giangab
Registered User
Hello all,
I am progressing on my restoration project of a PA18/95.
I wish to ask:
1. what is the tolerance on wing to fuselage triangulation, i.e. The allowable length difference betweeen Left and Right distances measured from each wing tip (nav light bolt on main spar) and rear top of tail fin.
2. Is the vertical fin perfectly on the vertical simmetry plane ... or should it have a side "twist" to compensate for prop wash?
Thanks for helping.
Gian
Sent from my iPhone using SuperCub.Org mobile app
I am progressing on my restoration project of a PA18/95.
I wish to ask:
1. what is the tolerance on wing to fuselage triangulation, i.e. The allowable length difference betweeen Left and Right distances measured from each wing tip (nav light bolt on main spar) and rear top of tail fin.
2. Is the vertical fin perfectly on the vertical simmetry plane ... or should it have a side "twist" to compensate for prop wash?
Thanks for helping.
Gian
Sent from my iPhone using SuperCub.Org mobile app