G-1_Aircraft_Data_Collection_Requirements_Template_-_30_Oct_15.xlsx
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- FA7014-16-R-5004
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G-1 Aircraft Data Collection Templates (DRAFT) 30 Oct 15
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PMP Hardware Technical
| HardwareTechnicalTable | UNCLASSIFIED, FOR OFFICIAL USE ONLY | TagName1 | TagValue1 |
| AFCAA CEM Templates | TagName2 | TagValue2 | |
| PMP Hardware Technical Template, Aircraft | TagName3 | TagValue3 |
| ColumnHead | Second Reference Design (e.g. Contractor A) | Third Reference Design (e.g. Contractor B) | Time each parameter is expected to be available | ||||||||||||||||||||||||||||||||||||||||
| WBS/CRS Number | WBS/CRS Element | Parameter Name | Value | Low | High | Margin | Unit of Measure | Unit Qualifer | Estimate or Actual | Objective | Threshold | Source | Notes | Value | Low | High | Margin | Unit of Measure | Unit Qualifier | Estimate or Actual | Source | Notes | Value | Low | High | Margin | Unit of Measure | Unit Qualifier | Estimate or Actual | Source | Notes | Definition | VocabularyID | Repeatable | MS A | PDR | MS B | CDR | MS C | Authoritative Data Source | Priority (Development) | Priority (Production) | |
| 1.0 | Aircraft | The complex of equipment (hardware/software), data, services, and facilities required to develop, produce, and support air vehicles. | |||||||||||||||||||||||||||||||||||||||||
| 1.1 | Air Vehicle | The complete flying aircraft. It also includes the design, development, and production of complete units (i.e., the prototype or operationally configured units, which satisfy the requirements of their applicable specification(s), regardless of end use). | |||||||||||||||||||||||||||||||||||||||||
| Crew Size | Quantity | Quantity | Quantity | Number of crew members on air vehicle | CEMVocab | Government | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Number Of Engines | Quantity | Quantity | Quantity | Number of engines on air vehicle | CEMVocab | Government | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Number Of Main Rotors | Quantity | Quantity | Quantity | Number of main rotors on air vehicle | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Number Of Passengers | Quantity | Quantity | Quantity | Number of passengers on air vehicle | CEMVocab | Government | 3 | 3 | |||||||||||||||||||||||||||||||||||
| Number Of Tail Rotor Blades | Quantity | Quantity | Quantity | Number of tail rotor blades on air vehicle | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Absolute Ceiling | Feet | Feet | Feet | The maximum altitude above sea level at which an aircraft can maintain level flight under Standard Air conditions. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Combat Ceiling | Feet | Feet | Feet | Altitude above which a plane cannot climb faster than a given rate | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Combat Radius | Nautical Miles | Nautical Miles | Nautical Miles | The distance from an airbase that an air vehicle can reach, patrol there for a set amount of time and return to base with minimal fuel left. Assume no external fuel pods, maximum takeoff weight, and refueling after takeoff. | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Engine Type | List | List | List | Type of engine on air vehicle | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Height | Feet | Feet | Feet | Height of air vehicle in feet | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Length | Feet | Feet | Feet | Length of air vehicle in feet | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Weight - Internal Fuel | Pounds | Internal Fuel | Internal Fuel | Pounds | Internal Fuel | Pounds | Internal Fuel | Weight of fuel on air vehicle | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Weight - Maximum Gross | Pounds | Pounds | Pounds | The maximum total aircraft weight at any moment during the flight or ground operation | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Maximum Ordnance Gross | Pounds | Pounds | Pounds | The maximum weight of military supplies including weapons, ammunition, armor, vehicles, etc. on aircraft | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Maximum Takeoff | Pounds | Takeoff | Takeoff | Pounds | Takeoff | Pounds | Takeoff | The maximum certificated design weight at which the aircraft meets the appropriate takeoff certification requirements. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Weight - Maximum Landing | Pounds | Landing | Landing | Pounds | Landing | Pounds | Landing | The maximum certificated design weight at which the aircraft meets the appropriate landing certification requirements. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | "Systems & Install" (S&I = Propulsion Group (Engine, Engine Installation, Exhaust System, Lubricating & Fuel Systems, Starters - Main & Aux, Aux. Power), Flight Controls, Instruments, Hydraulic & Pneumatic, Electrical, Avionics (Equipment, Install.), Armament , Furnishings & Equipment, Environmental Control (Air Conditioning, Anti-icing), Photographic Group, Load & Handling (Ballast), Manufacturer Variation) plus structural weight | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Wing, Rotor, Empannage, Fuselage, Alighting Gear (Incl. Wheels, Tires, Air), Nacelle, Air Induction | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Speed - Maximum | Knots | Knots | Knots | The maximum speed the air vehicle can achieve at standard sea level pressure and temperature | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Cruise Speed - Maximum | Knots | Knots | Knots | The speed that will provide the furthest distance traveled for a given amount of fuel burned at standard sea level pressure and temperature please insert assumed load in comments. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Range - Maximum | Nautical Miles | Nautical Miles | Nautical Miles | The distance an aircraft can fly between takeoff and landing at standard sea level pressure and temperature please annotate assumed load in comments. | CEMVocab | Contractor | 1 | 1 | |||||||||||||||||||||||||||||||||||
| Nuclear Hardened Components | Description | Description | Description | Electronic components and systems that have been made resistant to damage or malfunctions caused by ionizing radiation. Please annotate in the comments section the degree of hardening. | CEMVocab | Government | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1 | Airframe | The assembled structural and aerodynamic components of the air vehicle that support subsystems essential to designated mission requirements | |||||||||||||||||||||||||||||||||||||||||
| Material - Airframe | List | List | List | Materials that makes up the airframe | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight | Pounds | Airframe Unit | Airframe Unit | Pounds | Airframe Unit | Pounds | Airframe Unit | Weight empty minus AUW deductible items (Engine - Main & Aux, Engine Installation, Exhaust System, Fuel Cells - Rubber or Nylon, Starters - Main & Aux, Aux. Power Unit, Instruments - Indicators Only, Electrical Generators, Constant Speed Drive, Batteries, Conversion Equipment, Supply/Conversion Items for Instruments Only , Equipment Incl. Radome, NOT Installation, Armaments - Turrets & Power Op. Mounts, Environ. Control Units & Fluids, Anti-Icing Units & Fluids, Cameras, Optical Viewfinders & Mounts if stabilized) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.1 | Airframe Integration, Assembly, Test And Checkout | ||||||||||||||||||||||||||||||||||||||||||
| 1.1.1.2 | Fuselage | The structural airframe encompassing the forward, center and aft fuselage sections of the aircraft | |||||||||||||||||||||||||||||||||||||||||
| Materials - Fuselage | List | List | List | Materials that make up the fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Width | Inches | Inches | Inches | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.2.1 | Forward Fuselage | This element includes the design, production, materials and equipment procurements including vendor design/development efforts to provide the structural fuselage section for the forward section of the fuselage which includes the main and secondary structures; windshield/canopy assembly; radome; access doors; installation of airframe related subsystems; installation of nose landing gear doors/mechanisms and emergency release system; mounting provisions for mission peculiar avionics, armament/weapons delivery systems; and installation of flight test instrumentation. | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the forward fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of forward fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.2.2 | Center Fuselage | This element includes the design, production, materials and equipment procurements including vendor design/development efforts to provide the center fuselage section which includes main and secondary structures, access doors, fixed geometry inlet, installation of airframe related subsystems; installation of main landing gear doors/mechanisms and emergency release system; mounting provisions for the centerline pylon and installation of flight test instruments. | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the center fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of center fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.2.3 | Aft Fuselage | This element includes the design, production, materials and equipment procurements including vendor design/development efforts to provide the aft fuselage section which includes main and secondary structures, access doors, speed brake, installation of airframe related subsystems; installation of main landing gear doors/mechanisms and emergency release system and mounting provisions for installation of engines, arresting hook system, splicing of vertical tails to the Aft Fuselage and installation of flight test instrumentation. | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the aft fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of aft fuselage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.2.3 | Other Fuselage | This element includes other tasks related to fuselage that are either not listed above or tasks that cannot be categorized into one of the above elements. | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the other fuselage(s) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of the other fuselage(s) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.3 | Wing | The structure used to produce lift for flight through the air | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the wing | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of the wing | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Wing Area | Square Feet | Square Feet | Square Feet | The projected area of the planform and is bounded by the leading and trailing edges and the wing tips. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Wing Type | List | List | List | Aircraft's wing structure is sealed and used as a fuel tank (wet) or not (dry) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Wingspan | Feet | Feet | Feet | Distance from one onetip to the other wingtip in feet | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.4 | Empennage | The structural tail group encompassing the fin, stabilator and rudder as well as provisions for electrical wiring, plumbing, control linkages, antennae, and associated equipments | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the empennage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of empennage | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.1.5 | Nacelle | The streamlined enclosure separate from the fuselage used for sheltering the crew, cargo or housing an engine | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the nacelle | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Structural | Pounds | Pounds | Pounds | Weight of nacelle | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||
| 1.1.1.6 | Other Airframe Components | This element should be replaced with other product-oriented airframe components that are either not listed above or that cannot be categorized into one of the above elements. Each additional element is to be clearly identified and defined. | |||||||||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the other airframe components | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of other airframe components | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.2 | Engine/Propolsion | That portion of the air vehicle that pertains to installed equipment (propulsion unit and other propulsion) to provide power/thrust to propel the aircraft through all phases of powered flight. | |||||||||||||||||||||||||||||||||||||||||
| Engine Output Speed - Turbo Prop | Horsepower | Horsepower | Horsepower | The power, energy, or work produced by the engine. Shaft horsepower for Turbo Prop; Thrust for Turbojet assume at standard sea level pressure and temperature | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Engine Output Type | List | ??? | ??? | List | ??? | List | ??? | Define. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Engine Type | List | List | List | Type of engine | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Material Mix | List | List | List | Materials that make up the engine | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Engine Power - Maximum | ??? | ??? | ??? | Maximum power engine can generate at standard sea level and temperature. If it includes a safety margin, please annotate the margin in comment section. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Dry | Pounds | Dry | Dry | Pounds | Dry | Pounds | Dry | The weight of an engine exclusive of any fuel, oil, and coolant | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Weight - Wet | Pounds | Wet | Wet | Pounds | Wet | Pounds | Wet | Weight of engine with fuel and other consumables | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.2.1 | Propulsion Integration, Assembly, Test And Checkout | ||||||||||||||||||||||||||||||||||||||||||
| 1.1.3 | Vehicle Subsystems | The collection of core non-avionics subsystems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.1 | Vehicle Subsystems Integration, Assembly, Test And Checkout | ||||||||||||||||||||||||||||||||||||||||||
| 1.1.3.2 | Flight Control Subsystem | Primary and secondary mechanical devices and automatic equipment installed in the air vehicle when used with control surfaces, to control the flight path of the air vehicle as well as to provide additional lift, drag and trim effect. | |||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Unit | Unit | Pounds | Unit | Pounds | Unit | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.2.1…n | Flight Control Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.3 | Auxillary Power Subsystem | The equipment that performs engine start up on the ground, emergency starting during flight, ground checkout operations of aircraft accessories, and power takeoff for hydraulic pumps and electrical generator system and fuel motive flow pumps. | |||||||||||||||||||||||||||||||||||||||||
| Unit Weight | Pounds | Pounds | Pounds | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.3.1…n | Auxillary Power Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.4 | Hydraulic Subsystem | This system provides hydraulic power for the actuation of landing/launching gear subsystems, in-flight re-fueling probe, gun drive and flight control surfaces. | |||||||||||||||||||||||||||||||||||||||||
| Weight - Dry | Pounds | Pounds | Pounds | The weight of an engine exclusive of any fuel, oil, and coolant | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Wet | Pounds | Pounds | Pounds | Weight of engine with fuel and other consumables | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.4.1…n | Hydraulic Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.5 | Electrical Subsystem | Equipment installed to provide electrical power function, the AC and DC distribution of this power supply and the provision for exterior lighting | |||||||||||||||||||||||||||||||||||||||||
| Unit Weight | Pounds | Pounds | Pounds | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.5.1…n | Electrical Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.6 | Crew Station Subsystem | The provisions and space allocated to the human component of the weapon system that allow performance of specific functions to ensure mission success. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.6.1 | Canopy /cockpit System | Aircraft system human interfaces and components that sustain and protect the human operators, troops, and passengers. | |||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of canopy/cockpit system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.6.2 | Mechanical System | ||||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.6.3 | Fire Protection System | Set of equipment of fire alarm and fire extinguishing intended to notify air crew about the emergence and extinguishing of fire on board | |||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of fire protection system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.6.4…n | Crew Station Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.7 | Environmental Control Subsystem | Environmental equipment and distribution systems on board the air vehicle for air conditioning and cooling equipment compartments, pressurization of seals, fuel tanks and anti-icing. The distribution system provides for air ducts, cooling lines and other plumbing required in supplying air and other cooling media from supply sources to the controlled environment. | |||||||||||||||||||||||||||||||||||||||||
| Weight - Dry | Pounds | Pounds | Pounds | The weight of an engine exclusive of any fuel, oil, and coolant | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Weight - Wet | Pounds | Pounds | Pounds | Weight of engine with fuel and other consumables | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.7.1…n | Environmental Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.8 | Fuel Subsystem | Equipment and distribution systems installed in the air vehicle to provide fuel to the engines and the auxiliary power unit, including associated functions such as fuel pressurization, venting, gauging, defueling etc. | |||||||||||||||||||||||||||||||||||||||||
| Weight - Dry | Pounds | Pounds | Pounds | The weight of an engine exclusive of any fuel, oil, and coolant | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Dimensions | Length, Width, and Height, surface area, or volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||||
| Weight - Wet | Pounds | Pounds | Pounds | Weight of engine with fuel and other consumables | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.8.1…n | Fuel Subsystem Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.9 | Landing Gear | The structural and mechanical gear and associated equipment, including doors, for maneuvering of the air vehicle while on the ground, the devices for extension, retraction, and locking this gear, and the mechanical devices for arresting the air vehicle. | |||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Main Gear | Main Gear | Pounds | Main Gear | Pounds | Main Gear | Weight of main gear - The main gear assorb approximately 80% of the static weight and usually are positioned aft of the center of gravity. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Weight | Pounds | Alighting Gear Group | Alighting Gear Group | Pounds | Alighting Gear Group | Pounds | Alighting Gear Group | Weight of alighting gear group. The alighting gear group usually absorbs about 20% of the static weight and normally located under the nose of the aircraft. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.9.1…n | Landing Gear Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.10 | Rotor Group/Blades/Hub | Items that impact the pitch, raw, roll, and thrust forces, which provide the lift and direction for Air Vehicle powered flight for rotary aircraft | |||||||||||||||||||||||||||||||||||||||||
| Main Rotor Type | List | List | List | Type of main rotor | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Material Type - Rotor | List | List | List | Materials that make up the rotor group/Blades/Hub | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Main Blade Assembly | Pounds | Pounds | Pounds | Weight of main blade assembly | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Tail Blade Assembly | Pounds | Pounds | Pounds | Weight of tail blade assembly | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.10.1…n | Rotor Group/Blades/Hub Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.11 | Drive Subsystem | Those items that pertain to the engine control units such as transmissions and gear boxes | |||||||||||||||||||||||||||||||||||||||||
| Weight - Drive System | Pounds | Pounds | Pounds | Weight of drive system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Dry | Pounds | Pounds | Pounds | Weight of an engine exclusive of any fuel, oil, and coolant | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Wet | Pounds | Pounds | Pounds | Weight of engine with fuel and other consumables | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.3.11.1…n | Drive Subsystem Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.12…n | Vehicle Subsytems Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.13…n | Other Vehicle Subsystem 1….n | This element should be replaced with other product-oriented avionics subsystems that are either not listed above or that cannot be categorized into one of the above elements. Each additional element is to be clearly identified and defined. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.3.13.1…n | Other Vehicle Subsytems Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4 | Avionics | Mission equipment on board the air vehicle, which is primarily electronic in nature | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.1 | Avionics Integration, Assembly, Test And Checkout | ||||||||||||||||||||||||||||||||||||||||||
| 1.1.4.2 | Communication/Identification | That equipment (hardware/software) installed in the air vehicle for communications and identification purposes. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.2.1…n | Communication/Identification Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Frequency | Megahertz | Megahertz | Megahertz | Required frequency | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Line Of Sight Type | List | List | List | Line-of-sight or beyond-line-of-sight | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Rf Antenna # Elements | Count | Count | Count | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.2.2…n | Communication/Identification Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.3 | Navigation/Guidance | That equipment (hardware/software) installed in the air vehicle to perform the navigational guidance function. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.3.1…n | Navigation/Guidance Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Number Of Circuit Cards - Digital | Quantity | Digital Boards | Digital Boards | Quantity | Digital Boards | Quantity | Digital Boards | Number of digital cards | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Number Of Integrated Circuits | Quantity | Quantity | Quantity | Number of integrated circuits | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of navigation/Guidance equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Power - Required | Watts | Watts | Watts | Power required to operate system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.3.2…n | Navigation/Guidance Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.4 | Mission Computer/Processing | The master data processing unit(s) responsible for coordinating and directing the major avionic mission systems. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.4.1…n | Mission Computer/Processing Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| # Of Digital Cards | Count | Count | Count | Number of digital cards | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| # Of Integrated Circuits | Count | Count | Count | Number of integrated circuits | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Number Of Circuit Cards | Quantity | Quantity | Quantity | Total number of circuit cards | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight - Total Of Cards | Pounds | Circuit Cards | Circuit Cards | Pounds | Circuit Cards | Pounds | Circuit Cards | Total weight of circuit cards | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.4.2…n | Mission Computer/Processing Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.5 | Fire Control | That equipment (hardware/software) installed in the air vehicle, which provides the intelligence necessary for weapons delivery such as bombing, launching, and firing. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.5.1…n | Fire Control Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Number Of Antennas | Quantity | Quantity | Quantity | Number of antennas | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of fire control equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.5.2…n | Fire Control Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.6 | Data Display & Control | The equipment (hardware/software) that visually presents processed data by specially designed electronic devices through interconnection (on- or off-line) with computer or component equipment and the associated equipment needed to control the presentation of the primary flight information and tactical information to the crew | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.6.1…n | Data Display & Control Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Display Type | List | List | List | Type of display on data display and control equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of data display & control equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.6.2…n | Data Display & Control Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.7 | Survivability | Those equipments (hardware/software) installed in, or attached to, the air vehicle which assist in penetration for mission accomplishment | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.7.1…n | Survivability Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Power - Input | Watts | Input | Input | Watts | Input | Watts | Input | Length, Width, and Height, surface area, and volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of survivability equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.7.2…n | Survivability Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.8 | Reconnaisance | Those equipments (hardware/software) installed in, or attached to, the air vehicle necessary to the reconnaissance mission | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.8.1…n | Reconnaisance Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Input Power Reqd | W | W | W | Length, Width, and Height, surface area, and volume for installs/replacements of Aircraft hardware | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Sensor Type | List | List | List | Type of sensor on reconnaissance equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Spectral Band Range | ??? | ??? | ??? | the range of possible frequencies of electromagnetic radiation. the characteristic distribution of electromagnetic radiation emitted or absorbed by that particular object used for targeting | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.8.2…n | Reconnaisance Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.9 | Automatic Flight Control | Those electronic devices and sensors, which, in combination with the flight controls subsystem (under vehicle subsystems), enable the crew to control the flight path of the aircraft and provide lift, drag, trim, or conversion effects. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.9.1…n | Automatic Flight Control Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of automatic flight control equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Engine Type | Description | Description | Description | Description of item that defines the characteristics of the item | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Quantity | Quantity | Quantity | Quantity | amount or number of the item or material that cannot be accounted for by spatial measurement (count/numerical) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Power | Count | Count | Count | Power required to operate system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.9.2…n | Automatic Flight Control Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.10 | Health Monitoring System | That equipment (hardware/software) installed in the air vehicle for malfunction detection and reporting. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.10.1…n | Health Monitoring System Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of health monitoring system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Type | Descriptor | Descriptor | Descriptor | Description of item that defines the characteristics of the item | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Quantity | Quantity | Quantity | Quantity | amount or number of the item or material that cannot be accounted for by spatial measurement (count/numerical) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Power | Count | Count | Count | Power required to operate system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.10.2…n | Health Monitoring System Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.11 | Stores Management | The avionics subsystem that controls and monitors the operational state of aircraft installed stores and provides and manages the communications between aircraft stores, other aircraft subsystems and weapons. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.11.1…n | Stores Management Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight of stores management equipment | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Type | Descriptor | Descriptor | Descriptor | Description of item that defines the characteristics of the item | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Quantity | Quantity | Quantity | Quantity | amount or number of the item or material that cannot be accounted for by spatial measurement (count/numerical) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Power | Count | Count | Count | Power required to operate system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.11.2…n | Stores Management Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.12 | Radar | The system for detecting the presence, direction, distance, and speed of aircraft, ships, and other objects | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.12.1…n | Radar Box 1….n | ||||||||||||||||||||||||||||||||||||||||||
| Anti-jamming Capability | List | List | List | Any system or technique used to counteract the jamming of radar operation. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Material - Focal Plane | List | List | List | Material used for focal plane array | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Focal Plane Array Type | List | List | List | type of image sensing device consisting of an array (typically rectangular) of light-sensing pixels at the focal plane of a lens. | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Number Of Antenna - Rf Elements | Quantity | RF Elements | RF Elements | Quantity | RF Elements | Quantity | RF Elements | Number of elements in system | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.4.12.2…n | Radar Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.13…n | Avionics Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.14…n | Other Avionics Subsystem 1….n | This element should be replaced with other product-oriented avionics subsystems that are either not listed above or that cannot be categorized into one of the above elements. Each additional element is to be clearly identified and defined. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.4.14.1…n | Other Avionics Subsystem Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.5 | Armament/weapons Delivery | That equipment (hardware/software) installed in the air vehicle to provide the firepower functions and weapons delivery capability. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| 1.1.5.1…n | Armament/weapons Delivery Box 1….n | Power Required | List | List | List | Define. | |||||||||||||||||||||||||||||||||||||
| Power Required? | Yes/No | Yes/No | Yes/No | CEMVocab | Contractor | 2 | 2 | ||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.5.2…n | Armament/weapons Delivery Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.6 | Auxilary Equipment | Auxiliary airframe, electronics, and/or armament/weapons delivery equipment not allocable to individual element equipments, or which provide the ancillary functions to the applicable mission equipments. If lower level information can be collected, use the structure and definitions in Appendix B, Electronic Systems. | |||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Type | Descriptor | Descriptor | Descriptor | Description of item that defines the characteristics of the item | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Quantity | Quantity | Quantity | Quantity | amount or number of the item or material that cannot be accounted for by spatial measurement (count/numerical) | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | List | List | List | See definitions in instructions below | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.7 | Furnishings And Equipment | This element includes the provisions that sustain and support the passengers, typically consists of non-mission specific removable items. | |||||||||||||||||||||||||||||||||||||||||
| Weight | Pounds | Pounds | Pounds | Weight empty minus AUW deductible items | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Type | Descriptor | Descriptor | Descriptor | Description of item that defines the characteristics of the item | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| Quantity | Quantity | Quantity | Quantity | Number/count of items required | CEMVocab | Contractor | 2 | 2 | |||||||||||||||||||||||||||||||||||
| 1.1.8…n | Air Vehicle Software Release 1….n | Use Software Tabs for data | |||||||||||||||||||||||||||||||||||||||||
| 1.1.9 | Air Vehicle Integration, Assembly, Test And Checkout | NA |
| Column D: If data is available, enter value. If data is not available, enter "NA." | |
| Column E: If technical parameter has a range estimate, enter low value; else, N/A | |
| Column F: If technical parameter has a range estimate, enter high value; else, N/A | |
| Column G: If the value in column C contains a margin, record margin in this column (i.e. max engine thrust has 10% margin - 10% would go in this column). | |
| Column H: Identify the unit of measure for input in column C | |
| Column I: Identify if the value in column C is an actual value (A) or an estimated value (E). | |
| Column J: Where did the data come from (contractor, Government, etc.) | |
| Column K: Notes should include the following | |
| Any information to help understand any differences from the source data and the definition. | |
| Analogous system if used. | |
| If another estimate exists - value and source for other estimate i.e. Software SLOC - Program office value in the table and contractors value in the notes or vice versa. | |
| Power requirements for electronics should include start power in notes and steady state in the value column. |
Column L: WBS/Technical Parameter Definition
| TRL 1 Basic principles observed and reported: Transition from scientific research to applied |
| research. Essential characteristics and behaviors of systems and architectures. Descriptive tools |
| are mathematical formulations or algorithms. |
| TRL 2 Technology concept and/or application formulated: Applied research. Theory and |
| scientific principles are focused on specific application area to define the concept. Characteristics |
| of the application are described. Analytical tools are developed for simulation or analysis of the |
| application. |
| TRL 3 Analytical and experimental critical function and/or characteristic proof-ofconcept: |
| Proof of concept validation. Active Research and Development (R&D) is initiated with |
| analytical and laboratory studies. Demonstration of technical feasibility using breadboard or |
| brassboard implementations that are exercised with representative data. |
| TRL 4 Component/subsystem validation in laboratory environment: Standalone prototyping |
| implementation and test. Integration of technology elements. Experiments with full-scale |
| problems or data sets. |
| TRL 5 System/subsystem/component validation in relevant environment: Thorough testing |
| of prototyping in representative environment. Basic technology elements integrated with |
| reasonably realistic supporting elements. Prototyping implementations conform to target |
| environment and interfaces. |
| TRL 6 System/subsystem model or prototyping demonstration in a relevant end-to-end |
| environment (ground or space): Prototyping implementations on full-scale realistic problems. |
| Partially integrated with existing systems. Limited documentation available. Engineering |
| feasibility fully demonstrated in actual system application. |
| TRL 7 System prototyping demonstration in an operational environment |
| (ground or space): System prototyping demonstration in operational environment. System is at |
| or near scale of the operational system, with most functions available for demonstration and test. |
| Well integrated with collateral and ancillary systems. Limited documentation available. |
| TRL 8 Actual system completed and "mission qualified" through test and demonstration in |
| an operational environment (ground or space): End of system development. Fully integrated |
| with operational hardware and software systems. Most user documentation, training |
| documentation, and maintenance documentation completed. All functionality tested in simulated |
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