Airworthiness Directive

AD 2001-10-08 66 FR 27854 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-12523
Amendment
39-12234
Published
2001-05-21
Effective
2001-07-13
Models covered
1
Last live check
2026-10-02
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.
AD

2001-10-08

FR doc 01-12523 · 66 FR 27854

AD 2001-10-08Published 2001-05-21Effective 2001-07-13

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 you to inspect the airbrake levers in the wing for lower end corrosion and for play in flight direction when fully extended and retracting under load; replace the bearings if there is jamming under load or if corrosion…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Rolladen Schneider Flugzeugbau GmbH (Rolladen Schneider) Models LS 3, LS 4, and LS 6c sailplanes. This AD requires you to inspect the airbrake levers in the wing for lower end corrosion and for play in flight direction when fully extended and retracting under load; replace the bearings if there is jamming under load or if corrosion is found; and adjust the lower lever member (only for the Model LS 3). 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 detect and correct corrosion damage to the airbrake levers and bearings caused by collection of water in the airbrake boxes, not detected during postflight checks. This condition could result in the airbrakes locking in the extended position and a consequent off-field or short landing.

More directives for Rolladen-Schneider LS

  1. AD 86-25-07 R1 Airworthiness Directives; ROLLADEN-SCHNEIDER Flugzeugbau GmbH Model LS6 ... 2011-01-04
  2. AD 2001-01-11 Airworthiness Directives; Rolladen Schneider Flugzeugbau GmbH Models LS ... 2001-01-22
  3. AD 2000-01-06 Airworthiness Directives; Rolladen Schneider Flugzeugbau GmbH Model LS6-... 2000-01-12
  4. AD 98-22-14 Airworthiness Directives; Rolladen Schneider Flugzeugbau GmbH Models LS ... 1998-11-02

All Rolladen-Schneider LS directives

Applies to 1 model in our index