AD 2016-07-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A319 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue damage could appear on clips, shear webs, and angles at rear fuselage section 19, on Frame (FR) 72 and FR74.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the clips, shear webs, and angles at rear fuselage section 19, FR72, and FR74. Perform all applicable related investigative actions, including rotating probe testing for fastener hole cracking and high frequency eddy current inspections for stringer cracking. Repair if any cracking is found.
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 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.