AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2022-05-14 87 FR 13135 Active

Federal Aviation Administration · 14 CFR part 39

Requires repairing the support structure at the attachment to the attachment bolts on certain flight control surfaces, inspecting the support structure at the attachment bolts of all flight control surfaces, and taking corrective…

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
2022-04914
Amendment
39-21966
Published
2022-03-09
Effective
2022-03-24
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2022-05-14 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2022-05-14

FR doc 2022-04914 · 87 FR 13135

AD 2022-05-14Published 2022-03-09Effective 2022-03-24

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 repairing the support structure at the attachment to the attachment bolts on certain flight control surfaces, inspecting the support structure at the attachment bolts of all flight control surfaces, and taking corrective actions if discrepancies are detected.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all GROB Aircraft SE (type certificate previously held by GROB Aircraft AG) (GROB) Model G 115EG airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as in-flight detachment of a rudder actuator hinge bracket. This AD requires repairing the support structure at the attachment to the attachment bolts on certain flight control surfaces, inspecting the support structure at the attachment bolts of all flight control surfaces, and taking corrective actions if discrepancies are detected. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Grob

  1. AD 2025-20-07 Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG... Effective 2025-10-17
  2. AD 2022-03-08 Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG... Effective 2022-03-17
  3. AD 2017-08-12 Airworthiness Directives; GROB Aircraft AG Gliders Effective 2017-05-31
  4. AD 2016-12-08 Airworthiness Directives; GROB Aircraft AG Airplanes Effective 2016-07-20
  5. AD 2015-09-06 Airworthiness Directives; GROB-WERKE Airplanes Effective 2015-06-16

All Grob 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