AD 2020-23-06

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Helicopters

AD Number
2020-23-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2020-0652
FR Citation
85 FR 73613

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters Model AS332C Airworthiness Directives; Airbus Helicopters

Unsafe Condition

Incorrect assembly of the main rotor hub, which could result in failure of the main rotor hub components 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 at least one main rotor revolutions per minute (NR) sensor and borescope inspect the phonic wheel lock washer for correct height. If the height is correct, install the NR sensor. If the height is not correct, install the NR sensor and repair or replace the main rotor hub.

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

Compliance Time

Within 55 hours time-in-service

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

Affected Aircraft

Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters with a main rotor hub assembly part number 332A31-0001-00, 332A31-0001-01, 332A31-0001-02, 332A31-0001-03, 332A31-0001-04, 332A31-0001-05, or 332A31-0001-06 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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