F.
After completion of the high rpm adjustment, adjust the control system so that the governor con-
trol arm will contact the high rpm stop. The cockpit control lever should be .031 to .062 of an
inch from its full forward stop. ( Refer to Figure 61-4, Sheet 2 of 2) To adjust the control travel,
disconnect the control cable end from the control arm. Loosen the cable jam nut and rotate the
end to obtain the desired level clearance. Connect the cable end and tighten jam nut.
G .
It is only necessary to adjust the governor control system high rpm setting. This action
a u t o m a t ic a lly satisfies the positive high pitch setting.
RIGGING AND ADJUSTMENT OF PROPELLER GOVERNOR. (S/n’s 4495001 and up.) (Refer to
Figure 61-4.)
Information Pending.
ENGINE SYNCHROPHASER. (S/n’s 44-7995001 thru 44-8195026 and 44-8107001 thru 44-8207020.)
(Refer to Figures 61-5 and 61-6.)
The synchronizer installation is a Hartzell system which utilizes two pulse generators, a computer, and an
electrically slaved, mechanically operated propeller governor.
With this system, the right engine is utilized as the slave engine and the left engine as the master. The
pulse generators, attached in line with the tachometer cables or rods, on the 44-180 installation are intercon-
nected through the computer which senses the speed of the engines through the magnetic pickups in the pulse
generators. The computer synchronizes the right engine to the left, through a solenoid in the right propeller
governor (slave governor) .
TEST EQUIPMENT.
The Hartzell B-4467-1 Test Set should be used to perform the following tests. The test lights, as they
appear on the set, are defined as follows:
1. POWER light on, indicates power supply to the system computer is of the correct polarity.
— NOTE —
If the engine lights come ON, and STAY ON, when the propellers
are rotated, the pulse generator(s), cables, or tester are defective.
2. RIGHT ENGINE and LEFT ENGINE lights ON, indicate that their respective pulse generator is
wired, and working properly.
3. MANUAL and PHASE lights ON, indicate that, each respective function of the propeller synch switch
is wired correctly.
— NOTE —
The propeller governor with the solenoid is a Hartzell supplied
product. Contact Hartzell for replacement of coil or governor or
Piper for replacement of entire assembly. Hartzell also has the
D-4469 Computer Analyzer unit, which can be purchased from
them, to test the computer.
4. The COIL light ON indicates that the circuit for the propeller governor solenoid coil is correctly wired.
An open circuit, or a grounded wire on Pin 8 is indicated, should the COIL light fail to illuminate.
5. COIL SHORT light ON, indicates an internal dead-short in the right engine propeller governor sole-
noid coil, or a short between the coil leads. The light may also come on if power supply voltage
exceeds 14 volts.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
61-10-00
Page 61-06
Revised: June 20, 1995
3D8
Содержание SEMINOLE PA-44-180
Страница 18: ...CHAPTER AIRWORTHINESS LIMITATIONS PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 1A18 PIPER AIRCRAFT...
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Страница 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
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Страница 49: ...CHAPTER LIFTING AND SHORING 1C1...
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Страница 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
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Страница 58: ...CHAPTER TOWING AND TAXIING 1C10...
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Страница 62: ...CHAPTER PARKING AND MOORING 1C14...
Страница 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Страница 70: ...CHAPTER SERVICING 1C22...
Страница 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Страница 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Страница 189: ...CHAPTER AUTOFLIGHT 1H21...
Страница 192: ...CHAPTER COMMUNICATIONS 1H24...
Страница 202: ...CHAPTER ELECTRICAL POWER 1I10...
Страница 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Страница 233: ...CHAPTER FIRE PROTECTION 1J17...
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Страница 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Страница 304: ...2A18 CHAPTER FUEL...
Страница 325: ...2B17 CHAPTER HYDRAULIC POWER...
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Страница 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
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Страница 414: ...CHAPTER LANDING GEAR 2F13...
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Страница 479: ...2I6 CHAPTER LIGHTS...
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Страница 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Страница 503: ...2J7 CHAPTER OXYGEN...
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Страница 524: ...2K6 CHAPTER VACUUM...
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Страница 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
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Страница 547: ...2L7 CHAPTER STRUCTURES...
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Страница 582: ...CHAPTER DOORS 3A18...
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Страница 593: ...CHAPTER STABILIZERS 3B8...
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Страница 604: ...CHAPTER WINDOWS 3B22...
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Страница 611: ...CHAPTER WINGS 3C10...
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Страница 624: ...CHAPTER PROPELLER 3D1...
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Страница 643: ...CHAPTER POWER PLANT 3D21...
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Страница 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
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Страница 681: ...CHAPTER IGNITION 3F16...
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Страница 712: ...CHAPTER ENGINE INDICATING 3H1...
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Страница 730: ...CHAPTER EXHAUST 3H19...
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Страница 734: ...CHAPTER OIL 3I1...
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Страница 743: ...CHAPTER STARTING 3I11...
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Страница 755: ...CHAPTER TURBINES 3J1...
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Страница 787: ...CHAPTER CHARTS AND WIRING DIAGRAMS 4A18...
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