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AD 77-04-06 SUPERSEDED

Main Rotor Gearbox
WARNING: This AD has been superseded and is no longer active. Replaced by: 2022-24-07. Refer to the superseding AD(s) for current requirements.
Key Information
AD Number 77-04-06 Status Superseded
Effective Date August 23, 1979 Issue Date February 07, 1977
Docket Number Unknown Amendment 39-2835
Product Type ["Aircraft"] Product Subtype ["Rotorcraft"]
CFR Part --- - Part 39 CFR Section --- - _EMPTY_
Citation This information is not available.
Applicability
Manufacturer(s) Airbus Helicopters Deutschland GmbH
Model(s) BO-105A BO-105C
Related Airworthiness Directives
Superseded By 2022-24-07
Regulatory Text

77-04-06 MESSERSCHMITT-BOLKOW-BLOHM (MBB): Amendment 39-2835 as amended by amendment 39-3528. Applies to all Model BO-105A and BO-105C helicopters, certificated in all categories.
Compliance is required as indicated.
To prevent the possible failure of a main rotor gearbox support, P/Ns 105-10161 and 105-10162, replace the two supports with serviceable supports within the next 10 hours time in service after the effective date of this AD or prior to the accumulation of 6,800 hours time in service on the supports, whichever occurs later, and, thereafter, continue to replace the supports prior to the accumulation of 6,800 hours time in service.
Amendment 39-2835 became effective March 3, 1977.
This amendment 39-3528 becomes effective August 23, 1979.

Office of Primary Responsibility
["AIR-720: Operational Safety Branch"]