AD 2016-07-26

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Helicopters (previously Eurocopter France)

AD Number
2016-07-26
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-4112
FR Citation
81 FR 21234

Applicability

TypeManufacturerModelDetails
aircraft Airbus Various Airworthiness Directives; Airbus Helicopters (previously Eurocopter France)

Unsafe Condition

Vibration during descent at high speed, which could result in failure of the horizontal stabilizer 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

Revise the airspeed operating limitation in the Limitations section of the Rotorcraft Flight Manual (RFM) to limit VNE to 150 KIAS and add a 1,500 ft/min R/D limitation beyond 140 KIAS. Install one or more self-adhesive placards on the cockpit instrument panel stating the VNE and R/D limitations.

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

Airbus Helicopters (previously Eurocopter France) Model SA-365N, SA-365N1, AS-365N2, and AS 365 N3 helicopters, with specified horizontal stabilizer part numbers, except those with modification 0755B28 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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