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ARP4761, Guidelines for Conducting the Safety Assessment Process on Civil Aircraft, Systems, and Equipment is an Aerospace Recommended Practice from SAE International. [1]
Parameter / alternate Explanation name: Occurrence's commonly-known name (defaults to {{PAGENAME}}).: occurrence_type "Accident", "Hijacking" or "Occurrence". Few notable occurrences are classified as "incidents"; see Aviation accidents and incidents.
The management of unintended states is vital since they can result in serious aircraft accidents. For example, navigation problems on the cockpit display may lead a pilot to make an incorrect decisions, potentially causing injuries or fatality to passengers and crew members alike.
Metal fatigue and aircraft design flaw 6 Structural failure of the right horizontal stabiliser due to metal fatigue and aircraft design flaw 1978-06-26 Helikopter Service Flight 165: North Sea, Norway Sikorsky S-61: Fatigue 18 Rotor blade loosened after fatigue to the knuckle joint: crashed into the sea [10] 1979-05-25 American Airlines Flight 191
An infobox for articles about significant accidents, incidents or other occurrences involving one, two or three aircraft Template parameters [Edit template data] This template has custom formatting. Parameter Description Type Status Name name Name Occurrence's commonly-known name (usually the article's title) Default {{PAGENAME}} Example TWA Flight 800 String optional image image Crash image ...
[[Category:Aviation templates]] to the <includeonly> section at the bottom of that page. Otherwise, add <noinclude>[[Category:Aviation templates]]</noinclude> to the end of the template code, making sure it starts on the same line as the code's last character.
A fault model, falls under one of the following assumptions: single fault assumption: only one fault occur in a circuit. if we define k possible fault types in our fault model the circuit has n signal lines, by single fault assumption, the total number of single faults is k×n. multiple fault assumption: multiple faults may occur in a circuit.
An electronic centralised aircraft monitoring (ECAM) or electronic centralized aircraft monitoring is a system that monitors aircraft functions and relays them to the pilots. It also produces messages detailing failures and in certain cases, lists procedures to undertake to correct the problem.