NPRM FAA-2005-20441

Became AD 2003-19-14 R2

Proposed airworthiness directive · Burkhardt Grob Luft-Und

Published
March 23, 2005 · 70 FR 14580
Comments due
April 20, 2005
Action
Notice of proposed rulemaking (NPRM)
Docket
FAA-2005-20441
Project
2003-CE-35-AD
FR document
05-5693
Products
Aircraft

A proposal is not in force. If adopted, it becomes an AD, usually with changes. Only the Federal Register edition is official.

Summary

The FAA proposes to revise Airworthiness Directive (AD) 2003- 19-14 R1, which applies to certain BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG (GROB) Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO sailplanes. AD 2003-19-14 R1 requires you to modify the airspeed indicators, install flight speed reduction and aerobatic maneuver restrictions placards (as applicable), and revise the flight and maintenance manuals. AD 2003-19-14 R1 approves simple aerobatic maneuvers for Model G103A TWIN II ACRO sailplanes and provides an option for modifying the rear fuselage for Models G103A TWIN II ACRO and G103C TWIN III ACRO sailplanes to terminate the flight limitation restrictions for aerobatic maneuvers. This proposed AD retains all the actions from AD 2003-19-14 R1 for Models G103A TWIN II ACRO and G103C TWIN III ACRO and would reinstate certain operating limits for Model G103 TWIN ASTIR sailplanes. We are issuing this proposed AD to prevent damage to the fuselage during limit load flight, which could result in reduced structural integrity. This condition could lead to loss of control of the sailplane.

The resulting AD

Notices in this docket · 1