Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe
Service life of the PZL M28 is computed based on the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test objects were: (1) wing and wing load carry-through structure, (2) empennag...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Sciendo
2014-06-01
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| Series: | Fatigue of Aircraft Structures |
| Subjects: | |
| Online Access: | https://doi.org/10.1515/fas-2014-0008 |
| _version_ | 1797965238034759680 |
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| author | Brzęczek Józef Gruszecki Henryk Pieróg Leszek Pietruszka Janusz |
| author_facet | Brzęczek Józef Gruszecki Henryk Pieróg Leszek Pietruszka Janusz |
| author_sort | Brzęczek Józef |
| collection | DOAJ |
| description | Service life of the PZL M28 is computed based on the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test objects were: (1) wing and wing load carry-through structure, (2) empennage and attached fuselage structure. Additionally, there were fatigue tests carried out for the landing gear and other selected elements including control system elements. The aircraft load carry-through structure is metallic and the cabin is unpressurized. The fatigue tests were conducted stage-by-stage. As tests progressed, it was possible to extend the aircraft target service life, applying the safe-life philosophy with reference to the primary components of the load carry-through structure. |
| first_indexed | 2024-04-11T01:55:49Z |
| format | Article |
| id | doaj.art-ee02bd87dab64136a4a6af710c8f192d |
| institution | Directory Open Access Journal |
| issn | 2300-7591 |
| language | English |
| last_indexed | 2024-04-11T01:55:49Z |
| publishDate | 2014-06-01 |
| publisher | Sciendo |
| record_format | Article |
| series | Fatigue of Aircraft Structures |
| spelling | doaj.art-ee02bd87dab64136a4a6af710c8f192d2023-01-03T05:14:54ZengSciendoFatigue of Aircraft Structures2300-75912014-06-0120146889410.1515/fas-2014-0008fas-2014-0008Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic AirframeBrzęczek Józef0Gruszecki Henryk1Pieróg Leszek2Pietruszka Janusz3Polskie Zakłady Lotnicze Sp. z o.o., ul. Wojska Polskiego 3, 39-300 MielecPolskie Zakłady Lotnicze Sp. z o.o., ul. Wojska Polskiego 3, 39-300 MielecPolskie Zakłady Lotnicze Sp. z o.o., ul. Wojska Polskiego 3, 39-300 MielecPolskie Zakłady Lotnicze Sp. z o.o., ul. Wojska Polskiego 3, 39-300 MielecService life of the PZL M28 is computed based on the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test objects were: (1) wing and wing load carry-through structure, (2) empennage and attached fuselage structure. Additionally, there were fatigue tests carried out for the landing gear and other selected elements including control system elements. The aircraft load carry-through structure is metallic and the cabin is unpressurized. The fatigue tests were conducted stage-by-stage. As tests progressed, it was possible to extend the aircraft target service life, applying the safe-life philosophy with reference to the primary components of the load carry-through structure.https://doi.org/10.1515/fas-2014-0008metallic airframe structurefull scale fatigue tests |
| spellingShingle | Brzęczek Józef Gruszecki Henryk Pieróg Leszek Pietruszka Janusz Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe Fatigue of Aircraft Structures metallic airframe structure full scale fatigue tests |
| title | Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe |
| title_full | Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe |
| title_fullStr | Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe |
| title_full_unstemmed | Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe |
| title_short | Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe |
| title_sort | selected aspects related to preparation of a fatigue test plan of a metallic airframe |
| topic | metallic airframe structure full scale fatigue tests |
| url | https://doi.org/10.1515/fas-2014-0008 |
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