Airworthiness Directive

AD 2010-09-04 75 FR 22519 Active

Federal Aviation Administration · 14 CFR part 39

Requires revising the Limitations section of the airplane flight manual to incorporate the procedures necessary to recover from or work around a software anomaly in the FMS.

FR document
2010-9090
Amendment
39-16269
Published
2010-04-29
Effective
2010-05-14
Models covered
1

Last live check: 2026-08-19

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AD

2010-09-04

FR doc 2010-9090 · 75 FR 22519

AD 2010-09-04Published 2010-04-29Effective 2010-05-14

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires revising the Limitations section of the airplane flight manual to incorporate the procedures necessary to recover from or work around a software anomaly in the FMS.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Honeywell International Inc., Primus EPIC and Primus APEX flight management systems (FMS), as installed on the airplanes described above. This AD requires revising the Limitations section of the airplane flight manual to incorporate the procedures necessary to recover from or work around a software anomaly in the FMS. This AD results from discovery of software anomalies which, in certain situations, can cause the FMS to generate misleading navigational guidance to the pilots and to the autopilot system of various airplanes having this same system software. We are issuing this AD to provide the flightcrew with procedures to recover from or work around these software anomalies during flight, which could lead to an airplane departing from its scheduled flight path, and result in possible collision with other aircraft or terrain.

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Applies to 1 model in our index