2002-13-04
FR doc 02-16174 · 67 FR 43230AD 2002-13-04Published 2002-06-27Effective 2002-07-12
Requires the same replacement and inspections and adds TCM C-125 and C145 series reciprocating engines to the applicability, which were inadvertently omitted from the emergency AD.
1 correction to this AD FAA · 2002-07-26
Correction published 2002-07-26
- Issued by
- Federal Aviation Administration
- Published
- 2002-07-26
- Document
- Federal Register 02-19035 · Final rule; correction
- Corrects
- the version published June 27, 2002 at 67 FR 43230
This document makes a correction to Airworthiness Directive (AD) 2000-NE-19 applicable to Teledyne Continental Motors O-300, IO- 360, TSIO-360, and LTSIO-520-AE series reciprocating engines that was published in the Federal Register on June 27, 2002 (67 FR 43230). The superseded AD number was inadvertently omitted from the regulatory information, paragraph 2. of Sec. 39.13 [Amended]. This document corrects that omission. In all other respects, the original document remains the same.
A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.
Source: Federal Register document 02-19035, retrieved 2026-08-15
Full official abstract
This amendment supersedes emergency airworthiness directive (AD) 2000-11-51 that was sent previously to all known U.S. owners and operators of Teledyne Continental Motors (TCM) O-300, IO-360, TSIO-360, and LTSIO-520-AE series reciprocating engines. That action required within 10 flight hours after receipt of that AD, replacement of certain magnetos if they fall within the specified serial number range, inspection of the removed magneto to verify that the stop pin is still in place, and, if the stop pin is not in place, inspection of the engine gear train. This amendment requires the same replacement and inspections and adds TCM C-125 and C145 series reciprocating engines to the applicability, which were inadvertently omitted from the emergency AD. This amendment is prompted by reports of engine failures on certain TCM reciprocating engines. The actions specified by this AD are intended to prevent engine failure and loss of control of the airplane due to migration of the magneto impulse coupling stop pin out of the magneto frame and into the gear train of the engine.