AD 95-22-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; AIRBUS Model A320 Airplanes |
| aircraft | Airbus | A320-211 | Airworthiness Directives; AIRBUS Model A320 Airplanes |
| aircraft | Airbus | A320-212 | Airworthiness Directives; AIRBUS Model A320 Airplanes |
| aircraft | Airbus | A320-214 | Airworthiness Directives; AIRBUS Model A320 Airplanes |
| aircraft | Airbus | A320-231 | Airworthiness Directives; AIRBUS Model A320 Airplanes |
| aircraft | Airbus | A320-232 | Airworthiness Directives; AIRBUS Model A320 Airplanes |
| aircraft | Airbus | A320-233 | Airworthiness Directives; AIRBUS Model A320 Airplanes |
Unsafe Condition
Fatigue cracking in fuselage frame 20 between stringers 30 and 32 could adversely affect the structural integrity of this area of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Reinforce the left fuselage frame 20 between stringers 30 and 32 in accordance with Airbus Service Bulletin A320-53-1017, Revision 1. Alternative methods of compliance may be approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 14,000 total landings, or within 6 months after the effective date of this AD, whichever occurs later
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Affected Aircraft
AIRBUS Model A320 airplanes with manufacturer's serial numbers (MSN) 006, 008, 011, 017, 018, 039, 042, 045, 046, and 047
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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