Dornier_328Jet-Landing_Gear
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Main Landing Gear Assembly (LH Side Shown)Dornier 328Jet - Landing GearPage 1Main Gear Door Assembly (LH Side Shown)Dornier 328Jet - Landing Gear
Page 2Nose Landing Gear AssemblyDornier 328Jet - Landing Gear
Page 3Landing Gear Control LeverDornier 328Jet - Landing Gear
Page 4Nose Wheel Steering/BrakesDornier 328Jet - Landing Gear
Page 5Emergency Extension LeverDornier 328Jet - Landing Gear
Page 6Park Brake LeverDornier 328Jet - Landing Gear
Page 7NWS ButtonDornier 328Jet - Landing Gear
Page 8MESSAGE (SYNOPTIC)WARNINHIBITLocation(COLOR)TONECONDITION123
ALT ANTI SKID DEGRCAS Field(AMBER)X
ALT ANTI SKID DEGRAlternate anti–skid protection is lost on one main wheel.
HYDR Page(AMBER)ALT ANTI SKID FAILCAS Field(AMBER)X
ALT ANTI SKID FAILAlternate anti–skid system failure.
HYDR Page(AMBER)ALT BRK FAILCAS Field(AMBER)Norm BRK SymbolAlternate brake system not pressurized when expected.
HYDR PageALT BRK ONCAS Field(BLUE)ALT BRK SymbolAlternate brake system is pressurized as expected.
HYDR PageBRK COV FAILCAS Field(AMBER)BRK COV FAILChangeover valve position is uncertain.
HYDR Page(AMBER)BRK MAINTCAS Field(AMBER)One or more brake temps exceeded 4150C.XX
BRK TEMP FAILCAS Field(AMBER)One or more brake temps are invalid
XX
BRK TEMP FAIL (out of range sensor or BTMS failure).HYDR Page(AMBER)BRK TEMP HIGHCAS Field(AMBER)0
XX
BRK TEMP HIGHOne or more brake temperatures or trends are above 225 C.
HYDR Page(AMBER)
Message inhibit logic:1. WOW, Engines off and Electrical Bus Failure refer to section 12–31–17–042. Takeoff phase3. Landing phase
CAS Field and System Messages (Sheet 1 of 4)
Dornier 328Jet - Landing GearPage 9MESSAGE (SYNOPTIC)WARNINHIBITLocation(COLOR)TONECONDITION123
E/P–BRK ACCU PRSSCAS Field(AMBER)XX
E/P–BRK ACCU PRSSIlluminates when the accumulator has low hydraulic pressure.
HYDR Page(AMBER)LDG EMG ACTIVATEDCAS Field(AMBER)Illuminates when the emergency extension lever is pulled to extend
XX
ACTIVATEDposition.HYDR Page(AMBER)
NORM ANTI SKID DEGRCAS Field(AMBER)X
NORM ANTI SKID DEGRNormal anti–skid protection is lost on one main wheel.
HYDR Page(AMBER)NORM ANTI SKID FAILCAS Field(AMBER)X
NORM ANTI SKID FAILNormal anti–skid system failure.
HYDR Page(AMBER)NORM BRK FAILCAS Field(AMBER)X
NORM BRK FAILNormal brakes are not pressurized when expected.
HYDR Page(BLUE)NWS BYPASS FAILCAS Field(AMBER)XX
NWS BYPASS FAILBypass valve is not in the commanded position.
HYDR Page(AMBER)NWS FAILCAS Field(AMBER)NWS control unit detected a failure or NWS ECU not energized or NLG
XX
NWS FAILnot down locked.HYDR Page(AMBER)
NWS HIGHIlluminates when the NWS is selected to HIGH authority and T/O power
CAS Field(AMBER)is selected orif NWS is selected to HIGH authority and in flight.
Message inhibit logic:1. WOW, Engines off and Electrical Bus Failure refer to section 12–31–17–042. Takeoff phase3. Landing phase
CAS Field and System Messages (Sheet 2 of 4)
Dornier 328Jet - Landing GearPage 10MESSAGE (SYNOPTIC)WARNINHIBITLocation(COLOR)TONECONDITION123
NWS HIGHCAS Field(BLUE)Illuminates when the NWS is selected to HIGH authority and WOW
and T/O power is not selected.
NWS INOPCAS Field(BLUE)X
NWS INOPNLG down and locked and NWS manually switched off.
HYDR Page(BLUE)NWS PWR UP FAILNWS selector valve power on is more than 350 msec after NMS–ECU
CAS Field(AMBER)power on.XX
P–BRK ONCAS Field(AMBER)Park brake applied and T/O power is selected.X
P–BRK ONCAS Field(BLUE)P–BRK ONPark brake applied.
HYDR Page(BLUE)P–BRK OFFHYDR Page(BLUE)Park brake released.
PROXI ARINC FAILTotal failure of both PROXI ARINC buses
CAS Field(AMBER)XX
PROXI BYPASS FAILNWS bypass valve PROXI sensor has failed.
HYDR Page(AMBER)
PROXI LOCK FAILUplock or downlock failure detected by PSEU. Any single uplock, NLG
HYDR Page(AMBER)downlock, or combination of two main landing downlock sensor failures,or any combination of two NLG downlock discrete outputs fail.
PROXI MLG WOW FAILBoth primary or both redundant MLG proximity sensors have failedor
HYDR Page(AMBER)any combination of an inboard/outboard ground spoiler WOW 1 or 2failure orany combination of an alternate or normal anti–skid WOW 1 or 2 failure.
PROXI NLG WOW FAILEither primary or redundant NG WOW proximity sensor failed
HYDR Page(AMBER)orPSEU NG WOW outputs failed.
Message inhibit logic:1. WOW, Engines off and Electrical Bus Failure refer to section 12–31–17–042. Takeoff phase3. Landing phase
CAS Field and System Messages (Sheet 3 of 4)
Dornier 328Jet - Landing Gear
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