pdf GFA AD 628 Issue 1 Popular
By Tim Shirley Tagged in H201, H201B, H202, H301, H301B 1260 downloads
GFA AD 628 Issue 1.pdf
REPLACEMENT OF RUDDER GIMBAL DRIVE, REAR ACTUATOR ARM
Damage resulting in failure of the actuating arm can be caused by improper lifting of the rear fuselage by the rudder, or following severe rear fuselage damage of the Standard Libelle, Standard Libelle 201 B, H 301 Libelle and H 301 B. The LBA has issued AD-2005-118. Glasflugal-Flugzeugbau has issued Technical Notes No's 301-39 & 201-35 (combined document) and drawing number 301-45-13. These documents form part of this AD.
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