Airworthiness Directive

AD 91-21-01 R1 61 FR 29003 Active

Federal Aviation Administration · 14 CFR part 39

Requires the upgrade of the engine exhaust system to a new design configuration; and also establishes inspection intervals for engines incorporating the new design configuration, for engines incorporating the design configuration…

FR document
96-14220
Amendment
39-9470
Published
1996-06-07
Effective
1996-06-27
Models covered
1

Last live check: 2026-08-19

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

91-21-01 R1

FR doc 96-14220 · 61 FR 29003

AD 91-21-01 R1Published 1996-06-07Effective 1996-06-27

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 the upgrade of the engine exhaust system to a new design configuration; and also establishes inspection intervals for engines incorporating the new design configuration, for engines incorporating the design configuration required by a previous AD, and for engines not yet incorporating either design configuration.

1 correction to this AD FAA · 1996-09-06

Correction published 1996-09-06

Issued by
Federal Aviation Administration
Published
1996-09-06
Document
Federal Register 96-22773 · Final rule; correction
Corrects
the version published June 7, 1996 at 61 FR 29003

This document makes a correction to Airworthiness Directive (AD) 91-21-01 R1 applicable to Textron Lycoming Model TIO-540-S1AD reciprocating engines that was published in the Federal Register on June 7, 1996 (61 FR 29003). The reference to the New York Aircraft Certification Office in Note 3 following the paragraph describing the procedure for obtaining an alternative method of compliance was omitted. 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 96-22773, retrieved 2026-08-15

Full official abstract

This amendment revises an existing airworthiness directive (AD), applicable to Textron Lycoming Model TIO-540-S1AD reciprocating engines, that currently requires the upgrade of the engine exhaust system to a new design configuration; and also establishes inspection intervals for engines incorporating the new design configuration, for engines incorporating the design configuration required by a previous AD, and for engines not yet incorporating either design configuration. This amendment clarifies that an exhaust system disassembly is not necessary when inspecting the exhaust system after the installation of the new design One-piece Exhaust Riser Kit, and Manifold Retaining Kit. This amendment is prompted by reports from operators requesting clarification of two paragraphs in the compliance section. The actions specified by this AD are intended to prevent cracking or distortion of engine exhaust system flanges, V-band coupling, and pipes, which could result in engine compartment fire and smoke entering the cabin with possible loss to the aircraft.

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All Lycoming O-540 directives

Applies to 1 model in our index