AD 48-02-01

Active

Tail Rotor Drive Shaft

Key Information
48-02-01
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Rotorcraft"]
Scotts-Bell 47 Inc
47B 47B3
Regulatory Text

48-02-01 BELL: Applies to All 47B Series, Through Serial Number 78.

Compliance required before next 25 hours of operation.

Reinforce the tail rotor drive shaft bearing hangers by riveting reinforcement plates, Bell P/N 47-267-001-152, -153, -154, -155, -156, and -157, to the appropriate hangers with AN 470- AD3-4 rivets.

(Bell Service Bulletin 47C56 dated September 10, 1947, also covers this subject.)

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents