Airworthiness Directive

AD 96-23-03 61 FR 63704 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-30095
Amendment
39-9826
Published
1996-12-02
Effective
1996-12-17
Models covered
2
Last live check
2026-10-02
This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

96-23-03

FR doc 96-30095 · 61 FR 63704

AD 96-23-03Published 1996-12-02Effective 1996-12-17

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 a maintenance records check to determine if suspect high pressure fuel pumps are installed, and inspection to determine if the high pressure fuel pump has one of the suspect date codes.

Full official abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 96-23-03 that was sent previously to all known U.S. owners and operators of Textron Lycoming IO-320, LIO- 320, AEIO-320, IO- 360, LIO-360, AEIO-360, HIO-360, TO-360, IO-540, O- 540-L, LIO-540, and AEIO-540 series reciprocating engines by individual letters. This AD requires a maintenance records check to determine if suspect high pressure fuel pumps are installed, and inspection to determine if the high pressure fuel pump has one of the suspect date codes. If the high pressure fuel pump has a suspect date code, this AD requires disassembly and inspection of the high pressure fuel pump, and, if necessary, removal from service and replacement with a serviceable part. In addition, this AD requires reporting findings of unserviceable high pressure fuel pumps. This amendment is prompted by reports of inflight failures of high pressure fuel pumps. The actions specified by this AD are intended to prevent an inflight engine failure due to fuel starvation, which could result in a forced landing.

More directives for Lycoming O-320

  1. AD 2022-16-03 Airworthiness Directives; Continental Aerospace Technologies, Inc., Lyco... 2022-07-29
  2. AD 98-02-08 Airworthiness Directives; Certain Textron Lycoming 320 and 360 Series Re... 1998-01-28

All Lycoming O-320 directives

Applies to 2 models in our index