AD 2006-20-03

final rule
Data completeness: 80%

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

AD Number
2006-20-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-24990
FR Citation
71 FR 56854

Applicability

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

Unsafe Condition

Girt bar disengagement from the floor fitting during deployment tests of slide rafts at the forward passenger doors.

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

Required Actions

Within 200 days after the effective date, perform a general visual inspection to determine if the stiff part of the girt and girt bar position of the forward left-hand and right-hand passenger doors is incorrect. If incorrect, repair before further flight in accordance with Airbus Service Bulletin A320-25-1394, Revision 01.

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

Compliance Time

Within 200 days after the effective date of this AD.

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

Affected Aircraft

Airbus Model A319, A320, and A321 airplanes, certificated in any category, on which Airbus Modification 20233, 25902, or 24365 (installation of slide raft) has been done in production, excluding specific serial numbers listed in the AD.

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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