Instrument Air System Installation (Typical) - Piper Navajo Chieftain PA-31-350 Service Manual

NAVAJO CHIEFTAIN SERVICE MANUAL
1232
NOTE
ADVISORY CIRCULAR AC 43-203A
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 AC
43.13-1A, SECTION 4 OF CHAPTER
16. REFER TO PARTS CATALOG
FOR TYPICAL SYSTEM ROUTING.
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: 9/23/80
INSTRUMENTS
3A12