Piper PA-28-161 User Manual

Paragraph
No.
TABLE OF CONTENTS
SECTION 3
EMERGENCY PROCEDURES
Page
No.
3.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . 3-1
3.3 Emergency Procedures Checklist. . . . . . . . . . . . . . . . . . . . . 3-3
Engine Fire During Start . . . . . . . . . . . . . . . . . . . . . . . . . 3-3
Engine Power Loss During Takeoff . ; . . . . . . . . . . . . . . 3-3
Engine Pow~ Loss In Flight. . . . . . . . . . . . . . . . . . . . . . 3-3
Power Off Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-4
Fire
In Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-4
Loss
Of Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-5
Loss Of Fuel Pressure........... . . . . . . . . . . . . . . . . . 3-5
High Oil Temperature............................ 3-5
Electrical Failures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-5
Electrical Overload . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-5
Spin Recovery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-6
Open Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-6
Engi~e Roughness . . . . . . . . . . . . . . . . . • . . . . . . . . . . . . . 3-7
Carburetor Icing .................... ·. . . . . . . . . . . . . 3-7
3.5 Amplified Emergency Procedures (General) . . . . . . . . . . . 3-9
3.7 Engine Fire During Start ........... 0............... 3-9
3.9 Engine Power Loss During Takeoff 0 •••••••••• 0. 0 ••• 0 3-9
3.11 Engine Power Loss In Flight ............. 0 • • • • • • • • • • 3-10
3.13 Power Off Landing ............. 0.................. 3-ll
3.15 Fire In Flight .. . .. .. .. .. . . . .. . .. .. .. . .. .. .. .. .. .. . 3-ll
3.17 LossOfOiiPressure ............................... 3-12
3.19 Loss
Of Fuel Pressure.............................. 3-12
3.21 High Oil Temperature.............................. 3-13
3.23 Electrical Failures .. .. . . . . .. .. .. .. .. .. .. .. . .. . .. .. . 3-13
3.24 Electrical Overload . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-13
3.25
Spin Recovery . . . .. . . . . .. . . . .. .. . .. .. . .. . .. .. . .. .. 3-14
REPORT: VB-1180
3-i

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)