AD 2021-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Helicopters Model EC130B4 and EC130T2 | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
a jammed pilot collective pitch lever (collective) that could result in an untimely locking of the collective and subsequent reduced control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 90 hours time-in-service after the effective date of this AD or before the next autorotation training flight, whichever occurs first, remove the protective boot along the collective and measure the clearance between the edge of the collective tab hook (a) and the edge of the low pitch locking pin (b). If the clearance is less than 5 mm (0.196 in), adjust the clearance by following the Accomplishment Instructions, paragraph 3.B.3., of ASB EC130-67A019 and test the collective for proper engagement of the locking pin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 hours time-in-service after the effective date of this AD or before the next autorotation training flight, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Helicopters Model EC130B4 and Model EC130T2 helicopters, 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 4, 2026
Rights: U.S. Government Public Domain
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