AD 2001-16-14

final rule
Data completeness: 70%

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

AD Number
2001-16-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-138-AD
FR Citation
66 FR 42939

Applicability

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

Unsafe Condition

Failure of the telescopic girt bar of the escape slide/raft assembly to deploy correctly due to an incorrectly machined chamfer, allowing the mechanism to retract and detach from the door sill.

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

Required Actions

Modify the telescopic girt bar by reworking the trigger end and installing a U-shaped reinforcement section. Perform repetitive inspections for discrepancies and functional tests to ensure the girt bar does not retract under specified force. Replace discrepant parts with new ones if issues are found.

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

Compliance Time

Within 18 months after the modification, with repeat inspections at intervals not exceeding 18 months.

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

Affected Aircraft

Airbus Model A319, A320, and A321 series airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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