AD 98-04-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | A320-111 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A320-211 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A320-212 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A320-214 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A320-231 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A320-232 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A320-233 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A321-111 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A321-112 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
| aircraft | Airbus SAS | A321-131 | Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes |
Unsafe Condition
Possible delays in deceleration when landing with strong cross winds and/or on a contaminated runway, which could increase the potential for landing overrun.
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Required Actions
Activate the spoiler 'phased lift dumping' function by modifying the aircraft wiring at the level of the three spoiler elevator computer (SEC) connectors in accordance with Airbus Service Bulletin A320-27-1088, Revision 03, dated December 11, 1996.
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Compliance Time
Within 12 months after the effective date of this AD
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Affected Aircraft
Airbus Model A320 and A321 series airplanes on which Airbus Modification No. 24745 (Airbus Service Bulletin A320-27-1088, Revision 3, dated December 11, 1996) has not been accomplished, 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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