AD 2001-08-04

final rule
Data completeness: 70%

Airworthiness Directives; Bell Helicopter Textron Inc. Model 205A-1, 205B, 212, 412, 412CF, and 412EP Helicopters

AD Number
2001-08-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-SW-06-AD
FR Citation
66 FR 19850

Applicability

TypeManufacturerModelDetails
aircraft Textron Inc Airworthiness Directives; Bell Helicopter Textron Inc. Model 205A-1, 205B, 212, 412, 412CF, and 412EP Helicopters
aircraft Bell Helicopter Textron Inc Airworthiness Directives; Bell Helicopter Textron Inc. Model 205A-1, 205B, 212, 412, 412CF, and 412EP Helicopters

Unsafe Condition

Failure of the actuator end locking washer, leading to the servo lower piston rotating inside the lower servo head assembly and unthreading from the rod end, causing loss of collective control 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

Inspect the tab on the NAS513-6 locking washer on all applicable actuators for twisting or damage. Replace any twisted or damaged locking washer with an airworthy NAS1193K6C locking device before further flight. Replace all NAS513-6 locking washers with airworthy NAS1193K6C locking devices within 100 hours time-in-service or at the next actuator overhaul, whichever occurs first. Installing an airworthy NAS1193K6C locking device on all actuators constitutes terminating action.

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

Compliance Time

Within 25 hours time-in-service for initial inspection, and within 100 hours time-in-service or at the next actuator overhaul for replacement of all locking washers.

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

Affected Aircraft

Bell Helicopter Textron Inc. Model 205A-1, 205B, 212, 412, 412CF, and 412EP helicopters with specific actuators (P/N 41105950 with HR prefix up to 490, or P/N 41000470 with HR prefix up to 10010) 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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