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215 Cards in this Set
- Front
- Back
Where are the landing, runway turnoff, and taxi light switches?
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Lower edge of forward overhead panel, Captain's side
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Where are the position, anti-collision, wing, wheel well light switches?
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Forward Overhead panel, lower edge, F/O side
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Where is the dome light switch?
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Aft overhead panel
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Turning the EMER EXIT LIGHTS switch to OFF does what?
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Prevents emergency lights system operation if airplane electrical power fails or is turned off
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Turning the EMER EXIT LIGHTS switch to ARMED does what?
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All emergency lights illuminate automatically if: Airplane electrical power fails, or AC Power is turned off
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Turning the EMER EXIT LIGHTS switch to ON does what?
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All emergency lights illuminate
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The emergency exit lights may be illuminated by a switch on the [xxxxx], which will [xxxxx] the flight deck control.
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Aft attendant's panel, override
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How many emergency exits are there and where?
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10 (Two passenger entry doors, two service doors, two flight deck windows, four overwing exits)
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Which exit cannot be opened from outside?
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Captain's window
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Where are the indicators for open entry, service, equip, overwing, and cargo doors?
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Forward overhead panel
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If a door is unlocked or opened, what are the indications?
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Associated indicator light, Doors annunciator light, and MASTER CAUTION
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What is the minimum recommended pavement width for a 180 degree turn (737-800)?
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79 feet
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What does the overwing exit flight lock system do?
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Ensures that flight locks will automatically lock during takeoff, inflight, and landing and unlock on the ground
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How many life vests on the flight deck?
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3
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How many oxygen masks on the flight deck?
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3
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Name the type and quantity of emergency equipment on the flight deck:
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3 life vests, 1 fire extinguisher, 1 PBE, 1 ELT, 1 crash axe, 3 O2 masks
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Where are the PASS OXYGEN system controls?
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Aft Overhead Panel (center)
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What does placing the PASS OXYGEN switch in NORMAL do?
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Masks drop and system activates automatically if cabin altitude >14k'
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What does placing the PASS OXYGEN switch in ON do?
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Activates system and drops mask
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What are indications that PASS OXYGEN system is activated?
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PASS OXY ON light, OVERHEAD annunciator, MASTER CAUTION
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How long does PASS OXYGEN system flow?
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Approximately 12 minutes, cannot be shut off, individual systems at each station
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What does the BLEED TRIP OFF light indicate?
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Excessive engine bleed air temperature or pressure. Related engine bleed air valve closes automatically and must be reset to function.
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How do you regulate cabin temperature?
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Putting selector in AUTO provides automatic temperature control for the associated zone, while rotating toward C (cool) or W (warm) manually sets the desired temperature.
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If you rotate the cabin temperature selector to OFF, what happens?
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Associated trim modulating valve closes.
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Placing the ISOLATION VALVE switch to CLOSE does what?
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Closes isolation valve.
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What will be the position of the Isolation valve if the ISOLATION VALVE switch is placed in AUTO and either engine BLEED air, or AC PACK switch is positioned to OFF?
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OPEN
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What will be the position of the Isolation valve if the ISOLATION VALVE switch is placed in AUTO, both engine BLEED air switches are ON, and both PACK switches are AUTO or HIGH?
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CLOSED
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What will be the position of the Isolation valve if the ISOLATION VALVE switch is placed in AUTO, engine 1 BLEED air switch is in ON, engine 2 BLEED air switch is OFF, and both PACK switches are AUTO?
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OPEN
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What is the position of the isolation valve if any of the four “corner switches” are off, and the ISOLATION VALVE is in AUTO?
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OPEN
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What does pushing the TRIP RESET switch do?
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If fault correction is corrected: 1) Resets BLEED TRIP OFF, PACK, and ZONE TEMP lights, 2) Opens related bleed valve or pack valve, 3) lights remain illuminated until reset
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How is an alert provided if an overtemperature occurs in the E&E bay?
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Crew call horn in nose wheel well
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How is pressurization system controlled with Pressurization mode swith in AUTO?
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Automatically
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How is pressurization system controlled with Pressurization mode swith in ALTN?
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Using the ALTN controller
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How is pressurization system controlled with Pressurization mode swith in MAN?
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Manually by outflow valve switch – both auto controllers are bypassed
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Putting the pressurization system in ______ bypasses both automatic controllers.
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MAN
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At what altitude will the cabin altitude warning horn sound?
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10,000 feet
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How do you silence the cabin altitude warning sound?
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Push the ALT HORN CUTOUT switch
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What does an illuminated left WING-BODY OVERHEAT light indicate?
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Overheat from bleed air duct leak in left engine strut, left inboard wing leading edge, left air conditioning bay, keel beam, or APU bleed air duct.
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What does an illuminated right WING-BODY OVERHEAT light indicate?
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Overheat from bleed air duct leak in right engine strut, right inboard wing leading edge, or right air conditioning bay.
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An overheat in the keel beam or APU bleed air duct will illuminate what light?
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Left WING-BODY OVERHEAT
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Selecting SUPPLY DUCT on the AIR TEMP Source Selector will do what?
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Selects and displays appropriate zone supply duct temperature
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Selecting PASS CAB on the AIR TEMP Source Selector will do what?
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Selects and displays forward or aft passenger cabin temperature
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Selecting PACK on the AIR TEMP Source Selector will do what?
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Selects and displays left or right Pack temperatures
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What has happened if the left or right PACK light illuminates?
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Pack trip off or failure of both primary and standby pack controls for the associated pack.
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During MASTER CAUTION recall, illumination of the left PACK light indicates what?
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Failure of either the primary or standby pack control. Light will extinguish when MASTER CAUTION is reset.
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The CONT CAB light illuminates to indicate what?
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Duct temperature overheat or failure of the flight deck primary and standby temperature control.
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The FWD CAB or AFT CAB light illuminates to indicate:
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Duct temperature overheat
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During MASTER CAUTION recall, CONT CAB indicates:
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Failure of the flight deck primary or standby temperature control
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How can you check if only the primary or the standby temperature control in the flight deck have failed?
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Perform a MASTER CAUTION reset. If CONT CAB illuminates, one of the controls has failed.
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Explain the meaning of an illuminated OFF SCHED DESCENT light:
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The airplane has descended before reaching the planned cruise altitude set in the FLT ALT indicator.
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If you descend before reaching the planned cruise altitude set in the FLT ALT indicator, what will happen?
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OFF SCHED DESCENT light will illuminate.
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If a flight is aborted in climb and returns to the takeoff airport, will the OFF SCHED DESCENT light illuminate?
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No, unless the FLT ALT indicator is changed.
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Turning the TRIM AIR switch to OFF or ON regulates which control?
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The trim air pressure regulating and shutoff valve
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What does the RECIRC FAN do?
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Reduces air conditioning system pack load and engine bleed air demand.
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The RECIRC FAN draws air from the[xxxxx] and [xxxxx] to the [xxxxx], where it is filtered and re-circulated to the [xxxxx].
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Passenger cabin, electrical equipment bay, forward cargo bay, Mix manifold
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An illuminated Equipment Cooling Supply (Exhaust) light indicates:
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No airflow from selected cooling supply (exhaust) fan.
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What indicates that you have configured the air panel in a way that it would be possible to back pressure the APU?
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DUAL BLEED Light
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The DUAL BLEED light observes the APU Bleed [xxxxx] and the Engine Bleed Air [xxxxx].
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Valve, Switches
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Turning the engine and/or APU BLEED Air switches ON will open the associated bleed air valves if [xxxxx].
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The associated engine/APU is operating
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To command maximum flow rate to the pack on the ground, you must:
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Turn PACK and APU BLEED switch ON.
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Placing the WINDOW HEAT Test switch to OVHT does what?
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Simulates an overheat condition.
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Placing the WINDOW HEAT Test switch in PWR TEST does what?
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Provides confidence test to verify operation of system.
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To provide a confidence test to verify operation of the window heat system, place the WINDOW HEAT switch in:
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PWR TEST
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Which equipment is electrically heated with the PROBE HEAT switches ON?
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Pitot probes, TAT probe, Alpha vanes
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Which equipment is NOT heated on the ground unless the TAT Test switch is pushed?
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TAT probe
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Which pitot-static items are NOT heated?
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Static ports
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A bright wing or engine anti-ice light indicates what?
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Related valve in transit, or valve position disagrees with switch
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A dim wing or engine anti-ice light indicates what?
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Related valve is open
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Under which two conditions will the OVERHEAT light on the window heat panel illuminate?
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1) overheat, 2) electrical power to window(s) interrupted
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The PROBE HEAT light indicates [xxxxx]
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The related probe is NOT heated.
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If operating on standby power, probe heat lights...
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...do not indicate system status
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Illumination of the COWL ANTI-ICE light indicates...
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...overpressure condition in duct downstream of cowl anti-ice valve
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Does COWL ANTI-ICE light indicate an overheat?
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No
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Engine anti-ice heats what portion of the engine?
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Engine cowl lip
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What indications do you have that engine anti-ice is in use?
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Green “TAI” is displayed above N1 digital display
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What does an amber “TAI” indication above the N1 display indicate?
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Cowl anti-ice valve is not in commanded position
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What happens during takeoff if wing anti-ice is in use?
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Control valves close if either engine thrust is above takeoff warning setting, or thermal switch is activated in either duct. Switch remains on. At liftoff, switch trips to OFF.
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If both A/Ps are engaged, which FCC is the master?
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The first in CMD, regardless of which F/D is turned on first.
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Which FCC is the master with neither A/P on?
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The first F/D turned on.
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If both Flight Directors have the MA light on, what does this mean?
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Independent F/D operation
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Which roll modes are affected by bank angle selector?
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HDG SEL, VOR
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Moving the Autothrottle (A/T) ARM switch to ARM arms the A/T for engagement in which modes?
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N1, LVL CHG, VNAV, V/S, ALT HLD, and TO/GA
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How do you disengage A/T?
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Move A/T ARM switch to OFF, or push either A/T Disngage Switch
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How may A/T automatically disengage?
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1) 2 sec after landing, 2) 10 degree thrust lever separation (except during t/o), 3) significant thrust difference accompanied by control wheel roll input of 10 degrees or more
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What does a green indication in the FMA represent?
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Engaged or Captured mode
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What does a green box in the FMA indicate?
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Mode change. Lasts for 10 seconds after mode engagement
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What does white text in the FMA indicate?
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Armed modes for each axis.
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What does CMD displayed above the attitude indicator mean?
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One or both autopilots engaged
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What does FD displayed above the attitude indicator mean?
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Flight Director is ON, and autopilot either OFF or engaged in CWS
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What does CWS P displayed above the attitude indicator mean?
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Pitch mode engaged in CWS
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What does CWS R displayed above the attitude indicator mean?
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Roll mode engaged in CWS
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What does SINGLE CH (Amber) displayed above the attitude indicator mean during a single AP ILS approach?
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Turns on after localizer capture throughout approach
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What does SINGLE CH (Amber) displayed above the attitude indicator mean during a dual AP ILS approach?
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Illuminates after localizer capture and extinguishes after pitch monitor confidence test is successfully completed (then goes to CMD)
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When is SINGLE CH (Green) displayed above the attitude indicator?
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During IAN approach after FAC capture until AP disengaged or 100' RA
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If AUTOPILOT flashes in amber above the attitude indicator, what has happened?
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A/P is still engaged below 100' RA for an IAN approach
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What conditions must be met for a second autopilot to be engaged?
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1) Both NAV receivers tuned to ILS, 2) APP Mode Selected, 3) 2nd AP engaged in CMD prior to 800' RA
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Pulling down the A/P DISENGAGE bar does what three things?
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1) Exposes yellow background, 2) Disengages both autopilots, 3) Prevents A/P engagement
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Lifting up the A/P DISENGAGE bar does what two things?
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1) Conceals yellow background, 2) Enables A/P engagement
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What does an amber flashing A/P DISENGAGE light on the forward panel indicate?
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A/P reverted to CWS pitch or roll while in CMD
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What does a red flashing A/P DISENGAGE light on the forward panel indicate?
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A/P disengaged
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What does a red steady A/P DISENGAGE light on the forward panel indicate?
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1) Stab out of trim below 800' RA on dual A/P approach, or 2) ALT ACQ mode inhibited during A/P go-around if stab not trimmed for single A/P ops, or 3) automatic ground system tests fail
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What are the indications of a disengaged Autothrottle?
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Flashing red A/T P/RST light on the forward panel
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What does an amber STAB OUT OF TRIM light on the left forward panel indicate?
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Autopilot not trimming stab properly
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If you select TO/GA below 2000' RA with a single A/P engaged, what will happen?
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A/P disconnects. Requires manual F/D go-around.
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If you select TO/GA below 2000' RA with both A/Ps engaged, what will happen?
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A/P go-around mode is activated. A/Ps remain engaged.
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Pushing TO/GA once during a go-around activates a reduced N1 setting to produce a [xxxxx] fpm rate of climb.
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1000-2000
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Pushing TO/GA twice during a go-around does what?
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Advances A/T to full go-around N1 limit
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What are the three flight mode annunciations above the attitude indicator, from left to right?
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A/T, Roll, Pitch
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N1 in the A/T FMA annunciators means what?
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A/T maintains thrust at selected N1 limit displayed on thrust mode display
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GA in the A/T FMA annunciators means what?
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Reduced go-around setting (one push)
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RETARD in the A/T FMA annunciators means what?
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A/T moving thrust levers to aft stop
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FMC SPD in the A/T FMA annunciators means what?
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A/T maintains speed commanded by FMC
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MCP SPD in the A/T FMA annunciators means what?
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A/T maintains speed set in MCP IAS/MACH display
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THR HOLD in the A/T FMA annunciators means what?
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Thrust lever A/T servoss inhibited. Pilot can set thrust manually
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ARM in the A/T FMA annunciators means what?
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No A/T mode engaged.
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If ARM is displayed in the A/T FMA annunciator, is A/T protection is provided?
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Yes (minimum speed protection)
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TO/GA displayed during T/O in the FMA indicates what?
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TO/GA thrust set
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How do you select TO/GA thrust on the A/T during Takeoff?
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Turn both F/D switches on and push either TO/GA switch
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Selecting TO/GA on the A/T in flight requires what conditions above 2000' Radio Altitude?
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Not in T/O mode, flaps not up or G/S captured
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VNAV SPD in the FMA indicates what?
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AFDS maintains FMC speed displayed in airspeed indicator and/or CDU CLIMB or DESCENT pages
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VNAV PATH in the FMA indicates what?
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AFDS maintains FMC altitude or descent path with pitch commands
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V/S (engaged) in the FMA indicates what?
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Commands pitch to hold selected vertical speed
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How do you engage V/S?
|
Move Vertical Speed thumbwheel
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ALT ACQ in the FMA indicates what?
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Transition maneuver entered automatically during climb to selected MCP altitude
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ALT HOLD in the FMA indicates what?
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Commands pitch to hold MCP selected altitude, or uncorrected baro altitude at which ALT HOLD switch was pressed.
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MCP SPD in the FMA indicates what?
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Pitch commands to maintain IAS/MACH window airspeed/mach
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G/S in the FMA indicates what?
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AFDS follows ILS glideslope
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FLARE (armed) in the FMA indicates what during a dual A/P ILS approach?
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Below 1,500' RA after LOC and G/S Capture. Second A/P couples with flight controls and A/P go-around mode arms
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FLARE (engaged) in the FMA indicates what?
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During a dual-A/P ILS approach, flare engages at 50' RA and accomplishes autoland flare maneuver
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G/P in the FMA indicates what?
|
AFDS follows IAN glidepath
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LNAV in the FMA indicates what?
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AFDS intercepts and tracks active FMC route
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HDG SEL in the FMA indicates what?
|
AFDS turns to and maintains MCP-selected heading
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VOR/LOC in the FMA indicates what?
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AFDS intercepts and captures selected VOR/LOC course
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FAC in the FMA indicates what?
|
AFDS captures/maintains IAN final approach course
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B/CRS in the FMA indicates what?
|
AFDS captures/maintains localizer back-course course
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How do you arm/engage the Integrated Approach Navigation (IAN) modes?
|
Select APP button on MCP
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What FMA roll and pitch indications are present during an ILS approach?
|
VOR/LOC and G/S
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What FMA roll and pitch indications are present during an FMC IAN approach?
|
FAC and G/P
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What FMA roll and pitch indications are present during an ILS without G/S or a LOC approach?
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VOR/LOC and G/P
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What FMA roll and pitch indications are present during an ILS BC approach?
|
B/CRS and G/P
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When will LNAV engage during a go-around from autoland with FLARE arm or engage displayed?
|
400' AGL
|
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During a go-around from autoland with FLARE displayed, what will be the initial roll mode?
|
Track Hold
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During a go-around from an approach, without FLARE displayed/armed, and TO/GA pressed, when will LNAV engage?
|
50' AGL
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Pushing the SPEED switch on the MCP will do what?
|
1) Engage A/T in SPEED mode if compatible with engaged AFDS modes, 2) Illuminate SPEED switch light, and 3) Maintain MCP selected speed
|
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Pushing the SPEED switch on the MCP with the light already illuminated will do what?
|
Deselect SPEED mode, extinguish light, engage A/T in ARM mode
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Pushing the SPD INTV switch on the MCP cycles between which two displays and modes?
|
1) IAS/MACH display unblanked – AFDS maintains selected speed (FMC target speed still displayed). 2) IAS/MACH display blanked – AFDS maintains FMC computed target speed.
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What happens when you push the VNAV switch on the MCP?
|
1) VNAV switch light illuminates, 2) pitch modes annunciates VNAV SPD, VNAV PTCH, 3) A/T mode annunciates FMC SPD, N1, RETARD, or ARM; 4) IAS/MACH display blanks and airspeed cursors positioned to FMC commanded airspeed
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What does pushing the LVL CHG switch on the MCP do?
|
1) LVL CHG switch light illuminates; 2) Pitch mode annunciates MCP SPD for climb or descent; 3) A/T mode N1 for climb or RETARD followed by ARM for descent; 4) IAS/MACH display and airspeed cursors display target speed.
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What does pushing the ALT HLD switch on the MCP do?
|
1) engages ALT HOLD mode; 2) commands pitch to hold uncorrected baro altitude at which switch was pressed; 3) annunciates ALT HOLD and illuminates ALT HLD switch light
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What does pushing and turning the V/S Switch on the MCP do?
|
1) arms/engages V/S command mode; 2) commands pitch to hold vertical speed; 3) engages A/T in speed mode to hold selected airspeed; annunciates V/S in FMA and illuminates V/S switch light
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Pushing the ALT INTV switch during a VNAV climb does what?
|
1) Deletes lowest FMC altitude constraint below selected MCP altitude; 2) if aircraft is currently at FMC altitude constraints, resumes climb if MCP altitude is above current altitude; 3) each press deletes one constraint; if MCP altitude is set above current FMC altitude, FMC altitude resets to MCP altitude.
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How do you decrease the FMC altitude using the ALT INTV switch?
|
You cannot do so.
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If in VNAV cruise with MCP altitude set above FMC cruise altitude, what will pushing ALT INTV do?
|
FMC altitude resets to MCP altitude and aircraft initiates a cruise climb
|
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If in VNAV cruise with MCP altitude set below FMC cruise altitude, what will pushing ALT INTV do?
|
Initiates early descent
|
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If in VNAV descent, what does pushing ALT INTV do?
|
Deletes highest FMC altitude constraint above MCP altitude
|
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If all FMC altitude constraints are deleted during VNAV path descent, what does pushing ALT INTV do?
|
Automatic transition to VNAV speed descent
|
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What does pushing the LNAV switch on the MCP do?
|
Commands AFDS roll to intercept and track active FMC route, annunciates LNAV, and illuminates LNAV switch light
|
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What does pushing the VOR LOC switch on MCP do?
|
Commands AFDS roll to capture and track selected VOR or LOC course, annunciates VOR/LOC, and illuminates VOR LOC switch light
|
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What does pushing HDG SEL switch on MCP do?
|
Engages HDG SEL command mode, commands roll to follow selected heading, annunciates HDG SEL and illuminates HDG SEL switch light
|
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What does pushing CMD ENGAGE A or B switch do?
|
Engages respective A/P; enables all Command modes; displays CMD
|
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If not in approach mode and CMD A is selected, what happens if you push CMD B?
|
A/P B is engaged, A/P A is disengaged
|
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What does pushing CWS A or CWS B switch do?
|
Engages A/P; engages pitch and roll modes in CWS (Control Wheel Steering); displays CWS P and CWS R in FMA
|
|
While in ALT HOLD, you rotate Altitude SEL switch. What happens?
|
Altitude selected in 100' increments; V/S mode is ARMED
|
|
A flashing “A” on the MCP speed display indicates what?
|
Underspeed limiting – commanded speed cannot be reached
|
|
A flashing “8” on the MCP speed display indicates what?
|
Overspeed limiting – commanded speed is above Vmo, Mmo, Landing gear limit, or flap limit
|
|
What does pushing the Changeover (C/O) switch on MCP do?
|
Changes between IAS/MACH
|
|
If you don't push the C/O switch, when does automatic changeover occur?
|
Approximately FL260
|
|
Pushing the N1 switch on the MCP does what?
|
Engages or disengages N1 mode (if compatible with other AFDS modes engaged); illuminates or extinguishes N1 switch; ARMs A/Ts (if N1 deselected)
|
|
What are the cockpit indications of an incoming cabin or ground call?
|
CALL light illuminated with single high tone chime
|
|
What does an illuminated Offside Tuning Light on the RTP indicate?
|
Radio normally associated with this panel is being tuned by another panel, OR, the radio tuning panel is being used to tune a radio not normally associated with this radio tuning panel.
|
|
How do you activate the Oxygen Mask microphone?
|
Opening the O2 mask panel door, or depressing the reset/test switch with the panel door closed.
|
|
The service interphone system provides intercommunication between whom?
|
Flight deck, flight attendants, ground personnel
|
|
How many MIC SELECTOR switches may be selected on any ACP at one time?
|
One
|
|
If the MIC SELECTOR for a system is selected but the Receiver Switch is off, will you hear Transmissions?
|
Yes
|
|
With the RCP ALT-NORM switch in NORM, the ACP operates [xxxxxx]
|
Normally
|
|
With the RCP ALT-NORM switch in ALT, on which radio will the F/O communicate?
|
VHF2
|
|
With the RCP ALT-NORM switch in ALT, on which radio will the Capt communicate?
|
VHF1
|
|
With the RCP ALT-NORM switch in ALT, on which radio will the Observer communicate?
|
VHF1
|
|
Which microphone is not usable in the RCP ALT mode?
|
Handheld microphone
|
|
How can you use the PA system while your RCP is in ALT mode?
|
You cannot
|
|
What does turning the SERVICE INTERPHONE switch to OFF do?
|
Deactivates external jacks
|
|
Switching the GROUND SERVICE switch on the Fwd Attendant's panel ON does what?
|
Connects external power to ground service bus
|
|
What does the blue GRD POWER AVAILABLE light indicate?
|
Ground power connected and meets airplane power quality standards
|
|
What does the blue APU GEN OFF BUS light indicate?
|
APU is running and not powering a bus
|
|
What does a blue GEN OFF BUS light indicate?
|
Associated IDG is not supplying power to the related transfer bus
|
|
Where can you read voltage, frequency, and current (amps)?
|
AC and DC Metering panel (Forward Overhead Panel)
|
|
What does the amber DRIVE light indicate?
|
IDG under-frequency or low oil pressure
|
|
What does the amber TRANSFER BUS OFF light indicate?
|
Related transfer bus not powered
|
|
What does the amber SOURCE OFF light indicate?
|
No source has been manually selected to power the transfer bus, or the manually selected source has been disconnected
|
|
What does the amber BAT DISCHARGE light indicate?
|
With BAT switch ON, excessive battery discharge is detected
|
|
What does the amber TR UNIT light indicate?
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TR Failure
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What does the amber ELEC light indicate?
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Fault in DC or standby power system (ONLY ON GROUND)
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What does the amber STANDBY PWR OFF light indicate?
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One or more of the following busses are unpowered: AC standby, DC standby, Battery
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With fully charged batteries, standby power is available for [xxxxxxxx]
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60 minutes
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The GRD PWR switch is spring-loaded to
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Neutral
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Moving the GRD PWR switch to OFF does what?
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Disconnects ground power from AC transfer busses
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Moving the GRD PWR switch to ON does what?
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Removes previously-connected power from AC busses and connects ground power to AC busses (if ground power is available and correct)
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Using APU power and GRD power simultaneously [xxxxxxxxx]
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Is not possible (selecting one will disconnect the other)
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If neither transfer bus is powered by an IDG, moving an APU GEN switch to ON will...
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...power both AC transfer busses from the APU generator and disconnect external power, if connected
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If both AC transfer busses are powered by an IDG, moving an APU GEN switch to ON will...
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...power the related AC transfer bus from the APU generator, while the other transfer bus will continue to be powered by the IDG
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Which components are powered by the ground service bus?
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Utility outlets, cabin lighting, and battery chargers
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Where is the GROUND SERVICE switch?
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Forward Attendant's panel
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What happens when you turn a GEN switch OFF?
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Disconnects IDG from related AC transfer bus by opening generator circuit breaker
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What happens when you turn a GEN switch ON?
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Disconnects other power source to related AC transfer bus and connects bus to IDG by closing generator circuit breaker
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If the BUS TRANSFER switch is in AUTO, bus tie breakers...
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...Operate automatically to maintain power to AC transfer busses from any operating generator or external power
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How do you isolate AC transfer bus 1 from AC transfer bus 2?
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Move BUS TRANSFER switch to OFF
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Activating the Generator Drive DISCONNECT switch will
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Disconnect IDG if electrical power is avilable and engine start lever is in IDLE
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What two things does turning battery switch to ON perform?
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Provides battery power and provides automatic switching of standby electrical system to battery with loss of normal power.
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What does an amber “REV” indication above the N1 indicator mean?
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Thrust reverser moved from stowed position
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What does a green “REV” indication above the N1 indicator mean?
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Thrust reverser is deployed
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If the EEC detects a rapid rise in EGT or EGT approaches the Start limit, what is happening, what will your indications be, and what action is required?
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Impending hot start. White box surrounding EGT digital readout flashes. EEC automatically turns off ignition and shuts off fuel.
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During a start, the EGT display box and dial turn red. What has happened and what will EEC do?
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EGT exceeded start limit. EEC will turn off ignition and shut off fuel.
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What is a wet start?
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EGT does not rise after start lever is moved to IDLE. EEC will turn off ignition and shut off fuel to engine 15 seconds after start lever moved to IDLE.
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What does the amber REVERSER light on the aft overhead panel indicate?
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Reverser is commanded to stow. Will extinguish approximately 10 seconds later when isolation valve closes.
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If the REVERSER light illuminates for more than 12 seconds, what has happened?
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Malfunction has occurred. MASTER CAUTION and ENG system annunciator light will illuminate
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