# Proposed AD 97-CE-134-AD: Diamond Aircraft Industries GmbH Models H-36 ``Dimona'' and HK 36 R ``Super Dimona'' Sailplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 98-09-24
- Action: Notice of proposed rulemaking (NPRM).
- Published: February 13, 1998, 63 FR 7324
- Comments due: March 17, 1998
- Became: [AD 98-09-24](https://openairdocs.org/ad/98-09-24)
- Docket: 97-CE-134-AD
- FR document: 98-3638
- Official PDF: https://openairdocs.org/files/sha256/10/d3/10d3187a28bea7725c99163a6d7afdd22a2b429709ca1289be6a3e4d0fdf5e04 (from https://www.govinfo.gov/content/pkg/FR-1998-02-13/pdf/98-3638.pdf)
- Federal Register: https://www.federalregister.gov/documents/1998/02/13/98-3638/airworthiness-directives-diamond-aircraft-industries-gmbh-models-h-36-dimona-and-hk-36-r-super
- Page: https://openairdocs.org/proposed/97-CE-134-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Diamond Aircraft Industries GmbH (Diamond) Models H-36 ``Dimona'' and HK 36 R ``Super Dimona'' sailplanes. The proposed AD would require: inspecting the elevator rib area for damage on certain Models H-36 ``Dimona'' and HK 36 R ``Super Dimona'' sailplanes, and either immediately or eventually replacing the elevator ribs depending on the results of the inspection; replacing the M6 screws that attach the wheel axle to steel support with M8 screws on all of the affected airplanes; and inspecting the shoulder harness fittings for improper bonding on certain Diamond Model H-36 ``Dimona'' sailplanes, and repairing any harness with an improper bond. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Austria. The actions specified by the proposed AD are intended to prevent failure of either the shoulder harness fittings, elevator rib, or the wheel axle to steel support attachment, which could result in passenger injury caused by an inadequate restraint system; reduced sailplane controllability caused by structural damage to the elevator; and/or reduced sailplane controllability during takeoff, landing, and ground operations caused by the installation of incorrect wheel axle screws.

## Notices in this docket

- Feb 13, 1998: Notice of proposed rulemaking (NPRM). (first notice), FR document 98-3638, comments due Mar 17, 1998 (https://www.federalregister.gov/documents/1998/02/13/98-3638/airworthiness-directives-diamond-aircraft-industries-gmbh-models-h-36-dimona-and-hk-36-r-super)

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