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AD FAA-2012-0188

Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes

Summary

We are adopting a new airworthiness directive (AD) for all BAE SYSTEMS (Operations) Limited Model 4101 airplanes. This AD was prompted by reports of cracking found in the wing rear spar. This AD requires a one-time detailed inspection for cracks, corrosion, and other defects of the rear face of the wing rear spar, and repair if necessary. We are issuing this AD to detect and correct cracking in the rear spar, which could propagate to a critical length, possibly affecting the structural integrity of the area and resulting in a fuel tank rupture, with consequent damage to the airplane and possible injury to its occupants.

Directive Details

AD Number

FAA-2012-0188

Document Number

2012-13800

Type

Rule

Publication Date

June 18, 2012

Effective Date

July 23, 2012

Affected Manufacturer

BAE SYSTEMS (Operations) Limited

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2012-0188

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for BAE SYSTEMS (Operations) Limited →

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