ENGINE

Pratt & Whitney  PW545A

Takeoff Thrusy 3,804 lbs

@ 83°F sea level

(limited to 5 minutes)

3,767 pounds of thrust continuous

Bypass Ratio: 4.0:1

* XLS

Pratt & Whitney PW545B

Takeoff Thrust 3,990 lbs

Bypass Ratio  3.8:1

  Intake and Fan

  Compressor

  Combustion

  Turbine

  Exhaust

  Accessories

11 Fuel Nozzles

2  Ignitor Plugs

  (4 & 8 o'clock)

8  Thermocouples

Turbine Section

Single High-Pressure

Two Low-Pressure

Accessory Section

   Fuel Pump

   Oil Pump

   Hydraulic Pump

   Fuel Control

   Starter/Generator

OIL:

Check 10 min. after engine shutdown

1 QT over 10 hour period

May mix 2 quarts of different oil, limit of 400 hours operation before flush and refill.

THRUST REVERSERS:

Idle Reverse @ 60 KIAS

(Stowed at 40 KIAS - NJA SOP)

Limited to 30 seconds with the APU operating

Max setting limited to

75% T/O Power

FIRE LIGHT ON:

When ENG FIRE Light Pushed:

Fuel Firewall Valve - Closed

Hyd Firewall Valve - Closed

T/R Isolation Valve - Closed

Field Relay - Open

Squibbs - Armed

Exxon Turbo Oil 2380

Only Oil  used by EJA

Ignition Automatically Comes ON :

1. Start

2. Engine Anti- Ice Switch On

3. Available with EMER BUS when placed in Second position

Ground Idle: 48-51% N2

Flight Idle:    57-62% N2

Bleed Off Valve (BOV):

Bleeds off excessive P2.8 air, preventing compressor stalls.

Electrically controlled; reverts to pneumatic mode with loss of EEC inputs.

EEC:

Electronic Engine Control

EEC Manual - Light On

EEC Auto - Light On Until Airborne

EEC Auto - Light On 8  secs. after takeoff

EEC Does Not Sync the engines, but enables the switch.

TTO Probe  10 O'Clock

(heated by design)

(temp input for FCU)

TO  Probe     12 O'Clock

(electric heat)

(EEC/RAT Input from right engine)

T1  Probe 1  O'Clock

(heated by cont. bleed air)

(ITT)

* Select TCAS to TA ONLY during Single Engine Operations. TCAS Resolution Advisory (RA) maneuvers are  predicated on Two Engine Performance. (AFM/TCAS)