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90 Cards in this Set
- Front
- Back
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ADR 1(3)(2) pb
Fault: Off: |
Fault: amber with ECAM if a fault is detected in the ADR.
Off: (white) Air data output disconnected. |
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IR 1(3)(2) mode rotary selector
Off: NAV: ATT: |
Off: (white) ADIRU not energized. ADR and IR data not available.
NAV: Normal. Supplies full inertial data. ATT: IR mode supplying only attitude and heading information. |
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IR 1(3)(2) lights
Fault: (steady) Fault: (flashing) ALIGN: (steady) ALIGN: (flashing) |
Fault: (steady) steady amber when the IR is lost.
Fault: (flashing) Flashes amber when attitude and heading information may be recovered in ATT mode. ALIGN: (steady) IR is operating normally in the align mode. ALIGN: (flashing) Flashes white when: (1PAM) 1-IR alignment fault, or 2-No present position entry after 10 mins 3-Difference between position at shutdown and entered position exceeds 1 degree of lat. or long. 4-Aircraft movement |
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ON BAT light
ON BAT: |
ON BAT: one or more IR's is supplied by aircraft battery, or for a few seconds at the beginning of a full alignment. A horn sounds and ADIRU-AVNCS light comes on blue on the EXTERNAL POWER Panel.
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DATA Selector Knob
TK/GS: PPOS: WIND: HDG: STS: |
TK/GS: True Track and groundspeed
PPOS: Present latitude and longitude WIND: True wind direction and speed HDG: True heading and remaining minutes for alignment STS: Action code |
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SYS Selector Knob
OFF: 1(3)(2); |
OFF: Display isn't energized. ADIRS still energized if
associated IR mode rotary selectors aren't off. 1(3)(2): System selected for display |
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FLT CTL Panel
ELAC, SEC, FAC pb's: |
FAULT: amber with an ECAM when a failure is detected. Only the ELAC 1 FAULT light will illuminate during the ELAC power-up test.
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EVAC Panel
COMMAND pb (guarded) ON: In cabin: HORN SHUT OFF pb: |
COMMAND pb: Extinguished during normal operation.
ON: (white) in Flight deck the EVAC light flashes red and horn sounds. In cabin: EVAC light flashes at FWD and AFT attendant panels. Specific Evacuation tone sounds. HORN SHUT OFF pb: Silences the flight deck horn. |
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EVAC Panel
CAPT/CAPT and PURS sw: CAPT sw: |
CAPT/CAPT and PURS sw:Position not used by JetBlue
CAPT sw: The alert may be activated from fight deck or the cabin. If activated from cabin, it will only be apparent in the flight deck for 3 seconds. |
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EMER ELEC PWR Panel
EMER GEN TEST pb (guarded) Pressed: |
Pressed: Maintenance
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EMER ELEC PWR Panel
GEN 1 LINE pb SMOKE: OFF: |
SMOKE: amber with an ECAM/single chime when smoke is detected in the avionics ventilation duct.
OFF: (white) GEN 1 line contactor opens. The AC Bus 1 channel is supplied from GEN 2 through BTC. A separate circuit is energized from Gen 1 for power to one fuel pump in each main tank. |
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RAT & EMER GEN Light
FAULT: |
FAULT: red if the emergency generator is not supplying power when AC BUS 1 and AC BUS 2 aren't powered.
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EMER ELEC PWR Panel
MAN ON pb (guarded) AUTO: Pressed: |
AUTO: The RAT automatically extends if AC BUS 1 and AC BUS 2 are not electrically supplied and the aircraft speed is above 100 knots.
Pressed: Selects manual RAT extension. CAUTION: RAT will deploy even on the ground. Emergency generator coupling occurs a few seconds after the RAT is supplying sufficient pressure to the blue system. |
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GPWS Panel
TERR pb FAULT: OFF: |
FAULT: Illuminates with an ECAM if terrain detection fails.
OFF: (white) Inhibits the database terrain detection function, and keeps the basic GPWS modes 1-5 operative. |
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GPWS Panel
SYS pb FAULT: OFF: |
FAULT: amber with ECAM with mode malfunction
OFF: (white) All basic GPWS alerts selected off. |
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GPWS Panel
G/S MODEpb OFF: |
OFF: (white) Glideslope mode is inhibited.
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GPWS Panel
FLAP MODE pb OFF: |
OFF: (white) Flap mode 4 "TOO LOW FLAPS" is inhibited to avoid nuisance warnings when landing with reduced flaps.
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GPWS Panel
LDG FLAP 3 pb ON: |
ON: (white) Flap mode 4 "TOO LOW FLAPS" is inhibited when FLAPS CONF 3 is selected. ECAM LDG MEMO displays "FLAPS 3" instead of "FLAPS FULL".
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RCDR Panel
GND CTL pb AUTO: ON: |
AUTO: (Extinguished) The CVR FDR are energized when:
1- On the ground for 5 minutes after electrical power established. 2- On the ground after engine start. 3- Continuosly in flight (whether engines on or not) ON: (blue) The CVR and DFDR are energized. |
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RCDR Panel
CVR ERASE pb Pressed (2 seconds): TEST pb: |
Pressed (2 seconds): Erases the CVR tape, and a steady low frequency sounds if aircraft is on the ground with the parking brake is on.
TEST pb: Activates test if the CVR is energized and parking brake is on. A low frequency sounds 4 times. |
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OXYGEN Panel
MASK MAN ON pb (guarded) AUTO: Pressed: |
AUTO: The mask doors are signaled to open automatically when cabin altitude exceeds 14,000 feet.
Pressed: Manually signaled to open. |
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OXYGEN Panel
PASSENGER SYS ON Light: SYS ON: |
PASSENGER SYS ON Light: Extinguished during normal operation.
SYS ON: Illuminates white when the auto or manual signal is activated. |
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OXYGEN Panel
CREW SUPPLY pb: OFF: |
CREW SUPPLY pb: When extinguished, valve is open, supplying low pressure oygen to masks.
OFF: (white) Valve is closed along with an amber OXY on ECAM door page. |
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CALLS Panel
MECH pb Pressed and held Released: |
Pressed and held: COCKPIT CALL illuminates blue on external power panel in the nose L/G bay. Horn sounds.
Released: COCKPIT CALL remains illuminated. COCKPIT CALL and horn can be reset on EXTERNAL POWER panel |
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CALLS Panels
FWD and AFT pb: ALL pb: |
FWD and AFT pb: Illuminates a red light at the corresponding panel. CAPTAIN CALL appears on the corresponding panel with a green light. On low level high/low chime sounds.
ALL pb: All stations respond simultaneously. |
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CALLS Panel
EMER pb sw (guraded) Emergency call from flight deck to cabin: Emergency call from cabin to flight deck: |
Emergency call FD to cabin:
1- CALL: Light flashes amber 2- ON: Light flashes white 3- Pink light flashes at all panels 4- High/low chime 3 times. Emergency call from cabin to FD: 1- White ON and amber CALL lights flash 2- Amber ATT light illuminates on ACP 3- 3 long buzzers sound in FD. System resets when cabin crew hangs up handset. |
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FIRE Panel
AGENT 1(2), and APU pb SQUIB: DISCH: |
SQUIB: (white): Respective system is armed.
DISCH: amber when respective bottle has lost pressure. |
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ENG 1(2) FIRE pb (guarded)
FIRE: Pushed and released: |
ENG 1(2) FIRE pb (guarded) In and extinguished normally.
FIRE: Illuminates red with an ENGINE fire warning active. Pushed and released: pb pops out and sends electrical signal to perform the following: 1-Silences aural fire warning 2-Arms fire extinguisher squibs 3-Closes hydraulic fire valve 4-Closes LP fuel valve and IDG return valve 5-Closes engine bleed valve 6-Closes pack flow control valve 7-Cuts off FADEC power supply 8-Opens the generator line contactor. |
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ENG 1(2) TEST pb
TEST pb: |
1-CRC sounds
2-MASTER WARN lights flash (2) (red) 3-ENG FIRE 1(2) warning on ECAM (red) 4-ENG FIRE pb illuminates (red) 5-SQUIB lights illuminate white if discharge available 6-DISCH lights illuminate amber 7-FIRE light on ENG panel (pedestal) illuminates red |
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FIRE Panel
APU FIRE pb (guarded) FIRE: Pushed and released: |
FIRE: pb illuminates red with APU fire warning.
Pushed and released: pb pops out and sends electrical signal that: 1-Shuts down APU 2- Silences aural warning 3-Arms Squib 4-Closes the LP fuel valve 5-Shuts off APU fuel pump 6-Closes APU bleed valve and X-bleed valve 7-Deactivates the APU generator |
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APU TEST pb
Tests: |
1-CRC
2-MASTER WARN lights flash 3-APU FIRE warning on ECAM 4-APU FIRE pb illuminates red 5-SQUIB light llluminates white 6-DISCH light illuminates amber |
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HYD Panel
ENG 1(2) PUMP pb: FAULT: OFF: |
ENG 1(2) pb: Extinguished during normal operations. Pump pressurizes the system when engine is running.
FAULT: 1-Reservoir low fluid 2-Reservoir overheat 3-Reservoir low air pressure, or 4-Pump low pressure OFF: (white) Pump depressurized. FAULT light goes out when OFF is selected except during overheat. |
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HYD Panel
BLUE ELEC PUMP pb (guarded) AUTO: FAULT: OFF: |
AUTO: (extinguished) If AC power is available, electric pump operates:
1-In flight 2-On the ground if one engine running or the BLUE PUMP OVRD pb is pressed on maintenance panel. FAULT: amber with ECAM if: 1-Reservoir low fluid 2-Reservoir overheat 3-Reservoir low air pressure 4-Pump low pressure 5-Pump overheats OFF: (white) Pump de-energized FAULT light goes out when OFF is selected except during overheat. |
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HYD Panel
YELLOW ELEC PUMP pb: FAULT: ON: |
YELLOW ELEC PUMP pb: Extinguished during normal operations. Pump is off. Pump turns on automatically when lever of cargo door manual selector valve is moved to OPEN or CLOSED.
FAULT: Amber with ECAM if 1-Reservoir low fluid 2-Reservoir overheat 3-Reservoir low air pressure 4-Pump low pressure 5-Pump overheats (The light remains on if overheat is active ON: (white) Electric pump is on. If electrical supply is removed, pump remains off when electrical power is restored. |
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HYD Panel
PTU pb: AUTO: FAULT: OFF: |
AUTO: (extinguished) Bi-directional power transfer unit is armed and both yellow and green electro ydraulic valves are open. Operates automatically with a differential pressure of more than 500 psi between green and yellow systems. PTU is inhibited during first engine start and autoatically tested during second engine start.
FAULT: Illuminates with ECAM if: 1-Green or Yellow reservoir overheats 2-Green or Yellow reservoir has low air pressure 3-Green or Yellow reservoir has low fluid level (FAULT remains on with overheat) OFF: (white) Both Green and Yellow PTU electro hydraulic valves close. Power transfer stops. FAULT light extinguishes when selected OFF, except with overheat. Light goes out when overheat ends. |
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RAT MAN ON pb (guarded)
Guarded: Pressed: |
Guarded: RAT extends automatically if both AC 1 and AC 2 are lost and the airspeed is greater than 100 knots.
Pressed: RAT extends anytime, including on the ground. The RAT will allow restoration of the blue system pressure ONLY!. It does no re-couple electrics! |
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FUEL Panel
L TK PUMPS 1(2), R TK PUMPS 1(2): FAULT: OFF: |
L TK PUMPS 1(2), R TK PUMPS 1(2): Extinguished during normal operation. Pump is on but fuel feeds only when center tank pump delivery pressure drops below threshold.
FAULT: Illuminates amber with ECAM when delivery pressure drops. OFF: (white) Pump is off. |
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CTR TK PUMPS 1(2) pb
FAULT: OFF: |
CTR TK PUMPS 1(2) pb: Extinguished during normal operation. Pumps run if MAN mode is selected on with MODE SEL pb.
FAULT: Illuminates amber with ECAM when delivery pressure drops. OFF: (white) Pump is off. |
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FUEL Panel
MODE SEL pb: AUTO: FAULT: MAN: |
AUTO: (extinguished) Control of the center pumps is automatic when:
1-Center pumps run at engine start for 2 minutes 2-Before or after engine start sequence, if slats are retracted and there is fuel in the center tank. 3-Center pumps stop automatically 5 minutes after center tank low level is reached. FAULT: Amber with ECAM when center tank has more than 550 lbs of fuel and left or right wing tank has less than 11,000 lbs. MAN: (white) Pumps are controlled manually with center tank pb. |
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FUEL Panel
X FEED pb: OPEN: ON: |
X FEED pb: Extinguished during normal operation. Valve closed.
OPEN: Illuminates green when the cross feed valve is fully open. ON: (white) Valve is opening |
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ELECTRICAL Panel
BATT 1(2) indicator: |
BATT 1(2) indicator: Battery voltage
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ELECTRICAL Panel
BATT 1(2) pb sw: FAULT: OFF: (white) |
BATT 1(2) pb sw: Battery charger limiter automatically controls the connection and the disconnection of the corresponding battery to the DC BAT BUS via the battery line contactor.
FAULT: amber with ECAM if there's an internal problem with the battery or the battery charging system. OFF: Battery charger limiter is not operating. OFF light illuminates if the DC BATT BUS is supplied. Hot buses remain supplied. |
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IDG 1(2) pb sw (guarded)
FAULT: |
FAULT: amber with ECAM if:
1-Oil outlet overheats 2-Oil pressure is low. (extinguishes when the IDG is disconnected). |
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ELECTRICAL Panel
GEN 1(2) pb sw: FAULT: OFF: |
GEN 1(2) pb sw: field is energized and the line contactor closes if electrical parameters are normal.
FAULT: amber with ECAM if: 1-Associated GCU trips, or 2-The line contactor opens (except if GEN pb is OFF). OFF: Generatorfield is de-energized and the line contactor opens. The fault circuit is reset. |
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APU GEN pb:
FAULT: OFF: |
APU GEN pb: Generator field is energized and the line contactor closes if electrical parameters are normal.
FAULT: amber with ECAM if: 1-Associated GCU trips, or 2-The line contactor opens (Except if GEN pb is OFF) OFF: Generator field is de-energized and the line contactor opens. The fault circuit is reset. |
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EXT PWR pb
AVAIL: ON: |
AVAIL: green if external power is connected and good. Extinguishes if ON is illuminated or if the external power is disconnected.
ON: Cyan when external power is connected. |
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BUS TIE pb
AUTO: OFF: (white) |
AUTO: BTC will open or close automatically in order to maintain power supply to the AC buses. Generators have priority over external power. External power has priority over the APU.
OFF: Both BTC's are open. |
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AC ESS FEED pb
AC ESS FEED pb: FAULT: ALTN: |
AC ESS FEED pb: AC ESS BUS is being supplied fro AC BUS 1.
FAULT: amber with ECAM when the AC ESS BUS is not powered. ALTN: white if the AC ESS BUS is being supplied from AC BUS 2. |
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GALY & CAB pb
GALY & CAB pb: FAULT: OFF: |
GALY & CAB pb: Main and secondary galleys supplied. In flight with one generator only, will automatically shed main galley.
FAULT: amber with ECAM when load on any generator is more than 100% of rated output. OFF: white when the main galley and secondary galley are not supplied |
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COMMERCIAL pb
OFF: |
OFF: Switches off all aircraft commercial electrical loads. Turns off:
1-cargo and cabin lights 2-galley equipment/lights 3-water and toilet system 4-drain mast ice protection. |
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AIR COND Panel
ENG 1(2) BLEED pb Bleed valve opens if: |
PALES
1-Pressure (upstream) above 8psi. 2-APU Bleed pb is off / APU Bleed Valve closed. 3-Leak (wing or pylon), no overpressure, no overtemp. 4-ENG FIRE pb has not been activated. 5-Start valve (ENG) is closed. |
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AIR COND Panel
ENG 1(2) BLEED pb FAULT: |
VOLVO
1-bleed Valve not closed during engine start. 2-Overheat (bleed air). 3-Leak (wing or engine) on related side. 4-bleed Valve not closed with APU bleed ON. 5-Overpressure downstream of bleed valve. Fault goes out with pb OFF and the fault has disappeared. |
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AIR COND Panel
RAM AIR pb (guarded) ON: |
ON: RAM Air inlet is open if:
1-DITCHING pb is in normal position 2-Cabin differential pressure is less than 1 psi. |
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AIR COND Panel
APU BLEED pb When extinguished, the APU Bleed valve is closed? FAULT: ON: |
FAULT: amber with ECAM if leak detected.
ON: (blue) APU bleed valve selected open. |
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AIR COND Panel
X BLEED selector knob SHUT: AUTO: OPEN: |
SHUT: Closed
AUTO: X bleed valve is open if the APU bleed valve is open. OPEN: Open |
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AIR COND Panel
PACK 1(2) pb Normally automatic) FAULT: OFF: |
FAULT: amber with ECAM when:
1-Pack control valve disagrees with selected position 2-Compressor outlet overheats, or 3-Pack outlet overheats. OFF: Closed |
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AIR COND Panel
HOT AIR pb? FAULT: OFF: |
HOT AIR pb-valve operates hot air pressure autmatically to help regulate temperatures
FAULT: amber with ECAM when overheat detected. Valve and trim air valves close automatically. OFF: (white) Valve and trim air valves close. FAULT is reset. |
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AIR COND Panel
ZONE TEMPERATURE selectors Between what temperatures do the selectors regulate? |
64 Degrees F and 86 degrees F.
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AIRCOND Panel
PACK FLOW selector NORM: |
NORM:
1-Flow is controlled automatically. 2-Can be selected LOW or HIGH 3-HIGH is provided with APU bleed or single pack operation regardless of switch position. |
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PROBE/WINDOW and ANTI ICE Panel
WING pb (Normally closed) FAULT: ON: |
FAULT: amber with ECAM if:
1-Position of A/I valve is not in required position 2-Low pressure ON: (blue) A/I valves open if pneumatic supply available. |
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PROBE/WINDOW and ANTI ICE Panel
ENG 1(2) pb FAULT: ON: |
FAULT: amber with ECAM if position disagrees with selection.
ON: (blue) Valves are open and bleed air available. |
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PROBE/WINDOW HEAT pb
AUTO: ON: |
AUTO:
Automatic if: 1-In flight 2-On ground if one engine running (except TAT probes) ON: (blue) Probes and windows are heated continuously. |
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CABIN PRESS Panel
MAN V/S CTL Toggle: UP: DOWN: |
Toggle: Controls outflow valve with MAN motor if MODE SEL pb is in MAN position
UP: Valve moves towards open DOWN: Valve moves towards closed |
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CABIN PRESS Panel
MODE SEL pb AUTO: FAULT: MAN: |
AUTO: One of two systems controlling outflow valve.
FAULT: amber with ECAM when both CPC's are faulty. MAN: (white) Manual control of the outflow valve by MAN V/S/ CTL. |
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CABIN PRESS Panel
LDG ELEV selector AUTO: -2 to 14: |
AUTO: FMGS data contstructs optimum schedule.
-2 to 14: Pressurization schedule doesn't use FMGS L/E but uses the L/E from selector. |
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CABIN PRESS Panel
DITCHING pb (guarded) ON: |
ON: Closed signal to valves and inlets below the water line:
(ROPE) 1-Ram air inlet 2-Outflow valve (in Auto) 3-Pack flow control valves 4-Extract valves/Avionics Inlet |
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APU Panel
MASTER SW FAULT: ON: |
FAULT: amber with ECAM when auto shutdown occurs
ON: CYAN when selected. Provides electrical power for starting |
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APU Panel
START pb AVAIL: ON: |
AVAIL: Green when APU start is complete (N above 99.5% or 2 seconds after N reaches 95%.
ON: CYAN, signaling APU starter is energized. (N above 99.5% or 2 seconds after N reaches 95%). |
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SIGNS Panel
NO SMOKING ON: AUTO: OFF: |
ON: Turns NO SMOKING and EXIT signs on. (Chime) EMER LT battery charging inhibited.
AUTO: NO SMOKING signs stay lit. EXIT signs illuminate when gear is extended. (Chime) OFF: Turns signs off. (Chime) |
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SIGNS Panel
EMER EXIT LT selector ON: OFF: |
ON:
1-Overhead emergency lights 2-EXIT signs 3-floor proximity/escape path ESPU's not charged in this position and may only last 10 mins. ARM: EXIT and floor lights are illuminateds with loss of normal electrical power. Excessive altitude illuminates exit signs. OFF: Off |
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ENG Panel
ENG MAN START 1(2) pb ON: |
ON: CYAN when selected and the start valve opens if ENG MODE is set to CRANK or START.
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ENG Panel
N1 MODE 1(2) pb ON: |
ON: CYAN when selected. Thrust control reverts from EPR mode to N1 rated mode. Autothrust and Alpha Floor protections are lost.
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VENTILATION Panel
BLOWER pb, EXTRACT pb AUTO: |
AUTO:
1-On the ground before T/O power, system is in open circuit configuration or in the closed configuration when skin temperature is below ground threshold. 2-On the ground after T/O power, and in flight, the ventilation system is in the closed circuit. |
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VENTILATION Panel
BLOWER pb, EXTRACT pb FAULT: In EXTRACT pb, if: |
FAULT: amber in the BLOWER with ECAM if:
(BOSS) 1-Blowing pressure is low 2-Overheats (duct) 3-Supply (Computer) fails 4-Smoke warning activated In EXTRACT pb, if: (ESC) 1-Extract pressure is low 2-Computer power supply fails 3-Smoke warning is activated. |
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VENTILATION Panel
FAULT When either pb is in OVRD: When both pb's are in OVRD: |
When either pb is in OVRD: System goes to closed configuration. Air conditioning system adds ventilation air. (Blower fans stops if the BLOWER pb is in the OVRD position).
When both pb's are in OVRD: Air flows from the airconditioning system then overboard. Extract fan continues to operate. |
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VENTILATION Panel
CAB FANS pb Normally? OFF: |
Normally: automatically
OFF: fans stopped |
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CARGO SMOKE Panel
FWD and AFT lights SMOKE: TEST: |
SMOKE: RED with ECAM when system detects smoke in cargo compartment.
TEST pb: Maintenance function |
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CARGO SMOKE Panel
DISCH lights DISCH 1 or DISCH 2: DISCH AGENT 2 light: DISCH toggle selector: |
DISCH 1 or 2: amber when the bottle has low pressure
DISCH AGENT 2 light: amber 60 minutes after discharge of agent 1. It extinguishes when agen 2 squib is ignited. DISCH toggle selector: Permits discharge of agents 1 or 2 into the respective compartment. |
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MAINTENANCE Panel
OXYGEN TMR RESET pb: FAULT: ON: |
OXY TMR RESET pb: Maintenance uses this to reset control circuit
FAULT: Illuminates when door latch solenoids energized for more than 30 seconds ON: PASSENGER SYS ON light extinguishes |
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MAINTENANCE Panel
SVCE INT OVRD AUTO: ON: |
AUTO: Ground can communicate with crew by means of jacks 10 seconds after landing. Gear must be compressed
ON: Communication possible when gear is not compressed |
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MAINTENANCE Panel
AVIONCS COMPT light? |
AVIONCS COMOPT light? compartment lighting is controlled by door opening
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MAINTENANCE Panel
BLUE PUMP OVRD pb (guarded) ON: |
ON: Blue electric pump is ON if the ELECT PUMP pb on HYD panel is at AUTO.
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MAINTENANCE Panel
LEAK MEASUREMENT VALVES G (B) (Y) (guarded)? OFF: |
LM VALVES G (B) (Y)? electro-hydraulic valve opens to go back to normal hyd supply.
OFF: Off |
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MAINTENANCE Panel
ENG FADEC GND PWR 1(2) (guarded) ON: |
ON: (blue) FADEC has electrical power on the ground if the ENG FIRE pb is no released
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MAINTENANCE Panel
APU AUTO EXTING RESETS: OK: ON: |
RESETS: Resets test ciruit
OK: (amber) Indicates all components are functioning properly ON: (blue) Switch tests the APU FIRE warning automatic extinguishing and shutdown circuits. |
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GLARESHIELD
AUTOLAND light: |
AUTOLAND light: Flashes RED when RA is below 200 ft if:
1-Excessive deviation (LOC or GLIDESLOPE) 2-Failure of both autopilots 3-Failure of LOC transmitters or signal 4-Failure of GLIDESOPE transmitters or signal |
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GLARESHIELD
MASTER WARN pb: |
MASTER WARN pb: Flashes RED for Level 3 warnings accompanied by CRC. Push to extinguish.
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GLARESHIELD
MASTER CAUTION light pb: |
MASTER CAUTION light pb: Steady AMBER for a Level 2 caution and is accompanied by single chime aural caution. Push to extinguish light.
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GLARESHIELD
SIDESTICK PRIORITY light: |
SIDESTICK PRIORITY light: L or R RED in front of pilot losing authority. Accompanied by a "PRIORITY LEFT" or "PRIORITY RIGHT" each time priority is taken.
CAPT and F/O flash green when pilots move bot sidesticks together without either taking priority; it's accompanied by "Dual Inputs" aural warning |
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The following controls will be operated with the direct confirmation of BOTH crewmembers:
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-Retarding Thrust Levers
-Turning off ENG MASTER switches -Pushing ENG FIRE push buttons -Pushing IDG push buttons -Any rotation of ADIRS rotarty switches -Activating a CARGO SMOKE DISCH toggle switches |
