Piper PA-28-161 User Manual

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1. CLOCK
2. ADF INDICATOR
3. TURN INDICATOR
4. AIR SPEED INDICATOR
5. DIRECTIONAL GYRO
6. ATTITUDE GYRO
7. VERTICAL SPEED INDICATOR
8. ALTIMETER
9. ANNUNCIATOR TEST SWITCH
10. ANNUNCIATOR
11. MAGNETIC COMPASS
12. NAVIGATION INDICATORS
13. TRANSPONDER
14. AUDIO SELECTOR PANEL
16. AVIONICS
16. RADIO MASTER SWITCH
17. ADF
18.
HOUR METER
19.
GYRO GAUGE
20. CIGAR LIGHTER
21. MIKE/PHONE JACKS
22. AUTOPILOT CONTROL PANEL
23. NAVIGATION SELECTOR SWITCH
24. MAGNETO/STARTER SWITCH
26. PITCH CONTROL
26. LEFT FUEL GAUGE
27. ENGINE INSTRUMENT CLUSTER
28. TACHOMETER
29. RIGHT FUEL GAUGE
30. PRIMER
31. AIR COI\IDITIONEA DOOR WARNING LIGHT
32. THROTTLE QUADRANT
33. FRICTION LOCK
34. CARBURETOR HEAT CONTROL
35 MASTER AND ACCESSORY SWITCH PANEL
36. ALTERNATOR GAUGE
37. CIRCUIT BREAKER PANEL
38. CLIMATE CONTROL PANEL
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Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)