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Airworthiness Directive

AD 95-09-13 60 FR 22496 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-10833
Amendment
39-9217
Published
1995-05-08
Effective
1995-06-14
Models covered
5
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/95-09-13 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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.

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AD

95-09-13

FR doc 95-10833 · 60 FR 22496

AD 95-09-13Published 1995-05-08Effective 1995-06-14

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 repetitively inspecting each fuel inlet float valve in accordance with certain test procedures on Cessna Aircraft Company (Cessna) Models T303, 402C, 404, 414A, and 421C airplanes, and replacing any valve that does not…

Full official abstract

This amendment supersedes AD 93-05-03, which currently requires repetitively inspecting each fuel inlet float valve in accordance with certain test procedures on Cessna Aircraft Company (Cessna) Models T303, 402C, 404, 414A, and 421C airplanes, and replacing any valve that does not pass this test. The manufacturer has developed fuel inlet float valves of improved design, and the Federal Aviation Administration (FAA) has determined that the improved valves should be installed to reduce the number of repetitive tests currently required by AD 93-05-03. This action requires installing these fuel inlet float valves of improved design. The actions specified by this AD are intended to prevent possible loss of engine power caused by failure of a fuel inlet float valve.

More directives for Cessna 303 Crusader

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  2. AD 2008-26-10 Airworthiness Directives; Cessna Aircraft Company 172, 175, 177, 180, 18... 2008-12-24
  3. AD 2008-10-02 Airworthiness Directives; Cessna Aircraft Company 172, 175, 180, 182, 18... 2008-05-02
  4. AD 2000-01-16 Airworthiness Directives; Cessna Aircraft Company 300 and 400 Series Air... 2000-01-19
  5. AD 98-04-28 Airworthiness Directives; Cessna Aircraft Company Models T303, 310R, T31... 1998-02-17

All Cessna 303 Crusader directives

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Applies to 5 models in our index