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mil-hdbk-516

Knowledge base from MIL-HDBK-516C (Airworthiness Certification Criteria). Use for DoD air-system airworthiness planning: tailoring a certification basis, systems engineering criteria, and domain clusters for structures, flight technology, propulsion/installation, avionics/electrical/E3/diagnostics, computer systems/software, and crew systems (including applicable UAS control-station elements). Qualitative guidance handbook — not raw contractual requirements. Does not replace service airworthiness authority policy, civil FAA certification rules as authorities, or detailed JSSG/MIL performance specs.

한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.

설치 방법 보기

포함된 파일(14)

  • SKILL.md5.8 KB
  • chapters/ch01-scope-applicability-and-tailoring.md2.4 KB
  • chapters/ch02-systems-engineering-criteria.md2.3 KB
  • chapters/ch03-structures-criteria.md2.0 KB
  • chapters/ch04-flight-technology-criteria.md2.0 KB
  • chapters/ch05-propulsion-criteria.md1.9 KB
  • chapters/ch06-avionics-e3-and-diagnostics.md2.3 KB
  • chapters/ch07-computer-systems-and-software.md2.0 KB
  • chapters/ch08-crew-systems-criteria.md2.1 KB
  • cheatsheet.md1.7 KB
  • glossary.md1.7 KB
  • LICENSE1.2 KB
  • PACK.yaml1.5 KB
  • patterns.md1.9 KB

SKILL.md(원문)

설치하기 전에 에이전트에게 전달되는 지시 내용을 확인할 수 있습니다.

<!-- argument-hint: [airworthiness topic, certification basis, domain criteria, or chapter number] -->

MIL-HDBK-516C — Airworthiness Certification Criteria

Source: DoD MIL-HDBK-516C (US Government work, public domain; Distribution Statement A) | Chapters: 8

When to use

Use this pack when building or reviewing a DoD air system airworthiness certification basis from MIL-HDBK-516C — tailoring qualitative criteria, assigning methods of compliance, and navigating domain criteria clusters (SE, structures, flight, propulsion, avionics/E3, software, crew systems). Helpful for airworthiness engineers, SE leads, and domain SMEs aligning evidence to criteria.

Prerequisites: none — plain Markdown; no MCP server, API key, or licence tier needed at runtime.

How to Use This Skill

  • Without arguments — load the core frameworks below.
  • With a topic — ask about certification basis tailoring, SE criteria, structures, flight, propulsion, avionics/E3, software, or crew systems.
  • With a chapter — ask for ch01 through ch08.

Supporting files: glossary.md, patterns.md, cheatsheet.md.

Guidance only. 516C says it is not to be cited as a requirement. Criteria are qualitative; define acceptable in the implementing context.

Core Frameworks & Mental Models

Certification basis via tailoring

Select a necessary and sufficient subset of 516C criteria for the specific air system; document methods of compliance; maintain under configuration control.

Qualitative criteria plus evidence

Each section states criteria and often lists typical certification source data (analyses, tests, inspections). Closure is a reasoned evidence argument, not a single signature.

SE backbone then domains

Systems engineering criteria (design criteria, tools, materials, manufacturing/quality, tech data, CM) underpin domain sections.

Domain clusters in this pack

Structures; flight technology; propulsion plus installation; diagnostics/avionics/electrical/E3; computer systems/software; crew systems (including UAS/ROA control-station elements when applicable).

UAS applicability

Avionics and crew-systems material explicitly contemplates unmanned/remotely operated control segments where they affect airworthiness.

Chapter Index

#SectionKey content
ch01Scope, Applicability, TailoringHandbook role, certification basis, tailoring rules
ch02Systems EngineeringDesign criteria, tools, materials, quality, tech data, CM
ch03StructuresStructural airworthiness criteria and evidence patterns
ch04Flight TechnologyFlying qualities/performance/control evidence thinking
ch05Propulsion & InstallationPropulsion unit plus air-vehicle installation criteria
ch06Avionics / Electrical / E3 / DiagnosticsElectronics-heavy airworthiness cluster
ch07Computers & SoftwareSoftware/computer system airworthiness criteria
ch08Crew SystemsHMI, life support, escape, UAS control stations

Topic Index

  • Airworthiness authority / implementing office → ch01
  • Avionics → ch06
  • Certification basis → ch01
  • Certification source data lists → ch02–ch08
  • Configuration management (airworthiness) → ch02
  • Crew station / HMI → ch08
  • Diagnostics → ch06
  • E3 / EMI/EMC airworthiness → ch06
  • Electrical power system → ch06
  • Escape / life support / crash survivability → ch08
  • Flight technology / flying qualities → ch04
  • Materials selection (SE) → ch02
  • Methods of compliance → ch01
  • Propulsion installation → ch05
  • Software airworthiness → ch07
  • Structures / damage tolerance framing → ch03
  • Tailoring rules → ch01
  • UAS/ROA control station → ch06, ch08

Supporting Files

  • glossary.md — airworthiness terms used in 516C packing
  • patterns.md — implementation patterns with When/How/Trade-offs
  • cheatsheet.md — decision rules, maps, tells & smells

Scope & Limits

This pack covers selected MIL-HDBK-516C (12 Dec 2014) material: scope/tailoring, systems engineering, and major functional-area clusters (structures, flight, propulsion, avionics/electrical/E3/diagnostics, software, crew systems). Extraction metadata reports 527 PDF pages for the everyspec mirror copy used at build (build-sheet estimate ~320; PDF page objects differ — body text and DIST-A verified; chars/page floor passed). Not every handbook subsection is chaptered (for example armaments, passenger safety, materials-as-own-chapter, air transportability). Does not reproduce full criterion text catalogs or third-party FAA/SAE standards. Guidance only. US Government public domain work (Distribution Statement A). No source-material download link is published.

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