2026-06459Proposed RuleWallet

FAA Orders Regular Checks on Ontic Airplane Pitch Trim Actuators

Published Date: 4/2/2026

Proposed Rule

Summary

The FAA wants Ontic Engineering and Manufacturing airplane owners to regularly check and fix the pitch trim actuator because some have failed during flight. These inspections and fixes must happen often to keep planes safe, and certain parts can’t be installed unless properly sealed. Comments on this plan are open until May 18, 2026, so owners should prepare for some maintenance costs and deadlines.

Analyzed Economic Effects

4 provisions identified: 0 benefits, 4 costs, 0 mixed.

Mandatory pitch trim actuator inspections

If you operate affected Ontic (formerly M7) SA226/SA227 airplanes with Simmonds-Precision pitch trim actuator P/N DL5040M5, DL5040M6, or DL5040M8, you must inspect the actuator rod ends for cracked, missing, or compromised sealant. The initial inspection must occur within 1,000 flight hours or 6 calendar months since the actuator was put into service, whichever occurs first, or within 30 days after the AD effective date, and you must repetitively inspect and seal every 1,000 flight hours or every 12 calendar months thereafter; measurement of travel time and replacement actions are also required per the service bulletins.

FAA cost estimates for compliance

The FAA estimates this AD would affect 198 U.S.-registered airplanes. The FAA estimates inspection or measurement labor at 3 work-hours × $85/hr = $255 per airplane per inspection/measurement cycle (totaling $50,490 per cycle across U.S. operators). On-condition costs the FAA lists include sealing rod ends (labor 2 work-hours × $85/hr = $170 and parts $319, totaling $489 per actuator) and replacing a pitch trim actuator (labor 5 work-hours × $85/hr = $425 and parts $20,000, totaling $20,425 per actuator).

Installation ban on unsealed actuators

As of the AD effective date, you may not install a pitch trim actuator (the affected parts P/N DL5040M5, DL5040M6, or DL5040M8) unless the sealant on the rod ends is not cracked, missing, or compromised per the inspections required in the AD. This prohibition applies to all affected airplane models in both Group 1 and Group 2.

No special flight permits allowed

The proposed AD states that special flight permits under 14 CFR 21.197 and 21.199 are not allowed for affected airplanes. That means operators cannot rely on special flight permits to ferry affected airplanes for maintenance under this AD.

Your PRIA Score

Score Hidden

Personalized for You

How does this regulation affect your finances?

Sign up for a PRIA Policy Scan to see your personalized alignment score for this federal register document and every other regulation we track. We analyze your financial profile against policy provisions to show you exactly what matters to your wallet.

Free to start

Key Dates

Published Date
Comments Due
4/2/2026
5/18/2026

Department and Agencies

Department
Independent Agency
Agency
Transportation Department
Federal Aviation Administration
Source: View HTML

Related Federal Register Documents

Previous / Next Documents

Back to Federal Register

Take It Personal

Get Your Personalized Policy View

Start a Free Government Policy Watch to see how policy affects your household, then upgrade to PRIA Full Coverage for year-round monitoring.

Already have an account? Sign in