings. More than 38 teardown sections were processed, comprising over 2, individual parts. The database was developed to record all significant damage findings, such as cracks, corrosion, delaminations, etc. These protocols identified critical work instructions in documentation, technical procedures, and other guidelines to ensure validity of the data collected during the teardown.

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Ignatius, MT Primary Phone: Our personnel managed and performed these tasks on some of the most complex sections of the KC aircraft, including the cockpit, tail cone, and center-wing sections.

SMIMS provided the A Engineering and Analysis group at Mil-std-130c Air Force Base in Ogden, Utah, with a data collection and data mining tool that would allow statistical analysis of the data collected and vastly improve their ability mil-std-15330c manage the structural health of the A fleet. The teardown data allowed the System Program Office SPO to ensure continued technical and economic feasibility of the F mission and anticipate structural issues that may affect continued airworthiness and safety.

Specific tasks include coordinating the disassembly, inspection, and analysis of a retired C-5A aircraft The SMIMS database captures detailed information on the aging processes which occur in the aircraft, and thus supports the ongoing evaluation of structural integrity during sustainment. Our personnel managed and performed these tasks on some of the most complex sections of the KC aircraft, including the cockpit, tail cone, and center-wing sections.

Air Force relies on its Aircraft Structural Integrity Program ASIP to prevent mil-stf-1530c failures and anticipate required maintenance or preventative maintenance actions in order to mitigate major structural repair or replacement mll-std-1530c.

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Diligent record keeping is an essential element of this critical program. KTFAP generates load spectrum and stress spectrum for aircraft structural fatigue analysis and performs S-N analysis, damage tolerance analysis and internal load analysis. The Joint Council on Aging Aircraft also suggested that improvements be made to data collection processes to enable trend analysis.

Air Force relies on its Aircraft Structural Integrity Program ASIP to prevent structural failures and anticipate required maintenance or preventative maintenance actions in order to mitigate major structural repair or replacement events. The program supported continued environmental assessment, sustainment, and mission readiness of the fleet.

CFDAS support aircraft accident investigation by acquiring flight data from flight data recorder of KT-1 series aircraft to reproduce actual flight situation at aircraft accident time and provide data for analysis of cause of accident.

By examining the structural health of sample aircraft and verifying existing analysis predictions, current inspection intervals can be validated and modified as necessary.

Get In Touch Media Contact.