LISTOFEFFECTIVEPAGES
Jan 1090
SUBJECT
General Description and Operation
Storage Description and Operation Fuel Vent System Fault Isolation
PIPERAIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCEMANUAL
CHAPTER 28 -FUEL
TABLE OF CONTENTS
CHAPTER PAGE
28-00-00
1 1
28-10-00
1 1 1 2
Handling and Storage of Fuel Cells 3 Fuel Cell Replacement 3 Removal of Wing Tip Tanks 3 Installationof Wing Tip Tanks 6 Removal of Wing Fuel Cells 6 Molded Nipple Fittings 10 Installationof Inboard, Aft Inboard, and
Outboard Fuel Cells Testing of Fuel Cells Inspection of Fuel Cells Cleaning of Fuel Cells Repair of Fuel Cells Handling of Repair Materials Repair Limitations of Fuel Cells Repair Patch (Heat Cure Method) Repair Patch (Air Cure Method) Repair Patch (Quick Cure Method) Sealing Metal Surface Fittings Fuel Cell Accessory Replacement Repair of Fuel Cell Defects
Distribution Description and Operation Fuel Valves Fuel Filter Fuel Jet Pumps Fault Isolation- Fuel System Overhaul of Fuel Shutoff Valves Servicing Jet Scavenger Pump Removal of Fuel Valves Installation of Fuel Valves Removal of Fuel Filter Screen Installation of Fuel Filter Screen Installation of Fuel Filter Removal of Jet Transfer Pump Installation of Jet Transfer Pump
EFFECTIVITY: 040-999
10 13 14 14 15 15 16 19 21 23 24 25 26
28-20-00 1 1 1 1 4 4 5 7 8 8 8 8 9 9 10
CONTENTSJaGE1
PIPER AIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
CHAPTER28 -FUEL
TABLEOF CONTENTS (continued)
SUBJECT CHAPTER PAGE
28-20-00
Distribution(continued) Removal of Submerged Fuel Pump 10 Installationl of Submerged Fuel Pump 10 Adjustment of Fuel Shutoff and Crossfeed Valve 11 Leakage Test of Fuel Shutoff and Crossfeed Valve 12 FuelFlow and Pressure Test 12 Jet Pump Flow Check 14 Cleaning of Fuel Filter Screen 15
28-40-00
Indicating 1 Description and Operation 1 Fuel Quantity Indicating System 1 AutomaticFuel Pump System 1 Fault Isolation -Fuel System 3 Overhaul of Tank Sensor Units 5 Overhaulof Fuel QuantityIndicator 5 Removal of Tank Sensor Units 5 Installation of Tank Sensor Units 6 Fuel Quantity System Calibration Tests and Adjustments 7 Test of Automatic Fuel Pump System 15
EFFECTIVITY:
040-999
Jan 10/90CONTENTS
PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
Fuel
A. Descriptionand Operation
ThePA-42-720containsindividualfuel systems (refer to 28-00-00 Figure1) in each wing for each engine.Eachstandardfuel system consists of a wing tip tank, three bladder type tanks, and a nacelle tankwhich provide 281 gallons of fuel for each engine.
by feed and vent lines, and incorporate capacitancetype probes in each cell. The fuel probesare interconnected Thefuel vessels within each wing are interconnected
on each side to an individual indicatoron a common dualdisplaygauge,and give a linear responsefor each indicator's combined system.To vent the fuel systems, twoNACA non-siphoning vents,incorporating
and non-icing flame arrestorsare installed undereachwing.
The controls regulatingfuel flow, other than enginecontrols (start control lever and powercontrol lever),are used to control the crossfeedand fuel shutoff valves, bothof which are manuallycontrolled fromthe fuel control panel withinthe cockpit. The crossfeed valveis located on the left side of the aircraftattachedto the crossfeed and left engine main feed lines (refer to 28-20-00 Figure2)). The fuel shutoff valvesare in both main feed lines and mounted to front spar reinforcement
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本文鏈接地址：夏延飛機維護手冊 Cheyenne IIIA PA-42-720 AMM 1(125)
