What was found
MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA 380 BETWEEN S-8L AND S-9L HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPP ORT BRACKET (REPAIR PER W/C SEQ #1655 FIG 3 STEP 9) REF FLEETCYCLE N/R 9666842 REPAIRED FRAME STA 380 S-7L AND S-8L PER EC/RA # 5311-02160. ADD EMP:U244023 SEE FLEETCYCLE N/R 9666842 FOR ALL WORK ACCOMPLISHED. DIP 53-DIP NEED TERM LIMITS ADDED. SEE FLEETCYCLE N/R 9666842 FOR ALL WORK ACCOMPLISHED. INITIATE A DTA DIP TO -ACCOMPLISH INSPECTION REQUIREMENTS ON OR ADD EMP:U244023 REPAIRED FRAME STA 380 S-7L AND S-8L PER EC/RA # 5311-02160. G TO CONTACT ENGINEERING AFTER 43,000 TOTAL FLIGHT CYCLES BUT BEFORE 44,000 TOTAL FLIGHT CYCLES FOR THE INSPECTION REQUIREMENT BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES. PLANNIN . BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHTY