AD Amdt-39-14429

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 Airplanes

AD Number
Amdt-39-14429
Status
final_rule
Effective Date
Product Category
aircraft
Docket
FAA-2005-23400
FR Citation
70 FR 75932

Applicability

TypeManufacturerModelDetails
aircraft Airbus A320-111 Airworthiness Directives; Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 Airplanes

Unsafe Condition

Failure to install a bonding strip between the water scavenge jet pumps and the rear spar in section 21 could result in an ignition source for fuel vapor in the center wing fuel tank, leading to fire or explosion.

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

Required Actions

Rescind the requirement to install a bonding strip between each of the two water scavenge jet pumps of the center fuel tank and the rear spar in section 21. Operators are no longer required to comply with the previous AD 2005-19-16 due to duplicate actions addressed by subsequent service bulletins.

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

Compliance Time

Effective immediately upon publication (December 22, 2005)

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

Affected Aircraft

Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes not modified with Airbus Modification 25513 in production.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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