Epstein Secrets

53 FUSELAGE STRUCTURE Ballast 001 8 Weight Installation E.0: 100, 102 003 C Ballast Weight, Support Structure Assy. E.O.: .002,100 004 NC Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 54 NACELLES & PYLONS • 000- C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 100 D Firewall Rib, Side Engine E.0: 36

General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and operated in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the air

TA 1223 to BSTA 1243 W/L234.06 E.O: 105 STRUCTURE Ballast Weight Installation E.O: 100, 102 Ballast Weight, Support Structure Assy. E.O.: 002,100 Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 e. Chapter 54 NACELLES & PYLONS VA543000• C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 -VA543100 D Firewaii Rib,

eneral Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and opera4-ed in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the air

RUCTURE A530001 B Ballast Weight Instillaticin E.0: 100, 102 VA530003 C Ballast geight, Support Structure Assy. E.O.: 002,100 — VA530004 NC Ballast Weight Instl. STA 312 - 360,E.O.: 002, 100 Chapter 54 NACELLES & PYLONS - ,VA543000 C Main Strut Assy 2, & 5) E.O.:-003 VA543100 D Firewall Rib,.Side Eng

eral Aviation or Air Carrier Operations Inspector. ' 4. This aircraft shall not be flown unless it is maintained and operated in . accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. This aircraft shall contain the platards, markings, etc: required by FAR 91.31. 6. The cognizant FAA office must be