7. Observe the manometer connected to the ventilating air pressure tap, which should show a reading of 1.1
inches of water (minimum) at rated voltage.
8. Observe the manometer connected to the combustion air tube tap, which should show a reading of 1.5
inches of water (minimum) at rated voltage.
9. Open the power supply switch and reconnect the terminal lead disconnected in preceding Step 5.
10. Close the power supply switch and turn on the fuel supply. The heater should light within five seconds
(may require slightly longer for air to be purged from fuel lines on the first trial).
11. Observe operation of duct switch, which should control heater operation according to the switch setting.
12. If the duct switch fails to control the temperature according to the setting, place the control lever in high
“H” position and notice the control variation. A high reading of 250°F +/- 10° should be obtained
(reading will vary in different applications).
13. Connect a jumper across the terminals of the duct switch to make it inoperative and observe action of the
cycling switch. The cycling switch should cycle to control the outlet air temperature at approximately
250°F (nominal). This is a function of ambient temperature and airflow conditions. If operation is within
a range of 190°F to 290°F, the switch is operating normally. If the switch is out of range, it can be reset
in the same manner as described for the duct switch, except that no control lever or indicator stop are
used. If adjustment fails to restore proper temperature range, replace the switch.
14. With duct switch still jumped, place a jumper across the cycling switch terminals to check operation of
the overheat switch. Block the ventilating air outlet and notice if the overheat switch shuts off the heater.
It should open at between 300°F and 400°F. (This is also a function of ambient temperature and
airflow.) After the switch shuts off, remove ventilating air restriction; remove jumpers from cycling and
duct switches and press firmly on the overheat switch reset button until it “clicks.” The heater should
light and operate.
15. Shut down the heater and check all components visually to make sure no damage has occurred to any of
them.
16. Remove heater and other components from the test setup and install it in the airplane.
INSPECTION OF FUEL NOZZLE ORIFICE. (Refer to Figure 21-18)
1. Loosen the four screws and rotate the blower and motor housing to disengage the ventilating air blower
from the end of the heater jacket. It is not necessary to disconnect the electrical connections to remove
the nozzle.
2. Remove the fuel shroud cover by removing the screws. Remove solenoid and elbow.
3. Reach inside the inlet end of the jacket assembly with a 3/4 inch open-end wrench and, while holding the
fuel-tube fitting of the jacket, use a 3/4 inch deep socket to remove the nut, washer and gasket and lower
fuel shroud box.
4. Remove the two screws and carefully withdraw the nozzle holder and valve assembly from the
combustion head assembly.
5. Carefully unscrew and remove the spray nozzle from the nozzle holder. Remove the gasket.
6. After cleaning the nozzle, reinstall the parts removed in essentially the reverse order from removal. Be
sure to hold the fuel-tube fitting when tightening the nut to avoid damage to the fuel tube.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 4 6 - 0 0
Page 21-45
Revised: May 15, 1989
1G12
PIPER AIRCRAFT
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...