AD 75-17-13

Active

Tail Rotor Blade Tip Cap

Key Information
75-17-13
Active
August 18, 1975
Not specified
Unknown
39-2315
Applicability
["Aircraft"]
["Rotorcraft"]
Airbus Helicopters Deutschland GmbH
BO-105A BO-105C
Regulatory Text

75-17-13 MESSERSCHMITT-BOLKOW-BLOHM.: Amendment 39-2315. Applies to Messerschmitt-Bolkow-Blohm (MBB) Models BO-105A and BO-105C helicopters, certificated in all categories, incorporating tail rotor blade P/N 105-31742, Serial Numbers 548 and lower.
Compliance is required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished in accordance with MBB BO-105 Service Bulletin No. 30-8.
To prevent failure of the tail rotor blade tip cap, inspect tail rotor blades for condition, modify as prescribed, and return to service, in accordance with paragraph 2 of MBB BO-105 Service Bulletin No. 30-8, dated July 5, 1974, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.
This amendment becomes effective August 18, 1975.

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