Project description FK131 Jungmann

Size: px
Start display at page:

Download "Project description FK131 Jungmann"

Transcription

1 Project description FK131 Jungmann The FK131 ( C104FK) is a cooperation project between Co. B&F Technik GmbH Germany and Co. Podesva Air, Czech Republic. The aircraft design is widely based on the original Bücker 131A design, which was produced over longer times under Czech license named C104. The original Bücker 131A version was designed 1934 as a very light trainer and acrobatic aircraft (330kg empty) with a four cylinder 80hp HM60R Hirth engine. The concept of the FK131 is a replica coming as close as possible to the original, but been light enough to classify either as Experimental aircraft or as EU Ultralight. As the original airframe was very light there was no need to proceed significant changes in the way the structure is built. Basically it remains a steel tube fuselage with wooden wings. But instead of using the heavy original four cylinder Hirth engine the FK131 is powered by the today s version of the four cylinder air cooled aviation engine, the Walter Mikron. Both engines are having comparable cylinder capacity and same power. But the Mikron is made of modern materials and technology, saving a lot of weight compared to its original predecessor from In consequence the engine installation is coming very close to the original: Walter Mikron IIIC installation and engine cowl FK131 Jungmann - C104FK project descriptionrev page 1

2 Scaling of the FK131project: left: FK131prototype right: T131 Jungmann (polish license production) The FK131 is coming as close as possible to the original outlines and dimensions of the Bücker 131A. Just a few corrections are needed to compensate for the lighter engine and to enable the owner to register the plane under the design regulation LTF-UL or US-LSA: Wing halfspan is shortened by 70 mm The wingsection is slightly redesigned to a more modern version to improve low speed characteristic and general performance These modifications are not obvious when comparing the FK131 versus an original Bücker131A. FK131 Jungmann - C104FK project descriptionrev page 2

3 FK131 FK131 Jungmann - C104FK project descriptionrev page 3

4 Structural design The lighter engine will reduce empty weight but also includes the need to correct CG position by building tailplane and rudder not in steel tube but in aluminum tube technology. Solid welded steel fittings bonded and riveted into the aluminum tube structure are connecting fuselage and tailplane. From outside this is in fact not evident and the basic design remains very close to the original. The fuselage structure is a welded steel tube frame using today s seamless steel tubes but based on the original geometry. The wings and ailerons are made in wood, also based on the original design. FK131 Jungmann - C104FK project descriptionrev page 4

5 The stall speed is lower compared to an original B131A, making the plane more forgiving at landing and allows to fulfill EU LTFUL regulations. The FK131 Vne is at 253km/h and so less than the original B131A - but its stress calculations are based on the FAR23 acrobatic design regulation requirements. Additional tests should proof its capabilities for basic acrobatics in a later time of the project. FK131 Jungmann - C104FK project descriptionrev page 5

6 Also cockpit interiors are done pretty much according to the original style of the 1930 s Jungmann. The outcome is a replica looking the same like its original predecessor. Even engine sound is very similar to a typical Bücker Jungmann A Version with Hirth engine! But instead of the original B131 A the FK131 features an up-to-date aircraft engine where parts are available and affordable, a ballistic emergency parachute system and the possibility to classify it as an Ultralight! This means having much less obligations and requirements compared to the operation and maintenance of an original Bücker FK131 Jungmann - C104FK project descriptionrev page 6

7 Including the BRS ballistic parachute system the prototype came out well below 300kg, including all extras and options. The prototype of the FK131 made its first flight on October 24 th, Performance data are determined closer at present, but first results were coming pretty close to the original B131A specifications. A limited series of 10 ready to fly aircrafts is in production at present. Also a kit version will be available to qualify as an experimental aircraft. FK131 Jungmann - C104FK project descriptionrev page 7

8 For more details address to B&F Technik Vertriebs GmbH Anton Dengler Straße 8 D Speyer info@fk-leichtflugzeuge.de FK131 Jungmann - C104FK project descriptionrev page 8

9 original specification Bücker (brochure 1934) FK131 specification FK-Leichtflugzeuge 2013 FK131 Jungmann - C104FK project descriptionrev page 9

FK131 and BF 131 Jungmann projekt update

FK131 and BF 131 Jungmann projekt update FK131 and BF 131 Jungmann projekt update Jan. 3 rd, 2018 First of all we wish all our loyal and patient customers a happy new year 2018! With this short report we want to provide you an overview what was

More information

CONTINUOUS IMPROVEMENTS AND MODIFICATIONS

CONTINUOUS IMPROVEMENTS AND MODIFICATIONS CONTINUOUS IMPROVEMENTS AND MODIFICATIONS TO THE B&F FK 9 HAVE MADE A GOOD AIRCRAFT EVEN BETTER. JOCHEN EWALD VISITED SPEYER AIRFIELD, HOME OF B&F TO TEST THE LATEST VERSION replaced the Rotax engine fitted

More information

T-51 Mustang - 3/4 Scale Kit

T-51 Mustang - 3/4 Scale Kit T-51 Mustang - 3/4 Scale Kit Description Titan Aircraft is pleased to offer the T-51D Mustang. This P-51D replica incorporates material and systems not commonly found in comparably priced aircraft. This,

More information

Introduction. AeroJones Aviation Technology Co., Ltd.

Introduction. AeroJones Aviation Technology Co., Ltd. Contents 1. Introducing AeroJones 2. Business Concept 3. Operational Principle 4. Target Market 5. Technology Transfer 6. First Aircraft Testing 7. Product Introduction Introduction AeroJones Aviation

More information

State of Israel Ministry of Transport Civil Aviation Authority TYPE CERTIFICATE DATA SHEET

State of Israel Ministry of Transport Civil Aviation Authority TYPE CERTIFICATE DATA SHEET State of Israel Ministry of Transport Civil Aviation Authority TYPE CERTIFICATE DATA SHEET TC number: Revision: Aircraft make: Aircraft model: IA298 New BRM Aero BRISTELL RG This Data Sheet which is part

More information

European Aviation Safety Agency

European Aviation Safety Agency TCDS No. EASA.A.044 L 23 SUPER-BLANÍK Page 1 of 8 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.044 L 23 SUPER-BLANÍK Type Certificate Holder: Blanik Aircraft CZ s.r.o. Karolinská

More information

Instruction Manual EXTRA 260-EP. 1075mm (42.32 in) 1000mm (39.37 in) 1100gr gr. 4 channel - 4 mini servo. Axi motor 2820

Instruction Manual EXTRA 260-EP. 1075mm (42.32 in) 1000mm (39.37 in) 1100gr gr. 4 channel - 4 mini servo. Axi motor 2820 1075mm (42.32 in) 1000mm (39.37 in) 1100gr - 1400gr 4 channel - 4 mini servo Axi motor 2820 KIT CONTENTS: We have organized the parts as they come out of the box for better identification during assembly.

More information

Peak Me 109 A Microlight Messerschmitt

Peak Me 109 A Microlight Messerschmitt www.todayspilot.co.uk Peak Me 109 A Microlight Messerschmitt 2 Today s Pilot www.todayspilot.co.uk 3 Peak Me 109 A Microlight Messerschmitt JOCHEN EWALD REPORTS FROM GERMANY ON AN EXCITING SCALE REPLICA

More information

AIRCRAFT INFORMATION. Pipistrel Virus. 80 HP (Rotax 912 UL2) Page 1 MAY 2012, Revision 01

AIRCRAFT INFORMATION. Pipistrel Virus. 80 HP (Rotax 912 UL2) Page 1 MAY 2012, Revision 01 AIRCRAFT INFORMATION Pipistrel Virus 80 HP (Rotax 912 UL2) Page 1 MAY 2012, Revision 01 www.pipistrel-usa.com info@pipistrel-usa.com Introduction This document is published for the purpose of providing

More information

Instruction Manual MUSTANG P51 - EP. Wingspan : 1377mm (54.21in) : 1180mm (46.46 in) : 2200gr gr. : AXI motor 2826 or 4120

Instruction Manual MUSTANG P51 - EP. Wingspan : 1377mm (54.21in) : 1180mm (46.46 in) : 2200gr gr. : AXI motor 2826 or 4120 Instruction Manual MUSTANG P51 - EP Wingspan : 1377mm (54.21in) g Length : 1180mm (46.46 in) Weight : 2200gr - 2600gr Engine : AXI motor 2826 or 4120 Radio : 4 channel / 4 servos standard KIT CONTENTS:

More information

Instruction Manual. We wish you many enjoyable flights with your plane and once again thank you for your choosing a Phoenix Model product

Instruction Manual. We wish you many enjoyable flights with your plane and once again thank you for your choosing a Phoenix Model product Instruction Manual Wing span: 1590mm (626 in) Length: 1100mm (433 in) Weight: 1500gr - 1700gr Motor: AXI 2814/10 or Motor: 500-600 w/ gear box Radio: 4 Channel / 4 servos standar Propeller: 12 x 47 We

More information

EASA TYPE-CERTIFICATE DATA SHEET EASA.A.038 SWIFT S-1

EASA TYPE-CERTIFICATE DATA SHEET EASA.A.038 SWIFT S-1 Page 1 of 6 EASA TYPE-CERTIFICATE DATA SHEET EASA.A.038 SWIFT S-1 Type Certificate Holder: ZAKŁADY LOTNICZE Margański & Mysłowski S.A. ul. Strażacka 60 43-300 Bielsko-Biała POLAND Models: SWIFT S-1, 23/05/2016

More information

AIRCRAFT INFORMATION. Pipistrel APIS/Bee. with Hirth F33 BS engine. Page 1 MAY 2012, Revision 01

AIRCRAFT INFORMATION. Pipistrel APIS/Bee. with Hirth F33 BS engine. Page 1 MAY 2012, Revision 01 AIRCRAFT INFORMATION Pipistrel APIS/Bee with Hirth F33 BS engine Page 1 MAY 2012, Revision 01 www.pipistrel-usa.com info@pipistrel-usa.com Introduction This document is published for the purpose of providing

More information

OCT/NOV Texas Flying Legends P-47D-23RA

OCT/NOV Texas Flying Legends P-47D-23RA OCT/NOV Texas Flying Legends P-47D-23RA by Chuck Cravens The first joined large assemblies on the bench. Update In October and November, for the first time we began some assembly of the major components

More information

Building A Replica Aircraft. Part Two Construction Details Fuselage and Tail Group

Building A Replica Aircraft. Part Two Construction Details Fuselage and Tail Group Building A Replica Aircraft Part Two Construction Details Fuselage and Tail Group Brief Review After obtaining a partially complete Graham Lee 7/8 scale Nieuport 11 project I decided to reconfigure it

More information

Ultralight airplane Design

Ultralight airplane Design Ultralight airplane Design Ultralight airplane definitions: Airworthiness authorities define aircraft as vehicles that can rise or move in the air and enforce strict regulations and requirements for all

More information

Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics

Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics 10.3 Presentation of results 10.3.1 Presentation of results of a student project 10.3.2 A typical brochure 10.3 Presentation of results At the end

More information

Instruction Manual BULLDOG. Wingspan : 1410 mm (55.5in) : 1450 mm (57.1in) : 4900gr gr. Weight. : 6-9 Channel/ 7 servo high torque, 1standard

Instruction Manual BULLDOG. Wingspan : 1410 mm (55.5in) : 1450 mm (57.1in) : 4900gr gr. Weight. : 6-9 Channel/ 7 servo high torque, 1standard Wingspan : 1410 mm (55.5in) Length Weight Radio Engine : 1450 mm (57.1in) : 4900gr - 5600gr : 6-9 Channel/ 7 servo high torque, 1standard : 1.20/ 2 stroke 1.80/ 4 stroke KIT CONTENTS: We have organized

More information

AIRCRAFT INFORMATION. Pipistrel Sinus. 80 HP (Rotax 912 UL2) Page 1 MAY 2012, Revision 01

AIRCRAFT INFORMATION. Pipistrel Sinus. 80 HP (Rotax 912 UL2) Page 1 MAY 2012, Revision 01 AIRCRAFT INFORMATION Pipistrel Sinus 80 HP (Rotax 912 UL2) Page 1 MAY 2012, Revision 01 www.pipistrel-usa.com info@pipistrel-usa.com Introduction This document is published for the purpose of providing

More information

GlaStar / Sportsman Service Bulletin 64- MANDATORY

GlaStar / Sportsman Service Bulletin 64- MANDATORY GlaStar / MANDATORY Note: Subject: Applicability: This service bulletin supersedes 49. The service bulletin applicability was updated to include kits. No other changes were made Inspection of welded cage

More information

VENTRIX. Dear Customer, Thank you for purchase our Ventrix Sport jet product

VENTRIX. Dear Customer, Thank you for purchase our Ventrix Sport jet product VENTRIX Dear Customer, Thank you for purchase our Ventrix Sport jet product Following you can find greater information for build and fly this model. Before you get started building and setting-up your

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1 of 7 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.045 Type Certificate Holder: Blanik Aircraft CZ s.r.o. Karolinská 661/4 186 00 Praha 8 For models: Issue 05: 10 January

More information

Pilot s Operating Handbook & approved Flight Manual FK 14 B. Approved as Ultralight/ Light Sport Aircraft DPR 133/Annex V

Pilot s Operating Handbook & approved Flight Manual FK 14 B. Approved as Ultralight/ Light Sport Aircraft DPR 133/Annex V Pilot s Operating Handbook & approved Flight Manual FK 14 B POH FK 14 B Polaris Advanced Italien regulation type Airplane Serial Number: Airplane Registration Number: Date of issue: Manual Nr.: Approved

More information

RECOMMENDED MOTOR AND BATTERY SET UP

RECOMMENDED MOTOR AND BATTERY SET UP SPECIFICATION - Wingspan: 6000mm (236.2 in) - Length: 2873mm (113.1 in) - Flying weight: 14-18 kg - Wing area: 219.4 dm2 - Wing loading: 64g/dm2 - Wing type: HQ airfoils - Covering type: Genuine ORACOVER

More information

Introduction. Fuselage/Cockpit

Introduction. Fuselage/Cockpit Introduction The Moravan Zlin 242L is a fully aerobatic 2 seat aircraft designed to perform all advanced flight maneuvers within an envelope of -3.5 to +6 Gs. Many military and civilian flight-training

More information

Assembly and Operating Manual HR-100. Specification: *Length: 41-7/10"(1060 mm) *Wing span: 49-1/5"(1250 mm) *Flying weight: 45.

Assembly and Operating Manual HR-100. Specification: *Length: 41-7/10(1060 mm) *Wing span: 49-1/5(1250 mm) *Flying weight: 45. Assembly and Operating Manual HR-100 Specification: *Length: 41-7/10"(1060 mm) *Wing span: 49-1/5"(1250 mm) *Flying weight: 45.9 oz (1300g) Dear customer, Congratulations on your choice of a factory-assembled

More information

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC 69-04 Revision 6 MORAVAN-AEROPLANES a.s. Model Z 526 F 11.04.2007 TYPE CERTIFICATE DATA SHEET No. 69-04 This data sheet which is a part of Type Certificate

More information

Airplane Manual. FK 12 S2 Comet

Airplane Manual. FK 12 S2 Comet Airplane Manual FK 12 S2 Comet Certified as LSA or Ultralight according BFU 95 / LTF-UL 2003 Kennblatt Nr. 61158.4 This manual must be carried in the aircraft at all times. This is the Pilot s operating

More information

LAA TYPE ACCEPTANCE DATA SHEET TADS 334 ALPI PIONEER 200 AND PIONEER 200-M

LAA TYPE ACCEPTANCE DATA SHEET TADS 334 ALPI PIONEER 200 AND PIONEER 200-M Issue 5 Addition of mandatory modification LAA MOD/334/003 Dated 9/6/14 JV These TADS are intended as a summary of available information about the type and should be used during the build, operation and

More information

The implementation of highly advanced and efficient +25 kw RESLS - Retractable Electric Self-Launching System,

The implementation of highly advanced and efficient +25 kw RESLS - Retractable Electric Self-Launching System, The GP 14 E/SE VELO is the ultimate expression of 13.5 meter FAI racing class fully flapped and ballasted, combined with everyday usability traits and features. The implementation of highly advanced and

More information

I n s t r u c t i o n M a n u a l. Instruction Manual SPECIFICATION

I n s t r u c t i o n M a n u a l. Instruction Manual SPECIFICATION I n s t r u c t i o n M a n u a l Instruction Manual SPECIFICATION - Wingspan: 3200mm (125,9 in) - Length: 1650mm (64,9 in) - Flying weight: 3000gr 3200gr - Wing area: 64.5 dm2 - Wing loading: 46g/dm2

More information

70MM YAK-130 STABLE SMOOTH FLYING PERFORMANCE FMSMODEL.COM

70MM YAK-130 STABLE SMOOTH FLYING PERFORMANCE FMSMODEL.COM 70MM YAK-130 REALISTIC RETRACT & FLAPS INSTALLED RIGID STRONG DURABLE EPO STABLE SMOOTH FLYING PERFORMANCE FMSMODEL.COM Table of Contents Introductions 3 Contents of Kit 4 Assemble the plane 5 Battery

More information

LANCAIR LEGACY PRE-TEST FLIGHT INSPECTION (8-04)

LANCAIR LEGACY PRE-TEST FLIGHT INSPECTION (8-04) LANCAIR LEGACY PRE-TEST FLIGHT INSPECTION (8-04) OWNER PHONE # ADDRESS N SERIAL # AIRCRAFT TYPE DATE / / TACH TIME hrs. TOTAL TIME hrs. EMPTY WEIGHT CG. PAINT & INTERIOR? YES NO ENGINE TYPE PROPELLER ALL

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Aeroplanes 26 October 2000 The date above indicates the amendment date of this schedule. New or amended ADs are shown with an asterisk * Contents DCA/VIC/101 Nose Leg Shear

More information

JODEL D.112 INFORMATION MANUAL C-FVOF

JODEL D.112 INFORMATION MANUAL C-FVOF JODEL D.112 INFORMATION MANUAL C-FVOF Table of Contents I General Description...4 Dimensions:...4 Powertrain:...4 Landing gear:...4 Control travel:...4 II Limitations...5 Speed limits:...5 Airpeed indicator

More information

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design Tables No Component Primary function Major areas of influence 1 Fuselage Payload accommodations

More information

Easy to fly, affordable, and very durable CONTACT: Walter Janner Ebnit Dornbirn Austria / Europe

Easy to fly, affordable, and very durable CONTACT: Walter Janner Ebnit Dornbirn Austria / Europe ZENITH STOL CH-801 SN: 801-4161 Easy to fly, affordable, and very durable CONTACT: Walter Janner Ebnit 60 6850 Dornbirn Austria / Europe Email: info@flyingcircus.at Phone: +43-(0)664/45 21 572 Zenith STOL

More information

LAA TYPE ACCEPTANCE DATA SHEET TADS 162 ZENAIR CH 601HD/HDS

LAA TYPE ACCEPTANCE DATA SHEET TADS 162 ZENAIR CH 601HD/HDS Issue 7 Revision A New format. Dated 07/11/11 JV Revision B Link to sheets referenced in section 2.2 Dated 30/4/12 JV These TADS are intended as a summary of available information about the type and should

More information

Aeroplanes DAR ltd. Brief Flight Manual DAR Solo BRIEF FLIGHT MANUAL. DAR-Solo series. Sofia Page 1 of 25

Aeroplanes DAR ltd. Brief Flight Manual DAR Solo BRIEF FLIGHT MANUAL. DAR-Solo series. Sofia Page 1 of 25 BRIEF FLIGHT MANUAL DAR-Solo series Sofia 2015 Page 1 of 25 TABLE OF CONTENTS Introduction 3 Limitations and Safety Information 4 General View of DAR-Solo series 6 Ignition 7 Engine warm up 8 Taxiing 9

More information

Type Approval of the Cyclone AX3/503 3 Axis Microlight Aeroplane and Approval for a Permit to Fly

Type Approval of the Cyclone AX3/503 3 Axis Microlight Aeroplane and Approval for a Permit to Fly AIRWORTHINESS APPROVAL NOTE NO: 23042 APPLICANT: AIRCRAFT TYPE: REGISTRATION NO: Cyclone Airsports Ltd Cyclone AX3/503 G-MYER CONSTRUCTOR'S NO: CA 001 Type Approval of the Cyclone AX3/503 3 Axis Microlight

More information

Landing gear. The engine Why the Citroen AX and Peogeot 106? Moteur 1.4 diesel PSA"

Landing gear. The engine Why the Citroen AX and Peogeot 106? Moteur 1.4 diesel PSA Introduction Strong from the experience gained with the "Dieselis", http://membres.multimania.fr/dieselis/ I was aiming at creating a new two seater aircraft, powered by a diesel engine, highly efficient,

More information

: 7 channel - 9 servo, Hi-Torque ( Minimum 6 kg ).

: 7 channel - 9 servo, Hi-Torque ( Minimum 6 kg ). g Wingspan : 1820mm (71.65 inches) Length : 1625mm (63.98 inches) Weight : 6900gr Engine : 25cc - 35cc Radio : 7 channel - 9 servo, Hi-Torque ( Minimum 6 kg ). KIT CONTENTS: We have organized the parts

More information

Times are approximate, since I am flying the airplane after rebuild. 60 hours since new prop was made specifically for this airplane by McCauley.

Times are approximate, since I am flying the airplane after rebuild. 60 hours since new prop was made specifically for this airplane by McCauley. 1952 CallAir Cadet fact sheet: Times are approximate, since I am flying the airplane after rebuild. 1700 +/- hours total time, airframe and engine. The engine is original to the airframe. 70 hours since

More information

Reviewing the Sam LS An all-metal, fighter-like homebuilt/lsa

Reviewing the Sam LS An all-metal, fighter-like homebuilt/lsa The Spirit of Homebuilt Aviation I www.eaa.org Vol.2 No.10 I October 2013 Reviewing the Sam LS An all-metal, fighter-like homebuilt/lsa Meet the 2013 AirVenture Grand Champions Continental s Diesel Goes

More information

Form No. Issue Page No. Issue Date. NMAI/AW022 8 Rev.0 1 of 6 18 JAN 2018

Form No. Issue Page No. Issue Date. NMAI/AW022 8 Rev.0 1 of 6 18 JAN 2018 1 of 6 Note: This form shall be filled in using details from HADS /TADS and/or build manual. 1. Owner/Builder Details Name: NMAI No. Home Tel. Mobile Tel. Correspondence Address: Build location if Different:

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET Issue: 02 Date: 27 October 2017 TYPE-CERTIFICATE DATA SHEET NO. EASA. A.616 for Type Certificate Holder M&D Flugzeugbau GmbH & Co. KG Streeker Straße 5 b 26446 Friedeburg Germany For models: JS-MD 1C TE.CERT.00135-001

More information

I/C FLIGHT GUIDELINES

I/C FLIGHT GUIDELINES SPECIFICATION - Wingspan: 3500mm (137.8 in) - Length: 1650mm (64.96 in) - Flying weight: 3700-4000 gr - Wing area: 75 dm2 - Wing loading: 49g/dm2 - Wing type: HQ profile - Covering type: Genuine ORACOVER

More information

S p e e d, C o m f o r t a n d S t y l e I m p r o v e d

S p e e d, C o m f o r t a n d S t y l e I m p r o v e d DA40 XLS/CS S p e e d, C o m f o r t a n d S t y l e I m p r o v e d Whether you are a seasoned pilot or just learning to fly, the DA40 Diamond Stars give you and your passengers the best way to experience

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET NO. EASA.A.616 for Type Certificate Holder M&D Flugzeugbau GmbH & Co. KG Streeker Straße 5 b 26446 Friedeburg Germany For models: JS-MD 1C TE.CERT.00135-001 European Union Aviation

More information

Flight Manual DG-300. No. page description issue date. 2 4, 17, 21, 33 Installation of an additional tow hook TN Oct. 85

Flight Manual DG-300. No. page description issue date. 2 4, 17, 21, 33 Installation of an additional tow hook TN Oct. 85 Flight Manual DG-300 Manual amendments No. page description issue date 1 1, 2, 4-6, 8, 10- amendments and corrections TN 359/7 May 85 12, 15, 16, 19, 21, 22, 24, 25, 28, 30, 31, 33 2 4, 17, 21, 33 Installation

More information

About the EMB-312 T-27 Tucano

About the EMB-312 T-27 Tucano About the EMB-312 T-27 Tucano Projected in 1978 under Joseph Kovacs direction by Embraer, the EMB-312 is a single turbo prop engine basic trainer powered by Pratt & Whitney Canada PT6A-25C turning a HARTZEL

More information

Jet Provost Design & Development. First Came The Piston Provost:

Jet Provost Design & Development. First Came The Piston Provost: Jet Provost Design & Development First Came The Piston Provost: The Predecessor of the Jet Provost was the Percival P.56 Provost which was a British ab-initio trainer developed for the Royal Air Force

More information

LAA TYPE ACCEPTANCE DATA SHEET TADS 134 CORBY STARLET

LAA TYPE ACCEPTANCE DATA SHEET TADS 134 CORBY STARLET Issue 5 New format. Change of contact details for obtaining plans. Dated 19/03/18 JV This TADS is intended as a summary of available information about the type and should be used during the build, operation

More information

ATEC 212 SOLO ROTAX 912 UL

ATEC 212 SOLO ROTAX 912 UL Sole Manufacturer and Distributor in the Czech Republic: ATEC v.o.s. Location of factory: ATEC v.o.s., Opolanská 350, 289 07 Libice nad Cidlinou Czech Republic ATEC 212 SOLO ROTAX 912 UL Flight and Operations

More information

: 6 channel - 9 servo

: 6 channel - 9 servo g Wingspan : 2005mm (78.94 inches) Length : 1640mm (64.57 inches) Weight : 6400g - 6600g Engine : 25cc - 35cc Radio : 6 channel - 9 servo KIT CONTENTS: We have organized the parts as they come out of

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 1A13 Revision 27 Revo, Inc. COLONIAL C-1 COLONIAL C-2 LAKE LA-4 LAKE LA-4A LAKE LA-4P LAKE LA-4-200 LAKE

More information

Assembly and Operating Manual. SPECIFICATION Length inch (640mm) Wing Span inch (705mm) Flying Weight oz (330g)

Assembly and Operating Manual. SPECIFICATION Length inch (640mm) Wing Span inch (705mm) Flying Weight oz (330g) Assembly and Operating Manual SPECIFICATION Length 25.19 inch (640mm) Wing Span 27.76 inch (705mm) Flying Weight 11.64 oz (330g) Dear customer, Assembly and Operating manual VIPER The Radio Control System

More information

Assembly Manual. Version 01/01/2006

Assembly Manual. Version 01/01/2006 Assembly Manual ZI le chenet, 91490 Milly La Foret, FRANCE Tel : 33 1 64 98 93 93 Fax : 33 1 64 98 93 88 E-mail : aviation.design@wanadoo.fr www.adjets.com Version 01/01/2006 INTRODUCTION is our new jet

More information

Building A Replica Aircraft. Part One

Building A Replica Aircraft. Part One Building A Replica Aircraft Part One Project History Obtained a Graham Lee Nieuport 11 project in July 2005 Project History Intended to be a retirement project so was stored. Project History Researching

More information

LAA TYPE ACCEPTANCE DATA SHEET TADS 048 DRUINE D.31 AND D.31A TURBULENT. Issue 1 Initial Issue dated

LAA TYPE ACCEPTANCE DATA SHEET TADS 048 DRUINE D.31 AND D.31A TURBULENT. Issue 1 Initial Issue dated Issue 1 Initial Issue dated 8.1.07 1. UK contact Popular Flying Association, Turweston Aerodrome, Turweston, Nr Brackley, Northants, NN13 5YD. Tel: 01280 846786. E-mail: engineering@laa.uk.com LAA Inspector

More information

SD3-60 STRUCTURAL REPAIR MANUAL

SD3-60 STRUCTURAL REPAIR MANUAL SRM 1.0.0.0STRUCTURES - GENERAL 1. Introduction This chapter contains structural repair information of a general nature pertaining to the complete aircraft. Areas particularly prone to damage are shown.

More information

European Aviation Safety Agency XA42

European Aviation Safety Agency XA42 Page 1 of 13 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET A.507 XtremeAir GmbH Harzstrasse 2, Am Flughafen Cochstedt 39444 Hecklingen Germany For model: XA41 CONTENT Page 2 of 13 SECTION

More information

AE 451 Aeronautical Engineering Design I Propulsion and Fuel System Integration. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering December 2017

AE 451 Aeronautical Engineering Design I Propulsion and Fuel System Integration. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering December 2017 AE 451 Aeronautical Engineering Design I Propulsion and Fuel System Integration Prof. Dr. Serkan Özgen Dept. Aerospace Engineering December 2017 Propulsion system options 2 Propulsion system options 3

More information

TYPE CERTIFICATE DATA SHEET NO. A8SO

TYPE CERTIFICATE DATA SHEET NO. A8SO DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A8SO Revision 21 (Pitts) S-1S S-1T S-2 S-2A S-2S S-2B S-2C February 15, 2005 TYPE CERTIFICATE DATA SHEET NO. A8SO This data sheet, which is

More information

Thank you again, Jim McCormick. Jabiru Pacific LLC

Thank you again, Jim McCormick. Jabiru Pacific LLC Thank you for your inquiry about Jabiru Aircraft. Jabiru Aircraft PTY, Ltd, produces a line of kit aircraft that are among the most extensively tested and thoroughly developed kit planes in the entire

More information

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC 98-03 Revision 3 HPH spol. s r.o. Glasflügel 304 CZ Glasflügel 304 CZ-17 Glasflügel 304 C 15.07.2005 TYPE CERTIFICATE DATA SHEET No. 98-03 This data sheet

More information

Saberwing Aircraft Kit

Saberwing Aircraft Kit Saberwing Aircraft Kit By Azalea Aviation, LLC. Kit Information THE PURPOSE behind the DESIGN The SABERWING is a new aircraft designed and purpose built as an answer to many problems and challenges that

More information

Pilot s Operating Handbook FK 9 ELA

Pilot s Operating Handbook FK 9 ELA Pilot s Operating Handbook FK 9 ELA POH FK 9 Mk V ELA Airplane Serial Number: Airplane Registration Number: Date of issue: Manual Nr.: Approved as Light Sport Aircraft 9- -1LSAS Manufacturer and exclusive

More information

When Bryan Melborn (EAA ) and I began this Firefly project last year we had three. Proving it can be done legally. Steve Boetto, EAA 95196

When Bryan Melborn (EAA ) and I began this Firefly project last year we had three. Proving it can be done legally. Steve Boetto, EAA 95196 Proving it can be done legally Steve Boetto, EAA 95196 When Bryan Melborn (EAA 716464) and I began this Firefly project last year we had three goals: 1) Build an aircraft that we would enjoy flying; 2)

More information

SebArt professional line

SebArt professional line SebArt professional line The real plane SF260TP S 50E ARF scale ASSEMBLY MANUAL The SIAI-Marchetti SF260 is an Italian light aircraft marketed as an aerobatics and military trainer. It was designed by

More information

The. hots. The newest member of this fun fly family is also the lightest and 3D capable!

The. hots. The newest member of this fun fly family is also the lightest and 3D capable! construction by STEvEn SAnTIcH photos by STEvEn SAnTIcH The electro hots The newest member of this fun fly family is also the lightest and 3D capable! Today, in The competition 3d world, the models being

More information

Model 162 SkyCatcher Update - Cessna

Model 162 SkyCatcher Update - Cessna National Training Aircraft Symposium (NTAS) 2009 - Preparing Students for the Future: SMS & NextGen Model 162 SkyCatcher Update - Cessna Julie Filucci Cessna Pilot Center Manager Follow this and additional

More information

LAA TYPE ACCEPTANCE DATA SHEET TADS 385 BRISTELL NG5 SPEED WING

LAA TYPE ACCEPTANCE DATA SHEET TADS 385 BRISTELL NG5 SPEED WING Issue 2 Revised elevator trim tab deflections Dated 11/3/15 JV Revision A Amended fuel tank capacity, addition of Dated 7/5/15 JV Jabiru engine, amended agent website address Revision B Correction of Jabiru

More information

Cleveland Quickie Piper Cub

Cleveland Quickie Piper Cub Cleveland Quickie Piper Cub This plan package is not a 100% copy of the original kit. As you make your way through the instructions you will see the differences. Here s just a few of them: The one thing

More information

WHISPERAIRCRAFT.COM THE NEW

WHISPERAIRCRAFT.COM THE NEW WHISPERAIRCRAFT.COM THE NEW Welcome Welcome to the X350 Gen II "The X350 Gen II is one of those aircraft that makes you grin every time you take to the sky. To say the performance is spectacular would

More information

SAE Aero Design. Apr 29, 2016

SAE Aero Design. Apr 29, 2016 SAE Aero Design Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro Department of Mechanical Engineering Apr 29, 2016 Overview Introduction Need Statement

More information

Aircraft Assembly, Rigging & Weighing. Restoration steps leading to first flight. RON ALEXANDER PHOTOS Bin. HAMMOND AVIATION

Aircraft Assembly, Rigging & Weighing. Restoration steps leading to first flight. RON ALEXANDER PHOTOS Bin. HAMMOND AVIATION Nuts & Bolts Beginning the rigging process. OVER THE PAST SEVERAL months we've taken an indepth look at the process of restoring an antique or classic airplane. In March we discussed supplemental type

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A11EA Revision 9 American General Aircraft Holding Co. AA-1 AA-1A AA-1B AA-1C June 7, 1995 TYPE CERTIFICATE DATA SHEET NO. A11EA This data sheet,

More information

PAC 750XL PAC 750XL PAC-750XL

PAC 750XL PAC 750XL PAC-750XL PAC 750XL The PAC 750XL combines a short take off and landing performance with a large load carrying capability. The PAC 750XL is a distinctive type. Its design philosophy is reflected in the aircraft's

More information

European Aviation Safety Agency

European Aviation Safety Agency European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET VSO 10 Type Certificate Holder: Schempp-Hirth výroba letadel spol. s r.o U Dvořiska 1733 565 01 Choceň EASA TCDS No. A.442 For variants:

More information

We believe, this idea is wrong, as it means a setback in the Jungmann development process.

We believe, this idea is wrong, as it means a setback in the Jungmann development process. 1 / 21 Via internet, you might have got the news a German workshop in partnership with the distributor of the Polish built T-131 aircraft, are planning to construct the Bü-131-B airplane. We believe, this

More information

Instruction Manual. Wingspan : 1400 mm (55.12 inch) : 1480 mm (58.27 inch) : 5500gr gr. : 6-9 channel/ 8 servo high torque,1 standard

Instruction Manual. Wingspan : 1400 mm (55.12 inch) : 1480 mm (58.27 inch) : 5500gr gr. : 6-9 channel/ 8 servo high torque,1 standard Wingspan : 1400 mm (55.12 inch) g Length : 1480 mm (58.27 inch) Weight : 5500gr - 6000gr Radio : 6-9 channel/ 8 servo high torque,1 standard Engine : GT 22 OS KIT CONTENTS: We have organized the parts

More information

Instruction Manual book

Instruction Manual book book ITEM CODE:BH 115. SPECIFICATION Wingspan : 6,000 mm 236,22 in. Length : 2,740 mm 107,87 in. Weight : 17.5kg 38.5Lbs. Radio : 08 channels. Servo : 07-08 HS-5685MH(HITEC) Battery : 2 Cells-Li-Po 7.4V

More information

JIM BEDE ADDS TWO HOMEBUILTS TO HIS LINE - THE BD-5J AND THE ALL NEW BD-6

JIM BEDE ADDS TWO HOMEBUILTS TO HIS LINE - THE BD-5J AND THE ALL NEW BD-6 Newest homebuilt from Jim Bede is the BD-6, a single-place version of the popular four-place BD-4. A BD-6 FOR $2000 JIM BEDE ADDS TWO HOMEBUILTS TO HIS LINE - THE BD-5J AND THE ALL NEW BD-6 By WALTER SHELBOURNE

More information

the leading edge of the wing, at the fuselage - Length: 1540mm (60.6 in) 10% expo; High: 15mm up/down, 10% expo - Wing area: 40dm2

the leading edge of the wing, at the fuselage - Length: 1540mm (60.6 in) 10% expo; High: 15mm up/down, 10% expo - Wing area: 40dm2 SPECIFICATION - Gravity CG: 165-170 mm (6.5-6.7 in) Back from - Wingspan: 1400mm (55.1 in) the leading edge of the wing, at the fuselage - Length: 1540mm (60.6 in) - Control throw Ailerons: Low: 12mm up/down,

More information

RECOMMENDED EDF AND BATTERY SET UP

RECOMMENDED EDF AND BATTERY SET UP SPECIFICATION - Wingspan: 1150mm (45.3 in) - Length: 1587mm (62.5 in) - Flying weight: 5.0-5.3 kg - Wing area: 40dm2 - Wing loading: 125g/dm2 - Wing type: Naca airfoils - Covering type: Genuine ORACOVER

More information

Pilatus Aircraft Ltd. P.O. Box 992 CH Stans SWITZERLAND

Pilatus Aircraft Ltd. P.O. Box 992 CH Stans SWITZERLAND F -3 1 of 7 This Data Sheet which is a part of Type Certificate No. F -3 prescribes conditions and limitations under which the product, for which the Type Certification was issued, meets the airworthiness

More information

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 10 Weight of Components. Tables

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 10 Weight of Components. Tables Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 10 Weight of Components Tables No Aircraft MTOW/Payload Weight 1 Transport 3-4 2 Single engine light GA 3-6 3 Twin-engine

More information

CHAPTER 2 THE TUTOR. Introduction

CHAPTER 2 THE TUTOR. Introduction CHAPTER 2 THE TUTOR Introduction 1. AEFs. The Royal Air Force has 12 units throughout the country known as Air Experience flights (AEFs). Their role is to provide air experience flying for cadets and they

More information

the sky is your freeway

the sky is your freeway the sky is your freeway Discover new flight horizons Never before has flying been easier, more fun and safer than with the REMOS GX. That is the verdict of experienced professional civilian and military

More information

PilotRC Trainer USER MANUAL

PilotRC Trainer USER MANUAL PilotRC Trainer USER MANUAL Introduction Thank you for purchasing our Trainer plane. we strive to achieve a good quality quick build ARF aircraft. It requires the least amount of assembly of any ARF kit

More information

SAE Aero Design. Mid point Review. Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro Team 16

SAE Aero Design. Mid point Review. Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro Team 16 SAE Aero Design Mid point Review Ali Alqalaf, Jasem Alshammari, Dong Yang Cao, Darren Frankenberger, Steven Goettl, and John Santoro Team 16 Submitted towards partial fulfillment of the requirements for

More information

RECOMMENDED MOTOR AND BATTERY SET UP

RECOMMENDED MOTOR AND BATTERY SET UP SPECIFICATION - Wingspan: 2190mm (86.2 in) - Length: 1907mm (75 in) - Flying weight: 9000-12000 gr - Wing area: 92 dm2 - Wing loading: 98g/dm2 - Wing type: Naca airfoils - Retract gear type: Air-retract

More information

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC 74-01 Revision 5 MORAVAN-AEROPLANES a.s. Model Z 726 Model Z 726 K 11.04.2007 TYPE CERTIFICATE DATA SHEET No. 74-01 This data sheet, which is a part of Type

More information

FM-250 Vampire Flight Manual

FM-250 Vampire Flight Manual FM-250 Vampire Flight Manual Flight Manual Page 0 of 40 TABLE OF CONTENTS SECTION 1. General 2. Limitations 3. Normal Procedures 4. Emergency Procedures 5. Performance 6. Airplane Handling, Service & Maintenance

More information

to fly. Most hardware included and all replacement parts are available.

to fly. Most hardware included and all replacement parts are available. Instruction Manual The Thunderbolt P47 was perhaps the greatest of world war II in terms of all round performance and capability Phoenix Model has recreated a 2C - 60 class engine (or 4c 91 class) It was

More information

Center of Gravity Location and Longitudinal Stability and Control for Glasair II-S TD Aircraft

Center of Gravity Location and Longitudinal Stability and Control for Glasair II-S TD Aircraft SERVICE BULLETIN 113, SUPPLEMENT A (MANDATORY) NOTE: This Service Bulletin supplements and expands on the information presented in Service Bulletin 113. Any specifications, limits, or requirements published

More information

PIPER CUB J3-65 N68952 PRE-FLIGHT CHECKLIST

PIPER CUB J3-65 N68952 PRE-FLIGHT CHECKLIST PRE-FLIGHT CHECKLIST COCKPIT Check airworthiness certificate, registration, weight & balance documentation Battery - CONNECTED Plug in headsets or secure as required Fuel ON Primer CLOSED & LOCKED Carb

More information

RECOMMENDED MOTOR AND BATTERY SET UP

RECOMMENDED MOTOR AND BATTERY SET UP SPECIFICATION - Wingspan: 2567mm (101in) - Length: 2190mm (86.2 in) - Flying weight: 11-13 kg - Wing area: 101 dm2 - Wing loading: 99g/dm2 - Wing type: Naca airfoils - Covering type: Genuine ORACOVER -

More information

Installation Work for Alpha Systems Angle of Attack System DSTR-AOA-9600K 05/28/2015

Installation Work for Alpha Systems Angle of Attack System DSTR-AOA-9600K 05/28/2015 Installation Work for Alpha Systems Angle of Attack System DSTR-AOA-9600K 05/28/2015 Aircraft Information: Piper Arrow 200 PA-28R-200 Overall Description: A model DSTR-AOA-9600K Angle of Attack System

More information