EXHAUST GAS TEMPERATURE GAUGE. (Alcor)
This instrument, which is commonly referred to as EGT, is used to aid the pilot in selecting the economical
fuel-air mixture for cruising flight at a power setting of 75% or less. It is a sensing device to monitor the fuel
air mixture leaving the engine cylinders. This gauge is adjustable. If it is found defective after checking with
troubleshooting chart it should be replaced. If the leads to the gauge are defective in any way they should be
replaced. When replacing leads, it is very important to use the same type and length of wire as the resistance of
the leads is critical for the proper operation of this gauge.
REMOVAL OF EGT PROBE AND GAUGE.
1. Disconnect wires from the EGT gauge at the instrument panel.
2. Remove four bolts which secure the gauge to the instrument panel and remove the gauge.
3. Remove wires from the wire harness going to the engine.
4. Loosen the clamp which secures the EGT probe to the number two cylinder exhaust manifold and
remove the probe.
CLEANING AND INSPECTION OF EGT.
Unless mechanical damage is evident, broken glass, bent or broken pointer, or broken case, the following
checks should be performed before removing the instrument:
1. Remove the probe from the exhaust stack and check for a broken weld (at tip end) or a burnt off end.
The measured resistance of probe should be .8 ohms. Clean the connections with steel wool before reassembly.
2. Disconnect the lead wires at the instrument and measure. Resistance with the lead wires connected to
probe should be 3.3 ohms. Clean connections with steel wool before reassembly.
3. With the leads connected to instrument, heat probe with propane torch to dull red. The meter should
read up to the fourth graduation or approximately 1500° F. Before making this check, make sure that the
adjustment screw, located at the rear of the instrument case, is in the center of its travel. If this screw has been
turned to either end of full travel, it will shut the instrument off and no indication will be shown on the pointer.
If meter still does not read, replace it.
—CAUTION—
Do not connect ohmmeter across meter. It will burn out the
movement of the meter.
INSTALLATION OF EGT PROBE AND GAUGE.
1. Install the probe into the hole in the number two cylinder exhaust manifold and secure with clamp.
2. Route the thermocouple wires along with the existing wire harness to the instrument panel.
3. Install the EGT gauge into the instrument panel and secure with four bolts.
4. Connect the thermocouple wires to the rear of the EGT gauge.
77-20-05
Page 77-04
December 1, 1978
3F21
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Summary of Contents for Arrow IV
Page 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...
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Page 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Page 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Page 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Page 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Page 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Page 66: ...CHAPTER PARKING AND MOORING 1C18...
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Page 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Page 77: ...CHAPTER SERVICING 1D5...
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Page 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Page 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Page 169: ...CHAPTER AUTO FLIGHT 1H1...
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Page 176: ...CHAPTER COMMUNICATIONS 1H8...
Page 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Page 233: ...CHAPTER FLIGHT CONTROLS 1J17...
Page 297: ...CHAPTER FUEL 2A18...
Page 320: ...CHAPTER HYDRAULIC POWER 2B17...
Page 355: ...CHAPTER LANDING GEAR 2D4...
Page 418: ...CHAPTER LIGHTS 2F19...
Page 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Page 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Page 464: ...CHAPTER VACUUM SYSTEM 2H17...
Page 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Page 477: ...CHAPTER STRUCTURES 2I6...
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Page 496: ...CHAPTER DOORS 2J1...
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Page 505: ...CHAPTER STABILIZERS 2J10...
Page 514: ...CHAPTER WINDOWS 2J19...
Page 519: ...CHAPTER WINGS 2J24...
Page 550: ...CHAPTER PROPELLER 3A18...
Page 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Page 568: ...CHAPTER POWER PLANT 3B12...
Page 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Page 611: ...CHAPTER IGNITION 3D7...
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Page 655: ...CHAPTER ENGINE INDICATING 3F16...
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Page 664: ...CHAPTER EXHAUST 3G1...
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Page 669: ...CHAPTER OIL SYSTEM 3G6...
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Page 673: ...CHAPTER STARTING 3G10...
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Page 688: ...CHAPTER TURBINES 3H1...
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Page 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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