AD 2025-03-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Costruzioni | Aeronautiche Tecnam S.P.A | Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A Airplanes |
Unsafe Condition
The disconnection of a rudder pedals torque tube from one of its hinges could cause the rudder pedals assembly to slip out of its housing resulting in the inability of the flightcrew to maintain the safe flight and landing of the airplane and loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modifying the airplane by installing larger diameter retainer washers on both the left-hand (LH) and right-hand (RH) rudder pedals torque tube hinges, installing new self-locking nuts, doing a functional or operating test of the system to ensure the retaining washers are installed properly, and applying a torque stripe on the LH and RH nuts and bolts threads.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 25 hours time-in-service or 30 days, whichever occurs first after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Costruzioni Aeronautiche Tecnam S.P.A. Model P2010 and P2010 TDI airplanes, except those on which Tecnam Modification MOD2010/359 has been embodied.
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.