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Airworthiness Directive

AD 98-10-06 63 FR 26427 Active

Federal Aviation Administration · 14 CFR part 39

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FR document
98-12355
Amendment
39-10517
Published
1998-05-13
Effective
1998-06-28
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/98-10-06 · 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

98-10-06

FR doc 98-12355 · 63 FR 26427

AD 98-10-06Published 1998-05-13Effective 1998-06-28

Supersedes 96-19-07

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 the following on Burkhart Grob Luft-und Raumfahrt (Grob) Models G115C, G115C2, G115D, and G115D2 airplanes: installing a placard that restricts the never exceed speed (Vne) of the affected airplane models from 184 knots to 160 knots; installing on the airspeed indicator glass a red line at 296 km/h (160 knots); installing a placard that prohibits aerobatic maneuvers; and placing a copy of the AD in the Limitations Section of the airplane flight manual.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 96-19- 07, which currently requires the following on Burkhart Grob Luft-und Raumfahrt (Grob) Models G115C, G115C2, G115D, and G115D2 airplanes: installing a placard that restricts the never exceed speed (Vne) of the affected airplane models from 184 knots to 160 knots; installing on the airspeed indicator glass a red line at 296 km/h (160 knots); installing a placard that prohibits aerobatic maneuvers; and placing a copy of the AD in the Limitations Section of the airplane flight manual. This AD will temporarily retain the flight restrictions that are currently required by AD 96-19-07; and will eventually require accomplishing certain inspections and modifications, as terminating action for these flight restrictions. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent loss of control of the airplane caused by excessive speed or aerobatic maneuvers.

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  3. AD 2022-03-08 Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG... Effective 2022-03-17
  4. AD 2017-08-12 Airworthiness Directives; GROB Aircraft AG Gliders Effective 2017-05-31
  5. AD 2016-12-08 Airworthiness Directives; GROB Aircraft AG Airplanes Effective 2016-07-20

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