AD 70-19-03

Active

Jumper Wire Installation

Key Information
70-19-03
Active
September 22, 1970
Not specified
Unknown
39-1080
Applicability
["Aircraft"]
["Small/Large Airplane"]
Dornier Luftfahrt GmbH
Do 28 D-1
Regulatory Text

70-19-03 DORNIER AG: Amdt. 39-1080. Applies to Model Do-28D-1 Airplanes.

To prevent interference between the jumper wires and the aileron and flap control systems, within the next 50 hours' time in service after the effective date of this AD, unless already accomplished, rework the jumper wire installations located in the right and left wing by installing shorter jumper wires, covering the jumper wires with insulation tubing, and rerouting wires in accordance with Dornier Service Bulletin No. 1030-1408, dated 6 July 1970, or an FAA approved equivalent.

This amendment becomes effective September 22, 1970.

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