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Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes

airworthiness · Rule · Final rule. · Published 2008-04-14 · Effective 2008-05-19 · 73 FR 19979

Document

Document number
E8-7294
Federal Register citation
73 FR 19979
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440)
Publication date
2008-04-14
Effective date
2008-05-19
FAA docket
Docket No. FAA-2008-0047

Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 400) airplanes. That AD currently requires revising the airworthiness limitations section of the Instructions for Continued Airworthiness of the maintenance requirements manual (MRM) by incorporating procedures for repetitive functional tests of the pilot input lever of the pitch feel simulator (PFS) units. That AD also requires new repetitive functional tests of the pilot input lever of the PFS unit, and corrective actions if necessary; and after initiating the new tests, requires removal of the existing procedures for the repetitive functional tests from the MRM. This new AD requires revised procedures for the functional tests. This AD results from a report that the shear pin located in the input lever of two PFS units failed due to fatigue. We are issuing this AD to prevent undetected failure of the shear pins of both PFS units simultaneously, which could result in loss of pitch feel forces and consequent reduced control of the airplane.

Source

Authoritative
Federal Register document
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