ASSEMBLY 1.2 REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF CORROSION IS FOUND (GROUP 1. CONFIGURATION 6) MOS SB 737-53-1316 RI TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WI

ECURITY, WEAR, CHAFFING, AND ETC.. SPECIAL ATTENTION SHOULD BE GIVEN TO THE AIRCRAFT PRIMARY STRUCTURE WITH REGARDS TO FATIGUE AND STRESS CRACKING, CORROSION, AND ETC.. 6. TROUBLESHOOTING INFORMATION: REFERENCE THE ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM MAINTENANCE MANUAL PIN I50-1364-0

ECURITY, WEAR, CHAFFING, AND ETC.. SPECIAL ATTENTION SHOULD BE GIVEN TO THE AIRCRAFT PRIMARY STRUCTURE WITH REGARDS TO FATIGUE AND STRESS CRACKING, CORROSION, AND ETC.. 6. TROUBLESHOOTING INFORMATION: REFERENCE THE ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM MAINTENANCE MANUAL P/N 150-1364-0