Отрывок: Wing: cracks in tail part of wing, landing gear compartments doors, in wing fences; leakage fuel tanks placed in wing. Tail unit, control surfaces and wing high-lift devices: cracks in skin; tearing frictionless or slider bearing in hinges fitting; turning bearing cup in hinges fitting. Landing gear: cracks in welded seams and pin hinges landing gear; cracks in shock strut piston; deterioration and teases in shock strut bear...
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dc.contributor.authorMrykin S. V.ru
dc.contributor.authorMrykin S. V.ru
dc.contributor.authorThe Ministry of Education and Science of the Russian Federationru
dc.contributor.authorSamara State Aerospace University (National Research University)ru
dc.coverage.spatialсамолетные системыru
dc.coverage.spatialфункциональные отказыru
dc.coverage.spatialпоследствия функциональных отказовru
dc.creatorMrykin S. V.ru
dc.date.issued2011ru
dc.identifierRU/НТБ СГАУ/WALL/629.7.05/M 10-217066ru
dc.identifier.citationMrykin, S. V. Functional Failure Effects Airplane Systems [Электронный ресурс] : Electronic Manual / S. V. Mrykin ; [tr. S. V. Mrykin] ; The Ministry of Education and Science of the Russian Federation, Samara State Aerospace University (National Research University). - Samara, 2011. - on-lineru
dc.description.abstractТруды сотрудников СГАУ(электрон. версия).ru
dc.description.abstractИспользуемые программы: Adobe Acrobat.ru
dc.description.abstractAttributes classification of aircraft systems by failure effect, list and attributes special situations, arising owing to failures system according to AR-25 [1] are presented in the manual. List typical failures and examples of classification for specialru
dc.format.extentElectronic text (1 файл : 367,0 Kb)ru
dc.language.isorusru
dc.relation.isformatofFunctional Failure Effects Airplane Systems [Электронный ресурс] : Electronic Manualru
dc.titleFunctional Failure Effects Airplane Systemsru
dc.typeTextru
dc.subject.rugasnti55.47ru
dc.subject.udc629.7.05ru
dc.textpartWing: cracks in tail part of wing, landing gear compartments doors, in wing fences; leakage fuel tanks placed in wing. Tail unit, control surfaces and wing high-lift devices: cracks in skin; tearing frictionless or slider bearing in hinges fitting; turning bearing cup in hinges fitting. Landing gear: cracks in welded seams and pin hinges landing gear; cracks in shock strut piston; deterioration and teases in shock strut bear...-
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