— CAUTION —
TO PREVENT THE BUILDUP OF UNNECESSARY
PRESSURE ON THE ACTUATING CYLINDERS AND
CONNECTING HYDRAULIC LINES, WHEN THE GEAR
IS RAISED OR LOWERED MANUALLY WITH THE
AIRPLANE ON JACKS, PULL THE EMERGENCY
EXTENSION KNOB OUT. FAILURE TO COMPLY WITH
THIS PROCEDURE COULD RESULT IN THE BUILDUP
OF SUFFICIENT PRESSURE TO UNLOCK THE D O W N
LOCK, ALLOWING THE GEAR TO COL L A P S E
WHEN THE WING JACKS ARE REMOVED. PRIOR TO
REMOVING THE AIRPLANE FROM THE JACKS, PUSH
THE EMERGENCY EXTENSION KNOB IN, TURN THE
MASTER SWITCH ON, AND SELECT GEAR DOWN.
O B S E RVE THAT ALL THREE GREEN LIGHTS ARE
ENERGIZED, INDICATING THAT THE LANDING
G E A R S A R E D O W N A N D L O C K E D . T U R N T H E
M A STER SWITCH OFF.
CHART 2901. LEADING PARTICULARS, HYDRAULIC SYSTEM
TROUBLESHOOTING.
Malfunctions in the hydraulic system will result in failure of the landing gear to operate properly. When
trouble develops, jack up the airplane (refer to Chapter 7) and then proceed to determine the extent of the trou-
ble. Generally. hydraulic system troubles fall into two types, troubles involving the hydraulic supplying system
and troubles in the landing gear hydraulic system. Chart 2902 lists the troubles which may be encountered and
their probable cause and suggests a remedy.
— NOTE —
If it is found that the hydraulic pump is at fault and requires
d i sa s s e m b l y, it is recommended that it be overhauled by an
accredited overhaul facility. Pressure checks with adjustments
may be accomplished in accordance with instructions given.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
29-02-00
Page 29-05
Revised: June 20, 1995
2B24
HYDRAULIC PUMP
Hydraulic Pump
High Pressure
Low Pressure
Flow Rate @ 1000 psi
Hydraulic Fluid
Thermal Relief Valve
Shuttle Valve Delivered
Pressure
Pressure Switch
Open (OFF) Pressure
Close (ON) Pressure
HYC5005
PRESTOLITE
2000 to 2500 psi
650 ± 150 psi
45 cu. in. per min.
MIL-H-5606
2250 ± 250 psi.
400 - 800 psi
1800 ± 100 psi
200 to 400 psi
Piper P/N 481 879
OILDYNE
2400 ± 200 psi
600 ± 200 psi
60 cu. in. per min.
MIL-H-5606
3000 + 300 / -200 psi
400 - 800 psi
1800 ± 100 psi
300 ± 100 psi
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...