AD 2005-22-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | GROB-WERKE | Model G120A | Airworthiness Directives; GROB-WERKE Model G120A Airplanes |
Unsafe Condition
Chafing of the cables against the rear lip of the tray that holds the switch panels below the left-hand instrument panel, which could result in damage to cable insulation, arcing, and melting of insulation, potentially leading to smoke or fire in the cockpit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for signs of chafing damage to the attachment cables of the switch panels below the left-hand instrument panel, any damaged switch below the switch panels, and any damaged (sharp) edge of the support tray for the attachment cables. Correct any damage found during the inspection and apply a layer of anti-rub (protective padding) strips to the edge of the support tray.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 50 hours time-in-service (TIS) after December 19, 2005 (the effective date of this AD), unless already done.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
GROB-WERKE Model G120A airplanes, all serial numbers, 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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