AD 2006-24-06

final rule
Data completeness: 80%

Airworthiness Directives; Stemme GmbH & Co. AG Model STEMME S10-VT Sailplanes

AD Number
2006-24-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-24956
FR Citation
71 FR 68997

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Stemme GmbH & Co. AG Model STEMME S10-VT Sailplanes

Unsafe Condition

Ripped pressure lines between Airbox-Carburetor-Differential fuel pressure sensor, potentially caused by incomplete temperature resistance.

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

Required Actions

Inspect all 0.15 - 0.27 inch (4 x 7mm) pressure lines for porousness or cracks in specific areas. Replace all affected pressure lines with ROTAX part number 860 660 or Stemme P/N HZ-KLS041 (or FAA-approved equivalents) following Service Bulletin A31-10-73.

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

Compliance Time

Within 30 days after the effective date of this AD.

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

Affected Aircraft

Stemme GmbH & Co. AG Model STEMME S10-VT sailplanes, serial numbers 11-89 through 11-096, and all serial numbers where pressure lines were replaced between July 27, 2004, and June 22, 2005, inclusive, with parts provided by Stemme GmbH & Co. AG.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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