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Airworthiness Directive

AD 2003-13-14 68 FR 40481 Active

Federal Aviation Administration · 14 CFR part 39

Requires performing a continuity test, temporarily repairing any unairworthy chip detector, and replacing any repaired chip detectors.

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FR document
03-16686
Amendment
39-13216
Published
2003-07-08
Effective
2003-08-12
Models covered
1

Last live check: 2026-10-04

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This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2003-13-14

FR doc 03-16686 · 68 FR 40481

AD 2003-13-14Published 2003-07-08Effective 2003-08-12

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.

Requires performing a continuity test, temporarily repairing any unairworthy chip detector, and replacing any repaired chip detectors.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters that requires performing a continuity test, temporarily repairing any unairworthy chip detector, and replacing any repaired chip detectors. This amendment is prompted by reports of poor or no continuity between the insert and the chip detector housing on certain chip detectors. The actions specified by this AD are intended to prevent failure of a chip detector indication, loss of a critical component, and subsequent loss of control of the helicopter.

More directives for Bell 206 JetRanger / LongRanger

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  5. AD 2021-24-15 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2022-01-18

All Bell 206 JetRanger / LongRanger directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index