Airworthiness Directive

AD 2003-19-10 68 FR 55196 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the fuel boost pump wiring for any chafing, cracked insulation material, or evidence of bare wire(s) (referred to herein as damage), and replace any damaged wiring.

FR document
03-23931
Amendment
39-13313
Published
2003-09-23
Effective
2003-11-07
Models covered
1

Last live check: 2026-10-04

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AD

2003-19-10

FR doc 03-23931 · 68 FR 55196

AD 2003-19-10Published 2003-09-23Effective 2003-11-07

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 you to inspect the fuel boost pump wiring for any chafing, cracked insulation material, or evidence of bare wire(s) (referred to herein as damage), and replace any damaged wiring.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Fairchild Aircraft, Inc. (Fairchild Aircraft) SA226 and SA227 series airplanes. This AD requires you to inspect the fuel boost pump wiring for any chafing, cracked insulation material, or evidence of bare wire(s) (referred to herein as damage), and replace any damaged wiring. This AD also requires you to install protective tubing around the fuel boost pump wiring harness. This AD is the result of reports of chafed fuel boost pump wiring to either the inboard or outboard boost pump wiring. The actions specified by this AD are intended to prevent the fuel boost pump wiring from chafing, which could result in electrical arcing. This could serve as an ignition source inside the fuel tank and result in fire or explosion.

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All Fairchild SA226/SA227 Metro directives

Applies to 1 model in our index