Tecnam P2010 AMM Supplement S6
TECNAM P-2010 Gran Lusso · Maintenance Manual
Overview
The Tecnam P2010 Gran Lusso Maintenance Manual Supplement S6 provides detailed maintenance instructions and updates for aircraft equipped with the Lycoming IO-390 engine and G1000Nxi avionics. This document includes a list of effective pages, a record of revisions, and various chapters covering general descriptions, airworthiness limitations, maintenance schedules, and servicing practices.
- This is the 2nd Edition, Rev 2 of the maintenance manual.
- It covers modifications related to the Lycoming IO-390 engine.
- Includes a comprehensive inspection program.
- Contains updated procedures for exhaust installation and inspection.
- Maintains a record of revisions for operational updates.
- Provides dimensions and areas relevant to maintenance.
- Includes airworthiness limitations for safe operation.
- Details servicing practices for fuel and oil systems.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at regulations.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Maintenance Manual
- Year ·
- 2026
- File size ·
- 8.0 MB
- Copy found at ·
- regulations.gov
- Language ·
- en
What is the Tecnam P2010 AMM Supplement S6?
The Tecnam P2010 AMM Supplement S6 is a maintenance manual for the TECNAM P-2010 Gran Lusso, dated 2026.
What year was the Tecnam P2010 AMM Supplement S6 published?
The Tecnam P2010 AMM Supplement S6 — the TECNAM P-2010 Gran Lusso maintenance manual on file — is dated 2026.
Common. More common than 88% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the TECNAM P-2010 Gran Lusso.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
TECNAM P-2010 Gran Lusso for sale now
Free — save the P2010 to your watchlist and track it in one place.
More TECNAM P-2010 Gran Lussomanuals & documents
Related documents
- TECNAM P2010tdi - Aircraft Flight ManualTECNAM P2010 TDI · Weight & Balance
- Pilot's Operating Handbook for the Piper Pilot 100iPiper Pilot 100i · Pilot's Operating Handbook
- Starship 1 Maintenance ManualRaytheon 390 Premier 1 · Maintenance Manual
- DA-20 Katana FLIGHT MANUAL Day/NightDiamond DA20-A1 Katana · Pilot's Operating Handbook
- DA 40 AFMDiamond DA40 NG · Pilot's Operating Handbook
If you fly the TECNAM P-2010 Gran Lusso, you may also be researching these.
In this document
Introduction
The introduction outlines the purpose of the supplement and its importance for maintaining the aircraft's operational safety.
Airplane General Description
This section provides an overview of the aircraft's features and specifications.
Airworthiness Limitations
Details the airworthiness limitations that must be adhered to for safe operation.
Time Limits and Maintenance Schedule
Outlines the inspection program and maintenance schedules necessary for the aircraft.
Dimensions and Inspections Caps
Includes dimensions and areas relevant to the aircraft, along with control surfaces travel limits.
Servicing
Describes servicing practices for the fuel and oil systems, including refueling and oil level checking procedures.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
Tecnam P2010 AMM Supplement S6 2nd Edition, Rev 2 (08/01/2026) For airplanes embodying the Design Change MOD2010/078 “Lycoming IO-390 Engine and G1000Nxi avionic suite installation”. INTENTIONALLY LEFT BLANK 2nd Edition - Rev 2 SUPPLEMENT S6 LOEP Page 1 SUPPLEMENT S6 LOEP A List of Effective Pages (LOEP) for this Supplement is herein provided. All pages in the chapters are listed in sequence, together with the latest date of edition/revision of each page. 1st Edition, Rev 0 ..................... 21 September, 2017 1st Edition, Rev 1 ..................... 31 July, 2018 2nd Edition, Rev 0 ..................... 21 October, 2025 2nd Edition, Rev 1 ..................... 19 December, 2025 2nd Edition, Rev 2 ..................... 08 January, 2026 Section Page Edition / Revision LOEP 1 2nd Edition, Rev 2 2 2nd Edition, Rev 2 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 5 2nd Edition, Rev 0 6 2nd Edition, Rev 0 7 2nd Edition, Rev 1 8 2nd Edition, Rev 0 ROR 1 2nd Edition, Rev 0 2 2nd Edition, Rev 2 TOC 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 1 4 2nd Edition, Rev 0 Introduction 1 2nd Edition, Rev 1 2 2nd Edition, Rev 0 Chapter 03-00 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 Chapter 04-00 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 Chapter 05-20 1 2nd Edition, Rev 1 2nd Edition - Rev 2 SUPPLEMENT S6 LOEP Page 2 Section Page Edition / Revision Chapter 05-20 2 2nd Edition, Rev 1 3 2nd Edition, Rev 0 4 2nd Edition, Rev 2 Chapter 06-00 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 Chapter 06-20 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 Chapter 11-20 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 Chapter 11-30 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 5 2nd Edition, Rev 0 6 2nd Edition, Rev 0 Chapter 12-10 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 Chapter 12-20 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 Chapter 23-10 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 Chapter 28-10 1 2nd Edition, Rev 0 2nd Edition - Rev 0 SUPPLEMENT S6 LOEP Page 3 Section Page Edition / Revision Chapter 28-10 2 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 205 2nd Edition, Rev 0 206 2nd Edition, Rev 0 207 2nd Edition, Rev 0 208 2nd Edition, Rev 0 209 2nd Edition, Rev 0 210 2nd Edition, Rev 0 211 2nd Edition, Rev 0 212 2nd Edition, Rev 0 Chapter 31-00 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 5 2nd Edition, Rev 0 6 2nd Edition, Rev 0 7 2nd Edition, Rev 0 8 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 Chapter 34-20 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 5 2nd Edition, Rev 0 6 2nd Edition, Rev 0 2nd Edition - Rev 0 SUPPLEMENT S6 LOEP Page 4 Section Page Edition / Revision Chapter 34-20 7 2nd Edition, Rev 0 8 2nd Edition, Rev 0 9 2nd Edition, Rev 0 10 2nd Edition, Rev 0 11 2nd Edition, Rev 0 12 2nd Edition, Rev 0 101 2nd Edition, Rev 0 102 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 205 2nd Edition, Rev 0 206 2nd Edition, Rev 0 207 2nd Edition, Rev 0 208 2nd Edition, Rev 0 209 2nd Edition, Rev 0 210 2nd Edition, Rev 0 211 2nd Edition, Rev 0 212 2nd Edition, Rev 0 213 2nd Edition, Rev 0 214 2nd Edition, Rev 0 215 2nd Edition, Rev 0 216 2nd Edition, Rev 0 217 2nd Edition, Rev 0 218 2nd Edition, Rev 0 219 2nd Edition, Rev 0 220 2nd Edition, Rev 0 221 2nd Edition, Rev 0 222 2nd Edition, Rev 0 223 2nd Edition, Rev 0 2nd Edition - Rev 0 SUPPLEMENT S6 LOEP Page 5 Section Page Edition / Revision Chapter 34-20 224 2nd Edition, Rev 0 225 2nd Edition, Rev 0 226 2nd Edition, Rev 0 227 2nd Edition, Rev 0 228 2nd Edition, Rev 0 229 2nd Edition, Rev 0 230 2nd Edition, Rev 0 231 2nd Edition, Rev 0 232 2nd Edition, Rev 0 234 2nd Edition, Rev 0 235 2nd Edition, Rev 0 236 2nd Edition, Rev 0 237 2nd Edition, Rev 0 238 2nd Edition, Rev 0 239 2nd Edition, Rev 0 240 2nd Edition, Rev 0 241 2nd Edition, Rev 0 242 2nd Edition, Rev 0 243 2nd Edition, Rev 0 244 2nd Edition, Rev 0 245 2nd Edition, Rev 0 246 2nd Edition, Rev 0 247 2nd Edition, Rev 0 248 2nd Edition, Rev 0 249 2nd Edition, Rev 0 250 2nd Edition, Rev 0 Chapter 61-10 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 101 2nd Edition, Rev 0 2nd Edition - Rev 0 SUPPLEMENT S6 LOEP Page 6 Section Page Edition / Revision Chapter 61-10 102 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 205 2nd Edition, Rev 0 206 2nd Edition, Rev 0 207 2nd Edition, Rev 0 208 2nd Edition, Rev 0 Chapter 61-20 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 101 2nd Edition, Rev 0 102 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 205 2nd Edition, Rev 0 206 2nd Edition, Rev 0 207 2nd Edition, Rev 0 208 2nd Edition, Rev 0 Chapter 72-10 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 0 2nd Edition - Rev 1 SUPPLEMENT S6 LOEP Page 7 Section Page Edition / Revision Chapter 72-10 205 2nd Edition, Rev 0 206 2nd Edition, Rev 0 207 2nd Edition, Rev 0 208 2nd Edition, Rev 0 209 2nd Edition, Rev 0 210 2nd Edition, Rev 0 211 2nd Edition, Rev 0 212 2nd Edition, Rev 0 213 2nd Edition, Rev 0 214 2nd Edition, Rev 0 215 2nd Edition, Rev 0 216 2nd Edition, Rev 0 217 2nd Edition, Rev 0 218 2nd Edition, Rev 0
Show full textShow less
Chapter 78-10 1 2nd Edition, Rev 0 2 2nd Edition, Rev 1 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 201 2nd Edition, Rev 1 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 204 2nd Edition, Rev 1 205 2nd Edition, Rev 0 206 2nd Edition, Rev 0 207 2nd Edition, Rev 1 208 2nd Edition, Rev 1 Chapter 79-10 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 201 2nd Edition, Rev 0 202 2nd Edition, Rev 0 203 2nd Edition, Rev 0 2nd Edition - Rev 0 SUPPLEMENT S6 LOEP Page 8 Section Page Edition / Revision Chapter 79-10 204 2nd Edition, Rev 0 Chapter 92-00 1 2nd Edition, Rev 0 2 2nd Edition, Rev 0 3 2nd Edition, Rev 0 4 2nd Edition, Rev 0 5 2nd Edition, Rev 0 6 2nd Edition, Rev 0 7 2nd Edition, Rev 0 8 2nd Edition, Rev 0 9 2nd Edition, Rev 0 10 2nd Edition, Rev 0 11 2nd Edition, Rev 0 12 2nd Edition, Rev 0 13 2nd Edition, Rev 0 14 2nd Edition, Rev 0 2nd Edition - Rev 0 SUPPLEMENT S6 RECORD OF REVISIONS Page 1 SUPPLEMENT S6 RECORD OF REVISIONS In order to improve the aircraft safe and efficient operation, Tecnam, whenever considered necessary, will amend, add or delete information and instructions within the Supplement. A Record of Revisions to this Supplement is then provided and the operator is ad- vised to make sure that the record is kept up-to-date. The Supplement issue is identified by Edition and Revision codes reported on each page, lower right side. The revision code is numerical and consists of the number "0"; subsequent revisions are identified by the change of the code from "0" to "1" for the first revision to the basic publication, "2" for the second one, etc. Should be necessary to completely reissue a publication for contents and format changes, the Edition code will change to the next number (“2” for the second edi- tion, “3” for the third edition etc). Additions, deletions and revisions to existing text will be identified by a revision bar (black line) in the left-hand margin of the page, adjacent to the change. When technical changes cause expansion or deletion of text which results in un- changed text appearing on a different page, a revision bar will be placed in the right- hand margin adjacent to the page number of all affected pages providing no other revision bar appears on the page. These pages will be updated to the current regular revision date. NOTE: It is the responsibility of the owner to maintain this supplement in a current status when it is being used for operational purposes. 2nd Edition - Rev 2 SUPPLEMENT S6 RECORD OF REVISIONS Page 2 Record of Revisions Rev Revised page Description of Revision Tecnam Approval EASA Approval Or Under DOA Privileges DO OoA HDO 0 06-00 Added Section “Dimensions and Areas” Under DOA privileges (DOA ref. EASA21J.335) 1 INTRO/1 Updated Introduction 1 05-20/ 1, 2, 4 Updated Inspection Program 1 78-10/2 Updated Figure 1 78-10/204 Updated procedure “Exhaust In- stallation” 1 78-10/ 206 to 208 Added procedure “Exhaust Flame Tube Inspection” and related Figure 2 05-20/4 Updated Inspection Program 2nd Edition - Rev 0 SUPPLEMENT S6 TABLE OF CONTENTS Page 1 SUPPLEMENT S6 TABLE OF CONTENTS INTRODUCTION ................................................................................................. 1 CHAPTER 03 - AIRPLANE GENERAL DESCRIPTION .......................................... 1 General Features .................................................................................................... 1 CHAPTER 04 – AIRWORTHINESS LIMITATIONS ................................................ 1 AIRWORTHINESS LIMITATIONS TABLE ................................................................. 1 CHAPTER 05 – TIME LIMITS AND MAINTENANCE SCHEDULE ......................... 1 05 – 20 INSPECTION PROGRAM ............................................................................. 1 CHAPTER 06 – DIMENSIONS AND INSPECTIONS CAPS .................................... 1 06 – 00 Dimensions and Areas ............................................................................... 1 Control Surfaces Travel Limits .............................................................................. 1 06 – 20 Engine Cowling .......................................................................................... 1 Description and Operation ................................................................................................................. 1 Maintenance Practices ................................................................................................................... 201 Upper and Lower Cowling removal/installation ............................................................................. 203 CHAPTER 11- PLACARDS AND MARKINGS ....................................................... 1 11-20 – EXTERNAL PLACARDS ............................................................................... 1 11–30 – INTERNAL PLACARDS ............................................................................... 1 CHAPTER 12 – SERVICING............................................................................. 201 12 – 10 FUEL SYSTEM – Servicing Practices ..................................................... 201 General ........................................................................................................................................... 201 Refuelling Procedure ...................................................................................................................... 202 12 – 20 OIL SYSTEM – SERVICING PRACTICES ................................................. 201 General ........................................................................................................................................... 201 Oil Level Checking and Filling Procedure ........................................................................................ 202 Oil Change Procedure ..................................................................................................................... 203 CHAPTER 23 - COMMUNICATIONS .................................................................... 1 23-10 – SPEECH COMMUNICATIONS ..................................................................... 1 Description And Operation ..................................................................................... 1 CHAPTER 28 - FUEL SYSTEM ............................................................................ 1 28 – 10 Description And Operation ........................................................................ 1 Maintenance practices ................................................................................................................... 201 Fuel Quantity Indication Test ......................................................................................................... 203 Fuel Quantity Sender Replacement ................................................................................................ 204 Fuel Quantity Sender Calibration ................................................................................................... 205 CHAPTER 31 – INDICATING SYSTEM ................................................................ 1 Description and Operation ..................................................................................... 1 2nd Edition - Rev 0 SUPPLEMENT S6 TABLE OF CONTENTS Page 2 Garmin G1000NXi ................................................................................................... 3 MD – 302 Stand by Instrument ............................................................................... 8 Maintenance Practices ...................................................................................... 201 GDU 1050 display removal/ installation ......................................................................................... 203 CHAPTER 34 – NAVIGATION .............................................................................. 1 34-20 – GLASS COCKPIT – GARMIN G1000NXi ...................................................... 1 Description and Operation ................................................................................................................. 1 GDU 1050 (Display unit, PFD and MFD) ............................................................................................. 3 GIA 63W.............................................................................................................................................. 3 GRS 79 and GMU 44 ........................................................................................................................... 4 GDC 72 (Air Data Computer) .............................................................................................................. 4 GEA71 (Engine/Airframe Interface) .................................................................................................... 5 GTP 59 (OAT Probe) ............................................................................................................................ 6 GMA 1347 (Full Digital Audio Panel) .................................................................................................. 6 GTX 345R ............................................................................................................................................ 7 MD – 302 Stand by Instrument .......................................................................................................... 8 KN 63 DME .......................................................................................................................................... 9 ADF system (Automatic Direction Finder) (Optional) ....................................................................... 10 Emergency Locator Transmitter ....................................................................................................... 11 Troubleshooting ............................................................................................................................. 101 Maintenance practices ...................................................................................... 201 LRU Mechanical Installation General Features ................................................. 203 GDU 1050 display removal/installation & testing .............................................. 204 GMA 1347 removal/installation & testing .......................................................... 207 GIA 63W removal/installation & testing ............................................................. 207 GDC 72 removal/installation............................................................................... 208 GDC 72 testing and leak test ............................................................................. 210 GTX345R removal/installation & testing ........................................................... 212 GRS 79 removal/installation & testing ............................................................... 214 GMU44 removal/installation & testing ............................................................... 216 GEA71 removal/installation & testing ................................................................ 216 KN 63 removal/installation & testing................................................................. 216 ADF System removal/installation & testing ....................................................... 216 Software Upload ................................................................................................. 217 Single LRU SW Uploaded ................................................................................... 227 Option Equipment SW Upload ............................................................................ 235 SW Testing Procedure ........................................................................................ 242 ADF Check out .................................................................................................... 246 DME Checkout .................................................................................................... 246 Final Check-List.................................................................................................. 247 Configuration Mode ............................................................................................ 249 CHAPTER 61- PROPELLER ................................................................................. 1 61-10 – Propeller ..................................................................................................... 1 Description and Operation ................................................................................................................. 1 Troubleshooting ............................................................................................................................. 101 Maintenance Practices ................................................................................................................... 201 Propeller Removal .......................................................................................................................... 203 2nd Edition - Rev 1 SUPPLEMENT S6 TABLE OF CONTENTS Page 3 Propeller Installation ...................................................................................................................... 204 61-20 – Propeller Control ........................................................................................ 1 Troubleshooting ............................................................................................................................. 101 Maintenance Practices ................................................................................................................... 201 Governor replacement ................................................................................................................... 203 CHAPTER 72 - ENGINE ....................................................................................... 1 72-10 ENGINE ......................................................................................................... 1 Description and Operation ................................................................................................................. 1 Maintenance practices ................................................................................................................... 201 Engine Removal .............................................................................................................................. 203 Engine Installation .......................................................................................................................... 205 Powerplant Controls Rigging .......................................................................................................... 212 CHAPTER 78- EXHAUST..................................................................................... 1 78-10 Exhaust ......................................................................................................... 1 Description and Operation ................................................................................................................. 1 Maintenance Practices ................................................................................................................... 201 Exhaust Removal ............................................................................................................................ 203 Exhaust Installation ........................................................................................................................ 204 Heat Exchanger Inspection ............................................................................................................. 205 Exhaust Flame Tube Inspection ...................................................................................................... 206 CHAPTER 79 - OIL SYSTEM ............................................................................... 1 79 – 10 Oil System .................................................................................................. 1 Description and Operation ................................................................................................................. 1 Maintenance Practices ................................................................................................................... 201 Oil Tank Cleaning ............................................................................................................................ 203 Oil Cooler Replacement .................................................................................................................. 203 CHAPTER 92 – WIRING DIAGRAMS .................................................................... 1 2nd Edition - Rev 0 SUPPLEMENT S6 TABLE OF CONTENTS Page 4 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 1 SUPPLEMENT S6 INTRODUCTION Page 1 INTRODUCTION This AMM Supplement applies to aircrafts which embody the Design Change 2010/078. This will be accomplished by the installation of the following systems: Garmin G1000Nxi integrated flight deck suite Lycoming IO-390-C3B6 Engine, with a new nacelle and oil cooler Alternative MT propeller three blades variable pitch The installation of this design change will keep the operational capabilities of the basic type certificated A/C (full day/night IFR). Figure 1- P2010 with design change 2010/078 embodied Herein are reported the ATA Chapters impacted by the design changes mentioned 2nd Edition - Rev 0 SUPPLEMENT S6 INTRODUCTION Page 2 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 0 03-00 AIRPLANE GENERAL DESCRIPTION Page 1 CHAPTER 03 - AIRPLANE GENERAL DESCRIPTION GENERAL FEATURES Engine Manufacturer Lycoming Textron Model IO-390-C3B6 Maximum power 160.3 kW (215 hp) @ 2700 rpm Maximum continuous power 160.3 kW (215 hp) @ 2700 rpm (continuous) Certification base CS-E Amendment 4 (FAR 33) Certification approval EASA TCDS N° IM.E.097 Engine features Fuel injected (I), direct drive,4 cylinders horizontally op- posed (O), air cooled with down exhaust outlets Propeller Manufacturer MT-Propeller Entwicklung GmbH Type certificate EASA.P.013 Model MTV-12B/183-59L Blades 3 Diameter 1830mm Type Variable pitch propeller at constant speed Governor P-860-23 Governor type Hydraulic Constant Speed Governor 2nd Edition - Rev 0 03-00 AIRPLANE GENERAL DESCRIPTION Page 2 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 0 04-00 AIRWOTHINESS LIMITATIONS Page 1 CHAPTER 04 – AIRWORTHINESS LIMITATIONS AIRWORTHINESS LIMITATIONS TABLE The Airworthiness Limitations Section is not affected by the change. Refer to AMM Chapter. 04 “Airworthiness Limitations”. 2nd Edition - Rev 0 04-00 AIRWOTHINESS LIMITATIONS Page 2 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 1 05-20 INSPECTION PROGRAM Page 1 CHAPTER 05 – TIME LIMITS AND MAINTENANCE SCHEDULE 05 – 20 INSPECTION PROGRAM The following table shows the maintenance tasks performed at defined intervals to retain an item in a serviceable condition by systematic inspection, detection, replacement of wear out items, adjustment, calibration, cleaning, etc. as applica- ble. The inspections are grouped as follows: A – first 25 hr and every 50 hr B - every 100 hr or every year (WOF) C - every 600 hr or every 3 years (WOF) D - every 1200 hr or every 5 years (WOF) E - every 2000 hr A B C D E Flight hours First 25 hr and every 50 hr 100 hr 600 hr 1200 hr 2000 hr Calendar schedule - 1 year 3 years 5 years - Inspection program table The airframe inspection time limits may not exceed by one (1) month or +10% FH, with a maximum of 60 FH. At the same time, the inspections may be antici- pated as required, keeping the upcoming inspections interval unchanged. Limit excess cannot be accumulated. If, for example, the initial 100 FH hour in- spection is performed at 110 FH, the 600 hours inspection is still due at 600 FH and the next 100 FH inspection shall be accomplished after 90 FH. For engine and propeller, refer to related manuals. All the tasks are grouped in function of ATA-100 code. The first column shows the ATA code which the item belongs to, the second col- umn shows the system name, the third column shows the maintenance task and the last columns shows the task frequency required, namely: – Column A : if a “X” is indicated in this column, the task must be performed at each “A” inspection – Column B : if a “X” is indicated in this column, the task must be performed at each “B” inspection 2nd Edition - Rev 1 05-20 INSPECTION PROGRAM Page 2 – Column C : if a “X” is indicated in this column, the task must be performed ateach “C” inspection – Column D : if a “X” is indicated in this column, the task must be performed at each “D” inspection – Column E : if a “X” is indicated in this column, the task must be performed at each “E” inspection Equipment inspections, requiring a different time interval, are shown as well. In this case the frequency is declared. The instruction to make repairs or replacements of inspected items can be found in the related component/system ATA Chapter. A log book entry should be made upon completion of any inspections For checks and inspections to be carried out, refer to the following general rules: MOVABLE PARTS for lubrication, security of attachment, safetying, excessive wear, correct travel, cracked fittings, safety of hinges, defective bearings, cleanli- ness, corrosion, deformation and tension. FLUID LINES and HOSES for leaks, cracks, dents, kinks, chafing, proper radius, corrosion, obstructions and deterioration. METAL PARTS for security of attachment, cracks, metal distortion, broken spot- welds and riveting, corrosion and any other apparent damage WIRING for security, chafing, burning, defective insulation, loose or broken ter- minals, heat deterioration. BOLTS for correct torque, safetying and damaged thread FILTERS and FLUID for cleanliness, contamination and/or replacement if re- quired. Make sure that all Airworthiness Directives and Service Bulletins are imple- mented as required. Tecnam can change the time between checks publishing the change as a revision of this Maintenance Manual. 2nd Edition - Rev 0 05-20 INSPECTION PROGRAM Page 3 Engine inspections Refer to Lycoming Engine Maintenance Manual MM-IO-390-C Series -last issue – for en- gine inspections and maintenance with related schedule. Consult also applicable service bul- letins and instruction books regarding the repair and overhaul, inspection and installation of engines. Propeller and Governor inspections Refer to MT-Propellers Operation and Installation Manual E124 -last issue – for propeller inspections and maintenance with related schedule. Refer to MT-Governor Operation and Installation Manual E-1048 -last issue – for governor inspections and maintenance with related schedule. Vendor Equipment inspection For main vendor equipment installed make reference to applicable maintenance instructions addressed on related Component Maintenance Manuals (CMM). Inobservance of this rec- ommendation may affect the aircraft airworthiness. In addition to the basic Aircraft Maintenance Manual, the Maintenance instructions for MOD2010/078 “Lycoming IO-390 Engine and G1000Nxi avionic suite installation” are in- cluded in the manufacturer documents. In addition to the basic Aircraft Maintenance Manual, a list of applicable CMMs is herein reported: Table 1 - Vendor Equipment list Equipment Unit function Doc.No Doc. Description GDU 1050 Display Unit (PFD and MFD) 190-00303-92 GDU 105X Installation Manual GIA 63W COM/NAV/GPS interface 190-00303-05 Garmin GIA 63/GIA 63W Installation Manual GRS 79 AHRS 190-01852-00 Garmin GRS 79/GMU 44 Installation Manual GMU 44 Magnetometer 190-00303-10 GDC 72 ADC -Air Data Computer 190-01855-00 Garmin GDC 72 Installation Manual GEA 71 EIS units 190-00303-40 Garmin GEA 71 Installation Manual GAP 26 Heated Pitot Probe 190-01115-01 G3X/G3X Touch Installation Manual GTP 59 OAT Probe 190-01855-00 GDC 72 Installation Manual GMA 1347 Full digital audio panel 190-00303-20 GMA 1347 Installation Manual GTX 345R MODE-S/ADSB-OUT/ADSB- IN-FIS-B XPDR 190-01499-02 E GTX 3X5 Transponder TSO Installation Manual KN 63 DME 006-00176-0004 Bendix-King KN-63 Installation Man- ual MD-302 Stand-by instrument 9017782 Mid-Continent MD302 Installation Manual ELT Emergency Locator transmitter E04M ACK Model E-04 ELT – Installation Manual / Operation Manual RA-3502/AC- 3504 ADF System DV 30613.03 Becker ADF 3500 System Manual 2nd Edition – Rev 2 05-20 INSPECTION PROGRAM Page 4 1. Scheduled Maintenance In addition to the basic Aircraft Maintenance Manual, the following maintenance tasks need to be considered. NOTE: When the ATA Chapter and subchapter are included in the table below, they replace those in basic AMM. If the ATA Chapter and subchapter are not listed below, refer to inspection tasks in basic AMM ATA Item Maintenance Task FREQUENCY A B C D E 78 Exhaust Perform the exhaust flame tube in- spection (Refer to ATA 78-10-00 – Exhaust Flame Tube Inspection) Every 200 hrs, SB 937-CS 78 Exhaust Visually inspect exhaust manifold, muffler for condition and security of installation X 78 Exhaust Disassembly the exhaust system, in- cluding the removal of thermal coat and check it for deformation, dam- age or cracks X 78 Exhaust Muffler mounting springs and safety wire: check for integrity X 78 Exhaust Remove and inspect heat exchanger 200 hrs. 2nd Edition - Rev 0 06-00 DIMENSIONS AND AREAS Page 1 CHAPTER 06 – DIMENSIONS AND INSPECTIONS CAPS 06 – 00 DIMENSIONS AND AREAS Control Surfaces Travel Limits Ailerons Up 19°; Down 14 ° ( 2°) Stabilator (*) Up 6°; Down 17° ( 2°) Stabilator trim tab Up 3°; Down 15° ( 1°) Stabilator trim tab (**) Up 3°; Down 6° ( 1°) Rudder RH 25°; LH 25° ( 2°) Rudder trim RH 20°; LH 20° ( 2°) Flaps 0°; 40° ( 1°) (*) Degrees are measured from the Stabilator Leading Edge. (**) When MOD 2010/133 is installed 2nd Edition - Rev 0 06-00 DIMENSIONS AND AREAS Page 2 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 0 06-20 ENGINE COWLING – DESCRIPTION AND OPERATION Page 1 06 – 20 ENGINE COWLING Description and Operation The engine cowling is made of carbon fiber material and consists of two parts: 1. Upper engine cowling 2. Lower engine cowling Figure 2-Engine cowling All internal surfaces of engine cowlings including the internal side of engine oil level door are protected by an ablative varnish. An oil level inspection door is located on RH side of upper engine cowling. 2nd Edition - Rev 0 06-20 ENGINE COWLING – DESCRIPTION AND OPERATION Page 2 Figure 3 - Engine cowling oil level inspection door For others scheduled inspection operations the upper and lower engine cowlings are easily removable by a series of steel screws as indicated in figures below: Figure 4 - Engine cowling fittings side view 2nd Edition - Rev 0 06-20 ENGINE COWLING – DESCRIPTION AND OPERATION Page 3 Figure 5 - Engine cowling fittings front view Figure 6 – Cold air hose fitting 2nd Edition - Rev 0 06-20 ENGINE COWLING – DESCRIPTION AND OPERATION Page 4 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 0 06-20 ENGINE COWLING – MAINTENANCE PRACTICES Page 201 Maintenance Practices This Chapter contains the following maintenance tasks description: Upper and lower cowling removal/installation Ablative paint restoration 2nd Edition - Rev 0 06-20 ENGINE COWLING – MAINTENANCE PRACTICES Page 202 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 0 06-20 ENGINE COWLING – MAINTENANCE PRACTICES Page 203 Upper and Lower Cowling removal/installation The upper and lower removal/installation procedure is herein reported. Removal Procedure Step no. Upper and lower cowling removal Task description Additional info & References 1. Engage parking brake. 2. Unscrew the 2 screws that connect the upper cowl- ing to the fuselage. Refer to Figure 5 3. Unscrew the 8 quick fasteners and 4 screws (6 on RH side and 6 on LH side) that connect the upper cowling to the lower cowling Refer to Figure 4 4. Disconnect the Cold air hose from the firewall by lifting gently the upper cowling. Refer to Figure 5 5. Remove the upper cowling. Carefully lift the upper cowl- ing panel up to clear the air- plane. Put it in a safe place on a surface which does not dam- age the panel. 6. Disconnect the connector of taxing/landing lights from lower engine cowling 7. Unscrew the 10 screws (5 on RH side and 5 on LH side) that connect the lower cowling to the fuselage. Sustain the cowling during screws removal Refer to Figure 4 8. Remove the cold air hose form the alternate air valve and the hose from the front air intake 9. Remove the oil drainage hose from the lower cowl- ing 10. Remove the lower cowling. Carefully remove the lower cowling. Put it in a safe place, on a surface which does not damage the panel. 2nd Edition - Rev 0 06-20 ENGINE COWLING – MAINTENANCE PRACTICES Page 204 Installation Procedure Step no. Upper and lower cowling installation Task description Additional info & References 1. Engage parking brake. 2. Check the panels for damage, cracks and splits, blis- tering and flaking of the paint finish. 3. Check the screws for conditions. 4. Make sure cowlings are cleaned. If required clean the surfaces of the panels 5. Make sure that the ablative paint coat is not dam- aged. If required, restore ablative paint coat i.a.w. procedure ad- dressed on this Chapter 6. Remove the front net of lower cowling 7. Connect the Connect the cold air hose to alternate air valve and hose to front air intake 8. Connect the oil drainage hose to lower cowling 9. Put in position the lower cowling, if removed. Make sure that there are not in- terferences with the engine air intake and water and oil coolers 10. Adjust the hose on the alternate air valve through the intake where the net was installed, then reinstall the net 11. Connect the connector of taxing/landing lights of lower engine cowling 12. Fix the 10 screws which connect the lower cowling panel to the fuselage. Sustain the cowling during screws fixing Refer to Figure 4 13. Put in position the upper cowling. 14. Connect the Cold air hose to the firewall Refer to Figure 6 15. Fix the 8 fasteners and 4 screws (6 on LH and 6 on RH side) which connect the upper cowling to the lower cowling on front side of cowling. Refer to Figure 4 16. Fix the 2 screws that connect the upper cowling to the fuselage. Refer to Figure 5 2nd Edition - Rev 0 11-20 EXTERNAL PLACARDS – DESCRIPTION AND OPERATION Page 1 CHAPTER 11- PLACARDS AND MARKINGS 11-20 – EXTERNAL PLACARDS On both sides of oil inspection door are located two placards. On the external side is located the “Oil Check Placard”. Figure 7 – External oil inspection door placard On the internal side of the door is located the “Oil Filler” placard. Figure 8 – Internal oil inspection door placard Figure 9 – Internal and external oil inspection door placards installation 2nd Edition - Rev 0 11-20 EXTERNAL PLACARDS – DESCRIPTION AND OPERATION Page 2 INTENTIONALLY LEFT BLANK 2nd Edition - Rev 0 11-30 INTERNAL PLACARDS – DESCRIPTION AND OPEARATION Page 1 11–30 – INTERNAL PLACARDS Garmin G1000 NXi suite provides flight, trim, engine and map navigation information. The picture and table below show a detailed description of the instrument panel. Figure 10 – P2010 Instrument Panel No Description No Description 1 GDU 1050 (PFD) 14 Carburettor Heat 2 Limitation Placards 15 Defrost & Cabin Heat 3 Audio Panel 16 Throttle Lever 4 MD-302 Standby Attitude Module 17 Fuel Selector 5 Magnetic Compass 18 Lights Switches 6 GDU 1050 (MFD) 19 Pitot Heat 7 Breaker Panel 20 Trim Disconnect 8 Emergency Light 21 AP Master 9 Day/Night Switch 22 Avionic Master 10 Instruments/Panel lights dimmers 23 Fuel Pump 11 Flaps switch 24 Master/Generator 12 Mixture Lever 25 Engine Start 13 Cabin Heat 26 ELT Table 2 – P2010 Instrument Panel 2nd Edition - Rev 0 11-30 INTERNAL PLACARDS – DESCRIPTION AND OPEARATION Page 2 The main flight information is shown on PFD while map, trim and engine information is dis- played on the MFD. In the event of a PFD failure, the system automatically switches flight information on the MFD keeping the engine data on this display. The below picture shows default indications displayed on PFD. Figure 11 - Garmin G1000Nxi PDF Display As shown in the above figure flight information layout on PFD is as follows: Attitude indicator is located at the top center of display. Directional gyro indicator is located below the attitude indicator. Airspeed indicator is located on the left of attitude indicator. Altitude indicator is located on the right of attitude indicator. Vertical speed indicator is located on the right of altitude indicator.