Term
When is APR activated? How much? What indication? |
|
Definition
N1<67.6% on one engine 2% increase APR icon in N1 guage |
|
|
Term
|
Definition
|
|
Term
|
Definition
N1 - 1 fan, 4 stage turbine N2 - 14 stage compressor, 2 stage turbine |
|
|
Term
What is located on the accessory gearbox? |
|
Definition
Engine lubrication pumps Engine-driven HYD pumps Engine-driven fuel pumps Internal drive AC generator (IDG) Air turbine starter |
|
|
Term
How many ways can the fuel system be shut off? |
|
Definition
Thrust levers - shuts off fuel at FCU FIRE PUSH sw/lt - closes fuel SOV |
|
|
Term
What is the purpose of the engine-driven fuel pump? |
|
Definition
Generates motive flow for scavenge and main ejector pumps |
|
|
Term
What is the function of the ECU? |
|
Definition
Electronic Control Unit (N1 Control Amplifier) Trims FCU output fuel to maintain N1 for a given thrust setting |
|
|
Term
When are the engines under N1 Speed Control? N2? What is controlling? |
|
Definition
N1 Speed Control >79% (N1 Control Amplifier controls N1) N2 Speed Control <79% (FCU hydromechanically controls N2) |
|
|
Term
When is APR armed? How long? What indication? |
|
Definition
N1>79% 5 min "APR ARM" advisory |
|
|
Term
What is APR? When it is functional? How much increase? |
|
Definition
Automatic Performance Reserve System If N1 on one engine drops below 67.6%, the operating engine increases N1 by 2% (500 lbs thrust) |
|
|
Term
How is the engine oil system monitored? What are the warning indications? |
|
Definition
Pressure switch - "L/R ENG OIL PRESS" warning Pressure transmitter - EICAS readout turns red |
|
|
Term
Which bleed air stages extract air? |
|
Definition
7th - pressurization of oil seals, venting of engine sumps in lubrication system 10th - air conditioning, pressurization, engine starting 14th - engine cowl and wing anti-ice, thrust reversers |
|
|
Term
What are the minimum bleed air pressures for start when using the APU? External air? Cross-bleed? |
|
Definition
APU - 40psi External air - 45psi Cross-bleed - 60psi (approx 85% N2) |
|
|
Term
What is the maximum N2 that the Air Turbine Starter can dry motor to? |
|
Definition
|
|
Term
What happens when the "START" sw/lt is pushed? |
|
Definition
Left, right and isolation 10th state bleed air SOVs open Starter Control Valve opens White "START" sw/lt |
|
|
Term
How are Ignition A and B powered? |
|
Definition
A - AC ESS BUS B - Battery Bus through the static inverter |
|
|
Term
What are the three modes of ignition? |
|
Definition
Normal - A or B, ignited from starter engagement to cutout Continuous - A and B Auto-Ignition - Auto-continuous (stall warning computer) |
|
|
Term
Where are engine vibrations detected? What indications are there? |
|
Definition
N1 fan - "FAN VIB" at 2.7 mils N2 core - "VIB" icon in N2 gauge at 1.7 mils |
|
|
Term
Which computers and systems receive information from the thrust levers? |
|
Definition
N1 Control Amplifier FCCs, DCUs Landing gear warning system Takeoff config warning Cabin pressurization Ground spoilers |
|
|
Term
How many types of inflight protection are there for the thrust reversers? |
|
Definition
5 Thrust reverser relays - energized by WOW or wheel spin up Flexshaft lockpin and lockcam - prevents uncommanded travel by more than 1/4" Auto-stow - if lockcam fails, 14th stage engergizes stow solenoid, stows reverser Auto-retard - auto-retards thrust lever whenever thrust reverser is in transit Emergency stow - "UNLK" sw/lt directs PDU to stow unlocked reverser |
|
|
Term
When is the thrust reverser "UNLK" sw/lt illuminated? |
|
Definition
PDU is unlocked Flexshaft lock is released TR not fully stowed In flight, moves 1 1/4" |
|
|
Term
"ENGINE" warning and caution |
|
Definition
Warning - N1, N2, or ITT exceeds limit Caution - N2<57% in flight |
|
|
Term
"L/R ENG OIL PRESS" warning |
|
Definition
|
|
Term
|
Definition
APR has been inadvertantly activated on both engines |
|
|
Term
"REV UNLOCKED" and "REV UNSAFE" cautions |
|
Definition
REV UNLOCKED - moved away from stowed position without a deploy command REV UNSAFE - unarmed TR received a deploy command |
|
|
Term
|
Definition
Engine SOV is closed after activation of ENG FIRE PUSH sw/lt |
|
|
Term
Where are impending oil filter bypass indications provided? |
|
Definition
JB5 electrical box in aft equiptment bay |
|
|
Term
If both engines are started using APU bleed air, what is the limitation for the operating engine's thrust? |
|
Definition
|
|
Term
|
Definition
DCU has different readings for the same engine: N1, N2 - 5% ITT 40° difference |
|
|