AD 2008-05-12

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes

AD Number
2008-05-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25658
FR Citation
73 FR 13084

Applicability

TypeManufacturerModelDetails
aircraft Airbus A318 Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes

Unsafe Condition

Wear damage to the inboard flap trunnions after incorporation of the terminating modification could lead to loss of flap surface control, potentially resulting in the flap detaching from the airplane. A detached flap could cause damage to the tail of the airplane.

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

Required Actions

Inspect the inboard flap trunnions for wear marks and the sliding panels for cracking at the long edges. Perform corrective actions if necessary. The inspection type has been changed from repetitive detailed inspections to a different method specified in the AD.

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

Compliance Time

Before further flight

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

Affected Aircraft

Airbus Model A318, A319, A320, and A321 airplanes, including those recently added to the type certificate data sheet.

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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