Beech 90 Series

TTP B1-L3 ATA 33 Beech 90 Series B2-L3 Lights PTP  Beech 90 Series B1 LOC FOT SGH MEL B2 LOC FOT SGH R/I MEL

TTP B1-L2 ATA 61D Beech 90 Series B2-L3 Propeller  Electronic Control PTP  Beech 90 Series B1 LOC FOT SGH R/I MEL TS B2 LOC FOT SGH R/I MEL TS

  TTP B1-L2 ATA 73A Beech 90 Series B2-L3 FADEC Systems PTP  Beech 90 Series B1 LOC SGH R/I MEL TS B2 LOC FOT SGH R/I MEL TS

 Sys. Operation: Electrical/Fly-by-wire

TTP B1-L2 ATA 42 Beech 90 Series B2-L3 Integrated Modular Avionics PTP  Beech 90 Series B1 LOC B2 LOC FOT SGH R/I MEL TS

TTP B1-L3 ATA 83 Beech 90 Series B2-L1 Accessory Gear Boxes PTP  Beech 90 Series B1 LOC SGH B2

TTP B1-L3 ATA 80 Beech 90 Series B2-L1 Starting  Starting System PTP  Beech 90 Series B1 LOC FOT MEL TS B2

TTP B1-L3 ATA 70B Beech 90 Series B2-L1 Engine Performance PTP  Beech 90 Series B1 TS B2

TTP B1-L3 ATA 70A Beech 90 Series B2-L1 Constructional arrangement and operation The   engine  is d i vided into eight major sections as foll o ws:   1.    Compressor air inlet   2.    Compressor   3.    Com b ustion chamber   4.    Compressor turbine   5.    Po w er turbines   6.    Exhaust   7.    Reduction gearb o x   8.    Accesso r y dr i v e gearb o x   Comp r essor Air Inlet   The compressor air inlet, at the rear of the engine, fo r ms the main air inlet to the g as generator. The inlet includes a circular light all o y casting fo r ming a plenum chamber to all o w air to enter the compresso r . An int e g ral oil tank is pa r t of this assem b l y , immediate l y to the rear of the inlet plenum chambe r . The inlet assem b l ...