Document Mentions (4 shared documents)

EFTA01326943_sub_002 - EFTA01326943_200

2 mentions1 same-page

Page ?Same page

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

55.0 LT-4001-010 Master Caution Panel 1.3 87.0 Rev. Panel 373-91-3203-1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373-91.3203.3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-BB-E0Y47 AUX BATT (1/2) Annu

EFTA01326943_sub_004 - EFTA01326943_400

2 mentions1 same-page

Page ?Same page

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

55.0 LT-4001-010 Master Caution Panel 1.3 87.0 Rev. Panel 373-91-3203-1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373.91.3203-3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203-9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-BB-E0Y47 AUX BATT (1/2) Annu

EFTA00011669_sub_002 - EFTA00011868

2 mentions1 same-page

Page ?Same page

55.0 LT-4001-010 Master Caution Panel 1.3 87.0 Rev. Panel 373-91-3203.1 Pilot Reversion Panel 0.2 88.0 Rev. Panel 373-91-3203-3 Co-pilot Reversion Panel 0.2 88.0 9-PED 373-91-3203.9 9-Pedestal Panel 1.8 92.89 345-6196 ELT Switch 0.2 88.0 Annunciator Led-42-12-8B-E0Y47 AUX BATT (1/2) Annu