What was found
ON OCTOBER 11 A CART COLLIDED WITH THE AIRCRAFT. IT MADE A HOLE IN THE AIRCRAFT FOUR FEET AFT OF THE AC POWER PLUG. THE BS 328 FRAME WEB AND FAIL-SAFE CHORD WERE BUCKLED AND CRACKED ALONG A 12 INCH SECTION ADJ TO STRINGER 22R. THE FUSELAGE SKIN WAS PUNCTURED AND CRACKED LENGTHWISE BETWEEN BS 301 AND 341 AND CIRCUMFERENTIALLY BETWEEN WL 162 AND 173. *S/D* THE FRAME WEB WAS REPAIRED IN ACCORDANCE WITH 727 SRM 53-10-4, FIGURES 1 AND 11. THE FAIL-SAFE CHORD WAS REPAIRED PER 727 SRM 51-40-3, FIGURE 1. A REPAIR DOUBLER WAS INSTALLED EXTERNALLY IN ACCORDANCE WITH 727 SRM 53-30-3, FIGURE 3.