Epstein Secrets

echcraft Corporation 400A airplane, to replace Pratt & Whitney JT15D-5 series engines with Williams International F344-3AP engines (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems (Coatis. A) and (/or) the installation of Nextant Wingless (Config. B), in accordance with Nextant Aerospace Master D

Regulations effective December 1, 1969, as amended by 36.1 through 36.17; SPAR 27 effective February 1. 1974. as amended by 27-1 through 27-5; and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45.000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and

taVere?-4 1.91". 93kter Virverpt Replacement of Pratt &. Whitney ITI5D-5 series engine with Williams International FI44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-00I, Revision RI. dated 8/22/2011, or later F

Regulations effecliye December 1, 1969, as amended by 36-1 through 36-17; SPAR 27 effective February 1, 1974, as amended by 27-I through 27-5; and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45,000 feel), and Special Conditions No. 25-ANM-33 dated June I8, 1990 (Lightning and

400A alel;a4S• arb glvisw Mir Replacement of Pratt & Whitney 11-1510-5 series engine with Williams International F.144-3M' engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-001, Revision IR dated 8/22/2011, or later FA

n Regulations effective December 1, 1969, as amended by 36.1 through 36-17; SPAR 27 effective Febmary I, 1974, as amended by 27-1 through 27-5; and Special Conditions No. 25-ANM-32 dated Febmary 22, 1990 (High Altitude Operation at 45,000 fed), and Special Conditions No. 25•ANNI-33 dated here 18, 1990 (Lightning and

eechcraft Corporation 400A airplane, to replace Pratt Whitney JT15D-5 series engines with Williams International F.144-3AP engines (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems (Config. A) and (tor) the installation of Nextarrt Winglets (Config. B), in accordance with Nextant Aerospace Master

Regulations effective December 1, 1969, as amended by 36-1 through 36.17; SFAR 27 effective February 1. 1974. as amended by 27-1 through 27.5; and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45,000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and

t 400A Nvo*afeiis ifira Our Meir Replacement of Pratt &, Whitney 5D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-001, Revision 1R dated 8/22/2011, or later FA

Regulations effective December 1, 1969, as amended by 36-1 through 36-17; SPAR 27 effective February 1, 1974, as amended by 27-I through 27-5: and Special Conditions No. 25-ANM-32 dated February 22, 1990 (High Altitude Operation at 45,000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and

Stverfer4kn gam Ylis t refe.wyn. Replacement of Pratt & Whitney JT15D-5 series engine with Williams International F144.3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems, in accordance with Nextant Aerospace Master Drawing List No.: MDL-NXT-001, Revision IR dated 8/22/2011, or later FA

n Regulations effective December 1, 1969, as amended by 36-1 through 36-17; SPAR 27 effective Febmary 1, 1974, as amended by 27.1 through 27-5; and Special Conditions No. 25-ANM-32 dated Febmary 22, 1990 (High Altitude Operation at 45,000 feet), and Special Conditions No. 25-ANM-33 dated June 18, 1990 (Lightning and