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Airworthiness Concern Sheet

Piper Pilot 100i · Type Certificate

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Overview

This Airworthiness Concern Sheet (ACS) issued by the FAA addresses reported instances of un-commanded engine shutdowns during power reduction to idle in aircraft equipped with Lycoming IO-360 engines. The document specifically mentions the Piper Pilot 100i among other aircraft models. It seeks information from operators and maintainers regarding any similar occurrences, detailing the aircraft configuration, flight conditions, and specifics of the rollback events. The FAA has not yet determined the necessary corrective actions, which may include an Airworthiness Directive or a Special Airworthiness Information Bulletin. The document serves as a communication tool for the FAA to gather data and coordinate responses from the aviation community.

  • The document addresses un-commanded engine shutdowns in aircraft with Lycoming IO-360 engines.
  • The Piper Pilot 100i is specifically mentioned as one of the affected models.
  • Operators are requested to provide detailed information about any rollback events experienced.

Document

Source

Originally published by download.aopa.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Type Certificate
Year
2025
Pages
2
File size
125 KB
Publisher
download.aopa.org
Documentation completeness
2/7

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In this document

Airworthiness Concern Description

The FAA has identified a concern regarding un-commanded engine shutdowns, referred to as rollback events, occurring in aircraft with Lycoming IO-360 engines. These shutdowns happen when the throttle is reduced to idle. The concern is particularly noted in the Piper Pilot 100i and other aircraft models.

Request for Information

The FAA requests detailed information from operators regarding any rollback events experienced. This includes specifics about the aircraft configuration, flight conditions during the event, and any findings from post-flight inspections that may have contributed to the shutdown.

Potential Outcomes

The FAA has not yet determined what corrective actions may be necessary. Possible outcomes include issuing an Airworthiness Directive, a Special Airworthiness Information Bulletin, or concluding that no action is needed.

Safety notes

  • Operators should report any instances of engine rollback events to the FAA.
  • Details such as flight conditions and aircraft configuration are critical for evaluation.

Full document text

U.S. Department of Transportation Federal Aviation Administration Airworthiness Concern Sheet Date: December 16, 2025 Reply to: Eastern Certification Branch Name: David Bergeron Title: Engine & Propulsion Aviation Safety Engineer Office: Eastern Certification Branch Street Address: 1701 Columbia Ave. City, State, ZIP: College Park, GA 30337 Telephone: 860-386-1805 Electronic Mail: ECB-COS@faa.gov Make: Lycoming Model / Series: IO-360 Serial Numbers: N/A Reason for Airworthiness Concern: Engine shutdowns during power reduction to idle Federal Aviation Administration (FAA) Description of Airworthiness Concern Operators and Original Equipment Manufacturers have reported instances of un-commanded engine shutdowns on aircraft equipped with Lycoming IO-360 engines and AVStar manufactured vertical and horizontal mounted fuel servos when the throttle was reduced to idle (hereinafter “rollbacks” or “rollback events”). These events have been reported on production and in-service Cessna 172S and 172R as well as the Piper Archer III, Pilot 100i, and Seminole aircraft having IO-360 engines. The FAA is asking operators and maintainers of aircraft with IO-360 engines for information if they have experienced similar issues on their aircraft, regardless of fuel servo manufacturer or installation orientation. Request for Information: The FAA is interested in receiving any information on engine rollback occurrences while on the ground or during any phase of flight. Helpful information may include (but not limited to):  The configuration of the aircraft: o Model and serial number of the aircraft o Total flight hours and cycles on the aircraft and engine since new and overhaul and monthly usage rate o Fuel Servo manufacturer, part number, serial number, time since new, cycles since new, time since overhaul, cycles since overhaul, and installation orientation (horizontal or vertical) o Any installed modifications or replacement parts (e.g. fuel servo related PMA parts, engine STCs, etc.)  The flight conditions during the rollback event: o Phase of flight and maneuvers o Airspeed o Altitude o Weather conditions such as wind speed and direction, or any observed turbulence  Details of the rollback event including the event date, action(s) performed by the pilot, boost pump power state, and the outcome  Post-flight inspection findings after the event that may have contributed to the rollback event, e.g. sources of leakage, condition of parts, frequent idle adjustments, rough running engine, location of visible contamination, engine maintenance performed prior to the event, improper fuel, etc. Please provide any other information you feel may be helpful for us to consider as part of our evaluation. This Airworthiness Concern Sheet (ACS) is intended as a means for FAA Aviation Safety Engineers to coordinate airworthiness concerns with aircraft owners/operators through associations and type clubs. At this time, the FAA has not made a determination on what type of corrective action (if any) should be taken. The resolution of this airworthiness concern could involve Airworthiness Directive (AD) action or a Special Airworthiness Information Bulletin (SAIB), or the FAA could determine that no action is needed at this time. The FAA’s final determination will depend in part on the information received in response to this ACS. The FAA endorses dissemination of this technical information to all manufacturers and requests association and type club comments. Attachments: Service Difficulty Report Accident/Incident Data System Service Letter / Bulletin Special Airworthiness Information Bulletin Federal Aviation Administration or National Transportation Safety Board Safety Recommendation Airworthiness Directive Alternate Means of Compliance Risk Analysis Transmittal: Federal Aviation Administration Airplane Owners and Pilots Association Experimental Aircraft Association Type Club Type Certificate Holder Other: Flight school organizations including National Association of Flight Instructors and Flight School Associations of North America Response Requested By: Emergency (10 days) Alert (30 days) Information (90 days)