Airworthiness Directive

AD 2016-26-04 82 FR 716 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2016-30832
Amendment
39-18762
Published
2017-01-04
Effective
2017-02-08
Models covered
2
Last live check
2026-10-01
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

2016-26-04

FR doc 2016-30832 · 82 FR 716

AD 2016-26-04Published 2017-01-04Effective 2017-02-08

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 the main rotor blade (MRB).

Full official abstract

We are adopting a new airworthiness directive (AD) for Robinson Helicopter Company (Robinson) Model R44, R44 II, and R66 helicopters. This AD requires inspecting the main rotor blade (MRB). This AD was prompted by a determination that some MRBs may have reduced blade thickness due to blending out corrosion. The actions are intended to prevent the unsafe condition on these products.

More directives for Robinson R44

  1. AD 2025-11-07 Airworthiness Directives; Robinson Helicopter Company Helicopters 2025-06-06
  2. AD 2024-23-01 Airworthiness Directives; Robinson Helicopter Company 2024-12-03
  3. AD 2024-20-03 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-10-24
  4. AD 2024-19-11 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-09-26
  5. AD 2024-04-02 Airworthiness Directives; Robinson Helicopter Company Helicopters 2024-02-27

All Robinson R44 directives

Applies to 2 models in our index