Heater Trouble Diagnosis
South Wind (Steward Warner) Models 8240 through 8472 Series
The following are just basic troubleshooting tips. Most problems
will be identified using the following steps. For detailed servicing or overhaul
see the following manual. For 8240 thru 8259 series see service manual form
no 09-998. For 8472 series see form no. 09-1015.
- Test Equipment needed:
- Basic hand tools
- Voltmeter
- Temperature monitor 0-500
- Fuel pressure gauge 0-50 psi
- Auxiliary power supply
- Identifying features of the South Wind (Stewart
Warner) 8240 thru 8472 service heater
- . 2” exhaust
- Combustion air blower mounted separate from the
heater with a fuel pump on the end of the motor
- General: 35,000-45,000
BTU heaters
- Electrical:
- 24 Volt applications
- Terminal strip numbered “4, 5, 6, 7,
8, 10”
- Normal heater operation for all models with solid-state
ignitions will provide power at the heater terminal strip numbers “4,
5, 6, 7, 8, and 10.” As the heater reaches preset temperature,
power will remain at all but “8” on non-pressurized
aircraft until heat is again required at which time power will
again be present at terminal “8”.
Pressurized aircraft will interrupt power at terminal “7” for
heat control.
- Early heaters 8240A, 8259A and DL with mechanical
ignition will have no wires on “10” but still interrupt
power to “8” for
heat control
- Basic requirements for heater operation:
- . There are five basic requirements for a combustion heater
to function.
- Electrical power
- Ignition
- Fuel
- Combustion air
- Ventilating air
- If any of these are absent or out of tolerance the heater will not operate correctly
- Trouble Diagnosis: (The following basic troubleshooting steps are in
order of ease of inspection and are the most common cause of failure)
Note: It is suggested that one person operate the heater controls and another
person perform the checks at the heater.
- Common Problems
- Most common problems in order of their probability
are:
- Fuel pressure (22-30 psi) See step 4.
- Ignition (fuel dripping
from heater drain or exhaust) See step 3.
- Air flow switch See
step 2.
- b. Problem 1 - Heater inoperative or intermittent
- Step 1 - Ventilation
Air
- Verify air flowing from distribution points in the aircraft.
- If no air flow:
- Check for voltage on the heater terminal
strip numbered “5.”
- Power present at
terminal 5 means vent blower is bad.
- No power present, follow to source of power
and correct. Possibly circuit breaker for ventilation
blower, heater switch, or broken wire.
- Step 2 -
Combustion air and electrical power to heater
circuit troubleshooting
- Verify air is flowing from exhaust of heater. Any airflow
is sufficient for preliminary inspection.
- Airflow from exhaust:
- If power is present at heater
terminal #6 but not at terminal #7 then airflow switch
is sticking or bad.
- Clean only with electrical
contact cleaner. Do not lubricate.
- No Air flow
from exhaust:
- Check for power at terminal
number “6” on
the heater terminal strip.
- If power is present
and no air flow from
the exhaust, combustion
air blower is bad.
- If power is not present
at terminal “6” the
overheat switch has
probably activated. Reset.
(See wiring schematic
at end of troubleshooting.)
- The most common cause of overheat switch
activation is caused by the pilot not allowing
for the heater to cool off prior to shutting
down the aircraft.
- Step 3 – Ignition
troubleshooting (Note
wiring schematic)
- Verify there
is power to the
ignition unit from
heater terminal
number “10.” (on
very early heaters 8240A, 8259A & DL with mechanical ignitions it will
be terminal number “6” that supplies power to ignition. There
will be no wires on “10.”)
- If
power
is present
at the ignition
unit:
- Turn the heater off and remove the igniter
from the heater and reinstall
it in the lead.
- Allow the igniter to lie against
the heater to provide grounding to the
case. Make sure the igniter end disc
is not touching ground. Only the main
body should be grounded.
- Turn the heater back
on and observe the disc on the end of the
igniter.
- A bright blue consistent spark should be
visible.
- Weak, absent
of a single spark indicates
a faulty ignition and
it should be replaced.
- If power is not present at the ignition
unit:
- If power is
at terminal number “6” and not at “10” (early
heaters 8240A, 8259A & DL with mechanical ignitions power
on “6” but
not at ignition)
the airflow
switch
is faulty.
- Step
4 – Fuel
troubleshooting
- Remove
the fuel
pump cover
and visually
inspect the fuel
box below the
pump for brass
particles.
- If brass particles are
present replace the pump.
- Also turn
the heater
on and verify
the coupling between
the motor and pump
are complete and pump is
turning. Replace pump if
coupling is sheared.
- “Tee” in 0-50 PSI fuel pressure
gauge between the fuel pump and heater.
- Turn the heater on
and temperature control
in full hot.
- Verify fuel
pressure is
above 22 psi
with heater
calling for heat.
- If less than 22 psi with heater in operation
replace
pump. Fuel pressure must be more than 22 psi for proper operation especially
at altitude.
- If fuel pump and pressure is good check
the exhaust
for fuel smell.
- No fuel smell
at exhaust, no
fuel dripping from
heater drain, or
exhaust.
i. Check for power at terminal “8” (pressurized
aircraft “7”).
- If no power at “8” (pressurized aircraft “7”)
but if power is at “7” (pressurized aircraft
power at “8”)
the
thermostat
is
not
working.
Refer
to
wiring
schematic.
- The
thermostat
can be checked
by placing a
jumper across
terminals seven
and eight. If
heater operates with
jumper replace thermostat.
- Fuel smell at exhaust or fuel dripping:
- If all previous
steps check out good the
problem is most likely inside the heater. (i.e. fuel
solenoid or nozzle contamination)
- This will require
removal of the
heater from the aircraft for servicing. We
recommend at this point sending
the heater and combustion air blower/fuel
pump assembly to C&D
Associates Inc.
for evaluation/repair
View the troubleshooting
chart (pdf)
Disclaimer: The following info is to assist our customers. We accept no responsibility
for the outcome of the preceding procedures.