airworthiness · Rule · Final rule. · Published 2016-06-07 · Effective 2016-07-12 · 81 FR 36440
Document
Document number
2016-11928
Federal Register citation
81 FR 36440
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fokker Services B.V.
Publication date
2016-06-07
Effective date
2016-07-12
FAA docket
Docket No. FAA-2015-5810
Abstract
We are adopting a new airworthiness directive (AD) for certain Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This AD was prompted by a design review that revealed that a wiring failure, external to the center wing fuel tank, could cause a hot short circuit to a maximum level sensor wire, and result in excessive heating of the maximum level sensor element. This AD requires modifying the wiring of the maximum level sensors in the center wing fuel tank, performing after-installation tests, and corrective action if necessary. This AD also requires revising the airplane maintenance or inspection program to incorporate fuel airworthiness limitation items and critical design configuration control limitations. We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.