SILA 450C Spare Parts Catalog
Aero East Europe Sila 450 C · Parts Catalog
Overview
The Aero-East-Europe SILA 450C Spare Parts Catalog is a comprehensive guide for identifying and ordering replacement parts for the SILA 450C airplane. It includes detailed sections on various components of the aircraft, along with ordering instructions and contact information for the manufacturer.
- The catalog is intended for Aero East Europe personnel and authorized dealers only.
- It includes sections on fuselage, empennage, wings, landing gear, and fuel system.
- Each part listing contains position, name, barcode, description, price, and image.
- Ordering can be done via phone, fax, or email.
- The SILA 450C is certified according to German LTF-UL and French requirements.
- The airplane is designed for multiple purposes including sport flying and pilot training.
- Optional equipment varies by customer request.
- Hardware items are not supplied by Aero East Europe.
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 aeroeast.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Parts Catalog
- Year ·
- 2014
- File size ·
- 9.9 MB
- Copy found at ·
- aeroeast.net
- Language ·
- en
What is the SILA 450C Spare Parts Catalog?
The SILA 450C Spare Parts Catalog is a parts catalog for the Aero East Europe Sila 450 C, dated 2014.
What year was the SILA 450C Spare Parts Catalog published?
The SILA 450C Spare Parts Catalog — the Aero East Europe Sila 450 C parts catalog on file — is dated 2014.
Most owners only have the POH. Here's the essential set for the Aero East Europe Sila 450 C.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Aero East Europe Sila 450 Cmanuals & documents
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In this document
Introduction
The introduction outlines the purpose of the catalog and its intended audience, emphasizing the prohibition of copying and reproduction.
Parts Identification
This section describes the steps for identifying specific parts within the catalog, including using the table of contents and part listings.
Method for Parts Ordering
Details the process for ordering parts, including necessary information such as part name and barcode.
Optional Equipment
Lists optional equipment available for the SILA 450C, which varies based on customer requests.
Hardware
Explains that attaching hardware like nuts and bolts are not supplied by Aero East Europe but must meet aeronautical standards.
Company Background
Provides a brief history of Aero East Europe, including its founding, production history, and certifications.
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
Aero-East-Europe d.o.o. SILA 450C SPARE PARTS CATALOG 1 SILA 450C SPARE PARTS CATALOG ADRESS: Aerodromska BB 36000 Kraljevo Serbia PHONE: 063/318-660 FAX: 036/318-660 MAIL: aeroeasteurope@gmail.com INTRODUCTION In front of you is the first spare parts catalog of the Aero East Europe Company. The purpose of this parts catalog is for identification of all replacement parts of SILA 450C airplane. Using of this catalog is allowed only for Aero East Europe personnel and authorized dealers. Copying and reproduction of this parts catalog is prohibited. THE STRUCTURE OF THE PARTS CATALOG Parts catalog is divided into five major sections which are: Fuselage Empennage Wings Landing gear Fuel system Each sub section of the airplane contains data for every part of an subassembly such as position in the assembly, part’s name and bar code, description, price and image. The structure of the catalog is illustrated in the figure 1. PARTS IDENTIFICATION For the identification of a specific part, one should complete next steps, as follows: 1. According to figure 2 (Complete airplane) find the section of your interest 2. Turn to table of contents and find the section. Note that each section is divided into several different sub-sections 3. Find the corresponding sub-section. The sub-section contains a figure of the subassembly with labeled parts 4. In the parts listing, look for the corresponding part number for the complete description of your part. Major assembly Subassembly Part listing Position Name/B ar code Picture Descript ion Price Figure 1: The structure scheme of the part catalog HARDWARE Hardware Such as nuts, bolts, screws, etc. those who are available as commercial items, usually is not supplied by Aero East Europe. The parts listing will contain those items of attaching hardware required for main assemblies and installations. All hardware must be in aeronautical standard with proper quality. OPTIONAL EQUIPMENT Optional equipment depends from customer request, and is different for each particular model. Under the optional equipment there are GPS navigation, GYRO-directional, G meter, etc. 2 INTRODUCTION METHOD FOR PARTS ORDERING For ordering of a specific part one should provide the part’s name, bar code and / or part’s identification, with the respect to the part’s identification procedure, and the parts listing. THE WAYS FOR ORDERING PARTS Ordering by the telephone 036/318-660 Ordering by fax 036/318-660 Ordering by email aeroeasteurope@gmail.com For any additional information please contact us at: 036/318-660 Aero East Europe d.o.o. Technical Department 3 AERO EAST EUROPE D.O.O. Aero East Europe was founded in 2006. Assembling of the airplanes began in Italy where, during 2006-2007, 30 airplanes were assembled, after which the entire production was transferred to Kraljevo Serbia. In Serbia, in cooperation with the Faculty of Mechanical Engineering in Belgrade, and Kraljevo, the company continues to produce airplanes. Until now over 100 airplanes were produced, and in the same time a new airplane was designed and manufactured, the SILA 450 C (Serbian Industry of Light Aircraft). In the absence of the regulation for construction of ultra-light airplanes in Serbia, Aero East Europe was forced to comply with the requirements for production of general aviation, which is the JAR Part 21, according to which all airplanes are made using certified metal alloys and steel, aluminum and Cr Mo. In 2009 Aero East Europe was promoted for the best exporting product of the Year by SIEPA – Serbian Invest and Export Promotion Agency In 2013 SILA 450 C was promoted as the Investment of the Year by AUREA SILA 450C SPARE PARTS CATALOG The airplane from the SILA series, the SILA 450 C (C stands for Cruise) is the easiest of this category and is certified according to German LTF-UL airworthiness requirements, the most restrictive standard for this category of airplanes. SILA 450C is also certified in France. Each model of the factory Aero East Europe is manufactured according to VLA standards, from certified aeronautical material, from the easiest SILA 450 C to the SILA 950 (the airplane with four seats – MTOW=950kg). SILA 450 C In accordance with French requirements In accordance with German requirements Next: EASA certification!!! 4 Aero East Europe produces airplanes whose purpose may be multiple, with production and maintenance much cheaper than the aircrafts in the same or similar category. For example the fuel used is the same as for cars. Even dough the main purpose of this airplane is for sport flying, it can be used for training pilots, for monitoring traffic and controlling the borders areas and also for agriculture. SILA 750S Medical transport SILA 450 Aero photo shooting INTRODUCTION 5 AERO EAST EUROPE D.O.O. SILA 450C SPARE PARTS CATALOG SILA 6 INTRODUCTION 450 C 7 List of effective pages SILA 450C SPARE PARTS CATALOG Cockpit Page Issue Revision Revision date 13 01 01 28.11.2014 20 01 01 28.11.2014 24 01 01 28.11.2014 28 01 01 28.11.2014 31 01 01 28.11.2014 44 01 01 28.11.2014 57 01 01 28.11.2014 Rear fuselage Page Issue Revision Revision date 67 01 01 28.11.2014 72 01 01 28.11.2014 75 01 01 28.11.2014 78 01 01 28.11.2014 81 01 01 28.11.2014 84 01 01 28.11.2014 88 01 01 28.11.2014 98 01 01 28.11.2014 105 01 01 28.11.2014 115 01 01 28.11.2014 120 01 01 28.11.2014 127 01 01 28.11.2014 131 01 01 28.11.2014 135 01 01 28.11.2014 143 01 01 28.11.2014 151 01 01 28.11.2014 154 01 01 28.11.2014 160 01 01 28.11.2014 Horizontal tail Page Issue Revision Revision date 163 01 01 28.11.2014 166 01 01 28.11.2014 171 01 01 28.11.2014 174 01 01 28.11.2014 178 01 01 28.11.2014 181 01 01 28.11.2014 186 01 01 28.11.2014 190 01 01 28.11.2014 196 01 01 28.11.2014 Vertical tail Page Issue Revision Revision date 200 01 01 28.11.2014 205 01 01 28.11.2014 208 01 01 28.11.2014 213 01 01 28.11.2014 Installation of the empennage Page Issue Revision Revision date 217 01 01 28.11.2014 220 01 01 28.11.2014 225 01 01 28.11.2014
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228 01 01 28.11.2014 231 01 01 28.11.2014 Ailerons and flaps Page Issue Revision Revision date 237 01 01 28.11.2014 241 01 01 28.11.2014 245 01 01 28.11.2014 249 01 01 28.11.2014 253 01 01 28.11.2014 257 01 01 28.11.2014 262 01 01 28.11.2014 267 01 01 28.11.2014 271 01 01 28.11.2014 Wings Page Issue Revision Revision date 276 01 01 28.11.2014 279 01 01 28.11.2014 282 01 01 28.11.2014 285 01 01 28.11.2014 288 01 01 28.11.2014 292 01 01 28.11.2014 296 01 01 28.11.2014 301 01 01 28.11.2014 306 01 01 28.11.2014 310 01 01 28.11.2014 314 01 01 28.11.2014 318 01 01 28.11.2014 322 01 01 28.11.2014 326 01 01 28.11.2014 330 01 01 28.11.2014 334 01 01 28.11.2014 338 01 01 28.11.2014 344 01 01 28.11.2014 Installation of wings Page Issue Revision Revision date 351 01 01 28.11.2014 Composite wings and tail tips installation Page Issue Revision Revision date 362 01 01 28.11.2014 366 01 01 28.11.2014 369 01 01 28.11.2014 372 01 01 28.11.2014 8 INTRODUCTION Landing gear Page Issue Revision Revision date 377 01 01 28.11.2014 383 01 01 28.11.2014 Fuel system Page Issue Revision Revision date 388 01 01 28.11.2014 9 SILA 450C ASSEMBLY DRAWING WINGS EMPENNAGE LANDING GEAR FUSELAGE FUEL SYSTEM FUEL SYSTEM SILA 450C SPARE PARTS CATALOG 10 TABLE OF CONTENTS COCKPIT ................................................................................................................................................... 12 Firewall ....................................................................................................................................................... 13 Cockpit carrier ............................................................................................................................................ 20 Instrument panel ........................................................................................................................................ 24 Carrier of the main landing gear................................................................................................................. 28 Basic cockpit .............................................................................................................................................. 31 Interior ........................................................................................................................................................ 44 Instruments................................................................................................................................................. 57 REAR FUSELAGE .................................................................................................................................... 65 First framework........................................................................................................................................... 67 Second framework ..................................................................................................................................... 72 Third framework ......................................................................................................................................... 75 Fourth framework ....................................................................................................................................... 78 Fifth framework........................................................................................................................................... 81 Sixth framework.......................................................................................................................................... 84 Basic structure of the fuselage ................................................................................................................... 88 Installation of the fuselage structure .......................................................................................................... 98 Assembly of the fuselage structure ............................................................................................................ 105 Fuselage with the inner structure ............................................................................................................... 115 Rear Control Bridge in the fuselage ........................................................................................................... 120 Cockpit walls .............................................................................................................................................. 127 Levers on the rear control bridge ............................................................................................................... 131 Left door ..................................................................................................................................................... 135 Right door ................................................................................................................................................... 143 Assembly of the cockpit windows............................................................................................................... 151 Installation of the engine ............................................................................................................................ 154 Installation of the propeller ......................................................................................................................... 160 HORIZONTAL TAIL ................................................................................................................................... 162 Rear spar of the horizontal stabilizer ......................................................................................................... 163 Structure of the horizontal stabilizer ........................................................................................................... 166 Structure of the horizontal stabilizer with skin ............................................................................................ 171 Horizontal stabilizer .................................................................................................................................... 174 Assembly of the spar of the elevator .......................................................................................................... 178 Structure of the elevator ............................................................................................................................. 181 Trimmer of the elevator .............................................................................................................................. 186 Structure of the elevator with skin .............................................................................................................. 190 The elevator ............................................................................................................................................... 196 VERTICAL TAIL ........................................................................................................................................ 199 Structure of the vertical stabilizer ............................................................................................................... 200 Vertical stabilizer ........................................................................................................................................ 205 Structure of the rudder ............................................................................................................................... 208 The rudder .................................................................................................................................................. 213 TABLE OF CONTENTS FUSELAGE EMPENNAGE 11 INSTALLATION OF THE EMPENAGE ..................................................................................................... 216 Installation of the horizontal stabilizer ........................................................................................................ 217 Installation of the vertical stabilizer ............................................................................................................ 220 Installation of the elevator .......................................................................................................................... 225 Installation of the rudder ............................................................................................................................. 228 Installation of the tail controls ..................................................................................................................... 231 AILERONS AND FLAPS ........................................................................................................................... 236 Structure of the left aileron ......................................................................................................................... 237 Structure of the right aileron ....................................................................................................................... 241 Trimmer of the left aileron .......................................................................................................................... 245 Left aileron with the trimmer ....................................................................................................................... 249 Right aileron ............................................................................................................................................... 253 Structure of the left flap .............................................................................................................................. 257 Structure of the right flap ............................................................................................................................ 262 Left flap....................................................................................................................................................... 267 Right flap .................................................................................................................................................... 271 WINGS ....................................................................................................................................................... 275 Left rib with the lug for the flap ................................................................................................................... 276 Right rib with the lug for the flap................................................................................................................. 279 Left rib with the lug for the aileron .............................................................................................................. 282 Right rib with the lug for the aileron............................................................................................................ 285 Assembly of the rear left spar .................................................................................................................... 288 Assembly of the rear right spar .................................................................................................................. 292 Assembly of the front left spar .................................................................................................................... 296 Assembly of the front right spar ................................................................................................................. 301 Structure of the left wing ............................................................................................................................ 306 Structure of the right wing .......................................................................................................................... 310 Left wing box .............................................................................................................................................. 314 Right wing box ............................................................................................................................................ 318 Basic left wing ............................................................................................................................................ 322 Basic right wing .......................................................................................................................................... 326 Left wing ..................................................................................................................................................... 330 Right wing................................................................................................................................................... 334 Complete left wing ...................................................................................................................................... 338 Complete right wing ................................................................................................................................... 344 INSTALLATION OF WINGS ...................................................................................................................... 350 Installation of wings to the fuselage ........................................................................................................... 351 COMPOSITE WINGS AND TAIL TIPS INSTALLATION .......................................................................... 361 Installation of the wing tips ......................................................................................................................... 362 Installation of the vertical tail tip ................................................................................................................. 366 Installation of the horizontal tail tips (Elevator) .......................................................................................... 369 Installation of the horizontal tail tips (Stabilizer) 372 LANDING GEAR ....................................................................................................................................... 376 Installation of the nose leg ......................................................................................................................... 377 Installation of the main landing gear 383 FUEL SYSTEM .......................................................................................................................................... 387 Installation of the fuel system ..................................................................................................................... 388 EMPENNAGE WINGS LANDING GEAR FUEL SYSTEM SILA 450C SPARE PARTS CATALOG 12 13 FIREWALL Assembly identification: 5412-0.0.0-KB.02.00.68-00 SILA 450C SPARE PARTS CATALOG 14 Table of parts for the assembly of the firewall Assembly identification: 5412-0.0.0-KB.02.00.68-00 Bar code: 354000002 Position: 1 Part’s name: Firewall Part’s identification: 5412-0.0.0-KB.02.00.68 Bar code: 254000002 Position: 2 Part’s name: Upper carrier of the nose leg Part’s identification: 5343-0.0.1-KB.02.00.56 Bar code: 253000313 Position: 3 Part’s name: Rear reinforcement of the upper carrier of the nose leg Part’s identification: 5343-0.2.1-KB.02.00.55 Bar code: 253000312 Position: 4 Part’s name: Front reinforcement of the upper carrier of the nose leg Part’s identification: 5343-0.1.1-KB.02.00.53 Bar code: 253000311 Position: 5 Part’s name: Upper front reinforcement on the firewall Part’s identification: 5343-0.0.0-KB.02.00.42 Bar code: 253000310 FUSELAGE 15 Table of parts for the assembly of the firewall Assembly identification: 5412-0.0.0-KB.02.00.68-00 Bar code: 354000002 Position: 6 Part’s name: Lower front reinforcement on the firewall Part’s identification: 5343-0.0.0-KB.01.00.43 Bar code: 253000188 Position: 7 Part’s name: Left reinforcement of the firewall for the connection with the engine Part’s identification: 5346-1.0.0-KB.01.00.49L Bar code: 253000198 Position: 8 Part’s name: Right reinforcement of the firewall for the connection of the engine Part’s identification: 5346-2.0.0-KB.01.00.49R Bar code: 253000199 Position: 9 Part’s name: Left stiffening of the front lower reinforcement on the firewall Part’s identification: 5346-2.0.0-KB.01.00.48L Bar code: 253000196 Position: 10 Part’s name: Right stiffening of the front lower reinforcement on the firewall Part’s identification: 5343-2.0.0-KB.01.00.48R Bar code: 253000197 SILA 450C SPARE PARTS CATALOG 16 Table of parts for the assembly of the firewall Assembly identification: 5412-0.0.0-KB.02.00.68-00 Bar code: 354000002 Position: 11 Part’s name: Upper inner reinforcement of the firewall from the left Part’s identification: 5320-1.0.1-KB.02.00.59L Bar code: 253000316 Position: 12 Part’s name: Upper inner reinforcement of the firewall from the right Part’s identification: 5320-2.0.1-KB.02.00.59R Bar code: 253000317 Position: 13 Part’s name: Inner vertical reinforcement of the firewall Part’s identification: 5320-0.0.0-KB.02.00.60 Bar code: 253000318 Position: 14 Part’s name: Lower inner reinforcement of the firewall Part’s identification: 5320-0.0.2-KB.02.00.58 Bar code: 253000315 Position: 15 Part’s name: Bottom inner reinforcement of the firewall Part’s identification: 5320-0.0.0-KB.02.00.57 Bar code: 253000314 FUSELAGE 17 Table of parts for the assembly of the firewall Assembly identification: 5412-0.0.0-KB.02.00.68-00 Bar code: 354000002 Position: 16 Part’s name: Support of the bearing Part’s identification: 5343-0.0.0-KB.01.00.13 Bar code: 253000283 Position: 17 Part’s name: Teflon in the upper carrier of the nose leg Part’s identification: 5343-0.0.0-KB.01.00.52 Bar code: 253000203 Position: 18 Part’s name: Bracket of the teflon in the upper carrier of the nose leg Part’s identification: 5343-0.0.0-KB.01.00.51 Bar code: 253000202 Position: 19 Part’s name: Left reinforcement of the teflon bracket in the upper carrier of the nose leg Part’s identification: 5343-1.0.0-KB.01.00.54L Bar code: 253000254 Position: 20 Part’s name: Right reinforcement of the teflon bracket in the upper carrier of the nose leg Part’s identification: 5343-2.0.0-KB.01.00.54R Bar code: 253000255 SILA 450C SPARE PARTS CATALOG 18 Table of parts for the assembly of the firewall Assembly identification: 5412-0.0.0-KB.02.00.68-00 Bar code: 354000002 Position: 21 Part’s name: Left strut of the upper carrier of the nose leg Part’s identification: 5343-1.0.0-KB.01.00.50L Bar code: 253000285 Position: 22 Part’s name: Right strut of the upper carrier of the nose leg Part’s identification: 5343-2.0.0-KB.01.00.50R Bar code: 253000286 Position: 31 Part’s name: Cover of the nose leg Part’s identification: 5300-0.0.0-KB.01.00.84 Bar code: 253000239 Table: Bolts, screw nuts, washers and rivets used for the assembly of the firewall Position Name Description 23 1661-0410 Rivet 1/8-10 24 1661-0510 Rivet 5/32-12 25 1661-0512 Rivet 5/32-12 26 AN470AD5-10 Rivet S5/32-10 27 0917 4 WURTH Crumpling screw nut M4 28 AN3-4A Bolt 3/16-4 29 AN960-10L Washer 3/16 30 AN365-1032 Screw nut 3/16 32 DIN Bolt M4x15 Cilindrical FUSELAGE 19 (Intentionally left blank) SILA 450C SPARE PARTS CATALOG 20 COCKPIT CARRIER Assembly identification: 5347-0.0.0-KB.02.01.00 SILA 450C SPARE PARTS CATALOG 21 Table of parts for the assembly of the cockpit carrier Assembly identification: 5347-0.0.0-KB.02.01.00 Bar code: 353000034 Position: 1 Part’s name: Lateral seat carrier Part’s identification: 5347-0.0.0-KB.02.01.01 Bar code: 253000338 Position: 2 Part’s name: Left seat carrier Part’s identification: 5347-1.0.0-KB.01.01.02L Bar code: 253000260 Position: 3 Part’s name: Right seat carrier Part’s identification: 5347-2.0.0-KB.01.01.02R Bar code: 253000261 Position: 4 Part’s name: Profile for the connection of the seat carrier and the cross seat carrier Part’s identification: 5347-0.0.0-KB.01.01.04 Bar code: 253000264 Position: 5 Part’s name: Right profile for the connection of the seat carrier and the landing gear carrier Part’s identification: 5347-2.0.0-KB.01.01.03R Bar code: 253000263 FUSELAGE 22 Table of parts for the assembly of the cockpit carrier Assembly identification: 5347-0.0.0-KB.02.01.00 Bar code: 353000034 Position: 6 Part’s name: Left profile for the connection of the seat carrier and the landing gear carrier Part’s identification: 5347-1.0.0-kb.01.01.03l Bar code: 253000262 Table: Bolts, screw nuts, washers and rivets used for the assembly of the cockpit carrier Position Name Description 7 1661-0512 Rivet 5/32-12 SILA 450C SPARE PARTS CATALOG 23 (Intentionally left blank) FUSELAGE 24 INSTRUMENT PANEL Assembly identification: 5345-0.0.0-KB.02.03.00T SILA 450C SPARE PARTS CATALOG 25 Table of parts for the assembly of the instrument panel Assembly identification: 5345-0.0.0-KB.02.03.00T Bar code: 353000032 Position: 1 Part’s name: Lower carrier of the instrument panel Part’s identification: 5345-0.0.0-KB.02.03.01T Bar code: 253000356 Position: 2 Part’s name: Instrument panel Part’s identification: 5345-0.0.0-KB.02.03.02T Bar code: 253000357 Position: 3 Part’s name: Left sheet metal for the connection of the Instrument panel and over side Part’s identification: 5320-1.0.0-KB.02.03.03T Bar code: 253000358 Position: 4 Part’s name: Right sheet metal for the connection of the instrument panel and over side Part’s identification: 5320-2.0.0-KB.02.03.04T Bar code: 253000359 Position: 5 Part’s name: Left reinforcement of the lower carrier of the instrument panel Part’s identification: 5345-1.0.0-KB.01.03.05 Bar code: 253000353 FUSELAGE 26 Table of parts for the assembly of the instrument panel Assembly identification: 5345-0.0.0-KB.02.03.00T Bar code: 353000032 Position: 6 Part’s name: Right reinforcement of the lower carrier of the instrument panel Part’s identification: 5345-2.0.0-KB.01.03.06 Bar code: 253000354 Position: 7 Part’s name: Console carrier Part’s identification: 5320-0.0.0-KB.01.03.07 Bar code: 253000274 Position: 9 Part’s name: Reinforcement of the lower carrier of the instrument panel Part’s identification: 5320-0.0.0-KB.01.03.10 Bar code: 253000379 Table: Bolts, screw nuts, washers and rivets used for the assembly of the instrument panel Position Name Description 8 1661-0410 Rivet 1/8-10 SILA 450C SPARE PARTS CATALOG 27 (Intentionally left blank) FUSELAGE 28 CARRIER OF THE MAIN LANDING GEAR Assembly identification: 5343-0.0.0-KB.02.04.00 SILA 450C SPARE PARTS CATALOG 29 Table of parts for the assembly of the carrier of the main landing gear Assembly identification: 5343-0.0.0-KB.02.04.00 Bar code: 353000029 Position: 1 Part’s name: Main carrier of the landing gear Part’s identification: 5343-0.0.0-KB.02.04.01 Bar code: 253000339 Position: 2 Part’s name: Front reinforcement of the landing gear Part’s identification: 5343-0.1.0-KB.02.04.02 Bar code: 253000340 Position: 3 Part’s name: Rear reinforcement of the main landing gear carrier Part’s identification: 5343-0.2.0-KB.01.04.03 Bar code: 253000279 Table: Bolts, screw nuts, washers and rivets used for the assembly of the carrier of the main landing gear Position Name Description 4 AN470AD5-9 Rivet S5/32-9 FUSELAGE 30 (Intentionally left blank) SILA 450C SPARE PARTS CATALOG 31 BASIC COCKPIT Assembly identification: 5310-0.0.0-KB.02.00.00-09 SILA 450C SPARE PARTS CATALOG 32 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 1 Part’s name: Firewall Part’s identification: 5412-0.0.0-KB.02.00.68-00 Bar code: 354000002 NOTE Complete firewall as the subassembly of the basic cockpit Position: 2 Part’s name: Floor of the cockpit Part’s identification: 5321-0.0.0-KB.01.00.64C Bar code: 253000287 Position: 3 Part’s name: Central reinforcement beneath the floor Part’s identification: 5315-0.0.0-KB.01.00.62 Bar code: 253000209 Position: 4 Part’s name: Main left profile beneath the cockpit floor Part’s identification: 5315-1.0.0-KB.01.00.87L Bar code: 253000244 Position: 5 Part’s name: Main right profile beneath the cockpit floor Part’s identification: 5315-2.0.0-KB.01.00.87R Bar code: 253000365 FUSELAGE 33 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 6 Part’s name: Left side sheet metal beneath the door Part’s identification: 5330-1.0.0-KB.02.00.69L Bar code: 253000322 Position: 7 Part’s name: Right side sheet metal beneath the floor Part’s identification: 5330-2.0.0-KB.02.00.69R Bar code: 253000323 Position: 8 Part’s name: Left horizontal strut on the side sheet metal Part’s identification: 5320-1.0.0-KB.01.00.71L Bar code: 253000219 Position: 9 Part’s name: Right horizontal strut on the side sheet metal Part’s identification: 5320-2.0.0-KB.01.00.71R Bar code: 253000220 Position: 10 Part’s name: Longitudinal bottom reinforcement of the side sheet metal from the left Part’s identification: 5320-1.0.0-KB.01.00.74L Bar code: 253000224 SILA 450C SPARE PARTS CATALOG 34 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 11 Part’s name: Longitudinal bottom reinforcement of the side sheet metal from the right Part’s identification: 5320-2.0.0-KB.01.00.74R Bar code: 253000225 Position: 12 Part’s name: Rear bottom reinforcement in the cockpit and the connection of the control carrier and seats Part’s identification: 5315-0.2.0-KB.02.00.63 Bar code: 253000319 Position: 13 Part’s name: Bottom reinforcement in the cockpit in the middle Part’s identification: 5315-0.3.0-KB.02.00.66 Bar code: 253000320 Position: 14 Part’s name: Bottom reinforcement in the cockpit in the front Part’s identification: 5315-0.3.0-KB.02.00.67 Bar code: 253000321 Position: 15 Part’s name: Left slope strut of the firewall Part’s identification: 5320-1.0.0-KB.02.00.70L Bar code: 253000324 FUSELAGE 35 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 16 Part’s name: Right slope strut of the firewall Part’s identification: 5320-2.0.0-KB.02.00.70R Bar code: 253000325 Position: 17 Part’s name: Left upper slope profile Part’s identification: 5320-1.0.1-KB.02.00.38L Bar code: 253000302 Position: 18 Part’s name: Right upper slope profile Part’s identification: 5320-2.0.1-KB.02.00.38R Bar code: 253000303 Position: 19 Part’s name: Left lower slope profile Part’s identification: 5320-1.0.1-KB.02.00.39L Bar code: 253000304 Position: 20 Part’s name: Right lower slope profile Part’s identification: 5320-2.0.1-KB.02.00.39R Bar code: 253000305 SILA 450C SPARE PARTS CATALOG 36 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 21 Part’s name: Slope bottom profile from the left Part’s identification: 5320-1.0.1-KB.02.00.40L Bar code: 253000306 Position: 22 Part’s name: Slope bottom profile from the right Part’s identification: 5320-1.0.0-KB.01.00.40R Bar code: 253000307 Position: 23 Part’s name: Vertical connection of the slope struts of the firewall and cockpit cage from the left Part’s identification: 5320-1.0.0-KB.01.00.77L Bar code: 253000230 Position: 24 Part’s name: Vertical connection of the slope strut of the firewall and cockpit cage from the right Part’s identification: 5320-2.0.0-KB.01.00.77R Bar code: 253000231 Position: 25 Part’s name: Sheet metal for the connection of the horizontal and slope strut with the cockpit cage Part’s identification: 5320-1.0.0-KB.02.00.70L Bar code: 253000324 FUSELAGE 37 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 26 Part’s name: Middle reinforcement of the side sheet metal from the left Part’s identification: 5320-1.3.0-KB.01.00.76L Bar code: 253000228 Position: 27 Part’s name: Middle reinforcement of the side sheet metal from the right Part’s identification: 5320-2.3.0-KB.01.00.76R Bar code: 253000229 Position: 28 Part’s name: Front reinforcement of the side sheet metal from the left Part’s identification: 5320-1.3.0-KB.01.00.75L Bar code: 253000371 Position: 29 Part’s name: Front reinforcement of the side sheet metal from the right Part’s identification: 5320-2.3.0-KB.01.00.75R Bar code: 253000372 Position: 30 Part’s name: Left upper reinforcement for the connection of the engine mount Part’s identification: 5346-1.0.1-KB.01-12-00-00L Bar code: 353000038 SILA 450C SPARE PARTS CATALOG 38 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 31 Part’s name: Right upper reinforcement for the connection of the engine mount Part’s identification: 5346-2.0.1-KB.01-12-00-00R Bar code: 353000039 Position: 32 Part’s name: Left reinforcement of the connection of the slope strut of the firewall and the firewall Part’s identification: 5320-1.0.0-KB.02.00.36L Bar code: 253000299 Position: 33 Part’s name: Right reinforcement of the connection of the slope strut of the firewall and the firewall Part’s identification: 5320-2.0.0-KB.02.00.36R Bar code: 253000300 Position: 35 Part’s name: Central carrier of the pilot’s pedals Part’s identification: 2720-3.0.0-KB.01.00.95 Bar code: 227000037 Position: 36 Part’s name: Left pedals Part’s identification: 2720-1.0.0-KO.02-04-00-00i Bar code: 327000087 FUSELAGE 39 Table of parts for the assembly of the basic cockpit Assembly identification: 5310-0.0.0-KB.02.00.00-09 Bar code: 353000002 Position: 37 Part’s name: Right pedals Part’s identification: 2720-2.0.0-KO.02-04-00-00i Bar code: 327000011 Position: 38 Part’s name: Left carrier of the pilot pedals Part’s identification: 2720-1.0.0-KB.01.00.94L Bar code: 227000035 Position: 39 Part’s name: Right carrier of the pilot pedals Part’s identification: 2720-2.0.0-KB.01.00.94R Bar code: 227000036 Position: 40 Part’s name: Left reinforcement on the connection front side sheet metal-cockpit cover Part’s identification: 5320-1.0.0-KB.02.00.35L Bar code: 253000297 Position: 41 Part’s name: Right reinforcement on the connection front side sheet metal-cockpit cover Part’s identification: 5320-2.0.0-KB.02.00.35R Bar code: 253000298 SILA 450C SPARE PARTS CATALOG