Epstein Secrets

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 Drawing

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

cement of Pratt & Whitney JT15D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins 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

n: This Aircraft is a standard Beech let 400A with new Williams F144-3AP engines and upgraded avionics with full authority digital engine controls (FADEC) a. Maintenance Program 1. Hawker Beechcraft Maintenance Manual Chapter 5 Rev C22 or later with the exception of the . 1T1SD Engines. 2. Williams

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

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 Drawing

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

cement of Pratt & Whitney JT15D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins F

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

n: This Aircraft is a standard Beech let 400A with new Williams F144-3AP engines and upgraded avionics with full authority digital engine controls (FADEC) a. Maintenance Program 1. Hawker Beechcraft Maintenance Manual Chapter 5 Rev C22 or later with the exception of the .1115D Engines. 2. Williams

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