AD 2019-03-12

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Helicopters

AD Number
2019-03-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2018-0694
FR Citation
84 FR 8250

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters Model EC225LP Airworthiness Directives; Airbus Helicopters
aircraft Bell Various Airworthiness Directives; Airbus Helicopters

Unsafe Condition

a jammed bellcrank in a life raft jettison inflation cylinder percussion system (bellcrank). This condition could result in failure of a life raft to release in an emergency and subsequent injury to occupants.

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

Required Actions

Before further flight, and thereafter at intervals not to exceed 6 months: (1) Clean each bellcrank and pivot link and inspect each bellcrank hole for corrosion. If there is any corrosion in a bellcrank hole: (i) Remove the corrosion without exceeding a maximum depth of 0.1 millimeter (0.004 inch). (ii) Clean each pivot link using 400-grain abrasive paper. (iii) Apply corrosion protectant (Alodine 1200 or equivalent) to each bellcrank hole. (2) Lubricate each bellcrank hole with grease before assembling the bellcrank.

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

Compliance Time

Before further flight, and thereafter at intervals not to exceed 6 months

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

Affected Aircraft

Airbus Helicopters Model EC225 LP helicopters with a life raft installed, 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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