Instrument Air System Installation (Typical) - Piper Navajo PA-31 Service Manual

PIPER NAVAJO SERVICE MANUAL
1232
NOTE
ADVISORY CIRCULAR AC43-203A
DESCRIBES AN
ACCEPTABLE
MEANS OF COMPLYING WITH STATIC
SYSTEM TEST REQUIRED
BY FAR PART 91, SECTION
91.170 FOR AIRCRAFT OPERATED UNDER IFR
CONDITIONS. FOR STATIC SYSTEM TEST FOR
AIRCRAFT
NOT OPERATED IN CONTROLLED
AIRSPACE UNDER
IFR CONDITIONS, SEE ADVISORY
CIRCULAR AC43.13-1A,
SECTION 4 OF CHAPTER 16.
REFER TO PARTS CATALOG
FOR TYPICAL SYSTEMS
ROUTING.
/
/ /
/
1
1. PITOT HEAD
2. ALTERNATE STATIC SOURCE
3. ALTIMETER
4. AIRSPEED INDICATOR
5. RATE OF CLIMB INDICATOR
6. SUCTION
GAUGE
7. STATIC SOURCE FOR PILOT'S AND OPTIONAL
COPILOT'S STATIC INSTRUMENTS
8. STATIC SOURCE FOR ALTIMATIC V SERIES
ALTITUDE CONTROLLER
9. ALTITUDE CONTROLLER
Figure 10-2. Instrument Air System Installation (Typical)
Reissued: 10/12/79
INSTRUMENTS
3D2