Airworthiness Directive

AD 94-20-04 R2 68 FR 25811

Federal Aviation Administration · 14 CFR part 39

FR document
03-11977
Amendment
39-13147
Published
2003-05-14
Models covered
1
Last live check
2026-08-19
AD

94-20-04 R2

FR doc 03-11977 · 68 FR 25811

AD 94-20-04 R2Published 2003-05-14Effective 2003-06-27

Requires ruddervator inspections and modifications on certain Raytheon Aircraft Company (Raytheon) Beech Models C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, and V35B airplanes.

Full official abstract

This amendment revises Airworthiness Directive (AD) 94-20-04 R1, which currently requires ruddervator inspections and modifications on certain Raytheon Aircraft Company (Raytheon) Beech Models C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, and V35B airplanes. This AD maintains the actions of AD 94-20-04 R1, but makes the repetitive visual inspection of the empennage, aft fuselage, and ruddervator control system with any subsequent repair and the setting of the elevator controls, rudder and tab system controls, cable tensions, and rigging a one time action; and adds repetitive inspections of the fuselage bulkheads that were required by AD 94-20- 04. This AD is the result of the need to add a repetitive inspection of the fuselage bulkheads and change other inspections from a repetitive to a one-time action. The actions specified by this AD are intended to prevent structural failure of the V-tail, which could result in loss of control of the airplane.

Applies to 1 model in our index