AD 98-09-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | APEX Aircraft | R3000/160 | Airworthiness Directives; Avions Pierre Robin Model R3000/160 Airplanes. |
Unsafe Condition
Cracks on the flap control shaft and around the welds of the flap levers, which may occur due to fatigued welds, could result in loss of airplane control during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the flap control shaft and welds of the flap levers for cracks in accordance with Avions SB No. 141, Rev. 1. Replace cracked parts if found. Adjust flap travel if no cracks are found. Repeat inspections at intervals not exceeding 500 hours time-in-service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Avions Pierre Robin Model R3000/160 airplanes, all serial numbers.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.