AD 2010-12-51

final rule
Data completeness: 70%

Airworthiness Directives; Agusta S.p.A. (Agusta) Model A119 and AW119 MKII Helicopters

AD Number
2010-12-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-0824
FR Citation
75 FR 53859

Applicability

TypeManufacturerModelDetails
aircraft Agusta S.p.A. (Agusta) Model A119 and AW119 MKII Airworthiness Directives; Agusta S.p.A. (Agusta) Model A119 and AW119 MKII Helicopters

Unsafe Condition

Missing rod bushing in the tail rotor gearbox (TGB) could result in abnormal vibration and damage to the tail rotor system, loss of the yaw control function, and subsequent loss of control of the helicopter.

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

Required Actions

Remove the forward boot from the hub-locking nut and insert a 0.3 mm thickness gauge, not exceeding 10 mm in width, between the tail rotor control rod and nut until the gauge stops. Measure the depth the gauge is inserted between the rod and nut. If the depth is between 4 mm and 6 mm, reidentify the TGB by changing the last three digits of the part number (P/N) from -103 to -105. If the depth is greater than 6 mm, replace the TGB and associated parts with airworthy parts.

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

Compliance Time

Before further flight

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

Affected Aircraft

Agusta S.p.A. Model A119 and AW119 MKII helicopters with the affected tail rotor gearbox (TGB) installed.

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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