AD/MU-2/38 - Landing Gear Aural Warning System
1AD/MU-2/38 - Landing Gear Aural Warning System
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Mitsubishi MU-2 Series Aeroplanes
AD/MU-2/38 Landing Gear Aural Warning System 7/86
Applicability: Models MU-2B-25/-26/-26A/-40 with S/Nos. 313SA, 321SA, 365SA and 397SA through 457SA.
Requirement: Action in accordance with Mitsubishi SB 057/32-010. Compliance: Within 100 hours after 31 July 1986.
Background: It has been determined that the landing gear aural warning may not activate in all possible landing conditions.