load analysis will be performed to determine that the known current aircraft configuration is reflected. All data will be cross-referenced against Major Repair and Alteration FAA Form 337 found and the avionics inventory. Subject matter and date of Form 337 and any related Supplemental Type Certificates (Sits) numbers wil

l load analysis will be performed to determine that the known current aircraft configuration is reflected. All data will be cross-referenced against Major Repair and Alteration FAA Form 377 found and the avionics inventory. Subject matter and date of Form 337 and any related Supplemental Type Certificates (STC's) numbers w

s Auwonnin ' Cgicallis FAlit73 - . cadres willi::. (Oligtnal Allacht(11 V D. Current Weight and Balance InlosmatiOn Available in Aircraft . E, Major Repair and Alteration. FAA Forni 337 (Alraeh When iiquoitcli J. Current AnwortAiness nificat I's in Accordencesvah . ... . . . 1 1 FAR :2 11 .. 1 . ) • /Copy i