AD 73-19-03

Active

Nose Gear Actuating System Failure

Key Information
73-19-03
Active
October 08, 1973
Not specified
Unknown
39-1716
Applicability
["Aircraft"]
["Small Airplane"]
Mitsubishi Heavy Industries, Ltd.
MU-2B MU-2B-10 MU-2B-15 MU-2B-20 MU-2B-25
Regulatory Text

73-19-03 MITSUBISHI HEAVY INDUSTRIES, LTD: Amdt. 39-1716. Applies to Mitsubishi Model MU-2B airplanes (S/N 004, and 006 through 038); MU-2B-10, and -15 airplanes (S/N 101, and 103 through 120); MU-2B-20, and -25 airplanes (S/N 005, 102, and 121 through 271).
Compliance is required as indicated.
To prevent the failure of the nose gear actuating system, accomplish the following:
Within the next 100 hours' time in service after the effective date of this AD, unless already accomplished, modify the nose gear actuating assembly and its supporting structure in accordance with Mitsubishi MU-2 Service Bulletin No. 155, dated June 26, 1972, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Pacific- Asia Region.
This amendment becomes effective October 8, 1973.

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References
This information is not available.
--- - Part 39
FAA Documents