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Airworthiness Directive

AD 2024-08-03 89 FR 33218 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting for interference between the control column, rudder pedal adjuster cable, and any wiring (including the Koiled Kord) concurrently with performing a flight control full and free movement inspection, and taking…

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FR document
2024-09083
Amendment
39-22736
Published
2024-04-29
Effective
2024-06-03
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2024-08-03 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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

2024-08-03

FR doc 2024-09083 · 89 FR 33218

AD 2024-08-03Published 2024-04-29Effective 2024-06-03

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 inspecting for interference between the control column, rudder pedal adjuster cable, and any wiring (including the Koiled Kord) concurrently with performing a flight control full and free movement inspection, and taking corrective actions if necessary.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all Britten-Norman Aircraft, Ltd. Model BN-2, BN-2A, BN-2A-2, BN-2A-3, BN- 2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B- 20, BN-2B-21, BN-2B-26, BN-2B27, BN-2T, BN2T-4R, and BN2T-4S airplanes; and Model BN2A MK. III, BN2A MK. III-2, and BN2A MK. III-3 airplanes. This AD is prompted by reports of electrical cable (Koiled Kord) and flight control cables interference with the control column. This AD requires inspecting for interference between the control column, rudder pedal adjuster cable, and any wiring (including the Koiled Kord) concurrently with performing a flight control full and free movement inspection, and taking corrective actions if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Britten-Norman BN-2 Islander

  1. AD 2025-01-01 Airworthiness Directives; Britten-Norman Aerospace Ltd. Airplanes Effective 2025-03-11
  2. AD 2021-18-01 Airworthiness Directives; B-N Group Ltd. Airplanes Effective 2021-10-14
  3. AD 2016-26-09 Airworthiness Directives; B-N Group Ltd. Airplanes Effective 2017-02-09
  4. AD 2016-06-01 Airworthiness Directives; B-N Group Ltd. Airplanes Effective 2016-04-19
  5. AD 2016-04-05 Airworthiness Directives; B-N Group Ltd. Airplanes Effective 2016-03-24

All Britten-Norman BN-2 Islander 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