AD 2001-01-11

final rule
Data completeness: 70%

Airworthiness Directives; Rolladen Schneider Flugzeugbau GmbH Models LS 4 and LS 4a Sailplanes

AD Number
2001-01-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-CE-75-AD
FR Citation
66 FR 6446

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Rolladen Schneider Flugzeugbau GmbH Models LS 4 and LS 4a Sailplanes

Unsafe Condition

Damage to the airbrake locking bracket caused by asymmetric loads, resulting from improper rigging of the airbrake system, which could lead to cracks in the welding region of the airbrake tube and lateral deformation of the airbrake locking bracket.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the airbrake locking bracket on the rear landing gear box for signs of fatigue (cracks in the paint, paint chips, or cracks in the welding region to the tube) and inspect for proper rigging of the airbrake system. If improper rigging is found, reassemble the airbrake system. If any sign of fatigue is evident, disassemble the airbrake system, obtain a modified airbrake locking bracket from the manufacturer, install this bracket, and accomplish certain adjustments after reassembling the airbrake system. Report any damage found to the FAA.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the next 30 calendar days after the effective date of this AD (March 9, 2001).

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Rolladen Schneider Flugzeugbau GmbH Models LS 4 and LS 4a sailplanes, serial numbers 4000 through 4852, that are certificated in any category.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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