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1877 Issue 2 Date: 20 June 2005
MICROLIGHT AIRWORTHINESS APPROVAL NOTE MAAN NO:1877 ISSUE 2 DATE: 20 JUNE 2005 TITLE: Microlight Airworthiness Approval Note 1877, Shadow D, DD and D-SS aircraft, resolution of pitch circuit resonance (elevator flutter) concerns. STAGE: Approval. 1. INTRODUCTION The CFM Shadow D, DD and D-SS are Type Approved microlight types described in Microlight TADS BM55. During the flight testing of a prototype Shadow ED aircraft, G-THAI under authority of MAAN 1824 it was found that the aircraft suffered from a divergent resonance of the pitch control circuit; this was considered unacceptable and also non-compliant with BCAR S181. The sole currently flying example of the Shadow D-SS, G-MZLP was subsequently tested and shown to display similar characteristics. Following on from this, the BMAA conducted sample testing of two Shadow DD aircraft and four Shadow CD aircraft. Based upon this, the following conclusions were reached:- (1) Shadow CD aircraft (and thus by read-across, the B, BD and C aircraft) do not show any significant tendency towards pitch circuit resonance. (2) Shadow D-SS and DD aircraft (and thus by read-across D aircraft) do show a tendency towards pitch circuit resonance, which can become divergent. Where this becomes divergent it is unacceptable, in other cases, it is still a cause for concern. It was therefore decided that action was required to minimise the risk of a flutter related accident in a D, DD or D-SS Shadow. Issue 1 of this MAAN released Service Bulletin MAAN 1877/1 issue 1 which required a mandatory test flight before further flight, immediate grounding of any aircraft which showed divergent elevator flutter, and in any case grounding of all aircraft in this series from 20 June 2005 unless a permanent solution to the problem of elevator flutter could be found. -
Bmaa Technical Information Leaflet (Til) Til 069 Issue 2
BMAA TECHNICAL INFORMATION LEAFLET (TIL) TIL 069 ISSUE 2 SERIES MAJOR MODIFCATIONS 1. Introduction BMAA major modifications that have been both well defined by the original applicant and for which quality control procedures have been put in place are defined as ‘series’ modifications. Subsequent applicants apply for these in the same way as for ‘one-off’ BMAA modifications (using form BMAA/AW/002a), but do not need to provide a technical justification. Notes: o Series modifications must be identical to the first approval; if there is any change or non-compliance with respect to the original MAAN then a new approval is required. o Note that BMAA ‘series’ major modifications may not be applied for with a Permit revalidation application. This is because a Flight Release Certificate has to be issued and then signed by a BMAA Inspector. o BMAA 'series' major modifications are now charged at a reduced rate (compared to ‘one-off’ modifications). A list of existing BMAA 'series' modifications can be found below. 2. Existing BMAA Series Major Modifications The table below contains a list of issued BMAA ‘Series’ Major Modifications (up to January 2021 / MAAN 2864). The ‘Type(s)’ and ‘Brief description’ are indicative only; the BMAA Technical Office should be consulted prior to applying for the modification to confirm the details of the modification. MAAN Issue Type(s) Brief description 1001 1 Pathfinder Intro of 2.3:1 and 2.86:1 reduction drive ratios 1002 2 130SX/Halfpint E Rotax 337 and Newton 2-blade, 54" x 42.5" prop 1061 2 Hornet Duel Trainer Raven 45 litre plastic fuel tank 1066 1 Goldwing Intro Nicklow 2.86:1 reduction and Romain 2-blade 58" x 34" prop 1069 2 Goldwing Installation of Konig SC430 radial engine with Catto 56"X 28" prop 1076 1 Raven-X 3-blade Ivoprop, 62"x 9deg to Rotax 447. -
066-070 LAA Sept08 26/08/2008 3:08 Pm Page 67
066-070_LAA_Sept08 26/08/2008 3:07 pm Page 66 Classifieds For all display or commercial advertising AIRCRAFT FOR SALE enquiries please call our Advertising Manager Victoria Griffiths on +44 (0) 1223 497068 or email [email protected] You can email your classified DYN-AERO MCR01 CLUB. Excellent advertisement direct to the LAA condition, completed 2005, permit to at the following address: TWO SEAT VERSION OF CURRIE July 2009. 110hrs TTE/AF. Rotax 912S [email protected] WOT. Fantastic open cockpit fun with with PV50 CS prop. Comprehensive Next issue: August 2008 new aerobatic LAA permit. Zero timed panel inc. Txpdr (C), horizon, EIS, fuel Deadline for booking and copy: 14th July 2008 Lycoming O-320 (150 HP) engine and computer. Always hangared. Great per- formance, handling and economy £52k. Classified advertising rates full recent aircraft overhaul Only two owners from new. Selling after 10 year View at Branscombe E Devon. £15 per single column cm (one-off) affair due to limited time! A fraction of tel: 01404 871599 £13 per single column cm (Series of six) £10 per single column cm (Series of 12) the price of a Pitts or Skybolt at £16,950 e-mail [email protected] or without engine for £9,950 Contact Display advertising rates Ian Hannah on 0773 960 0421 or Full page cover position £1500 [email protected] EMERAUDE CP301A Continental C90 14F. Full page £1100 TTAF and engine 1400hrs. Permit until April Half page £600 Quarter page £350 ARV SUPER 2. As new. 10 hours airframe, 0 09. -
Diseño Y Construcción Del Avión Fumigador Usb-001-X
DISEÑO PRELIMINAR DEL AVIÓN USB – 001 – X PARA APLICACIÓN DE INSUMOS AGROQUÍMICOS ROGER ALPHONSE ACEVEDO CARLOS GUSTAVO CAMARGO GÓMEZ PEDRO MAURICIO CARO CARO SAMUEL ALBERTO CASTILLO MARTÍNEZ JAIME GIOVANNY CORTÉS GUTIÉRREZ EDGAR SAUL CHAVES JIMÉNEZ CARLOS ENRIQUE ESPAÑA RAMÍREZ JUAN FELIPE GONZÁLEZ CARREÑO VIVIANA ANGÉLICA MARTÍN CAMACHO LENIN EDUARDO MORALES PEÑA EMILIO MORELL PAZ PABLO CÉSAR NAVARRO RUIZ JUAN FELIPE OCHOA RESTREPO JOSÉ LUIS VALLEJO ROMO UNIVERSIDAD DE SAN BUENAVENTURA FACULTAD DE INGENIERÍA PROGRAMA DE INGENIERÍA AERONÁUTICA BOGOTÁ, D.C. 2003 DISEÑO PRELIMINAR DEL AVIÓN USB – 001 – X PARA APLICACIÓN DE INSUMOS AGROQUÍMICOS ROGER ALPHONSE ACEVEDO CARLOS GUSTAVO CAMARGO GÓMEZ PEDRO MAURICIO CARO CARO SAMUEL ALBERTO CASTILLO MARTÍNEZ JAIME GIOVANNY CORTÉS GUTIÉRREZ EDGAR SAUL CHAVES JIMÉNEZ CARLOS ENRIQUE ESPAÑA RAMÍREZ JUAN FELIPE GONZÁLEZ CARREÑO VIVIANA ANGÉLICA MARTÍN CAMACHO LENIN EDUARDO MORALES PEÑA EMILIO MORELL PAZ PABLO CÉSAR NAVARRO RUIZ JUAN FELIPE OCHOA RESTREPO JOSÉ LUIS VALLEJO ROMO Trabajo de investigación presentado como requisito parcial para optar al título de Ingeniero Aeronáutico Director: Ing. Miller Bermúdez UNIVERSIDAD DE SAN BUENAVENTURA FACULTAD DE INGENIERÍA PROGRAMA DE INGENIERÍA AERONÁUTICA BOGOTÁ D.C. 2003 Nota de Aceptación __________________________________ __________________________________ __________________________________ __________________________________ __________________________________ __________________________________ Presidente del Jurado Jurado __________________________________ Jurado Bogotá D.C. 28 de mayo de 2003 AGRADECIMIENTOS Los autores expresan sus más sinceros agradecimientos a: Fray Fernando Garzón Ramírez Rector de la Universidad de San Buenaventura, por el apoyo brindado durante todo el proceso, como pioneros del gran proyecto institucional que es el USB-001-X. Miller Bermúdez. Ingeniero Aeronáutico y director técnico del trabajo de investigación, por la confianza y orientación en busca de la mejor solución a los problemas planteados. -
Cfm Shadow D, D-D Tads 206 Cfm Streak Shadow Sa Tads 206A Cfm Star Streak Shadow Sa-Ii Tads 206B Cfm Streak Shadow Sa-M
LAA TYPE ACCEPTANCE DATA SHEET TADS 161 CFM SHADOW D, D-D TADS 206 CFM STREAK SHADOW SA TADS 206A CFM STAR STREAK SHADOW SA-II TADS 206B CFM STREAK SHADOW SA-M Introduction of other Shadow variants and Issue 6 Dated 24/01/18 JP expanded information Addition of Standard Modifications at section 3.6. Revision A Amended descriptions of Streak Shadow and Star Dated 01/03/19 JV Streak. Revision B Addition of Safety Spot articles Dated 28/11/19 JH Updated contact information. Addition of SB 10 in Revision C Dated 14/01/21 JV section 3.3 This TADS is intended as a summary of available information about the type and should be used during the build, operation and permit revalidation phases to help owners and inspectors. Although it is hoped that this document is as complete as possible, other sources may contain more up to date information, e.g. the manufacturer’s website. Section 1 contains general information about the type. Section 2 contains information about the type that is MANDATORY and must be complied with. Section 3 contains advisory information that owners and inspectors should review to help them maintain the aircraft in an airworthy condition. If due consideration and circumstances suggest that compliance with the requirements in this section can safely be deferred, is not required or not applicable, then this is a permitted judgement call. This section also provides a useful repository for advisory information gathered through defect reports and experience. Section 1 - Introduction 1.1 UK contact The original manufacturers are no longer in existence. -
Genesis of a Shadow
GENESIS OF A SHADOW An academic, John Dickenson OAM, BA Psycho, FAI, DIP, reinvented the hang glider in 1963. It was a triangular flex wing type with a sail that was very different from the original rigid types designed in the late nineteenth century. This design led to the worldwide sport of hang gliding, even reviving the rigid wing types too. This sport allowed the ordinary citizen to be part of the flying scene, previously costing far too much for the dream of flying. Pretty soon small engines were added to the hang gliders and, being foot launched, led this sport into powered hang gliding. As the weight of these machines gradually increased, foot launching became difficult – wheels and a seat were added and many now resembled small aircraft. This sport was totally unregulated with some designs being questionable as to their structural integrity. There were serious injuries occurring and soon regulation by the CAA (Civil Aviation Authority UK) devised a set of standards in the 1980’s. This fresh category of aircraft was termed Microlights, whether they were flex wing or rigid types. Within certain limits the rules for this category were minimum wing area, empty weight, and maximum two places for crew. 1 This allowed myself to initiate a design series called Shadow. My interest was to try to eliminate many poor and sometimes dangerous aspects of normal aircraft. Poor design has always been apparent to me in many military and private types. I was going to try to design out initial poor conception. My elderly friend, Volmer Jensen in Glendale, California, who designed and built 24 different aircraft, said to me, “Get it wrong at the beginning and it’s wrong at the end”.