AD 96-04-04

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A340 Series Airplanes

AD Number
96-04-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-262-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus A340-211 Airworthiness Directives; Airbus Model A340 Series Airplanes
aircraft Airbus A340-212 Airworthiness Directives; Airbus Model A340 Series Airplanes
aircraft Airbus A340-213 Airworthiness Directives; Airbus Model A340 Series Airplanes
aircraft Airbus A340-311 Airworthiness Directives; Airbus Model A340 Series Airplanes
aircraft Airbus A340-312 Airworthiness Directives; Airbus Model A340 Series Airplanes

Unsafe Condition

Failure of the shortening mechanism pins due to improper grinding of the chrome plating during manufacture, leading to stress corrosion and cracks, which could result in significant reduction of the shock absorber capability or damage to the MLG components, and eventually MLG failure.

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

Required Actions

Conduct repetitive visual inspections to detect corrosion and cracking of the shortening mechanism pins in the main landing gear (MLG), and repair or replace as necessary. Replace the shortening mechanism pin and retraction mechanism pins; forward pintle pin; shortening mechanism bellcrank pin; and bellcrank subassembly of the shortening mechanism, following specified service bulletins.

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

Compliance Time

Initially, inspections must be accomplished before further flight. Replacement actions must be completed in accordance with the referenced service bulletins.

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

Affected Aircraft

Airbus Model A340-211, A340-212, A340-213, A340-311, A340-312 airplanes with shortening mechanism pins, forward pintle pins, shortening mechanism bellcrank pins, or bellcrank subassembly affected by improper chrome plating grinding during manufacture.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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