Epstein Secrets

aintenance instructions to ensure continued airworthiness any time the above equipment Is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded JAW the prescribed loading' Information from the manufacturer.

D TO MODIFICATION • B. Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989. Subject: Fuselage - Station 1182 Pressure Bulkhead web, Crack Repair and Preventive Modification • C. D. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Man

istrator on request. II. All.work Performed utilizing acceptable methods; techniques, and practices per AC 43.13-1A. . , III. Aircraft weighed.. Weight and Balance amended. • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246945 EFTA01331408 1Litat IMMPOILIOCIPI a ( FOSNIa AvIA110

ded to modification. B. Boeing 727 Service Bullekln 127-53A0171, dated December 14, 1989. Subject: Fuselage - Station 1182 Pressure Bulkhead Web, Crack Repair and Preventive Modification EXHAUST Engine Strut controls Instl. E.O.: 002 Flt Deck Indicator Instl. T/R Sys. E.0.• 003, 004 Thrust Reverser Sys

aintenance instructions to ensure continued airworthiness any time the above equipment is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded IAW the prescribed loading information from the manufacturer. E

ADDED TO MODIFICATION Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989 SUbject: Fuselage - Station 1182 Pressare Bulkhead web, . Crack Repair and Preventive Modification • • . . , C.. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Ba