EFFECTIVITY:
040-999
1090 34-10-00
Jan
10/90 34-10-00
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
A. FlightEnvironmentalData (continued)
16 15 18
12
Pitot/Static Installation Figure1 (Sheet 1 of 3)
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PIPER AIRCRAFT
PA-42-720(Advanced Trainer)
MAINTENANCEMANUAL
A. FlightEnvironmentalData (continued)
35.
FlexibleHose (Static 2) 48. FlexibleHose (Pitot 1)
36.
FlexibleHose (Pitot 2) 49. Flexible Hose(Static 1 to ADS)
37.
FlexibleHose(Static 1) 50. Flexible Hose (Static)
38.
FlexibleHose (Pitot 1) 51. Flexible Hose(Pitot2)
39.
FlexibleHose (Pitot ) 52. FlexibleHose (Static 2)
40.
FlexibleHose (Static) 53. Flexible Hose to Test Ports
41.
FlexibleHose(Pitot2 to ADS) 54. Pitot and StaticTest Port Plac
42.
FlexibleHose(Static 2 to ADS) 55. Pitot and Static Test Ports
43.
FlexibleHose(Pitot)
44.
LineAssembly(Static)
45.
q -SensorSwitch
46.
Line Assembly (Static)
47.
FlexibleHose(Pitot1 to ADS)
Pitot/StaticInstallation
Figure1 (Sheet 2 of 3)
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Jan 10/90
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
A. Flight Environmental Data (continued)
1.
MainStatic Vent Line (Pilot)
2.
MainStatic Vent Line (Co-Pilot)
56.
Static Line Assembly (Co-Pilot)
57.
Static Line Assembly (Pilot)
58.
Static Line (Pilot)
59.
StaticLine(Co-Pilot)
60.
Tee Fitting(Pilot)
61.
Tee Fitting (Co-Pilot)
62.StaticLine(Co-Pilot)
63.
StaticLine(Pilot)
64.
Static Vent Fitting (Co-Pilot)
65.Static Vent Fitting (Pilot)
66.
Static Vent Fitting (Co-Pilot)
67.
Static Vent Fitting (Pilot)
58
1
67.
Pitot/Static Installation
Figure1 (Sheet 3 of 3)
EFFECTIVITY: 040-999
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Jan10/90
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
A. Flight Environmental Data (continued)
1.Pitot Tubes-Electric Heated
2.AlternateStatic Source
7.Pressure Bukhead
To Deice/GyroPressure System
3.Static Source Selector Valve -
Differential
Pressure
Switch
("q" Switch)
4.Condensate Drain Valve/Sump
A A/S PG
R/C
C/A
AP ADC
S q
- Altimeter
Airspeed
Deice/Gyro System Pressure Rateof Climb II 5.StaticPorts
CabinAltitude/Pressure
Diffential
Autopilot
- Air Data Computer
- Static Source Selector Diff. Press Switch - StaticLines
- PitotLines
Pitot/Static Schematic Figure 2
EFFECTIVITY: 040-999
Jan 10/90 34-10-00
Jan 10/90 34-10-00
PIPERAIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCEMANUAL
A. Flight Environmental Data (continued)
1. Pitot/StaticSystem Test
CAUTION: DO NOT USE ANY PETROLEUM PRODUCTS OR LOOSE SEALING MATERIALS ON OR ABOUT ANY TEST EQUIPMENT, STATIC SYSTEM LINES, OR CONNECTORS. DURING THE FOLLOWING PROCEDURES, TAKE PRECAUTIONSTO PREVENT INGESTION OF FOREIGN MATERIALS INTO THE TEST EQUIPMENT AND AIRCRAFT SYSTEMS.
NOTE: The PA-42-720 is equipped with quick-disconnecting test ports forward of bulkhead at F.S.
17.00which use an alternate static system test unit. The following procedure is provided if the procedure using the quick-disconnect ports is not used. The following procedures are to be accomplished only by qualified personnel per FAR
91.171and 91.172, and in conjunction with FAR 23 and AC 43.13-1A.
Use a Barfield Static Leak Tester (Barfield P/N 2397F) or equivalent to perform the following test. A suitable line adapter must also be attained for connection to the aircraft pitot tubes and static vent ports.
(a)
Inspect all vents, ports, plumbing, and instruments for loose connections and physical damage. Replace the appropriate parts as required.
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