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| 01311nam##2200241za#4500 |
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| 001 | 9.571342 |
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| 003 | CaOODSP |
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| 005 | 20210624182658 |
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| 007 | cr ||||||||||| |
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| 008 | 150406|2005||||xxc|||||o f|0| 0 eng|d |
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| 040 | |aCaOODSP|beng |
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| 043 | |an-cn--- |
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| 086 | 1 |aTU3-5/05-17E-PDF |
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| 110 | 2 |aTransportation Safety Board of Canada. |
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| 245 | 10|aComponent failure, wing-to-fuselage attach angle, Bradley Air Services Ltd. (First Air), Lockheed L382G Hercules C-GHPW, vicinity of High Lake, Nunavut, 12 April 2005 |h[electronic resource] |
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| 260 | |aGatineau - Quebec : |bTransportation Safety Board of Canada |c[2006]. |
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| 300 | |a9p.|bfig., photographs |
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| 490 | 1 |aAviation investigation report |vA05W0059 |
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| 500 | |a"The Board authorized the release of this report on 07 February 2006."--p.9 of 9. |
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| 590 | |a12-19-Supp|b2012-04-30 |
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| 775 | 08|tDéfaillance d'un composant (cornière de fixation de l'aile au fuselage) du Lockheed L382G Hercules C-GHPW exploité par Bradley Air Services Ltd. (First Air), près de High Lake (Nunavut), le 12 avril 2005 |w(CaOODSP)9.601957 |
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| 830 | #0|aAviation investigation report ;|vA05W0059|w(CaOODSP)9.504825 |
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| 856 | 40|ahttp://publications.gc.ca|qPDF|s267 KB|uhttps://publications.gc.ca/collections/collection_2011/bst-tsb/TU3-5-05-17-eng.pdf|yA05W0059 |
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