Downloaded from https://www.everyspec.com SIL SOF SOW Software Integration Laboratory Safety-of-Flight Statement of Work - - . - - - - SRS I Software Requirements Speclflcat~on System Safety Hazard Analysis System Safety Management Plan System Safety Program Plan System Safety Risk Assessment SystemlSubsystem Specification Standardization Agreement Software Test Description Software Test Plan STR SVD TNDS TC TEMP TEPP TP SSHA SSMP SSPP SSRA SSS STANAG STD STP ~- . .-. . .
Software Test Report Software Version Description Target Acquisition and Designation Subsystem Type Classified or Type Classification Test and Evaluation Master Plan Test and Evaluation Program Plan Target Practice UAV RDECOM WCA WlLl Unmanned Aerial Vehicle Research, Development and Engineering Command Warning, Caution, Advisory Weapon Inhibits, Limits, and Interrupts 4. GENERAL REQUIREMENTS 4.1 .Tailorinq. The processes defined in this handbook should be tailored to the specific armament and aircraft configuration and installation. For new armament development programs, all components affecting airworthiness should be considered and their qualification procedures identified.
For modification programs, only those subsystems added, modified, or affected by addition or modification of other components should be considered. Minor modifications may be qualified using a Mini- Weapons Survey (MWS) that demonstrates safe operation of the modified armament system. 4.2.Armv airworthiness. The airworthiness qualification of U.S. Army aircraft systems is governed by AR 70-62. Airworthiness is defined as a demonstrated capability of an aircraft or aircraft subsystem or component to function satisfactorily when used within prescribed limits. An airworthy aircraft is safe to fly within prescribed limits.
These limits, which have their basis in data, may not make the aircraft mission capable. As shown by Figure 1, the difference between an airworthy aircraft and a "qualified" aircraft is the degree to which the aircraft meets the specified requirements and provides the performance expected by the user. In addition to safety-related requirements, the system specification includes many other requirements such as technical performance parameters, reliability and maintainability, and operating and support costs. An Airworthiness Release (AWR) is a technical document that provides