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The Bell 47 Helicopter Story by Robert S
The Bell 47 Helicopter Story By Robert S. Petite and Jeffrey C. Evans Reviewed by Parrish Kelley and Todd Carlson AHS asked Parrish Kelley, son of Bartram Kelley (Bell Helicopter’s first chief engineer), and Todd Carlson, son of Floyd Carlson (its first chief pilot), to review this book. Here are their views. Todd Carlson Parrish Kelley hen we were children, my brothers – Blair and Rand ometime around 1990, I went with my father, Bartram – and I were always aware of the presence in our Kelley, to the Bell Helicopter Textron plant in Hurst, Wfamily of the Bell helicopter, specifically the Model STexas, to look for the original 16 mm movies he and 47 and its predecessor, the Model 30. This presence took the other engineers had shot during the project that produced physical form of a large box of photos, newspaper clippings, the Bell Model 47 in Gardenville, New York. I was hoping to letters, awards and log books. Although poorly maintained find the many hours of raw footage from which he had and totally disorganized, it was always there, just as are my selected scenes for his one-hour movie, The Birth of the Bell memories of growing up with a helicopter in the back yard in Helicopter , which I saw as merely an engineering record. Williamsville, New York, the occasional rides over Niagara Falls Unfortunately, the audiovisual department didn’t have the and other sights, and the many stories shared among family original footage, but they did show us their vast array of still and friends. photographs going back to the founding of the company, a While Dad lived and breathed the helicopter all of his collection virtually unseen by the public. -
Aero Ae 45 & Ae
This production list is presented to you by the editorial team of "Soviet Transports" - current to the beginning of January 2021. Additions and corrections are welcome at [email protected] Aero Ae 45 & Ae 145 181 Ae 45 built by Aero at Prague-Vysocany from 1947 to 1951 The c/n consisted of the year of manufacture and a sequential number. 1 OK-BCA Ae 45 Aero f/f 21jul47 the first prototype; rgd 11sep47; underwent trials with the SVZÚ sep47 OK-BCA Ae 45 Ministers. dopravy trf unknown Ministry of Transport OK-BCA Ae 45 CSA trf unknown canx 1953 2 OK-CCA Ae 45 Aero rgd 09apr48 the second prototype; f/f 12mar48 OK-CCA Ae 45 Celulozka Bratisl. trf unknown Celulozka Bratislava; canx 1958 not known Ae 45 Czechoslovak AF trf unknown 49 003 G-007 (1) Ae 45 Hungarian AF d/d 15may49 HA-AEB Ae 45 MÉM Rep. Szolgálat trf 06apr52 Hungarian Flying Association; damaged 29apr52 when the landing gear broke HA-AEB Ae 45 OMSZ trf 18jun57 Hungarian Air Ambulance; w/o (or canx ?) 22nov62 49 004 OK-DCB Ae 45 rgd 21apr49 canx to Italy I-CRES Ae 45 Aero Club Milano rgd 18jul59 Aero Club Milano of Linate; owner also reported as Franco Rol; based at Torino; canx 1970 F-GFYA Ae 45 Pierre Cavassilas res aug88 Pierre Cavassilas of Chavenay; possibly never fully registered F-AZJX Ae 45 Pierre Cavassilas rgd 08jul94 seen Chavenay 20may94 with a 'W' taped over the 'A' of the registration; still current in 2007; under restoration near Paris in 2008; was to be reflown jan09; seen Compiègne 19jun09 and 27jun09 in all-grey c/s with large blue registration, in great condition; seen Soissons-Courmelles 28may12 with smaller black registration; l/n Compiègne 15jun13, active 49 005 OK-DCA Ae 45 rgd 23apr49 I-AERA Ae 45 Luigi Leone rgd 11oct61 based at Torino 49 006 HB-EKF Ae 45 Mr. -
R&T Activities on Composite Structures
PUBLIC RELEASE R&T activities on composite structures for existing and future military A/C platforms at Airbus DS, Military Aircraft Mircea Calomfirescu, Rainer Neumaier, Thomas Körwien, Kay Dittrich Airbus Defence and Space GmbH Rechliner Str. 1 85077 Manching GERMANY [email protected] ABSTRACT This paper gives a short overview on the state of the art in composite aerostructures for civil and military aircraft. Major challenges are highlighted in this context and the requirements from military aircraft point of view are illustrated, derived from existing and future military aircraft perspectives. The main objective of the paper is to present the R&T activities in the aerostructure research program called FFS, advanced aerostructures. The activities range here from structural bonding, advanced radomes, new thermoplastic composite technologies and new materials and structures for low observability purposes. A brief insight is given to each of the topic highlighting the challenges and approaches, finishing with a summary of future trends and emerging technologies. 1.0 INTRODUCTION Composites offer several advantages over metallic aerostructures in civil as well as in military aircraft industry including reduced weight, less maintenance effort and costs due to “corrosion-free” composites and a superior fatigue behaviour compared to aluminium. The thermal expansion is much less and the material waste (“buy to fly ratio”) is more advantageous compared to aluminium structures. However, these advantages come along with higher material and manufacturing costs. For the prepreg technology for example the material has to be stored at -18°C, energy and investment intensive autoclaves are necessary and for quality assurance 100% non-destructive testing (NDT) is required in contrast to aluminium structures. -
Federal Register/Vol. 73, No. 161/Tuesday, August 19, 2008
48310 Federal Register / Vol. 73, No. 161 / Tuesday, August 19, 2008 / Proposed Rules DEPARTMENT OF TRANSPORTATION Docket Management Facility between 9 3. The modifications in paragraphs 1 and a.m. and 5 p.m., Monday through 2 above are to be accomplished in accordance Federal Aviation Administration Friday, except Federal holidays. The AD with de Havilland Service Bulletin 6/508 docket contains this proposed AD, the dated 15 December 1989, or later revisions 14 CFR Part 39 approved by the Director, Airworthiness regulatory evaluation, any comments Branch, Transport Canada, Ottawa. received, and other information. The [Docket No. FAA–2008–0891; Directorate Based on preliminary investigation, the Identifier 2008–CE–046–AD] street address for the Docket Office (telephone (800) 647–5527) is in the FAA and NTSB believe that an RIN 2120–AA64 ADDRESSES section. Comments will be attempted takeoff with the gust locks available in the AD docket shortly after installed could be the cause of a recent Airworthiness Directives; Viking Air receipt. accident in Hyannis, Massachusetts. Limited DHC–6 Series Airplanes FOR FURTHER INFORMATION CONTACT: Relevant Service Information AGENCY: Federal Aviation Fabio Buttitta, Aerospace Engineer, Boeing Canada de Havilland Division Administration (FAA), Department of FAA, New York Certification Office, issued Service Bulletin No. 6/508, Transportation (DOT). 1600 Stewart Avenue, Suite 410, Revision ‘‘A’’, dated January 31, 1990. ACTION: Notice of proposed rulemaking Westbury, New York 11590; telephone: The actions described in this service (NPRM). (516) 228–7303; fax: (516) 794–5531. information are intended to correct the SUPPLEMENTARY INFORMATION: unsafe condition identified in the SUMMARY: We propose to adopt a new MCAI. -
Canadian Airmen Lost in Wwii by Date 1943
CANADA'S AIR WAR 1945 updated 21/04/08 January 1945 424 Sqn. and 433 Sqn. begin to re-equip with Lancaster B.I & B.III aircraft (RCAF Sqns.). 443 Sqn. begins to re-equip with Spitfire XIV and XIVe aircraft (RCAF Sqns.). Helicopter Training School established in England on Sikorsky Hoverfly I helicopters. One of these aircraft is transferred to the RCAF. An additional 16 PLUTO fuel pipelines are laid under the English Channel to points in France (Oxford). Japanese airstrip at Sandakan, Borneo, is put out of action by Allied bombing. Built with forced labour by some 3,600 Indonesian civilians and 2,400 Australian and British PoWs captured at Singapore (of which only some 1,900 were still alive at this time). It is decided to abandon the airfield. Between January and March the prisoners are force marched in groups to a new location 160 miles away, but most cannot complete the journey due to disease and malnutrition, and are killed by their guards. Only 6 Australian servicemen are found alive from this group at the end of the war, having escaped from the column, and only 3 of these survived to testify against their guards. All the remaining enlisted RAF prisoners of 205 Sqn., captured at Singapore and Indonesia, died in these death marches (Jardine, wikipedia). On the Russian front Soviet and Allied air forces (French, Czechoslovakian, Polish, etc, units flying under Soviet command) on their front with Germany total over 16,000 fighters, bombers, dive bombers and ground attack aircraft (Passingham & Klepacki). During January #2 Flying Instructor School, Pearce, Alberta, closes (http://www.bombercrew.com/BCATP.htm). -
Experimental Analysis of Composite Jet Engine Air Inlet
36th Danubia-Adria Symposium on Advances in Experimental Mechanics 24–27 September 2019, Plzeň, Czech Republic EXPERIMENTAL ANALYSIS OF COMPOSITE JET ENGINE AIR INLET Karel DOUBRAVA1, Milan DVOŘÁK2, Nikola SCHMIDOVÁ3, Tomáš KOSTROUN4, Jan VÁCLAVÍK5 and Milan RŮŽIČKA6 1 Czech Technical University in Prague, Faculty of Mechanical Engineering, Technická 4, 166 07 Prague, Czech Republic, E-mail: [email protected] 2 Czech Technical University in Prague, Faculty of Mechanical Engineering, Technická 4, 166 07 Prague, Czech Republic, E-mail: [email protected] 3 Czech Technical University in Prague, Faculty of Mechanical Engineering, Technická 4, 166 07 Prague, Czech Republic, E-mail: [email protected] 4 Czech Technical University in Prague, Faculty of Mechanical Engineering, Technická 4, 166 07 Prague, Czech Republic, E-mail: [email protected] 5 AERO Vodochody AEROSPACE a.s., U Letiště 374, 250 70 Odolena Voda , Czech Republic, E- mail: [email protected] 6 Czech Technical University in Prague, Faculty of Mechanical Engineering, Technická 4, 166 07 Prague, Czech Republic, E-mail: [email protected] 1. Introduction 2. Air inlet Aero L-39 light jet trainer is widely used in many The complete air inlet (see Fig. 2) is composed countries around the world. One important element of three main composite parts. of the structure is the air inlet. Fatigue life of the metal air inlet is one of the factors limiting service life of entire aircraft. The new generation L-39NG jet trainer (see Fig. 1) represents deep modernization of the L-39 combining latest engine and aircraft systems technology with traditional advantages of L-39s legacy. -
ATR-42/72 Rev 6
U.S. Department of Transportation Federal Aviation Administration Washington, DC Flight Standardization Board (FSB) Report Revision: 6 Date: 10/14/2016 Manufacturer ATR – GIE Avions de Transport Régional Type Certification Data Sheet (TCDS) A53EU TCDS Identifiers ATR-42 ATR-72 ATR-42-200-300-320-500-600 ATR-72-101-102-201-202-211-212A-212 Pilot Type Rating ATR42 ATR72 Timothy C. Hayward, Chair Flight Standardization Board Federal Aviation Administration Flight Standards Division Seattle Aircraft Evaluation Group 1601 Lind Avenue SW Renton, WA 98057-3356 Telephone: (425) 917-6600 Fax: (425) 917-6638 Revision 6 10/14/2016 ATR-42/ATR-72 FSB Report RECORD OF REVISIONS REVISION SECTION PAGES DATE 1 9.2.4 17–27 01/10/1994 2 ALL ALL 02/01/1996 3 VARIOUS VARIOUS 07/01/1997 4 VARIOUS VARIOUS 7/15/2002 5 ALL ALL 12/05/2014 6 ALL ALL 10/14/2016 HIGHLIGHTS OF CHANGE All Sections All Pages: This revision contains minor editorial changes on every page for clarity, consistency, standardization, updated terminology, acronyms, and United States Workforce Rehabilitation Act Section 508 compliancy. Added Clarity for Training for Seat-Dependent Tasks (6.1.7 and 6.1.7). Added Clarity for Second-in-Command (SIC) Training Tasks (6.1.8). Added Clarity for Unique Training Provisions (6.2.6.1). Page 2 of 26 Revision 6 10/14/2016 ATR-42/ATR-72 FSB Report CONTENTS SECTION PAGE RECORD OF REVISIONS .......................................................................................................2 HIGHLIGHTS OF CHANGE ...................................................................................................2 1. PURPOSE AND APPLICABILITY .........................................................................................4 2. PILOT “TYPE RATING” REQUIREMENTS ..........................................................................7 3. “MASTER COMMON REQUIREMENTS” (MCRs) ..............................................................7 4. -
2000 Annual Report
ON THE COVER: THE COLOR SPECTRUM DEPICTED ON THE COVER REPRESENTS THE ESSENCE OF THE FIBER OPTICS INDUSTRY. THIS YEAR’S TELEDYNE TECHNOLOGIES ANNUAL REPORT FEATURES A STORY ON TELEDYNE OPTOELECTRONICS, A NEWLY FORMED OPERATING UNIT WITHIN THE TELEDYNE ELECTRONIC TECHNOLOGIES DIVISION. THE PHOTO ABOVE SHOWS A COMPONENT THAT IS USED IN THE F-22 JET FIGHTER. TELEDYNE TECHNOLOGIES INCORPORATED 1 2000 ANNUAL REPORT 2000 Highlights Year 2000 Stock Price Performance $30 20 10 0 Dec. 99 March 00 June 00 Sept. 00 Dec. 00 Financial Information (1) For the 2000, 1999 and 1998 fiscal years (Amounts in millions, except per-share amounts) 2000 1999 1998 Sales $ 795.1 $ 761.4 $ 733.0 Net income from continuing operations before opto/wireless costs (2) $ 46.1 $ 40.9 $ 37.5 Opto/wireless costs, net of tax $ 5.6 —— Net income from continuing operations (2) $ 40.5 $ 40.9 $ 37.5 Diluted earnings per-share from continuing operations before opto/wireless costs (2) $ 1.56 $ 1.50 $ 1.33 Diluted earnings per-share from continuing operations (2) $ 1.37 $ 1.50 $ 1.33 Weighted average diluted common shares outstanding 29.5 (3) 27.3 28.1 (1) On a proforma basis and restated to reflect Teledyne Cast Parts as a discontinued operation (2) Excludes after tax charges of $8.6 million and $1.8 million in 2000 and 1999, respectively, for product recall reserves taken in 2000 and 1999 and other charges taken in 2000 (3) Reflects the impact of 4.6 million shares of common stock issued in the third quarter in connection with a required public offering Electronics and Communications Segment Sales by Segment 2000 vs. -
TAC Register Rev 6 22 Feb 2017
2/22/2017 Aircraft TAC TAC Register Rev 6 22 Feb 2017 THE REPOSITORY (SPREADSHEET): This data presented in this repository is a list of approved SACAA TACs as conferred to current foreign TC holders. Aircraft Type/Model File No. Conditions Category TAC Issue Issue Date Reissue Date Common Name 328 Support Services GmbH Dornier 328-100 & Dornier 328-300 J15/12/529 As per Type Certficate Data Sheet EASA.A.096 Standard Original 11 April 2007 - 328JET (328-300) Agusta S.p.A. (Now Leonardo Helicopter) A109E, A109K2, A109S, AW109SP and A109C J15/12/395 This certificate is issued as per EASA Type Certificate number EASA.R.005 Standard Reissue 15 September 1996 01 August 2013 AB139 J15/12/493 This certificate is issued as per EASA Type Certificate number EASA.R.006 Standard Original 21 April 2006 - AB139, AW139 AW189 J15/12/625 This certificate is issued as per EASA Type Certificate number EASA.R.510 Standard Original 24 November 2016 AW189 Air Tractor Inc. AT-402, AT-402B, AT-502, AT-502A, AT-502B & AT-504, AT-402A J15/12/327 This certificate is issued as per FAA Type Certificate number A17SW Restricted Original 15 October 2013 28 July 2016 AT-602, AT-802 and AT-802A J15/12/380 This certificate is issued as per FAA Type Certificate number A19SW Restricted Original 15 October 2013 - Airbus SAS A300B4-622R J15/12/565 This certificate is issued as per DGAC Type Certificate number 72. Standard Original 23 December 2009 - A320-232, A320-233 J15/12/593 This certificate is issued as per EASA Type Certificate number EASA.A.064 Standard Original 23 December 2011 - A330-301, A330-321, A330-322, A330- 341, A330-342, A330-202, A330-223, A330-243, A330-323, A330-343, A330- 203, A330-201, A330-302, A330-303, A330-223F and A330-243F J15/12/584 This certificate is issued as per EASA Type Certificate number EASA.A.004 Standard Original 08 December 2010 10 November 2016 A340-200, A340-300 and A340-600 series J15/12/382 As per DGAC Type Certficate number 183. -
L-39 Albatros
L-39 ALBATROS Type: L-39 Albatros Max Speed: 490 KIAS / Mach 0.80 Max Range: 864 NM G-Limits: +8.0g / -4.0g Ceiling: 36,000 ft Max Climb Rate: 4,130+ fpm Max Endurance: 3.8 hours The L-39 Albatros is a highly capable, stable, subsonic aircraft that first flew in November 1969. The aircraft is produced in the Czech Republic and it is constructed in conjunction with plans developed by Aero Vodochody and its chief designer, Jan Vlček. The L-39 is flown worldwide, principally with former Soviet allies. The aircraft continues to fly in countries as diverse as Iraq, Chechnya, Libya, Syria and Russia. The Albatros is flown primarily as a trainer or light attack aircraft similar in mission to the Italian MB339 or M-346, the British Hawk and the US Goshawk. The L-39 is designed with many distinguishing characteristics. The aircraft possesses a uniquely tall vertical tail that is swept back and is one of its dominant features. The tail, with its inset rudder, provides directional control to the aircraft. The L-39 has thick wings that provide ample lift for the airframe, and each wing has provisions to mount stores or fuel tanks that extend the range of the L-39. Operational g-force limits at 4,200 kg are +8g/-4g. Side-by-side airbrakes are located under the L-39 fuselage slightly ahead of the wing’s leading edge. The L-39 has variable-incidence horizontal stabilizers mounted on the rear of the aircraft at the base of the rudder. -
\Aircraft Recognition Manual
Jf V t 9fn I 4-'!- Vw'^ ' 'o | ^ renai; 408.$ /•> ,A1.AI / -3o FM DEPARTMENT OF THE ARMY FM 30-30 DEPARTMENT OF THE NAVY NavWeps 00-80T-75 DEPARTMENT OF THE AIR FORCE AFM 50-40 MARINE CORPS NavMC 2522 \AIRCRAFT RECOGNITION MANUAL SI ISSUED BY DIRECTION OF\ CHIEF OF BUREAU OF NAVAL WEAPONS \ \ I 4 DEPARTMENT OF THE ARMY FM 30-30 DEPARTMENT OF THE NAVY NavWeps 00-80T-75 DEPARTMENT OF THE AIR FORCE AFM 50-40 MARINE CORPS NavMC 2522 AIRCRAFT RECOGNITION MANUAL •a ISSUED BY DIRECTION OF CHIEF OF BUREAU OF NAVAL WEAPONS JUNE 1962 DEPARTMENTS OF THE ARMY, THE NAVY AND THE AIR FORCE, WASHINGTON 25, D.C., 15 June 1962 FM 30-30/NAVWEPS 00-80T-75/AFM 50-40/NAVMC 2522, Aircraft Recognition Manual, is published for the information and guidance of all concerned. i BY ORDER OF THE SECRETARIES OF THE ARMY, THE NAVY, AND THE AIR FORCE: G. H. DECKER, General, Umted States Army, Official: Chief of Staff. J. C. LAMBERT, Major General, United States Army, The Adjutant General. PAUL D. STROOP Rear Admiral, United States Navy, Chief, Bureau of Naval Weapons. CURTIS E. LEMAY, Official: Chief of Staff, United States Air Force, R. J. PUGH, Colonel, United States Air Force, Director of Administrative Services. C. H. HAYES, Major General, U.S. Marine Corps, Deputy Chief of Staff (Plans). H DISTRIBUTION: ARMY: Active Army : DCSPER (1) Inf/Mech Div Co/Btry/Trp 7-2 44-112 ACSI (1) (5) except Arm/Abn Div 7- 44-236 52 DCSLOG (2) Co/Trp (1) 8- 44-237 137 DCSOPS(5) MDW (1) 8-500 (AA- 44-446 ACSRC (1) Svc Colleges (3) AH) 44447 CNGB (1) Br Svc Sch (5) except 10-201 44^536 -
CHAMPION AEROSPACE LLC AVIATION CATALOG AV-14 Spark
® CHAMPION AEROSPACE LLC AVIATION CATALOG AV-14 REVISED AUGUST 2014 Spark Plugs Oil Filters Slick by Champion Exciters Leads Igniters ® Table of Contents SECTION PAGE Spark Plugs ........................................................................................................................................... 1 Product Features ....................................................................................................................................... 1 Spark Plug Type Designation System ............................................................................................................. 2 Spark Plug Types and Specifications ............................................................................................................. 3 Spark Plug by Popular Aircraft and Engines ................................................................................................ 4-12 Spark Plug Application by Engine Manufacturer .........................................................................................13-16 Other U. S. Aircraft and Piston Engines ....................................................................................................17-18 U. S. Helicopter and Piston Engines ........................................................................................................18-19 International Aircraft Using U. S. Piston Engines ........................................................................................ 19-22 Slick by Champion .............................................................................................................................