Att L-1 Verification Matrix.xlsx
XLSX spreadsheet 17 KB Posted
- Attached to
- SOLICITATION -- MULTI-ENGINE TRAINING SYSTEM (METS) AIRCRAFT PROCUREMENT Federal contract opportunity
- Solicitation number
- N00019-21-R-0077
About this file
This document provides details for a solicitation seeking proposals for a Multi-Engine Training System aircraft to replace the T-44C aircraft currently used by the United States Navy for aviator and flight officer training. The Naval Air Systems Command will award a single firm fixed price contract for the procurement and total quantity of commercial aircraft through options. Proposals are due by March 16, 2022, and contract award is targeted for the first quarter of fiscal year 2023. Interested offerors should direct any questions to the named procuring contracting officer and contract specialist. The solicitation requires the aircraft to execute training missions in accordance with provided profiles and meet performance specifications for operating conditions, weight, speed, altitude, navigation, communication and surveillance equipment, displays, controls, egress, and other defined characteristics. The document includes a verification matrix for offerors to indicate how their proposed aircraft will meet each requirement.
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Text version
Instructions
| Verification Matrix Instructions | |
| The following are Government provided entries and do not require input from the Offeror | |
| Column A | References the requirement number in the performance based specification. |
| Column B | States the requirement in the performance based specification. |
| Column C | Identifies whether the requirement is mandatory or not. |
| Column D | Identifies the section L paragraph reference. |
| Column E | Identifies the section M paragraph reference. |
| Column F | Identifies the performance work statement paragraph reference. |
| The following require Offeror input | |
| Column G | The Offeror shall specify "Yes" if the Offeror's proposed solution meets the associated requirement or "No" if the Offeror's proposed solution does not meet the requirement. If the Offeror specifies "No" in column G, the Offeror shall enter N/A in columns H, I, and J. |
Note: If the Offeror specifies "No" for an item that had been designated as Mandatory ("Yes" in Column D), this will result in a deficiency in the Offeror's proposal.
| Column H | The Offeror shall organize the information to align with the volume and book number with the section L paragraph reference. The Offeror shall identify the paragraph number in its document where the response is provided. |
| Column I | The Offeror shall identify where the substantiating information is provided for each requirement, including the specific location within the document (e.g., Annex X, OEM Manual, Section 3.2, page 18). |
N0001921R0077 &F
Verification Matrix
| Offeror's Response | |||||||
| Requirement No. | PBS Requirement | Mandatory Yes/No | Section L Reference | Section M Reference | PWS Paragraph | Proposed Yes/No | Volume # |
Book #
| Paragraph # | Reference to Substantiating Documentation | ||||||
| AV-006 | The METS shall execute Appendix B profiles in operational day environmental conditions at or below Mission Takeoff Gross Weight (MTGW) with the Environmental Control System on (ECS-ON). | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | 3.23.1 | Vol 2, Book 1, 2.1.1 | |
| AV-007 | The METS cruise airspeed shall be greater than or equal to 195 Knots True Airspeed (KTAS) in accordance with the Appendix B profiles in operational day environmental conditions with ECS-ON. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD | |
| AV-008 | The METS shall have a service ceiling greater than or equal to 20,000 feet (FT) Mean Sea Level (MSL). | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD | |
| AV-011 | All requirements of this specification shall be satisfied with mission aircrew equipped with the following personal aircrew gear: |
• Flight suit, gloves, boots, and jacket
• Communication headset
| Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD | ||
| AV-015 | The METS shall meet emergency egress requirements for pilots, student pilot, and passengers equipped with personal aircrew gear. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-017 | The METS shall be operable from either pilot seat. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-020 | The METS jump seat shall be adjustable permitting the student pilot to view the cockpit instruments and displays and then stow the seat. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-025 | The METS physical controls and displays shall be within human performance limitations, while wearing a glove, with respect to actuation, dimensions, resistance, displacement, separation, orientation, color, and illumination. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-026 | The METS automated systems shall provide information to keep the aircrew continuously informed of each system’s operating mode, intent, function, output, automation failures, and potentially unsafe modes being manually selected. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-027 | The METS shall be equipped with a lavatory and relief tube. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-031 | The METS autopilot shall capture and hold attitude, altitude, airspeed, vertical speed, course, and heading. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-032 | The METS autopilot shall be integrated with the flight management system to control the approach modes. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-033 | All flying quality requirements shall apply to both pilot stations. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-034 | The METS shall incorporate independent, mechanically linked controls between the pilot stations for pitch, roll, and yaw axes of control. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-035 | The METS shall have a stall warning system. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-041 | The METS shall be equipped with full-face, quick-donning oxygen masks for both pilot stations and the jump seat station. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-047 | The METS shall execute the Appendix B profiles with a simulated single engine failure during climb-out, cruise, holding, approach, and landing phases of flight. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | 3.23.1 | Vol 2, Book 1, 2.1.1 |
| AV-053 | The METS shall be certified for flight into known icing conditions. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-058 | The METS avionics equipment controls shall be accessible from either pilot position. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-059 | The METS cockpit shall provide an integrated crew vehicle interface through independent, digital cockpit Multi-Function Displays (MFD). | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-062 | The METS avionics equipment output shall be within the field of view for both pilots. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-064 | The METS shall be equipped with an emergency standby attitude indicator within the field of view of both pilots. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-065 | The METS shall be equipped with one Very High Frequency (VHF) radio and one combined VHF and Ultra High Frequency (UHF) commercial radio. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-070 | The METS shall be equipped with an ICS receive and transmit capability for each pilot and jump seat station. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-072 | The METS shall support VOR/DME approaches. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-076 | The METS shall support Performance Based Navigation functionality to include Enroute (RNP 2.0), Terminal (RNP 1.0), and RNAV(GPS) Approach (RNP 0.3). | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-081 | The METS shall be equipped with a mid-air collision avoidance capability which provides cues and warning to the aircrew of conflicting air traffic. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-087 | The METS shall be equipped with a radar altimeter that displays from zero to a minimum of 2000 feet above ground level with an adjustable low altitude alert to the pilots. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-088 | The METS shall be equipped with a color weather radar and displayed on the MFDs. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-090 | The METS shall support TACAN approaches. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-092 | The METS shall be equipped with an AOA indexer on the glare shield above the instrument panel for each pilot that displays the symbology and color coding for the aircraft conditions in Table 3-3. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | 3.8 | Vol 2, Book 1, 2.1.1, SPD |
| AV-093 | The METS shall be equipped with an AOA indicator for each pilot with a circular scale that displays the AOA value, the AOA on-speed mark at the three o’clock position, and the AOA impending stall mark above the on-speed mark. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | 3.8 | Vol 2, Book 1, 2.1.1, SPD |
| AV-099 | The METS FMS shall determine steering commands necessary to maintain the defined path for all supported flight plan legs in an active flight plan. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-100 | The METS FMS shall determine steering commands necessary to fly coupled ILS and GPS approaches. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-101 | The METS FMS shall provide steering commands to the autopilot and be displayed to both pilots. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-112 | The METS DMM shall present an independent digital map display at each pilot station. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-113 | The METS DMM shall provide the ability to selectively overlay on any map display, the active flight plan, obstacle database, any navigation aid, any airfield, any fix, and any reference point or waypoint contained in the aeronautical database. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-114 | The METS FMS shall provide each pilot the ability to declutter the MFD. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-115 | The METS shall be equipped with exterior and interior lighting. | Yes | Vol 2, Book 1, Element 2.1.1, SPD | II.A.1 | N/A | Vol 2, Book 1, 2.1.1, SPD |
| AV-117 | The METS shall be equipped with corrosion protection design features. | Yes | Vol 2, Book 1, Element 2.1.1 | II.A.1 | N/A | Vol 2, Book 1, 2.1.1 |
| AV-005 | The METS should execute the Appendix B missions on a runway length less than or equal to 5,000 feet, with one engine inoperative takeoff, with three crew, at operational day temperature 95°F (35°C), at sea level pressure altitude, and at maximum takeoff weight. | No | Vol 2, Book 1, Element 2.1.2 | II.A.1 | 3.23.1 | Vol 2, Book 1, 2.1.2 |
| AV-009 | The METS should operate for greater than or equal to 3.5 flight-hours endurance while executing Appendix B profiles. | No | Vol 2, Book 1, Element 2.1.2 | II.A.1 | 3.23.1 | Vol 2, Book 1, 2.1.2 |
| AV-018 | The METS should meet the anthropometric attributes shown in Table 3‑1. | No | Vol 2, Book 1, Element 2.1.2 | II.A.1 | N/A | Vol 2, Book 1, 2.1.2 |
| AV-077 | The METS system should include all ARINC 424 leg types required for RNP RNAV departure and arrival procedures. | No | Vol 2, Book 1, Element 2.1.2 | II.A.1 | N/A | Vol 2, Book 1, 2.1.2 |
| AV-036 | The METS should have stall warning buffet furnished through the inherent aerodynamic qualities of the airplane. | No | Vol 2, Book 1, Element. 2.1.3 | II.A.1 | N/A | Vol 2, Book 1, 2.1.3 |
| AV-038 | The METS ECS should maintain the cockpit and cabin temperature ranges identified in Figure 3‑1. | No | Vol 2, Book 1, Element. 2.1.3 | II.A.1 | N/A | Vol 2, Book 1, 2.1.3 |
| AV-079 | The METS should be equipped with ADS-B In capability. | No | Vol 2, Book 1, Element. 2.1.3 | II.A.1 | N/A | Vol 2, Book 1, 2.1.3 |
| AV-080 | The METS should display ADS-B In flight information services-broadcast weather and aeronautical information to the pilots. | No | Vol 2, Book 1, Element. 2.1.3 | II.A.1 | N/A | Vol 2, Book 1, 2.1.3 |
&"-,Bold"&14METS Verification Matrix N0001921R0077 &F
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