Page 26 - Piper PA-20 Interactive Digital Parts Catalog
P. 26

TABLE OF CONTENTS




             Figure                                  Page        Figure                                  Page
             Number Figure Title                  Fig.  List     Number Figure Title                   Fig.  List
             1       Exploded View of Complete Airplane  ab  ab  20      Instrument Panel Installation, Directional   62  61
                                                                         Gyro and Gyro Horizon, 1952 and 1953
                                                                         Models
               SECTION I – WING AND FUEL TANK INSTALLATION GROUP
             2       Wing and Fuel Tank Installation  1  2       21      Instrument Panel Installation, Directional   64  65
                                                                         Gyro, 1950, 1951 and 1952 Models
             3       Lift Strut Installation       5     4       22      Vacuum Pump Installation, When   68  69
             4       Aileron Installation          7     7               Regulating Valve Installed on Engine Side
             5       Flap Installation             8     8               of Firewall
                                                                 23      Vacuum Pump Installation, When   70  71
                      SECTION II – WING ASSEMBLY GROUP                   Regulating Valve Installed Inside of
             6       Sheet 1 of 3 sheets, Wing Panel Assembly  9  10     Cockpit
             6       Sheet 2 of 3 sheets, Wing Panel Assembly  12  11  24  Litter Installation          72   72
             6       Sheet 3 of 3 sheets, Wing Panel Assembly  15  14  25  Floorboard and Carpet Installation  73  74
             7       Wing Panel Assembly, “115”    19   20       26      Cockpit Finishing Installation  77  78
                                                                 27      Sheet 1 of 2 sheets, Cockpit Finishing   81  80
                                                                         Installation
                        SECTION III – FUSELAGE GROUP
             8       Fuselage Frame Assembly       21   22       27      Sheet 2 of 2 sheets, Cockpit Finishing   83  82
                                                                         Installation
             9       Fuselage Covered Assembly     25   26

                                                                              SECTION V – CONTROL GROUP
                         SECTION IV – COCKPIT GROUP              28      Control Column and Rudder Pedal   85  86
             10      Rear Seat Installation        30   29               Installation
             11      Front Seat Installation       32   33       29      Stabilizer Adjustment Crank Installation  88  89
             12      Front Door Assembly, 1950, 1951 and   36  37  30    Stabilizer Adjustment Mechanism   90  91
                     1952 Models                                         Installation
             13      Front Door Assembly, 1953 Model  40  39     31      Aileron, Elevator and Stabilizer   92  93
             14      Rear Door Assembly, 1950, 1951 and   42  43         Adjustment Control
                     1952 Models                                 32      Aileron and Rudder Inter-Connecting   95  96
             15      Rear Door Assembly, 1953 Model  45  44              System
             16      Baggage Compartment Installation  47  46    33      Rudder and Flap Control System  97  98
             17      Instrument Panel Installation, Standard   48  49  34  Tail Surfaces Installation   99  100
                     and Primary, 1950 and 1951 Models
             18      Sheet 1 of 2 sheets, Instrument Panel   54  53         SECTION Vl – FUEL SYSTEM GROUP
                     Installation, Standard and Primary, 1952    35      Fuel System Installation      102  103
                     and 1953 Models
             18      Sheet 2 of 2 sheets, Instrument Panel   57  56
                     Installation, Standard and Primary, 1952                SECTION VII – CHASSIS GROUP
                     and 1953 Models                             36      Wheel Fender Installation, Model PA-20  106  105
             19      Instrument Panel Installation, Standard   59  58  37  Landing Gear Shock Unit and Fairings   107  108
                     and Primary, 1952 and 1953 Models                   Installation


            Date of Issue – March 1954
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