DAS-OAT Requirements.pdf

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DEPARTURE ALERTING SYSTEM AND OUTSIDE AIR TEMPERATURE DISPLAY FOR F-5 AIRCRAFT
Solicitation number
N00421DASOAT1
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About this file

This is a technical requirements document specifying threshold and objective requirements for a Departure Alerting System (DAS) for F-5 aircraft. The document outlines five key requirements: pilot cuing method must be aural and/or visual, departure anticipation must be ≥3 seconds (objective ≥5 seconds), false positive warnings must occur at ≤10% rate (objective 0%), false negative warnings must occur at ≤10% rate (objective 0%), and aircraft system integration is required as needed with an objective of not requiring gyro or inertial navigation integration.

This requirements document is part of a pre-solicitation issued by the Naval Air Systems Command (NAVAIR) PMA-226 for procuring a DAS and Outside Air Temperature (OAT) display system for F-5N/F aircraft. The anticipated quantity is 20-40 units, with an 18-month period of performance for non-recurring engineering and 4 months for airworthiness approval. Capability statements are due March 21, 2025 at 11:00 AM EDT, with a 10-page limit. The NAICS code is 334511 with a size standard of 1,350 employees.

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DAS Requirements

Requirement Threshold Objective

Pilot cuing method Aural and/or visual Same as threshold

Departure anticipation ≥3 seconds ≥5 seconds

False positive (nuisance) warnings Rate of occurrence ≤10% Rate of occurrence 0%

False negative (missed) warnings Rate of occurrence ≤10% Rate of occurrence 0%

Aircraft system integration As required No gyro or inertial navigation integration required

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