Airworthiness Directive

AD 98-19-13 64 FR 1715 Active

Federal Aviation Administration · 14 CFR part 39

Prompted by analysis and test data which revealed that the life limit of the driveshaft is less than that which is stated in the applicable maintenance manual.

FR document
99-615
Amendment
39-10990
Published
1999-01-12
Effective
1999-01-27
Models covered
1

Last live check: 2026-10-04

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AD

98-19-13

FR doc 99-615 · 64 FR 1715

AD 98-19-13Published 1999-01-12Effective 1999-01-27

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Prompted by analysis and test data which revealed that the life limit of the driveshaft is less than that which is stated in the applicable maintenance manual.

Full official abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 98-19-13, which was sent previously to all known U.S. owners and operators of BHTC Model 407 helicopters by individual letters. This AD requires, on or before the accumulation of 50 hours total time-in-service (TIS) on the engine-to- transmission driveshaft (driveshaft), replacing the driveshaft with an airworthy driveshaft. This amendment is prompted by analysis and test data which revealed that the life limit of the driveshaft is less than that which is stated in the applicable maintenance manual. The actions specified by this AD are intended to prevent failure of the driveshaft, loss of engine drive to the rotor system, damage to critical structural components, and subsequent loss of control of the helicopter.

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All Bell 407 directives

Applies to 1 model in our index