PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL

PIAGGIO P-180 AVANTI II · Maintenance Manual

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Overview

The Piaggio P.180 Avanti II Maintenance Manual provides detailed instructions and guidelines for the maintenance of the aircraft's navigation systems. It includes information on the pitot-static system, air data system, and standby instruments, along with maintenance practices and operational tests.

The manual is structured into chapters and sections for easy navigation.
It includes a list of effective pages with revision dates.
Maintenance practices cover removal and installation of various components.
Functional tests for systems are outlined to ensure proper operation.
The manual is intended for training purposes by the International AeroTech Academy.

Document

Source

Originally published by intaerotechamt.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Maintenance Manual
Year: 2012
File size: 12 MB
Publisher: intaerotechamt.com
Language: en

About this document

What is the PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL?

The PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL is a maintenance manual for the PIAGGIO P-180 AVANTI II, dated 2012.

Where does the PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL come from?

This copy of the PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL was originally published by intaerotechamt.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL published?

The PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL — the PIAGGIO P-180 AVANTI II maintenance manual on file — is dated 2012.

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the PIAGGIO P-180 AVANTI II.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More PIAGGIO P-180 AVANTI IImanuals & documents

In this document

Navigation - Description and Operation

This section provides an overview of the navigation systems in the Piaggio P.180 Avanti II.

Pitot-Static System - Description and Operation

Details the function and maintenance of the pitot-static system, including draining and leak testing.

Air Data System - Description and Operation

Describes the air data system's components and their operational roles.

Standby Instrument - Description and Operation

Covers the standby instruments used for air data and their operational significance.

Maintenance Practices

Outlines general maintenance practices for various systems, including removal and installation procedures.

Adjustment/Test Procedures

Includes procedures for testing and adjusting the air data computer and other systems.

Full document text

: PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL CHAPTER NAVIGATION International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 1 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER 34 - NAVIGATION LIST OF EFFECTIVE PAGES 34-LOEP 1 Sep.21/12 2 Sep.21/12 3 Sep.21/12 4 Sep.21/12 5 Sep.21/12 6 Sep.21/12 7 Sep.21/12 8 Sep.21/12 9 Sep.21/12 10 Sep.21/12 11 Sep.21/12 12 Sep.21/12 34-TOC 1 Nov. 15/10 2 Nov. 15/10 3 Nov. 15/10 4 Nov. 15/10 5 Nov. 15/10 6 Sep.21/12 7 Sep.21/12 8 Sep.21/12 9 Sep.21/12 10 Sep.21/12 11 Sep.21/12 12 Sep.21/12 34-00-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 34-10-00 1 Nov. 15/10 2 Dec. 15/09 34-11-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 CHAPTER SECTION SUBJECT PAGE DATE Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 2 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 34-11-00 201 Nov. 15/10 202 Nov. 15/10 203 Nov. 15/10 204 Nov. 15/10 205 Nov. 15/10 206 Nov. 15/10 207 Nov. 15/10 208 Nov. 15/10 209 Nov. 15/10 210 Nov. 15/10 211 Nov. 15/10 212 Nov. 15/10 213 Nov. 15/10 214 Nov. 15/10 215 Nov. 15/10 216 Nov. 15/10 217 Nov. 15/10 218 Nov. 15/10 219 Nov. 15/10 220 Nov. 15/10 221 Nov. 15/10 222 Nov. 15/10 223 Nov. 15/10 224 Nov. 15/10 225 Sep.21/12 226 Sep.21/12 227 Sep.21/12 228 Sep.21/12 229 Sep.21/12 230 Sep.21/12 231 Sep.21/12 232 Sep.21/12 233 Sep.21/12 234 Sep.21/12 34-11-00 501 Dec. 15/09 502 Dec. 15/09 503 Dec. 15/09 504 Dec. 15/09 505 Dec. 15/09 506 Dec. 15/09 34-12-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 3 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 9 Dec. 15/09 10 Dec. 15/09 11 Dec. 15/09 12 Dec. 15/09 34-12-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 34-12-00 501 Dec. 15/09 502 Dec. 15/09 34-13-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 9 Dec. 15/09 10 Dec. 15/09 11 Dec. 15/09 12 Dec. 15/09 34-13-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Jan.16/12 205 Jan.16/12 206 Dec. 15/09 34-14-00 1 Nov. 15/10 2 Nov. 15/10 3 Nov. 15/10 4 Nov. 15/10 34-14-00 201 Nov. 15/10 202 Nov. 15/10 203 Nov. 15/10 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 4 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 204 Nov. 15/10 205 Nov. 15/10 206 Nov. 15/10 34-20-00 1 Dec. 15/09 2 Dec. 15/09 34-21-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 9 Dec. 15/09 10 Dec. 15/09 34-21-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 207 Dec. 15/09 208 Dec. 15/09 34-21-00 501 Dec. 15/09 502 Dec. 15/09 34-22-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 34-22-00 201 Dec. 15/09 202 Dec. 15/09 34-23-00 1 Dec. 15/09 2 Dec. 15/09 34-23-00 201 Dec. 15/09 202 Dec. 15/09 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 5 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 34-40-00 1 Dec. 15/09 2 Dec. 15/09 34-41-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 9 Dec. 15/09 10 Dec. 15/09 34-41-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 34-42-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 34-42-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 34-43-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 34-43-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 6 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 206 Dec. 15/09 207 Dec. 15/09 208 Dec. 15/09 209 Nov. 15/10 210 Dec. 15/09 34-44-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 34-44-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 207 Dec. 15/09 208 Dec. 15/09 209 Dec. 15/09 210 Dec. 15/09 211 Dec. 15/09 212 Dec. 15/09 34-45-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 34-45-00 201 Dec. 15/09 202 Dec. 15/09 34-46-00 1 Sep.21/12 2 Sep.21/12 3 Sep.21/12 4 Sep.21/12 5 Sep.21/12 6 Sep.21/12 7 Sep.21/12 8 Sep.21/12 9 Sep.21/12 10 Sep.21/12 11 Sep.21/12 12 Sep.21/12 13 Sep.21/12 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 7 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 14 Sep.21/12 15 Sep.21/12 16 Sep.21/12 17 Sep.21/12 18 Sep.21/12 19 Sep.21/12 20 Sep.21/12 21 Sep.21/12 22 Sep.21/12 23 Sep.21/12 24 Sep.21/12 25 Sep.21/12 26 Sep.21/12 27 Sep.21/12 28 Sep.21/12 29 Sep.21/12 30 Sep.21/12 34-46-00 201 Sep.21/12 202 Sep.21/12 203 Sep.21/12 204 Sep.21/12 205 Sep.21/12 206 Sep.21/12 207 Sep.21/12 208 Sep.21/12 209 Sep.21/12 210 Sep.21/12 34-47-00 1 Sep.21/12 2 Sep.21/12 3 Sep.21/12 4 Sep.21/12 5 Sep.21/12 6 Sep.21/12 7 Sep.21/12 8 Sep.21/12 9 Sep.21/12 10 Sep.21/12 11 Sep.21/12 12 Sep.21/12 13 Sep.21/12 14 Sep.21/12 15 Sep.21/12 16 Sep.21/12 17 Sep.21/12 18 Sep.21/12 Sep.21/12

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International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 8 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 19 Sep.21/12 20 Sep.21/12 21 Sep.21/12 22 Sep.21/12 23 Sep.21/12 24 Sep.21/12 25 Sep.21/12 26 Sep.21/12 34-47-00 201 Sep.21/12 202 Sep.21/12 203 Sep.21/12 204 Sep.21/12 205 Sep.21/12 206 Sep.21/12 207 Sep.21/12 208 Sep.21/12 209 Sep.21/12 210 Sep.21/12 211 Sep.21/12 212 Sep.21/12 34-50-00 1 Dec. 15/09 2 Dec. 15/09 34-51-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 34-51-00 201 Dec. 15/09 202 Dec. 15/09 34-52-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 34-52-00 201 Dec. 15/09 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 9 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 202 Dec. 15/09 34-53-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 9 Dec. 15/09 10 Dec. 15/09 11 Dec. 15/09 12 Dec. 15/09 13 Dec. 15/09 14 Dec. 15/09 15 Dec. 15/09 16 Dec. 15/09 17 Dec. 15/09 18 Dec. 15/09 19 Dec. 15/09 20 Dec. 15/09 21 Dec. 15/09 22 Dec. 15/09 34-53-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 207 Dec. 15/09 208 Dec. 15/09 209 Dec. 15/09 210 Dec. 15/09 211 Dec. 15/09 212 Dec. 15/09 213 Dec. 15/09 214 Dec. 15/09 34-54-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 10 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 8 Dec. 15/09 34-54-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 34-55-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 7 Dec. 15/09 8 Dec. 15/09 9 Dec. 15/09 10 Dec. 15/09 34-55-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 34-56-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 34-56-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 34-57-00 1 Dec. 15/09 2 Dec. 15/09 3 Dec. 15/09 4 Dec. 15/09 5 Dec. 15/09 6 Dec. 15/09 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 11 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE 34-57-00 201 Dec. 15/09 202 Dec. 15/09 203 Dec. 15/09 204 Dec. 15/09 205 Dec. 15/09 206 Dec. 15/09 207 Dec. 15/09 208 Dec. 15/09 34-60-00 1 Dec. 15/09 2 Dec. 15/09 34-61-00 1 Sep.21/12 2 Sep.21/12 3 Sep.21/12 4 Sep.21/12 5 Sep.21/12 6 Sep.21/12 7 Sep.21/12 8 Sep.21/12 9 Sep.21/12 10 Sep.21/12 11 Sep.21/12 12 Sep.21/12 34-61-00 201 Sep.21/12 202 Sep.21/12 203 Sep.21/12 204 Sep.21/12 205 Sep.21/12 206 Sep.21/12 207 Sep.21/12 208 Sep.21/12 209 Sep.21/12 210 Sep.21/12 211 Sep.21/12 212 Sep.21/12 213 Sep.21/12 214 Sep.21/12 215 Sep.21/12 216 Sep.21/12 217 Sep.21/12 218 Sep.21/12 219 Sep.21/12 220 Sep.21/12 221 Sep.21/12 222 Sep.21/12 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 12 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-LOEP CHAPTER SECTION SUBJECT PAGE DATE INTENTIONALLY LEFT BLANK Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 1 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER 34 - NAVIGATION TABLE OF CONTENTS 34 NAVIGATION - Description and Operation 34-00-00 1 1. General 1 FLIGHT ENVIRONMENT DATA - Description and Operation 34-10-00 1 1. General 1 PITOT-STATIC SYSTEM - Description and Operation 34-11-00 1 1. General 1 PITOT-STATIC SYSTEM - Maintenance Practices 34-11-00 201 1. General 201 2. Pitot-Static System - Draining 201 3. Pitot Tube - Removal 202 4. Pitot Tube - Installation 207 5. Static Selector - Removal 207 6. Static Selector - Installation 208 7. Pitot-Static Leak Test 210 8. Pilot Pitot Line Check and Clean 210 9. Pilot Static Line Check and Clean 213 10. Co-pilot Pitot Line Check and Clean 215 11. Copilot Static Line Check and Clean 217 12. Static (Outer) Plate and Inner Port Step Height Measurement 225 13. Visual Inspection of the Region Surrounding the Static Ports (RVSM Critical Region) 230 PITOT-STATIC SYSTEM - Adjustment/test 34-11-00 501 1. Pitot-Static System - Functional Test 501 2. Autopilot (Altitude Hold) Performance Test 503 3. RVSM - Ground Test 504 CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY Nov. 15/10 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 2 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY AIR DATA SYSTEM - Description and Operation 34-12-00 1 1. Description 1 2. Operations 7 AIR DATA SYSTEM - Maintenance Practices 34-12-00 201 1. General 201 2. Air Data Computer - Removal 201 3. Air Data Computer - Installation 203 4. Total Air Temperature Probe - Removal 204 5. Total Air Temperature Probe - Installation 204 AIR DATA COMPUTER - Adjustment/test 34-12-00 501 1. Air Data Computer - Operational Test 501 STANDBY INSTRUMENT (AIR DATA SECTION) - Description and Operation 34-13-00 1 1. Description 1 2. Operations 4 3. Display 6 STANDBY INSTRUMENT - Maintenance Practices 34-13-00 201 1. General 201 2. Standby Instrument - Removal 201 3. Standby Instrument - Installation 203 4. Standby Instrument - Functional Check 203 5. Pneumatic Pressure Checks 204 6. Standby Instrument - Operational Check 205 LIGHTNING DETECTION SYSTEM - Description and Operation 34-14-00 1 1. Lightning Detection System (LDS) 1 Nov. 15/10 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 3 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY LIGHTNING DETECTION SYSTEM - Maintenance Practices 34-14-00 201 1.General 201 2. WX-1000E Processor - Removal 201 3. WX-1000E Processor - Installation 201 4. Lightning Detection Antenna - Removal 204 5. Lightning Detection Antenna - Installation 204 6. Lightning Detection System - Operational Test 205 ATTITUDE AND HEADING - Description and Operation 34-20-00 1 1. General 1 ATTITUDE AND HEADING SYSTEM - Description and Operation 34-21-00 1 1. Description 1 2. Operations 3 ATTITUDE AND HEADING SYSTEM - Maintenance Practices 34-21-00 201 1. General 201 2. Attitude and Heading Computer - Removal (AHC) 201 3. Attitude and Heading Computer(AHC) - Installation 203 4. Flux Detector Unit (FDU) - Removal 203 5. Flux Detector Unit - Installation 204 6. External Compensation Units (ECU) - Removal 206 7. External Compensation Units (ECU) - Installation 206 ATTITUDE AND HEADING SYSTEM - Adjustment/Test 34-21-00 501 1. Attitude and Heading Computer (AHC) - Operational Test 501 STANDBY INSTRUMENT (ATTITUDE SECTION) - Description and Operation 34-22-00 1 1. Description 1 2. Operations 3 3. Display 4 Nov. 15/10 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 4 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY STANDBY INSTRUMENT (ATTITUDE SECTION) - Maintenance Practices 34-22-00 201 1. General 201 MAGNETIC COMPASS - Description and Operation 34-23-00 1 1. Description 1 MAGNETIC COMPASS - Maintenance Practice 34-23-00 201 1. General 201 2. Magnetic Compass - Removal 201 3. Magnetic Compass - Installation 201 4. Magnetic Compass - Adjustment / Test 201 INDEPENDENT POSITION DETERMINING - Description and Operation 34-40-00 1 1. General 1 WEATHER RADAR SYSTEM - Description and Operation 34-41-00 1 1. Description 1 2. Operations 4 3. Displays 9 WEATHER RADAR SYSTEM - Maintenance Practices 34-41-00 201 1. General 201 2. Weather Radar Receiver/Transmitter - Removal 201 3. Weather Radar Receiver/Transmitter - Installation 203 4. Weather Radar Receiver/Transmitter - Inspection 203 5. Weather Radar Receiver/Transmitter - Operational Test 203 6. Weather Radar Receiver/Transmitter - Cleaning and lubrication 206 RADIO ALTIMETER SYSTEM - Description and Operation 34-42-00 1 1. Description 1 Nov. 15/10 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 5 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY 2. Operations 4 RADIO ALTIMETER SYSTEM - Maintenance Practices 34-42-00 201 1. General 201 2. Radio Altimeter Transceiver - Removal 201 3. Radio Altimeter Transceiver - Installation 203 4. Radio Altimeter Transceiver - Operational Test 203 5. Radio Altimeter Antenna - Removal 204 6. Radio Altimeter Antenna - Installation 206 TCAS I - Description and Operation 34-43-00 1 1. Description 1 2. Operation 3 3. Display 3 TCAS I - Maintenance Practices 34-43-00 201 1. General 201 2. Transmitter Receiver Computer (TRC) - Removal 201 3. Transmitter Receiver Computer (TRC) - Installation 203 4. TCAS I Antenna - Removal 203 5. TCAS I Antenna - Installation 205 6. TCAS I Configuration 205 7. TCAS I Antenna Calibration 207 8. TCAS I Data Verification 208 9. TCAS I System - Test 209 10. TCAS I Operate / Standby function 209 11. TCAS I Memory Configuration Module - Removal / Installation 209 TAWS - Description and Operation 34-44-00 1 1. Description 1 2. Operation 2 3. Displays 2 Nov. 15/10 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 6 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY TAWS - Maintenance Practices 34-44-00 201 1. General 201 2. TAWS Remote Computer - Removal 201 3. TAWS Remote Computer - Installation 202 4. TAWS Database - Updating 204 5. TAWS Configuration 206 6. TAWS Data Verification 208 7. TAWS Self Test 209 8. TAWS Inhibit 209 9. TAWS Audio Delay (TCAS I Installed) 210 10. TAWS Audio Priority (TCAS I Installed) 210 11. TAWS Failure Annunciations (TCAS I Installed) 210 12. TAWS Memory Configuration Module - Removal / Installation 210 TURBULENCE RADAR SYSTEM - Description and Operation 34-45-00 1 1. Description 1 2. Operations 2 TURBULENCE RADAR SYSTEM - Maintenance Practices 34-45-00 201 1. General 201 ACAS II - Description and Operation 34-46-00 1 1. Description 1 2. Operational Details 4 3. Operation 16 ACAS II - Maintenance Practices 34-46-00 201 1. General 201 2. ACAS II Computer - Removal 201 3. ACAS II Computer - Installation 201 4. ACAS II Directional Antenna - Removal 202 5. ACAS II Directional Antenna - Installation 203 6. ACAS II Self- Test 206 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 7 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY 7. ACAS II Functional Test 207 EGPWS - Description and Operation 34-47-00 1 1 1. Description 1 2. Operation 10 3. Enhanced Function 12 4. Controls 20 EGPWS - Maintenance Practices 34-47-00 201 1. General 201 2. EGPWS Remote Computer - Removal 201 3. EGPWS Remote Computer - Installation 202 4. EGPWS Database - Updating 204 5. Database Upload on EGPWS 206 6. EGPWS Configuration 209 7. EGPWS Self Test 210 8. EGPWS Inhibit 212 9. EGPWS Audio Priority (TCAS I or ACAS II Installed) 212 10. EGPWS Failure Annunciations 212 11. EGPWS Configuration Module - Removal / Installation 212 DEPENDENT POSITION DETERMINING - Description and Operation 34-50-00 1 1. General 1 RADIO TUNING UNIT (RTU) - Description and Operation 34-51-00 1 1. Description 1 2. Operation 4 RADIO TUNING UNIT (RTU) - Maintenance Practices 34-51-00 201 1. General 201 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 8 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY 2. Radio Tuning Unit - Removal 201 3. Radio Tuning Unit - Installation 201 4. Radio Tuning Unit - Test 201 CONTROL DISPLAY UNIT (CDU) - Description and Operation 34-52-00 1 1. Description 1 2. Operation 4 CONTROL DISPLAY UNIT (CDU) - Maintenance Practices 34-52-00 201 1. General 201 2. Control Display Unit - Removal 201 3. Control Display Unit - Installation 201 4. Control Display Unit - Test 201 VOR/ILS/MKR/ADF RECEIVER (VHF NAV) SYSTEM - Description and Operation 34-53-00 1 1. Description 1 2. Operation 6 3. Displays 16 VOR/ILS/MKR/ADF RECEIVER (VHF NAV) SYSTEM - Maintenance Practices 34-53-00 201 1. General 201 2. Navigation Receiver - Removal 201 3. Navigation Receiver - Installation 203 4. Navigation Receiver - Operational Test 203 5. Glideslope Antenna - Removal 203 6. Glideslope Antenna - Installation 205 7. Marker Beacon Antenna - Removal 205 8. Marker Beacon Antenna - Installation 206 9. VOR/LOC Antenna - Removal 208 10. VOR/LOC Navigation Antenna - Installation 210 11. ADF Antenna - Removal 210 12. ADF Antenna - Installation 211 13. Diplexer - Removal 213 14. Diplexer - Installation 213 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 9 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY DME SYSTEM - Description and Operation 34-54-00 1 1. Description 1 2. Operation 4 DME SYSTEM - Maintenance Practices 34-54-00 201 1. General 201 2. DME Transceiver - Removal 201 3. DME Transceiver - Installation 203 4. DME Transceiver - Operational Test 203 5. DME Antenna - Removal 203 6. DME Antenna - Installation 205 ATC TRANSPONDER - Description and Operation 34-55-00 1 1. Description 1 2. Operation 6 ATC TRANSPONDER - Maintenance Practices 34-55-00 201 1. General 201 2. ATC Transponder (TDR-94D) - Removal 201 3. ATC Transponder (TDR-94D) - Installation 203 4. ATC Transponder - Operational Test 203 5. Top and bottom ATC Transponder Antenna - Removal 203 6. Top and bottom ATC Transponder Antenna - Installation 204 GLOBAL POSITIONING SYSTEM (GPS) - Description and Operation 34-56-00 1 1. Description 1 2. Operation 4 GLOBAL POSITIONING SYSTEM (GPS) - Maintenance Practices 34-56-00 201 1. General 201 2. GPS Receiver - Removal 201 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 10 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY 3. GPS Receiver - Installation 203 4. GPS Antenna - Removal 203 5. GPS Antenna - Installation 205 6. GPS Receiver and Antenna - Operational Test 205 SECONDARY ATC TRANSPONDER - Description and Operation 34-57-00 1 1. Description 1 2. Operation 5 SECONDARY ATC TRANSPONDER - Maintenance Practices 34-57-00 201 1. General 201 2. Secondary ATC Transponder (TDR-94D) - Removal 201 3. Secondary ATC Transponder A (TDR-94D) - Installation 203 4. Secondary ATC Transponder - Operational Test 203 5. Top and bottom ATC Transponder Antenna - Removal 203 6. Top and bottom ATC Transponder Antenna - Installation 204 7. ATC Coaxial Relay - Removal 206 8. ATC Coaxial Relay - Installation 206 FLIGHT MANAGEMENT COMPUTING - Description and Operation 34-60-00 1 1. General 1 FLIGHT MANAGEMENT SYSTEM - Description and Operation 34-61-00 1 1. Description 1 2. Operation 9 FLIGHT MANAGEMENT SYSTEM - Maintenance Practices 34-61-00 201 1. General 201 2. Flight Management Computer - Removal/Installation 201 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 11 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY 3. Control Display Unit - Removal/Installation 201 4. Data Base Unit (DBU 4100 / DBU 5000) - Removal 201 5. Data Base Unit DBU 4100 / (DBU 5000) - Installation 202 6. Data Base Unit - Test 204 7. FMS Data Base Acquisition 204 8. FMS Data Base Upload - Preparation - DBU 4100 206 9. Upload 210 10. FMS Data Base Upload - DBU 5000 217 11. FMC-3000 - Battery Check 222 Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 12 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-TOC CHAPTER SECTION SUBJECT SUBJECT PAGE EFFECTIVITY INTENTIONALLY LEFT BLANK Sep.21/12 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 1 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 NAVIGATION - DESCRIPTION AND OPERATION 23-00-00 1. General A. Navigation system includes those systems, components and units which provide aircraft navigational information. The Maintenance Manual Chapter 34-00-00 “Navigation” consists in the following sections: 34-10-00 Flight Environment Data; 34-12-00 Attitude and Direction; 34-40-00 Independent Position Determining; 34-50-00 Dependent Position Determining System; 34-60-00 Flight Management Computing. Note that for the P180 AVANTI II avionics suite Localizer, Glide Slope and Marker Beacon functions (typically represented into the chapter 34-30-00, namely Landing and Taxing Aids) are integrated into a unique equipment, including VOR, ILS, MKR and ADF capability. These equipments have been included into the Section 34-50-00 “Dependent Position Determining System”. The Stand By Instrument, model GH-3100, is an independent equipment including both Air Data and Attitude data source capability. The Air Data section is represented in part of 34-10-00, while Attitude section, is represented on part of 34-20-00. The Radio Tuning Unit, model RTU-3000, that includes controls for both Communication and Navigation systems has been included into Section 34-50-00, while Communication section is recalled on the chapter 23-00-00, Communication Systems. The Control Display Unit, model CDU-3000, that includes controls for both Communication and Navigation systems has been included into Section 34-50-00, while Communication section is recalled on the chapter 23-00-00 Communication Systems and Flight Management Computing section is recalled into the 34-60-00. For general information, Navigation System schematic block diagram is shown in Fig. 1, Equipments location in the Nose Avionics Bay, in the Cockpit Instrument Panels and Antennas location are shown in the Fig. 2, 3 and 4. Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 2 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 B. In detail the chapter 34-00-00 “Navigation” consists of: (1) 34-10-00 “Flight Environment Data” The Section 34-10-00 “Flight Environment Data” includes that portion of the system which senses environmental conditions and uses the data to influence navigation. Includes such items as Air Data Computers, pitot/static systems, air temperature, rate-of-climb, airspeed, high speed warning, altitude reporting, altimeter correction system, etc. Specifically, the Section 34-10-00 “Flight Environment Data”, includes: 34-11-00 Pitot / Static System; 34-12-00 Air Data System; 34-13-00 Standby Instrument (Air Data section); Note that the Standby Instrument is an independent source including both Air Data and Attitude capability. Therefore the description of this component is shared between Sections 34-13-00 and 34-22-00. (2) 34-20-00 “Attitude & Direction” The Section 34-20-00 “Attitude and Direction” includes the portion of the system which uses magnetic or inertia forces to sense and display the direction or attitude of the aircraft. This includes sensing, computing, indicating, and warning devices, such as magnetic compasses, vertical and directional references, magnetic heading systems, attitude director systems, etc. Specifically, the Section 34-20-00 “Attitude and Direction” includes: 34-21-00 Attitude and Heading System; 34-20-00 Standby Instrument (Attitude section); 34-23-00 Magnetic Compass;. (3) 34-40-00 “Indipendent Position Determining” The Section 34-40-00 “Independent Position Determining” includes that portion of the system which provides information to determine position and is mainly independent of ground installation or orbital satellites. Includes items such as inertial guidance systems, weather radar, proximity warning, etc. Specifically, the Section 34-40-00 “Independent Position Determining” includes: 34-41-00 Weather Radar System. 34-42-00 Radio Altimeter. 34-43-00 TCAS I 34-44-00 TWAS 34-45-00 Turbulence Radar System Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 3 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 (4) 34-50-00 “Dependent Position Determining” The Section 34-50-00 “Dependent Position Determining” includes that portion of the system which provides information to determine position and is mainly dependent on ground installation or orbital satellites. Includes items such as DME, transponders, radio compass, VOR, ADF, GLOBAL POSITIONING, etc. Specifically, the Section 34-50-00 “Dependent Position Determining” includes: 34-51-00 Radio Tuning Unit; 34-52-00 Control Display Unit; 34-53-00 VOR/ILS/MKR/ADF Receiver(NAV); 34-54-00 DME System; 34-55-00 ATC Transponder; 34-56-00 Global Positioning System (GPS); 34-60-00 Secondary ATC Transponder. (5) 34-60-00 “Flight Management Computing” The Section 34-60-00 “Flight Management Computing” includes that portion of the system which combines navigational data to compute or manage aircraft’s geographical position or theoretical flight path. Includes items such as course computers, flight management computers, performance data computers, and associated control display unit, etc. Specifically, the Section 34-60-00 “Flight Management Computing” includes: 34-61-00 Flight Management System; Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 4 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 Fig. 1 - Navigation System Block Diagram Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 5 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 Fig. 2 - Nose Avionics Bay (Typical Lay-out) Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 6 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 Fig. 3 - Cockpit Instruments Panel (Typical Lay-out) 1. PFD #1 2. DCP #1 3. MFD 4. Reversionary Panel 5. Standby Instrument 6. DCP #2 7. PFD #2 8. RTU 9. CCP 10. CDU Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 7 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 Fig. 4 - A/C 3 view with Antennas (Typical Lay-out) Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 8 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-00-00 INTENTIONALLY LEFT BLANK Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 1 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-10-00 FLIGHT ENVIRONMENT DATA - DESCRIPTION AND OPERATION 1. General In this Section 34-10-00 “Flight Environment Data”, description is given for the systems which senses environmental conditions and uses the data to influence navigation. This section includes: 34-11-00 Pitot / Static System; 34-12-00 Air Data System; 34-13-00 Standby Instrument (Air Data section); 34-14-00 Lightning Detection System (LDS); The Standby Instrument is an independent source including both Air Data and Attitude capability. In this Section only the Air Data section is described. For attitude section refer to Section 34-22-00. The air data display, that uses pitot and static air pressure are: PFD 1, PFD 2, MFD and Standby instrument. In this section are described the data displays of these instruments. For the “MAINTENANCE PRACTICE” of the PFD 1, PFD 2, MFD, make reference to Chapter 31-00-00. Pitot and static air pressure is the source of the Air Data computers (refer to 34-12-00) and also the source of the Standby instrument (refer to 34-13-00). Other aircraft systems utilizing pitot and static air pressure are the cabin pressurization control and autopilot systems. – Refer to Chapter 22-00-00 for further information on the auto flight system. – Refer to Chapter 21-00-00 for further information on the cabin pressurization system. Nov. 15/10 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 2 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-10-00 INTENTIONALLY LEFT BLANK Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 1 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-11-00 PITOT-STATIC SYSTEM - DESCRIPTION AND OPERATION 23-11-00 1. General A. The Pitot-Static system supplies total and static air pressure for the operation of pilot and co-pilot equipments, instruments and the cabin pressure control system. The Pitot/Static system consists of two-Pitot probes located on the front fuselage under the forward wing, two double static-ports installed on the both sides of the fuselage, downward the second windows, an alternate static port on the right side of the fuselage and the related lines to equipments. The pilot and co-pilot Pitot/Static system are completely independent, the pilot Pitot/Static system provides static pressure and Pitot to primary Air Data Computer. The pilot static pressure can also be supplied by way of the alternate static port when the Static selector is turn from normal (STATIC TUBE) to alternate source (ALTERNATE SOURCE). The co-pilot system provides static pressure and Pitot to secondary Air Data Computer and to Stand-by Instrument, refer to schematic Block Diagram at Fig. 1. B. Pitot Probes: The Pitot probes, one installed on the left side and other on the right side of forward fuselage under the forward wing, provide ram air to the pilot and co-pilot air data systems. Each Pitot tube supplies the total pressure to the related side Air Data Computer. Additionally, the right side co-pilot Pitot tube supplies the total pressure also to the Stand-by instrument. (see Fig. 2). Each Pitot probe head is equipped with an electrical heating element to prevent icing. An Pitot heating monitor device is installed on the central instrument panel to provide the indication to the pilot that the pitot heating system electrical circuit is not operating or it has been interrupted. Indicator lights L PITOT HTR and R PITOT HTR, installed on annunciator panel, are controlled by monitor device according to the current sensitive relays, installed on the lines supplying power to the pitot heaters, detecting the current to the heating elements. For further detail refer to Chapter 24-00-00. Each Pitot Probe is provided with a drain hole to allow the draining of Pitot lines. Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 2 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-11-00 Fig. 1 - Pitot and Static System Schematic Block Diagram Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 3 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-11-00 Fig. 2 - Pitot probe Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 4 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-11-00 C. Static Ports: Three static ports are installed on the aircraft. Two static ports, are located on both sides of the fuselage, downward the second windows, the alternate static port, is located on the right side of the fuselage. Each port is provided with two static source openings. There is a set of openings (one per each side) for the pilot’s primary ADC and a set for the co-pilot’s secondary ADC. The right side static port provides also static pressure to Stand-by instrument. These static ports are aerodynamically compensated to minimize position error (see Fig. 3). The alternate static port, provides a selectable third independent static pressure line that can supply static pressure to the pilot primary Air Data Computer. Selection is made through a selector in the cockpit (see Fig. 4). Each port is equipped with an electrical heating element to prevent icing. For further detail refer to Chapter 24-00-00 The static system lines are drained through three screw plugs, two in the aircraft nose and a third one in the cockpit. For the location of screw plugs, refer to Fig. 202 in this Chapter. D. Static selector The static Selector, is located just below the switch panel, pilot side (see Fig. 4). The Static selector allows the selection of the normal (STATIC TUBE) or alternate source (ALTERNATE SOURCE) for the static pressure supply to the pilot primary Air Data Computer. Dec. 15/09 International AeroTech Academy For Training Purpose Only EFFECTIVITY: Page 5 PIAGGIO P.180 AVANTI II MAINTENANCE MANUAL 34-11-00 Fig. 3 - Static Ports Dec. 15/09 International AeroTech Academy For Training Purpose Only

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