AD 2007-11-11

Recurring final rule
Data completeness: 80%

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

AD Number
2007-11-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-24983
FR Citation
72 FR 29241

Applicability

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

Unsafe Condition

Cracking in the main landing gear (MLG) sliding tubes, which could result in failure of the sliding tube, loss of one axle, and consequent reduced controllability of the airplane.

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

Required Actions

Inspect both MLG sliding tubes for cracking, including detailed inspections and magnetic particle inspections (MPI). Replace both MLG shock absorbers eventually to terminate repetitive inspection requirements.

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

Compliance Time

Within 10 days for initial inspection; repetitive inspections not to exceed 2,500 flight cycles or 21 months, whichever occurs earlier.

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

Affected Aircraft

All Airbus Model A318, A319, A320, and A321 airplanes.

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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