AD 81-18-01

Superseded

Main Rotor Trunnions

Key Information
81-18-01
Superseded
September 22, 1981
Not specified
81-ASW-27
39-4192
Applicability
["Aircraft"]
["Rotorcraft"]
Bell Helicopter Textron (Canada) Bell Helicopter Textron (Canada) Bell Helicopter Textron (Canada) Bell Helicopter Textron (Canada) Bell Helicopter Textron (Canada) Bell Helicopter Textron (Canada) Bell Helicopter Textron (Canada)
206A 206A-1 (OH-58A) 206B 206B-1 206L 206L-1
Regulatory Text

81-18-01 BELL: Amendment 39-4192. Applies to Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 helicopters, equipped with main rotor trunnions, P/N 206-010-104-3, 206-011- 113-001, 206-011-120-001, 206-011-113-103, and 206-011-120-103, certificated in all categories (Airworthiness Docket No. 81-ASW-27).

Compliance required as indicated.

To prevent possible failure of the main rotor trunnion, P/N's 206-010-104-3, 206-011- 113-001, 206-011-120-001, 206-011-113-103, and 206-011-120-103, due to fatigue cracks, accomplish the following, unless already accomplished:

a. Main rotor trunnions, P/N 206-011-120-001, with 1,100 or more hours' time in service on the effective date of this AD must be retired from service within the next 100 hours' time in service.

b. Main rotor trunnions, P/N 206-011-120-001, with less than 1,100 hours' time in service on the effective date of this AD must be retired from service prior to or on attaining 1,200 hours' time in service.c. Main rotor trunnions, P/N 206-010-104-3, 206-011-113-001, and 206-011-120- 103, with 2,300 or more hours' time in service on the effective date of this AD must be retired from service within the next 100 hours' time in service.

d. Main rotor trunnions, P/N 206-010-104-3, 206-011-113-001, and 206-011-120- 103, with less than 2,300 hours' time in service on the effective date of this AD must be retired from service prior to or on attaining 2,400 hours' time in service.

e. Main rotor trunnions, P/N 206-011-113-103, with 4,700 or more hours' time in service on the effective date of this AD must be retired from service within the next 100 hours' time in service.

f. Main rotor trunnions, P/N 206-011-113-103, with less than 4,700 hours' time in service on the effective date of this AD must be retired from service prior to or on attaining 4,800 hours' time in service.

g. The helicopter may be flown in accordance with FAR 21.197 to a base where compliance with this AD can be performed.

h. The retirement times, for the main rotor trunnions, established by this AD, are as follows:

Part Number
Service Life-Hours
206-011-120-001
1,200
206-010-104-3
2,400
206-011-113-001
2,400
206-011-120-103
2,400
206-011-113-103
4,800

(Bell Helicopter Textron Alert Service Bulletins 206-80-7, Rev. B, dated October 15, 1980, and 206L-80-9, Rev. B, dated October 15, 1980, pertain to this subject.)

This amendment becomes effective September 22, 1981.

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Related ADs
81-18-01 R1 Replaced by the above
References
This information is not available.
--- - Part 39
FAA Documents