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Airworthiness Directive

AD 96-19-07 61 FR 49250 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires 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…

Superseded by AD 98-10-06Federal Register (opens in a new tab)

FR document
96-23988
Amendment
39-9765
Published
1996-09-19
Effective
1996-09-27
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/96-19-07 · 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

96-19-07

FR doc 96-23988 · 61 FR 49250

AD 96-19-07Published 1996-09-19Effective 1996-09-27

Superseded by 98-10-06

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 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 this AD in the Limitations Section of the airplane flight manual.

Full official abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 96-19-07, which was sent previously to all known U.S. owners and operators of Burkhart Grob Luft-und Raumfahrt (Grob) Models G115C, G115C2, G115D, and G115D2 airplanes. This AD requires 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 this AD in the Limitations Section of the airplane flight manual. An in-flight breakup of a Grob Model G115D airplane prompted priority letter AD 96-19-07. 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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All Grob directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 96-19-07 (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