AD 2013-20-18

final rule
Data completeness: 70%

Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell) Helicopters

AD Number
2013-20-18
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0500
FR Citation
78 FR 63858

Applicability

TypeManufacturerModelDetails
aircraft Textron Various Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell) Helicopters
aircraft Bell Helicopter Textron Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell) Helicopters

Unsafe Condition

fatigue cracking of a yoke, failure of the yoke, and subsequent loss of control of the helicopter.

Required Actions

Within 10 hours time-in-service (TIS), review the helicopter records to determine all of the helicopter models on which an affected yoke has been installed since its production and the hours TIS of each affected yoke. If an affected part-numbered yoke has ever been installed on a Model 412CF helicopter or on a Model 412 or 412EP helicopter with a slope landing kit, P/N 412-704-012-101, installed, do the following: reidentify the P/N on the side of the yoke by using a vibrating stylus and etching two lines through the last three digits of the existing P/N and etching “137FM” adjacent to where you etched through the last three digits of the original P/N. This converts each affected yoke P/N to a new yoke P/N 412-010-101-137FM. The serial number remains the same. Treat the etched surface with chemical film, and apply primer and paint. Record the reidentified P/N on the applicable component history card or equivalent record. For each reidentified yoke, P/N 412-010-101-137FM, reduce the retirement life from 5,000 hours TIS to 4,500 hours TIS. Record the revised life limit on the applicable component history card or equivalent record. Revise the Airworthiness Limitations section of the applicable maintenance manual or the Instructions for Continued Airworthiness by reducing the retirement life from 5,000 hours TIS to 4,500 hours TIS for each reidentified yoke, P/N 412-010-101-137FM.

Compliance Time

Within 10 hours time-in-service (TIS)

Affected Aircraft

Model 412 and 412EP helicopters with a main rotor yoke assembly (yoke), part number (P/N) 412-010-101-123, -127, -129, or -133, installed; and Model 412CF helicopters with a yoke, P/N 412-010-101-127 or -129, installed; certificated in any category.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.