AD 70-21-01

Active

Cabin Door Structure

Key Information
70-21-01
Active
November 05, 1970
Not specified
Unknown
39-1091
Applicability
["Aircraft"]
["Small/Large Airplane"]
Dornier Luftfahrt GmbH
Do 28 D-1
Regulatory Text

70-21-01 DORNIER, AG: Amdt. 39-1091. Applies to Model DO-28D-1 airplanes.

To prevent separation of the skin from the cabin door structure, within the next 100 hours' time in service after the effective date of this AD, unless already accomplished, secure the door skin by installing additional screws in accordance with Dornier Service Bulletin No. 015- 1206, dated October 1, 1969, or later LBA-approved issue or an FAA-approved equivalent.

This amendment becomes effective November 5, 1970.

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