Airworthiness Directive

AD 98-26-05 63 FR 69999

Federal Aviation Administration · 14 CFR part 39

FR document
98-33244
Amendment
39-10946
Published
1998-12-18
Models covered
1
Last live check
2026-08-17
AD

98-26-05

FR doc 98-33244 · 63 FR 69999

AD 98-26-05Published 1998-12-18Effective 1999-01-29

Requires repetitively inspecting (using visual methods) the internal and external surfaces of the brake torque tube assemblies in the cockpit area for cracks.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all British Aerospace (Operations) Limited (British Aerospace) Model B.121 Series 1, 2, and 3 airplanes. This AD requires repetitively inspecting (using visual methods) the internal and external surfaces of the brake torque tube assemblies in the cockpit area for cracks. This AD also requires obtaining and incorporating repair procedures for any brake torque tube assembly found cracked. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by this AD are intended to detect and correct cracks in the brake torque tube assemblies, which could result in reduced brake efficiency with possible reduced and/or loss of airplane control.

Applies to 1 model in our index