Pour les CESSNA 180 jusqu’aux Modèle ‘’K’’, 182 jusqu’au Modèle ‘’ D ’’ et tous les 185 !
Puis Répétitive aux 500 heures ou 5 ans, selon le premier atteint!
Les informations suivantes ont été récemment publiées sur le site Web des consignes de navigabilité de Transports Canada : Le sujet et l’applicabilité sont alimentés à partir du document original. Les informations provenant de sources étrangères ne sont pas soumises à la Loi sur les langues officielles, il n’y a donc pas de traduction disponible.
Numéro: US2020-21-22
Sujet: ATA 55 - INSPECTION OF HORIZONTAL STABILIZER ATTACHMENT STRUCTURE FOR CRACKS AND CORROSION IN THE TAIL CONE REINFORCEMENT ANGLE, STABILIZER HINGE BRACKET AND STABILIZER.
Applicabilité: Textron Aviation Inc. (Cessna) Models 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 182, 182A, 182B, 182C, 182D, 185, 185A, 185B, 185C, 185D, 185E, A185E, and A185F airplanes, all serial numbers.
Lien: https://wwwapps.tc.gc.ca/saf-sec-sur/2/ ... -21-22.PDF
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(g) Inspect, Repair, and Replace Within the next 100 hours time-in-service (TIS) after the effective date of this AD (December 07, 2020) or within the next 12 months after the effective date (December 07, 2020) of this AD, whichever occurs later, and thereafter every 500 hours TIS or 5 years, whichever occurs first, visually inspect each stabilizer hinge bracket, tailcone reinforcement angle, corner reinforcement, stabilizer hinge reinforcement channel, stabilizer hinge assembly, stabilizer aft spar reinforcement, and the lower half of the stabilizer aft spar from station (STA) 16 on the left side to STA 16 on the right side for corrosion and cracks; remove any corrosion; and replace any part with a crack by following the Accomplishment Instructions, paragraphs 9 9 through 11 and 13, of Textron Aviation Single Engine Mandatory Service Letter SEL-55-01, dated December 7, 2017. Also inspect for loose rivets and sheared rivets. If there is a loose or sheared rivet, before further flight, replace the rivet.
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