Univair Aircraft (Stinson) 108 Series AeUnivair Aircraft (Stinson) 108 Series Aeroplanes

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Univair Aircraft (Stinson) 108 Series Aeroplanes

AD/STINSON 108/2	Stabilizer Leading EdgeAttachment - Inspection	17/2018

Applicability:	Univair Aircraft Corporation Stinson 108 series aircraft, serial numbers 1 through 3500.
Requirement:	1. Inspect stabilizer leading edge attachment in accordance with the instructions in Stinson Service Bulletin 254 dated 5 September 1947, as in force at the commencement of this AD.2. If during the Requirement 1 inspection, fatigue cracks of the stabilizer leading edge attachment are found, reinforcements to the stabilizer fitting must be added in accordance with the instructions in Stinson Service Bulletin 254 dated 5 September 1947, as in force at the commencement of this AD.Note: FAA AD 47-50-12 refers.
Compliance:	1. Within 30 days after the commencement date of this AD, unless previously accomplished, and thereafter at intervals not to exceed 100 hours’ time in service.2. Before further flight.
	This AD commences on 31 August 2018.
Background:	A review of the Australian Aircraft Register found that this aircraft type has been registered in Australia since 1987. There are currently 12 aircraft of this type on the register with the majority having been registered in 1994/95.This AD is issued detect and correct fatigue cracking of the stabilizer leading edge attachment.

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Pieter van Dijk
Delegate of the Civil Aviation Safety Authority

21 August 2018