SOL_Attach_14_TERMS OF AGREEMENT (TOA).xlsx
XLSX spreadsheet 19 KB Posted
- Solicitation number
- FA812126R0010
About this file
This is a Terms of Agreement (ToA) spreadsheet that details specific components and subassemblies required for the T56 Series 3.0/-15 and 3.5/-15A engine repair and overhaul contract. The document specifies work breakdown structure (WS) items, contract line item numbers (CLIN), National Stock Numbers (NSN), component nomenclature, engineering release and revision codes (ERRC), source of supply (SOS), budget codes, and authorized requisition quantities across multiple engine modules including ADH Assembly, Compressor Module, RGB (Reverse Gear Box), and Turbine Module. Each component entry includes a replacement rate percentage and authorized quantity, with replacement rates ranging from 1% to 100% and authorized quantities varying from 1 to 360 units depending on the part type.
The ToA covers a comprehensive list of engine components critical to T56 engine sustainment operations, including major assemblies such as turbine vane cases, turbine wheels across multiple stages, compressor housings, gear boxes, and various seals and supports. Components are coded with budget code "T" and SOS designation "FHZ" with quantity-per-assembly (QPA) values of 1, 2, 6, or 12. Notable high-volume requirements include Vane Segment Assemblies for turbine stages (180-360 units authorized) and the Propeller Shaft with a 23% replacement rate and 65 authorized units. This ToA serves as the baseline supply and component requirement document supporting the Air Force Sustainment Center's indefinite delivery, indefinite quantity contract for T56 engine repair and overhaul across USAF, USN, and Foreign Military Sales customers.
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ToA
| WS/CLIN/NSN GFM is going into | Primary GFM NSN | Nomenclature | ERRC | SOS | Budget Code | QPA | Replacement Rate % | Authorized Requisition Qty |
| ADH Assy / 2840-01-481-7439 / X016 | 2840-00-793-2896 | Cover Assy | T | FHZ | 8 | 1 | 40% | 8 |
| ADH Assy / 2840-01-481-7439 / X016 | 2840-01-216-8046 | Accy Drive Housing | T | FHZ | 8 | 1 | 20% | 4 |
| Compressor Module / 2840-01-487-1830 / X057 | 2840-01-288-5028 | Front Comp. Lab Seal | T | FHZ | 8 | 1 | 5% | 1 |
| RGB / 2840-01-492-9017 / X059 | 2840-00-011-0692 | Prop Shaft | T | FHZ | 8 | 1 | 23% | 65 |
| RGB / 2840-01-492-9017 / X059 | 2840-00-169-0159 | RR Planetary Carrier | T | FHZ | 8 | 1 | 5% | 14 |
| RGB / 2840-01-492-9017 / X059 | 2840-00-522-6376 | Strut Assy | T | FHZ | 8 | 2 | 2% | 6 |
| RGB / 2840-01-492-9017 / X059 | 2840-01-092-8378 | RGB Front Housing | T | FHZ | 8 | 1 | 2% | 6 |
| RGB / 2840-01-492-9017 / X059 | 2840-01-142-5637 | RGB Rear Housing | T | FHZ | 8 | 1 | 1% | 3 |
| RGB / 2840-01-492-9017 / X059 | 2840-01-472-3745 | Stiffened Main Diaphragm | T | FHZ | 8 | 1 | 1% | 3 |
| RGB / 2840-01-492-9017 / X059 | 3020-01-196-8937 | Main Drive Gear | T | FHZ | 8 | 1 | 1% | 3 |
| RGB / 2840-01-492-9017 / X059 | 2840-01-049-5938 | DIAPHRAGM ASSY,CASE | T | FHZ | 8 | 1 | 1% | 1 |
| Turbine Module / 2840-01-337-2608 / X022 | 2840-01-408-6595 | Turbine Vane Case | T | FHZ | 8 | 1 | 63% | 9 |
| Turbine Module / 2840-01-337-2608 / X022 | 2840-01-410-6751 | Metallic Seal | T | FHZ | 8 | 1 | 19% | 3 |
| Turbine Module / 2840-01-337-2608 / X022 | 2840-01-525-9303 | Front Turb. Brg Support | T | FHZ | 8 | 1 | 39% | 5 |
| Turbine Module / 2840-01-337-2608 / X022 | 2840-01-642-5604 | 1st Stage Turbine Wheel | T | FHZ | 8 | 1 | 64% | 9 |
| Turbine Module / 2840-01-337-2608 / X022 | 2840-01-642-6244 | 3rd Stage Turbine Wheel | T | FHZ | 8 | 1 | 64% | 9 |
| Turbine Module / 2840-01-337-2608 / X022 | 2840-01-643-3528 | 2nd State Turbine Wheel | T | FHZ | 8 | 1 | 66% | 9 |
| Turbine Module / 2840-01-337-2608 / X022 | 2840-01-643-3535 | 4th Stage Turbine Wheel | T | FHZ | 8 | 1 | 59% | 8 |
3.5 GFM
WS/CLIN/NSN GFM is going into Primary GFM NSN Nomenclature ERRC SOS Budget Code QPA Replacement Rate % Authorized Requisition Qty
| Turbine Module / 2840-01-652-6038 / X214 | 2840-01-658-7575 | Support, Turbine Guide Vane and Seal | T | FHZ | 8 | 1 | 5% | 2 |
| Turbine Module / 2840-01-652-6038 /X214 | 2840-01-656-3799 | Vane Segment Assy, Turbine - 2nd Stage | T | FHZ | 8 | 12 | 100% | 360 |
| Turbine Module / 2840-01-652-6038 /X214 | 2840-01-657-0577 | Vane Segment Assy, Turbine - 3rd Stage | T | FHZ | 8 | 6 | 100% | 180 |
| Turbine Module / 2840-01-652-6038 /X214 | 2840-01-658-5437 | Vane Segment Assy, Turbine - 4th Stage | T | FHZ | 8 | 6 | 100% | 180 |
| Compressor Module / 2840-01-652-8921 / X212 | 2840-01-674-2650 | Housing Assy, Compressor Air Inlet | T | FHZ | 8 | 1 | 1% | 1 |
| Compressor Module / 2840-01-652-8921 / X212 | 2840-01-656-7200 | Compressor Case (Bare) | T | FHZ | 8 | 1 | 1% | 1 |
| Compressor Module / 2840-01-652-8921 / X212 | 2840-01-657-5166 | 3.5 Accessory Drive Gear Box | T | FHZ | 8 | 1 | 1% | 1 |
| Compressor Module / 2840-01-652-8921 / X212 | 2840-01-657-6118 | 3.5 Accessory Drive Gear Box Housing | T | FHZ | 8 | 1 | 1% | 1 |
File details come from the government source that posted it. Updated .