Airworthiness Directive

AD 2002-01-07 67 FR 2317 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-1055
Amendment
39-12598
Published
2002-01-17
Effective
2002-02-21
Models covered
1
Last live check
2026-09-30
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.
AD

2002-01-07

FR doc 02-1055 · 67 FR 2317

AD 2002-01-07Published 2002-01-17Effective 2002-02-21

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 changes to the electrical power distribution system.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 430 helicopters that requires changes to the electrical power distribution system. This amendment is prompted by design deficiencies in the electrical systems. The actions specified by this AD are intended to prevent failure of both generators, loss of primary electrical power, and subsequent loss of control of the helicopter.

More directives for Bell 430

  1. AD 2026-13-12 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2026-07-07
  2. AD 2025-09-03 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2025-04-28
  3. AD 2021-24-09 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2021-11-22
  4. AD 2021-19-01 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2021-09-08
  5. AD 2016-21-01 Airworthiness Directives; Bell Helicopter Textron Helicopters 2016-10-14

All Bell 430 directives

Applies to 1 model in our index