Uncontrolled decompression: Difference between revisions

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Revision as of 19:42, 27 February 2025

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Modern aircraft are specifically designed with longitudinal and circumferential reinforcing ribs in order to prevent localised damage from tearing the whole [[fuselage]] open during a decompression incident.<ref>{{cite book|url=https://books.google.com/books?id=B3ng54W3sQ8C|pages=141–142|title=Beyond the Black Box|author=George Bibel|year=2007|isbn=978-0-8018-8631-7|access-date=2008-09-01|publisher=JHU Press}}</ref> However, decompression events have nevertheless proved fatal for aircraft in other ways. In 1974, explosive decompression onboard [[Turkish Airlines Flight 981]] caused the floor to collapse, severing vital flight control cables in the process. The [[Federal Aviation Administration|FAA]] issued an [[Airworthiness Directive]] the following year requiring manufacturers of wide-body aircraft to strengthen floors so that they could withstand the effects of in-flight decompression caused by an opening of up to {{convert|20|sqft|m2}} in the lower deck cargo compartment.<ref>{{cite web|url=http://www.faa.gov/about/media/b-chron.pdf|title=FAA Historical Chronology, 1926–1996|date=2005-02-18|access-date=2008-09-01|publisher=[[Federal Aviation Administration]] |archive-url = https://web.archive.org/web/20080624211236/http://www.faa.gov/about/media/b-chron.pdf <!-- Bot retrieved archive --> |archive-date = 2008-06-24}}</ref> Manufacturers were able to comply with the Directive either by strengthening the floors and/or installing relief vents called "[[Dado (architecture)|dado panels]]" between the passenger cabin and the cargo compartment.<ref>{{patent|US|6273365}}</ref>

Cabin doors are designed to makeprevent itlosing nearlycabin impossiblepressure tothrough losethem pressurizationby throughmaking openingit anearly cabinimpossible to open doorthem in flight, eitherwhether accidentally or intentionally. The [[plug door]] design ensures that when the pressure inside the cabin exceeds the pressure outside, the doors are forced shut and will not open until the pressure is equalized. Cabin doors, including the emergency exits, but not all cargo doors, open inwards, or must first be pulled inwards and then rotated before they can be pushed out through the door frame because at least one dimension of the door is larger than the door frame. Pressurization prevented the doors of [[Saudia Flight 163]] from being opened on the ground after the aircraft made a successful emergency landing, resulting in the deaths of all 287 passengers and 14 crew members from fire and smoke.

Prior to 1996, approximately 6,000 large commercial transport airplanes were [[type certificate|type certified]] to fly up to {{convert|45000|ft}}, without being required to meet special conditions related to flight at high altitude.<ref>{{Cite web|url=https://rgl.faa.gov/|title=RGL Home Page|website=rgl.faa.gov|access-date=2022-11-06|archive-date=2022-12-14|archive-url=https://web.archive.org/web/20221214143433/https://rgl.faa.gov/|url-status=dead}}</ref> In 1996, the FAA adopted Amendment 25–87, which imposed additional high-altitude cabin-pressure specifications, for new designs of aircraft types.<ref name="FAA_25.841">{{cite web|url=http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgFAR.nsf/0/FED94F31539484AB852566720051AA5D?OpenDocument|title=Section 25.841: Airworthiness Standards: Transport Category Airplanes|publisher=[[Federal Aviation Administration]]|date=1996-05-07|access-date=2008-10-02|archive-date=2009-02-02|archive-url=https://web.archive.org/web/20090202140424/http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgFAR.nsf/0/FED94F31539484AB852566720051AA5D?OpenDocument|url-status=dead}}</ref> For aircraft [[type certificate|certified]] to operate above 25,000&nbsp;feet (FL&nbsp;250; 7,600&nbsp;m), it "must be designed so that occupants will not be exposed to cabin pressure altitudes in excess of {{convert|15000|ft}} after any probable failure condition in the pressurization system."<ref name="FARs, 14 CFR, Part 25, Section 841">{{Cite web|url=http://www.flightsimaviation.com/data/FARS/part_25-841.html|title=Flightsim Aviation Zone - Number 1 Flight Simulation & Aviation Resource! - Flight Simulator, Aviation Databases|website=www.flightsimaviation.com}}</ref> In the event of a decompression which results from "any failure condition not shown to be extremely improbable," the aircraft must be designed so that occupants will not be exposed to a cabin altitude exceeding {{convert|25000|ft}} for more than 2 minutes, nor exceeding an altitude of {{convert|40000|ft}} at any time.<ref name="FARs, 14 CFR, Part 25, Section 841"/> In practice, that new FAR amendment imposes an operational [[Ceiling (aeronautics)|ceiling]] of 40,000 feet on the majority of newly designed commercial aircraft.<ref name="Exemption No. 8695">{{cite web|url=http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgEX.nsf/0/9929ce16709cad0f8625713f00551e74/$FILE/8695.doc|title=Exemption No. 8695|publisher=[[Federal Aviation Administration]]|date=2006-03-24|___location=Renton, Washington|access-date=2008-10-02|archive-date=2009-03-27|archive-url=https://web.archive.org/web/20090327094608/http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgEX.nsf/0/9929ce16709cad0f8625713f00551e74/$FILE/8695.doc|url-status=dead}}</ref><ref>{{cite web|url=http://rgl.faa.gov/Regulatory_and_Guidance_Library%5CrgPolicy.nsf/0/90AA20C2F35901D98625713F0056B1B8?OpenDocument|publisher=[[Federal Aviation Administration]]|date=2006-03-24|title=PS-ANM-03-112-16|access-date=2009-09-23|author=Steve Happenny}}</ref><ref group="Note">Notable exceptions include the [[Airbus A380]], [[Boeing 787]], and [[Concorde]]</ref>