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时间:2011-04-25 08:35来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Electrolyteleveltoolow.
Chargingratetoo low in
service.
Too little usageor shallow discharges.
Batterylefton load.
Chargernotoperating
properly.
Internalconnectinglinks
loose.
Externalconnectorburned
or pitted.
Remedy
Inspectforelectrolyteleakage andremoveand replace de-fectivecellsorvents.
Adjustgeneratorcontrolunit voltageto 28 + 1 Vdc.
Discharge;constant-current charge. Replacedefective cells.
Replacedefectivecells.
Replaceor tighten links and connector.Replace defectivecell.
Charge,adjust electrolyte level,andcapacitytest.
Chargeandcapacitytest. Checkchargingsystem.
Doa reconditioning cycle per periodicbatterycheck paragraph.
Rechargeandcapacitytest.
Rechargeandcapacitytest
battery.Checkcharger operation.
Tightento proper torque
value;rechargeandcapacity
test.
Clean or replace; recharge
andcapacitytest.

EFFECTIVITY:

24-30-00 Jan 10/90

PIPER AIRCRAFT PA-42-720 (Advanced Trainer)
MAINTENANCEMANUAL
A. DC Generation (continued)
18. FaultIsolation(continued)
CHART 3 FAULT ISOLATION (BATTERY) (Sheet 3 of 3)
Fault
Terminallinks discolored or burned.
Burned or pitted terminals.
Burnedorpitted output receptacleterminals.
Distortionof cell case and cover.
Distortion of battery case or cover.
Cause

Loose terminal hardware.
Foreign metallic objects in the battery; tools dropped into the open battery.
Improperlyfitting or loose mating output connections.
Cellwith internal short.
Charger failure.
Plugged vent caps, minor explosion.
Overheatedbattery, improper cooling.
Major explosion: Loose links Dry cells
High charge voltage
Charger failure
Remedy
Clean or replacelinks and tighten all terminal hardwareto specified torque values.
Locateand remove foreign objectsand replace defective parts.
Replaceboth mating connectors.
Discharge,disassemble,and replace defective cells.
and replace defective cells.
Discharge,disassembly,
Discharge,disassemble,and replacedefective cells, and replacevents.
Discharge,disassemble,
and replacedefectiveparts.
and replacedefectivecells, link, vent caps, hardware,and case. Replace battery caseand cover.
Discharge,disassemble,
EFFECTIVITY:
040-999

 

Jan 10/90
24-30-00
Jan 10/9024-30-00
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL

A. DC Generation (continued)
CHART 4
NICKEL CADMIUM BATTERY SPECIFICATIONS

BatteryType: 40776
Capacity: 40 AH at the 1 hour rate
Numberof series connectedcells -20 -Nominal Voltage-24
ConstantCurrentCharging:
Startingrate(Is) -8.5 to 22 amperes--Control Point30.5 volts
FinishingRate(If) -4.0 to 10 amperes--TrickleRate215to 430 milliamps
ConstantPotentialCharging:
Voltage(Ec)(See ConstantPotentialChargingV/T Table) 43 amperes min.
Inrushcurrent at above voltage:350 amperes max.
Floating Voltages:
0°F 29.0 to 31.0 volts
75°F 28.0 to 30.0 volts

100°F 27.4 to 29.4 volts
Discharge Rates: Cutoff Voltage:
Max. Short Time:
10 sec. 1720amperes
30 sec. 860 amperes
Max.Continuous:
15.0

430 amperes
20.0

1 hour rate: 43 amperes
5 hour rate: 9 amperes 21.0
22.0

20 hour rate: 2.25amperes
(Cell)TerminalType: Screw--Thread Size: 10/32--Torque: 34-38in. Ibs Depthin Baffle: ElectrolyteLevel: 20 mm Duringlast 20 minutesof charge
CHART 5
CONSTANT POTENTIAL CHARGING V/T TABLE

Battery Temp. (°F) Volts/Cell Voltage
0° 1.565 31.3 ± 0.5
20° 1.545 30.9 ± 0.4
40 ° 1.525 30.5 ± 0.3
1.505 30.1 ± 0.2

60°
80° 1.485 29.7 ± 0.2

1000 1.460
29.2 ±0.2 120° 1.440 28.8 ± 0.1 140 ° 1.420 28.4 ± 0.1
EFFECTIVITY:

040-999
24-30 00 PAGE 17
Jan 10/90
PIPERAIRCRAFT

PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL

A. DCGeneration (continued)
Circuit DiagramNo.1
Ammeter

Load Load Resistor Resistor
Shunt
Discharge Circuit (Preferred) DischargeCircuit (Alternate)
Circuit Diagram No. 2
Ammeter
TemperatureProbe Ammeter

Temperature Probe I Knife Switch Shunt
ChargingCircuit (Preferred) Charging Circuit (Alternate)
Charge/ Discharge Schematics (Typical Service) Figure 301
EFFECTIVITY:
040-999

Jan 10/9024-30-00
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
 
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