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Voltage
Regulator
Setting
5 6 2-4 7.5-7.75 7.50
10 12 2-4 15.0-15.5 15.00
12 15 2-4 18.0-18.5 18.00
19 22.8 2-4 28.0-29.0 28.50
20 24 2-4 28.5-30.0 30.00
22 26.0 2-4 31.0-33.5 33.00
* Constant potential charging voltage and time apply to all ampere-hour ratings,
subject only to number of cells per battery
MarathonNorco Aerospace, Inc.
OPERATING and MAINTENANCE MANUAL
NICKEL-CADMIUM AIRCRAFT BATTERIES
24-34-00 Page 104
APR 15/06
Figure 3
Temperature vs. Charge Voltage Relationship
MAXIMUM RECOMMENDED CONSTANT POTENTIAL CELL
CHARGE VOLTAGE AT VARIOUS TEMPERATURES
Temperature vs Charge Voltage
MAXIMUM RECOMMENDED
CONSTANT POTENTIAL CHARGE
VOLTAGE
AT VARIOUS TEMPERATURES
1.35
1.45
1.55
1.65
1.75
-40 -20 0 20 40 60 80 100 120
Battery Temperature, F°
Charge Voltage, V/cell
MarathonNorco Aerospace, Inc.
OPERATING and MAINTENANCE MANUAL
NICKEL-CADMIUM AIRCRAFT BATTERIES
24-34-00 Page 105
APR 15/06
1.3 Inspection - Received in for Service
When a battery is received in the shop for routine servicing, the following inspections should be
performed:
Visually inspect can and cover for dents, damage, epoxy coating separation, vent tube obstruction,
latch function and cover seal condition.
Any evidence of discrepancies, in above shall be cause for replacement of the parts.
Remove the battery cover and inspect for the following:
Clean top of cells and connectors with a nylon brush. Blow out residue with oil-free compressed air
using standard safety precautions. If cells are exceptionally dirty, connecting links, hardware, and
cells may need to be removed, washed in warm water and dried. If this is required, discharge the
battery before disassembly.
Verify that the polarity of the cells and position of the internal connections are correct.
Inspect intercell connectors for corrosion, burns or discoloration. Clean with an eraser or replace
as required.
Remove vent plugs and inspect “O” rings and vent sleeves for damage or hardening. Replace if
defective. If necessary, wash vent plugs in warm water to remove the white powder (potassium
carbonate) from vent holes. Dry with oil-free compressed air using standard safety precautions.
1.3.1 Inspection of Battery Power Connector
Inspect for corrosion or pitting on the contact pins.
Inspect for arcing or burn marks on the contact pins. This is caused when the disconnect is
removed under electrical load.
Inspect for battery electrolyte leakage through the receptacle body and/or the contact pins.
NOTE: Electrolyte leakage can be noticed by a discoloration of the receptacle body with
the glass fibers exposed.
Gauge each contact pin diameter using dial calipers that are capable of reading to .001 inch.
The diameter shall be .375 ± .005 inches.
1.3.2 Inspection of Sensor Receptacle (if so equipped)
Examine sensor connector for pin or locking mechanism damage.
CAUTION: The electrolyte used in the battery is a caustic solution of Potassium Hydroxide. Avoid
contact with any part of the body.
MarathonNorco Aerospace, Inc.
OPERATING and MAINTENANCE MANUAL
NICKEL-CADMIUM AIRCRAFT BATTERIES
24-34-00 Page 201
APR 15/06
2.0 ELECTRICAL LEAKAGE
To determine if external leakage is of such a magnitude as to require a complete battery cleaning
set the range selector of a multimeter to the 500 milliampere range or higher.
Place the positive lead of the meter on the positive terminal of the battery receptacle and touch the
negative lead of the meter to any exposed metal on the battery can.
NOTE: Many MarathonNorco batteries are supplied with epoxy coated battery cans and
covers. Where epoxy coated cans are used, current flow may be measured
between the battery terminals and the screws that are used to mount the main
connector.
If the measurement is within the meter limits, connect the negative lead of the meter to the battery
can. Record this current value.
Repeat the above, connecting the negative lead of the meter on the negative terminal of the battery
receptacle and the positive meter lead to any exposed metal on the battery can.
If the above current measurements exceed 50 milliamperes, flush the tops of the cells and dry.
(Reference Paragraph 9.0)
Repeat the above current test on the positive and negative terminals. If the tops of the cells were
cleaned properly and the current measurement is still greater than 50 milliamperes, one or more of
the cells may be leaking. To isolate this cell or cells, proceed as follows:
Using a voltmeter of 1000 ohms-per-volt, or greater, place one of the meter leads on either
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Operating and Maintenance Manual For Nickel-Cadmium Aircraft(7)
