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.

004, 005, Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.O.: .101, 103 Fuselage Skin E.O.: 106, 114A, 114, 116 Intercostal Assy - BSTA 1223 lo BSTA 1243 W/L244.39 E.0: 106- Intercostal Any - BSTA 1223 to BSTA 1243 W/L234.06 E.0: 105 STRUCTURE Ballast Weight Installation E.0: 100, 1

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

ead Reinforcement Sect. 48-727 E.O.: 101, 102 200 C Frame Assy Sta 1263 E.O.: 101, 103 300 C Fuselage Skin E.O.: 106s 114A, 114, 116 324' NC Intercostal Assy - BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 325 NC Intercostal Assy - BSTA 1223 to BSTA 1243 II/L234.06 E.0: 105 53 FUSELAGE STRUCTURE Ballast 001 8

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

0004 - NC Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.0.:.101, 103 Fuselage Skin E.O.: 106, 114A, 114, 116 Intercostal Assy - BSTA 1223-to BSTA 1243 W/L244.39 E.0: 106, Intercostal Assy - BSTA 1223 to BSTA 1243 W/L234.06 E.O: 105 STRUCTURE Ballast Weight Installation E.O: 100,