Tecnam P2002 JF - Flight Control System (Flaps)

Tecnam P2002 JF

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Page 7 2

nd

Edition – Rev 0

03-00

AIRPLANE GENERAL DESCRIPTION

Rudder is operated through a cable system. The rudder has a trim tab adjustable on the

ground: allows aircraft directional trimming.

Figure 7: Flight control system (Flaps)

Table of Contents

Chapter 0 113
- Foreword13
- Manual Breakdown and Organization14
- Abbreviations17
- Occurrence Reporting Instructions19
Chapter 10189
- General189
- Procedure189
- Mooring190
- Markings and Placards195
Chapter 11201
- Markings and Placards201
- Exterior Colour202
Chapter 20252
- Maintenance Practices252
- General252
- Torque Values254
- Hot Air System282
Chapter 21282
- Description and Operation282
Chapter 23306
- Description and Operation306
- Garmin GNS 530W307
Chapter 24332
- General332
- Power Generation334
- Generators334
Chapter 25366
- Equipment and Interiors - General366
- Cabin Interiors366
Chapter 27 Description and Operation405
- Ailerons407
- Description and Operation407
Chapter 28457
- Description and Operation457
Chapter 32513
- Landing Gear513
- Mlg and Brakes514
- Description and Operation514
Chapter 33571
- Description and Operation571
- Navigation588
CHAPTER 34 Pitot-Static System593
- Alternate Static Port595
- Stall Warning System595
- Troubleshooting596
- Maintenance Practices597
- Instruments Replacement598
Chapter 52681
- Maintenance Practices681
- Canopy Handle Support Installation682
Chapter 56744
- Description and Operation744
- Maintenance Practices748
- Windshield Replacement749
- Side Windows Replacement752
Chapter 61788
- Description and Operation788
- Troubleshooting790
- Maintenance Practices791
- Propeller Removal792
- Power Plant798
Chapter 54803
- Engine Cowlings803
- Description and Operation803
- Maintenance Practices806
- Engine Cowling Removal807
Chapter 78851
- Description and Operation851
Chapter 79 Description and Operation869
- Rotax 912S Oil Circuit Schematic (Oil Temperature below 90°C)870
- Rotax 912S Oil Circuit Schematic (Oil Temperature 90°C to 100°C)871
- Rotax 912S Filter Cartridge (Section)872
- Rotax 912S Oil Circuit Schematic (Oil Temperature > 100°C)872
- Oil Radiator873
- Radiator873
- Oil Tank874
- Oil Tank Ventilation Flow874
- Maintenance Practices877
- Oil Tank Cleaning878
- Oil Tank Replacement878
- Oil Cooler Replacement880
Chapter 80893
- Description and Operation893
Chapter 12 - Servicing912
Chapter 55 - Stabilator and Rudder920
Chapter 57 - Wings928
- Control Cable and Hoses Pre-Installation Procedure930
- Wing Installation930
- Wing Pre-Installation Procedure930
Chapter 72 - Engine944
- Maintenance Practices944
- Engine Check944
- Powerplant Controls Rigging944
Chapter 5 - TIME LIMITS and MAINTENANCE SCHEDULE1041
Chapter 31 - INDICATING SYSTEM1067
- Troubleshooting1067
- GDU 620 PFD/MFD Removal/Installation1079
- GRS 77 AHRS Removal/Installation1079
- GMU 44 Removal/Installation1079
- GDC 74A (ADC) Removal/Installation1079
- Software Upload1084
- Maintenance Practices1101
- Standby Attitude Indicator Replacement and Testing1101
Chapter 92 - WIRING DIAGRAMS1110
- Tecnam P2002-JF AMM Supplement S21140
- Maintenance Practices1152
- Seats Installation1153
- Seats Removal1153
- Chapter 55 - Stabilator and Rudder1158
- Maintenance Practices1160
- Stabilator Pre-Installation Procedure1160
- Control Cable and Hoses Pre-Installation Procedure1168
- Wing Installation1168
- Wing Pre-Installation Procedure1168
- Engine Check1182
- Maintenance Practices1182
- Powerplant Controls Rigging1182
- Tecnam 2002-JF AMM Supplement S-11192

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