USAF T53-L-703 Engine Component Improvement Program
Engine CIP provides critical sustaining engineering for in-service military engines to maintain flight safety, correct service-related deficiencies, improve system Operational Readiness, and R&M, reduce engine Life Cycle Cost, and improved the sustainment of engines throughout their service life. Historically, aircraft systems change missions, tactics, and environments to meet changing/emerging threats; and new problems are often identified. These problems can be identified during deployment, production, and/or service; Engine CIP is the only funding vehicle to develop fixes for these field problems. The funding is driven by field events and type/maturity of engines, not by engine quantity. Engine CIP begins upon delivery of the first production engine purchased with procurement funds and continues over the engine’s life to address any safety issues, as well as achieve established metric goals in availability, reliability, maintainability, and affordability as documented in each Type/Model/Series (TMS) Engine Life Management Plan (ELMP). Since operational and safety problems arise throughout a system’s service life, Engine CIP must be maintained at a level to provide the engineering and test support to make the changes essential for continued system performance at affordable costs.
This contract will provide RDT&E, sustaining engineering, technical data, drawings, change proposals, manpower support, design activities, prototype hardware, testing, product and procedure improvements, reports, etc. for the T53 engine. The CIP program is funded with RDT&E funds.
. The T53 turboshaft engine provides the main source of power during flight of the TH-1H Iroquois training helicopters. Engineering services for turboshaft engines is highly specialized because of the following:
- Detailed knowledge of helicopter engine operation, theories, concepts, applications, systems, performance, operability, and airframe and jet engine integration.
- Strict requirements and high precision for flightworthy, aircraft components
- Complex manufacturing techniques for small turboshaft jet engines and associated components
- Intricate details of design and manufacturing of jet engine components
- Specialized bench testing of components, jet engine testing and test criteria and post test analysis
- Possession of proprietary data for aircraft and jet engine interface details and part details for redesign efforts
- Experience with military airworthiness requirements
The government has identified these as Key Performance Parameters (KPP) that any vendor should have in order to possess the capability to provide the services required. Therefore, this acquisition is for the development of highly specialized aircraft parts and for performance of a highly specialized engineering service.
FA8626-24-D-0053 Department of the Air Force Materiel Command Lifecycle Management Center Wright Patterson Air Force Base
5/24/23, 2:52 PM Notice of Intent to Award Sole Source - USAF T53 Engine Component Improvement Program Support
The Department of the Air Force Materiel Command Lifecycle Management Center awarded a sole source contract to OZARK AEROWORKS LLC for $2,600,000 on July 29, 2024 to provide support for the T53 Engine Component Improvement Program. The justification cites the need for continued technical and engineering support from the incumbent contractor to maintain configuration control, address technical issues, and manage program risk. The award is for a one-year period with options to extend up to five years.
FA8626-CIP-LPA Department of the Air Force Materiel Command Lifecycle Management Center Wright Patterson Air Force Base
8/2/24, 12:48 PM USAF T53-L-703 Engine Component Improvement Program
The United States Air Force, at Wright Patterson AFB is issuing this Sources Sought Synopsis as a means of conducting market research to identify parties having an interest in, and the resources to support and address requirements for the USAF only Component Improvement Program (CIP) initiatives for the T53 engine, with emphasis on maintaining the engine fleet in operational status with the best hardware currently available. The T53 is a mature, relatively simple engine with a three-level maintenance (3LM) concept. The field unit performs removal and replacement activities. The engine is removed every 1,250 hours for a scheduled hot section inspection and every 2,500 hours for scheduled mid-life inspection, with full overhauls performed after 5,000 hours of flight. Based on USAF force structure guidance, the T53 Program Office has no official retirement date of the TH-1H.
The CIP contract contains annual delivery orders with two overarching Engineering Project Description (EPD) to oversee and manage the day-to-day activities of the CIP contract. The purpose of the first EPD is to provide the program management functions required for the execution of the CIP contract and encompasses the management of the various activities within the CIP to ensure all technical, schedule, reporting, safety, logistics, financial goals and responses required to questions from USAF, MAJCOM, and other customers. This EPD includes the preparation of all contracted CIP reports, support of CIP conferences and technical meetings on an as needed basis, and control of Government-owned property.
Additionally, the T53 CIP provides the engineering designs, material costs, testing, and reporting of new hardware for T53-L-703 engines currently in the field.
The second EPD manages the Service Related Deficiencies (SRD). The SRD EPD is to investigate service-related deficiencies on engine components and systems that are identified by the T53 community as having a safety or reliability impact and recommend a corrective action. Investigations may encompass engineering analysis, failure laboratory analysis, and other data gathering exercises. This EPD is anticipated to operate for the duration of T53 CIP.
Potential vendors MUST possess necessary technical data, specialized tooling, testing equipment, and facilities to inspect, produce and test the T53 engine and components in accordance with the applicable drawings.
THIS IS NOT A SOLICITATION. This request for capability information does not constitute a request for proposals; submission if any information in response to this market survey is purely voluntary; the government assumes no financial responsibility for any costs incurred.
If your organization has the potential capacity to produce the specified items, please provide the following information listed in the attachment:
FA8626-CIP-LPA Department of the Air Force Materiel Command Lifecycle Management Center Wright Patterson Air Force Base
2/17/23, 11:29 AM Notice of Intent to Award Sole Source - USAF T53 Engine Component Improvement Program Support
The United States Air Force, at Wright Patterson AFB is issuing this Notice to Award Sole Source Synopsis as a means of conducting market research to identify parties having an interest in, and the resources to support and address requirements for the USAF only Component Improvement Program (CIP) initiatives for the T53 engine, with emphasis on maintaining the engine fleet in operational status with the best hardware currently available. The T53 is a mature, relatively simple engine with a three-level maintenance (3LM) concept. The field unit performs removal and replacement activities. The engine is removed every 1,250 hours for a scheduled hot section inspection and every 2,500 hours for scheduled mid-life inspection, with full overhauls performed after 5,000 hours of flight. Based on USAF force structure guidance, the T53 Program Office has no official retirement date of the TH-1H.
The CIP contract contains annual delivery orders with two overarching Engineering Project Description (EPD) to oversee and manage the day-to-day activities of the CIP contract. The purpose of the first EPD is to provide the program management functions required for the execution of the CIP contract and encompasses the management of the various activities within the CIP to ensure all technical, schedule, reporting, safety, logistics, financial goals and responses required to questions from USAF, MAJCOM, and other customers. This EPD includes the preparation of all contracted CIP reports, support of CIP conferences and technical meetings on an as needed basis, and control of Government-owned property.
Additionally, the T53 CIP provides the engineering designs, material costs, testing, and reporting of new hardware for T53-L-703 engines currently in the field.
The second EPD manages the Service Related Deficiencies (SRD). The SRD EPD is to investigate service-related deficiencies on engine components and systems that are identified by the T53 community as having a safety or reliability impact and recommend a corrective action. Investigations may encompass engineering analysis, failure laboratory analysis, and other data gathering exercises. This EPD is anticipated to operate for the duration of T53 CIP.
Potential vendors MUST possess necessary technical data, specialized tooling, testing equipment, and facilities to inspect, produce and test the T53 engine and components in accordance with the applicable drawings.
Submit any data according to the attachment.
FA8626-24-R-0053 Department of the Air Force Materiel Command Lifecycle Management Center Wright Patterson Air Force Base
6/9/23, 8:57 AM