12. Remove the brushes, one at a time, from the ventilating air blower motor by removing the brush cap and
carefully withdrawing the brush from its guide. Remove foreign material from the brush guide and
commutator with a stream of filtered compressed air. Check for brush wear. Inspect the commutator for
grooved brush track, pitting or burning. The commutator surface should be smooth and medium brown
in color. Replace the motor if the commutator or other parts show damage.
13. Inspect the combustion air blower motor as described in the preceding step.
14. Inspect the blower wheel for broken or bent vanes and replace it for either condition.
TESTING.
The following tests should be performed as outlined in the succeeding paragraphs:
1. Check ventilating air and combustion air motors for correct RPM and current draw:
A.
Connect motor to 12 volt DC power supply. Rotation should be counterclockwise when viewed
from the shaft end.
B.
Both motors should rotate at approximately 7500 RPM at rated voltage. Current draw is
approximately five amperes.
C.
If current draw is excessive or if speed is too low, replace the brushes. Recheck both current draw
and RPM after brushes are properly run in.
D.
If after replacing brushes operation is still unsatisfactory, replace the motor.
— Note —
The motor checks described above should be made without the blower housing
attached, for both the ventilating air and combustion air motors.
2. Test the combustion tube assembly for leaks as follows:
A.
Fashion a sealing plate from approximately 1/8 inch thick flat stock to seal the combustion head
opening in the combustion tube assembly. (Refer to Figure 21-16) Use a rubber gasket under
the.plate and attach the plate with six screws.
B.
Make up seals for all remaining openings, except the one used to connect the air pressure source.
(Refer to Figure 21-16) Use rubber stoppers as shown. The combustion air inlet tube can be sealed
best with a drilled stopper and clamp. Other openings should be sealed with expansion plugs. The
seal used in the exhaust tube should be formed so that it will not deform the air pressure switch tube
which protrudes into the exhaust.
C.
Install plugs and caps in all openings except the one to which the combustion air pressure switch is
attached. (Any opening can be used to connect the air pressure source, however, the combustion air
pressure switch opening is usually the most convenient. The drain opening would normally be
considered a second choice.)
D.
Connect a regulated air supply to the opening that has not been plugged and apply a pressure of
between three and five psi to the combustion tube assembly.
E.
Submerge the combustion tube assembly in water for several minutes while watching for bubbles
which would indicate leaks. No air leakage is permitted from the combustion tube assembly. No
weld or braze repairs are permitted on a combustion tube assembly.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 4 4 - 0 6
Page 21-37
Revised: May 15, 1989
1G4
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...