MISCELLANEOUS CORRECTIONS TO WING PLANS A. Page 31 Add note under “INSTALLING REAR SPAR” prior to paragraph 18 as follows: Note: Rear spar flanges should be checked and both of them trimmed, if necessary, to obtain a constant .60″ width. B. Page 31 Revise the note following paragraph 35 to Continue Reading
BD Plans Change Notice: PCN 5-4
MANDATORY: ABRASION SHIELD ON AILERON TORQUE TUBE A. Page 411 Before final assembly of the flap and aileron to the wing, abrasion shield A18 should be installed on the aileron torque tube. This shield should be located inside hinge pin F11 of the flap centre hinge bracket to protect the Continue Reading