AD 73-20-05

Active

Float To Fuselage Bolts

Key Information
73-20-05
Active
October 03, 1973
Not specified
Unknown
39-1725
Applicability
["Aircraft"]
["Small Airplane"]
Viking Air Limited
DHC-6-1 DHC-6-100 DHC-6-200 DHC-6-300
Regulatory Text

73-20-05 de HAVILLAND: Model DHC-6. Amdt. 39-1725. Applies to de Havilland Model DHC-6 Twin Otter Floatplanes, all Series, certificated in all categories, equipped with Canadian Aircraft Products Model 12000A or 12000B Floats installed prior to Float Serial No. 71.

1. Compliance is required within the next ten hours in service from the effective date of this Airworthiness Directive, unless already accomplished.

To prevent loosening and subsequent pullout failure of certain float to fuselage bolts, comply with accomplishment instruction of de Havilland Service Bulletin 6/296, Revision A, dated May 11, 1973, or an equivalent alteration approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

This amendment is effective October 3, 1973.

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