AD 95-22-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
| aircraft | Airbus | A320-211 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
| aircraft | Airbus | A320-212 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
| aircraft | Airbus | A320-214 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
| aircraft | Airbus | A320-231 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
| aircraft | Airbus | A320-232 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
| aircraft | Airbus | A320-233 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
Unsafe Condition
Fatigue cracking can occur in the heads of the rear pintle pins of the main landing gears (MLG), which could lead to failure of the pintle pins and consequent collapse of the MLG.
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Required Actions
Replace the rear pintle pin of both main landing gears (MLG) with an improved pintle pin assembly in accordance with Airbus Service Bulletin A320-32-1024. The improved assembly includes thicker heads and walls and an anti-rotation plate.
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Compliance Time
Prior to the accumulation of 20,000 total landings, or at the next overhaul of the main landing gear, whichever occurs first.
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Affected Aircraft
Airbus Model A320 series airplanes as listed in Airbus Service Bulletin A320-32-1024, dated January 29, 1990, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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