TEST PROCEDURE.
GENERAL INFORMATION.
A test of all components should have been made after overhaul to insure proper operation. Some shops may
not have complete testing facilities for measuring airflows, pressure drops, and other factors which would be
accomplished in a laboratory-type test. If such a test cannot be made, install the heater and check operation on
the ground and in the air to determine if operation is normal. In shops where complete test equipment is available
and a complete functional test can be performed, the test routine described in subsequent paragraphs should be
made.
EQUIPMENT REQUIRED. (Refer to Figure 21-20.)
1. An improvised stand to hold the heater during test. The heater should be located far enough away from
any combustible material or atmosphere to avoid hazard. A location should be chosen where exhaust can
be dispelled. Do not add an excessive extension to the heater exhaust.
2. A source of fuel capable of being regulated at seven psi.
3. The combustion air blower to be used with the heater should be used for the test.
4. A 12 volt current supply which may be a DC generator with a rheostat, ammeter, and voltmeter in the line
to control and indicate the current draw and voltage output.
5. Two water manometers (zero to 5.0 inch water column) for measuring the pressure in the ventilating air
duct and in the combustion air stream.
6. A piece of duct to be attached to the downstream end of the heater. It should have a minimum length of
24 inches and the same diameter as the heater being tested. A 2.25 inch diameter orifice should be
centrally located at the outlet end. An aperture should be provided for the thermometer and duct switch
and a static tap should be attached as shown in Figure 21-20.
7. A thermometer with 500° F scale.
8. A fuel-pressure gauge.
9. A controlled source of compressed air for final leakage test.
OPERATIONAL TEST (ON TEST BENCH). (Refer to Figures 21-20 and 21-21)
mounted securely and that the heater is clamped to its supporting stand.
2. Insert the duct switch in the sheet metal extension tube at the location shown in Figure 21-20.
3. Connect components and heater as outlined in the wiring connection diagram, Figure 21-21. The power
supply switch should be open.
4. Connect the power source to the heater.
5. Disconnect wire lead from terminal No. 3 on the heater side of heater terminal strip to prevent the heater
from lighting and close the power source switch to check operation of blowers. The combustion air
blower and ventilating air blower should operate at full speed with no blower wheel interference. If
either blower fails to run, locate and correct the trouble before proceeding with the test.
6. Connect a voltmeter from open side of combustion air pressure switch terminal to ground to determine if
the switch is closed, which would be indicated by a full voltage reading on the meter. If a full voltage
reading is not obtained, the combustion air supply is either inadequate or the switch is defective or
improperly adjusted. Make necessary corrections.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 4 5 - 0 3
Page 21-44
Revised: May 15, 1989
1G11
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...