Modifications / Certification
MODIFICATIONS FOR "HB-YNA"
ALREADY IMPLEMENTED
Reduce Friction in Elevator Circuit (LAA, Standard Modification SM10366)
Reinforcement of horizontal tail attachment (doublers on fuselage attachment brackets)
Reinforcement of rudder attachment (doubler on fuselage upper hinge)
Reinforcement of nose wheel upper bearing (according to newer drawings Zenair)
Steel plates for sealing of rudder control push-pull-rods through firewall (according to newer drawings Zenair)
Ballstic Recovery System Galaxy GRS6-600
WILL BE IMPLEMENTED SOON
Elevator Deflection Limits (Zenith, März 2008)
L-angles in fuselage aft side panels (according plans CZAW)
Aileron gussets (Zenair/AMD 7.1.2009)
Secondary canopy locking device (Arworthiness Notification, Recreational Aviation Australia)
Aileron balancing weights (according to
UK LAA Mandatory Modifications
)
Reinforcement of main wing center spar/fuselage attachment , rear wing spar fuselage attachment, wing upper main spar, (according to
Zenithair Mandatory Modifications
)
L-angles in wing upper skins (longerons)
CERTIFICATION IN OTHER
COUNTRIES
DAeC Gerätekennblatt Zodiac CH601XL - Ultraleicht (DAeC, Deutschland)
PFA Type Acceptance Data Sheet Zodiac CH601XL - Experimental (LAA, UK)
AIRWORTHINESS DIRECTIVES / SERVICE BULLETINS
Zenithair Important Updates Zodiac XL
Zenair ULM Europe (All Zenair Service Bulletins)
UK LAA Modifications AUG09
SPECIAL LOAD ANALYSIS BY MARTIN POHL
Main Gear Legs CH601XL Comlet
Engine Mount Rotax 912ULS
Installation of Ballistic Recovery System Galaxy GRS6-600
CERTIFICATION DOCUMENTS "HB-YNA"
Project Acceptance EAS HB-YNA
Project Application EAS HB-YNA
51%-FAA-Checklist HB-YNA
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