Downloaded from https://www.everyspec.com MIL-STD-3001-2A(AS) 5.2.4.1.2 Aircraft arrangement work package . This WP (see figure 1 ) shall describe and identify the major sections of the aircraft, such as fuselage, wings, empennage, and booms. 5.2.4.1.3 Aircraft systems description work package . This WP shall contain brief descriptive data that includes the purpose, type, content, and main features of each of the aircraft’s major systems. Illustrations shall not be used to support the descriptive data. 5.2.4.1.4 Aircraft instrument panel location work package >. A description and location of cockpit, instrument panels, and consoles shall also be provided.
Supporting illustrations shall be used to locate all instrument panels and consoles in the aircraft. 5.2.4.1.5 Danger areas and precautionary measures work package >. Safety information, such as hazardous areas on, in, and around the aircraft shall be clearly identified. Information on ground run-up areas, movable surfaces, personnel survival equipment (ejection seat), no-step areas, handholds, walkups, physiological hazards, safety pins, and safety precautions peculiar to the aircraft shall be shown on one or more line drawings.
Illustrations showing the hazard areas which exist during ground and air operations with radar systems turned on, both singly and in combination, shall be prepared (see figure 2 ). The illustrations shall provide safe separation distances and distribution patterns for personnel and Hazards of Electromagnetic Radiation to Ordnance (HERO) unsafe ordnance. Distances shall be presented in meters as well as feet. The safe separation distances shall be calculated and measured by the methods shown in IEEE C95.3. The safe exposure level of personnel to electromagnetic radiation is defined in IEEE C95.1.
Safe exposure levels of HERO susceptible and HERO unsafe ordnance are functions of radar frequency as shown in NAVSEA OD 30393. 5.2.4.1.6 Aircraft stations work package >. Station numbers shall be identified with their exact location by connecting lines. The location of station zero shall be clearly identified in the diagram. The zero waterline of the aircraft shall be indicated on the fuselage drawing. The numbering system used to identify aircraft coordinates and stations shall be used consistently throughout all WPs. 5.2.4.1.7 Aircraft dimensions work package >. The dimensions to stations from a reference or datum line shall be identified in this WP.
Illustrations shall be included to effectively convey this information. 5.2.4.1.8 Aircraft access and inspection panels and provisions work package acacesswp >. This WP shall identify all aircraft access and inspection panels and provisions. Illustrations shall be included to effectively convey this information. 5.2.4.1.9 Aircraft external power source connections work package acextpwrwp >. Identification of external power source connections and the authorized power sources that may be connected to the aircraft shall be identified and described in this WP. Illustrations shall be included to effectively convey this information. 7