AD 2016-02-02

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2016-02-02
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2015-1991
FR Citation
81 FR 4169

Applicability

TypeManufacturerModelDetails
aircraft Airbus A318-111 and -112 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracked cadmium-plated lock nuts that attach the hinge to the fan cowl door, which could result in separation of the hinge from the fan cowl door, in-flight loss of the door, and consequent damage to the airplane.

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

Required Actions

Inspect to determine the serial number of each engine fan cowl door. Inspect for cracking of the hinge lock nuts of any affected door. Replace the lock nuts if necessary.

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

Compliance Time

Within 24 months after the effective date of this AD.

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

Affected Aircraft

Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, and -115 airplanes; Model A320-214 airplanes; and Model A321-111, -112, -211, -212, and -213 airplanes, all manufacturer serial numbers.

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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