EFTA01105629.pdf

GULFSTREAM AEROSPACE GIV AIRPLANE FLIGHT MANUAL SECTION 1 LIMITATIONS THE CERTIFICATE AND THE OPERATIONAL LIMITATIONS ARE PART OF THE CONDITIONS OF THE TYPE AND AIRWORTHINESS CERTIFICATE, AND MUST BE COMPLIED WITH AT ALL TIMES, IRRESPECTIVE OF THE TYPE OF OPERATION BEING CONDUCTED. THE PERFORMANCE LIMITATIONS AND INFORMATION PRESENTED IN THE AIRPLANE FLIGHT MANUAL SHOW COMPLIANCE WITH FEDERAL AVIATION REGULATIONS PART 25. THIS AIRPLANE IS TO BE OPERATED IN ACCORDANCE WITH THE LOADING SCHEDULE PROVIDED IN THE SEPARATE AIRPLANE WEIGHT AND BALANCE MANUAL. WEIGHT LIMITATIONS AIRPLANE MAXIMUM MAXIMUM MAXIMUM MAXIMUM SERIAL NUMBER ZERO FUEL RAMP TAKEOFF (1) LANDING (2) 1000 THRU 1213 46,500 lb 73,600 lb 73,200 lb 58,50016 (21,092 kg) (33,385 kg) (33,204 kg) (26,536 kg) 1000 THRU 1213 49,000 lb 73,600 lb 73,20016 (58,50016 ) ASC 61 (22,226 kg) (33,385 kg) (33,204 kg) (26.536 kg) 1000 THRU 1213 49.000 16 75,000 16 74,60016 66.000 lb ASC 190 (22,226 kg) (34,020 kg) (33,838 kg) (29,937 kg) 1214 AND SUBS- 49,00016 75,000 16 74,600 16 66,00016 (22,226 kg) (34,020 kg) (33.838 kg) (29,937 kg) NOTES: (1) Maximum takeoff weight, unless restricted by climb performance, brake energy, or tire speed for approved altitudes and ambient temperature or by field length. See Section 6 for WEIGHT LIMITATIONS. (2) Maximum landing weight, unless restricted by climb requirements. See Section 6 for WEIGHT LIMITATIONS. FAA APPROVED 1-1 30 September 1994 EFTA01105629