European Aviation Safety Agency 13 May 2009
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Runway Analysis
CHAPTER 5 RUNWAY ANALYSIS 5 5 RUNWAY ANALYSIS INTRODUCTION The primary issue to be addressed in the William R. Fairchild International Airport (CLM) Master Plan involves the ultimate length and configuration of the runway system. At present there are two runways; primary Runway 8/26 and crosswind Runway 13/31. Runway 8/26 is 6,347 feet long and 150-feet wide with a displaced threshold of 1,354 feet on the approach end to Runway 26. The threshold was displaced to provide for an unobstructed visual approach slope of 20:1. Runway 13/31 is designated as the crosswind runway and is 3,250-feet long by 50-feet wide. In the 1997 ALP Update, the FAA determined that this runway was not required to provide adequate wind coverage and would not be eligible for FAA funding of any improvements in the future. The Port of Port Angeles has committed to keeping this runway functional without FAA support for as long as it is feasible. Subsequent sections of this analysis will reexamine the need for the runway. Both runways are supported by parallel taxiway systems with Taxiway A serving Runway 8/26 and Taxiway J for Runway 13/31. Taxiway A is 40 feet wide and Taxiway J is 50 feet wide. AIRFIELD REQUIREMENTS In determining airfield requirements, FAA Advisory Circular (AC) 150/5300-13, Airport Design (Change 14), has been consulted. This circular requires that future classification of the airport be defined as the basis for airfield planning criteria. As shown in the forecast chapter, the critical aircraft at CLM is expected to be the small business jet represented by the Cessna Citation within 5-years. -
Communiqué De Presse
Paris, 6th June 2017 PRESS RELEASE First Flight of Russian Aircraft MC-21 Nexeya supplies avionics integration and simulation tools Russia United Aircraft Corporation (UAC) successfully completed the maiden flight of their new MC-21- 300 commercial aircraft at Irkutsk Aviation Plant airfield. Being a modern aircraft, the MC-21 operates with numerous state of the art computer-controlled systems supporting safety-critical flight functions. While this may have been the first time its complex avionics systems have been tested in flight, they have been successfully integrated and tested on the ground thanks to TechSAT’s Avionics Development System ADS2 platform solution. This ADS2 platform enabled UAC Integration Center to test and validate the full MC-21 avionic suits prior to the first flight. Holistic tests including complex operational scenarios were performed during every phases of the design and development of the program ensuring maximum safety and superior performance of the aircraft. TechSAT (a Nexeya company) is proud to be part of the MC-21 program. «TechSAT solutions were designed and built on schedule; all test rigs were thus completed on time», says Victor SINITSYN, head of section at the UAC Integration Center. «ADS2 is a powerful, flexible, and stable product, to perform all required tests. ADS2 keeps its promises. ADS2 functionality is 100% reliable. TechSAT teams are open and skilled to meet customer needs». Marco Häde, TechSAT director of operations : «The key feature of TechSAT’s solutions for MC-21 simulation systems is the integration of all LRUs involved and the cockpit into a real hardware-in-the-loop setup. -
National Transportation Safety Committee Ministry of Transportation Republic of Indonesia 2012
FINAL KNKT.12.05.09.04 NNAATTIIOONNAALL TTRRAANNSSPPOORRTTAATTIIOONN SSAAFFEETTYY CCOOMMMMIITTTTEEEE Aircraft Accident Investigation Report Sukhoi Civil Aircraft Company Sukhoi RRJ–95B; 97004 Mount Salak, West Java Republic of Indonesia 9 May 2012 NATIONAL TRANSPORTATION SAFETY COMMITTEE MINISTRY OF TRANSPORTATION REPUBLIC OF INDONESIA 2012 This Final report was produced by the National Transportation Safety Committee (NTSC), 3rd Floor Ministry of Transportation, Jalan Medan Merdeka Timur No. 5 Jakarta 10110, Indonesia. The report is based upon the investigation carried out by the NTSC in accordance with Annex 13 to the Convention on International Civil Aviation Organization, the Indonesian Aviation Act (UU No. 1/2009) and Government Regulation (PP No. 3/2001). Readers are advised that the NTSC investigates for the sole purpose of enhancing aviation safety. Consequently, the NTSC reports are confined to matters of safety significance and may be misleading if used for any other purpose. As the NTSC believes that safety information is of greatest value if it is passed on for the use of others, readers are encouraged to copy or reprint for further distribution, acknowledging the NTSC as the source. When the NTSC makes recommendations as a result of its investigations or research, safety is its primary consideration. However, the NTSC fully recognizes that the implementation of recommendations arising from its investigations will in some cases incur a cost to the industry. Readers should note that the information in NTSC reports and recommendations -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2014. By Aaron M. U. Church, Associate Editor I 2015 USAF Almanac BOMBER AIRCRAFT flight controls actuate trailing edge surfaces that combine aileron, elevator, and rudder functions. New EHF satcom and high-speed computer upgrade B-1 Lancer recently entered full production. Both are part of the Defensive Management Brief: A long-range bomber capable of penetrating enemy defenses and System-Modernization (DMS-M). Efforts are underway to develop a new VLF delivering the largest weapon load of any aircraft in the inventory. receiver for alternative comms. Weapons integration includes the improved COMMENTARY GBU-57 Massive Ordnance Penetrator and JASSM-ER and future weapons The B-1A was initially proposed as replacement for the B-52, and four pro- such as GBU-53 SDB II, GBU-56 Laser JDAM, JDAM-5000, and LRSO. Flex- totypes were developed and tested in 1970s before program cancellation in ible Strike Package mods will feed GPS data to the weapons bays to allow 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft weapons to be guided before release, to thwart jamming. It also will move added 74,000 lb of usable payload, improved radar, and reduced radar cross stores management to a new integrated processor. Phase 2 will allow nuclear section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in and conventional weapons to be carried simultaneously to increase flexibility. Iraq during Desert Fox in December 1998. -
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. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber. -
NPA 2018-13 Table of Contents
European Aviation Safety Agency Notice of Proposed Amendment 2018-13 Appendix I to AMC to Annex III (Part-66) Aircraft type ratings for Part-66 aircraft maintenance licences RMT.0541 (66.024) EXECUTIVE SUMMARY This Notice of Proposed Amendment (NPA) addresses a regulatory coordination issue related to aircraft type ratings. According to the AMC to Annex III (Part-66), type ratings should be endorsed on an aircraft maintenance licence (AML) in accordance with Appendix I to AMC to Part-66 ‘List of type ratings’. An NPA is issued regularly to amend this list, after assessing feedback received from the industry, and to add new aircraft types or to remove aircraft types whose type certificate (TC) has been revoked or surrendered. This NPA adds also the tables of the new Group as a consequence of the introduction of the ‘L’ licence subcategories by Commission Regulation (EU) 2018/1142. The main objective is to ensure a common standard throughout the Member States. Action area: Regular updates/review of rules Affected rules: AMC/GM to Annex III (Part-66) to Commission Regulation (EU) No 1321/2014 Affected stakeholders: Maintenance certifying staff; maintenance training organisations; maintenance organisations; competent authorities Driver: Efficiency/proportionality Rulemaking group: No Impact assessment: None Rulemaking Procedure: Standard 12.5.2009 5.12.2018 2019/Q2 TE.RPRO.00034-008 © European Aviation Safety Agency. All rights reserved. ISO 9001 certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA intranet/internet. Page 1 of 186 An agency of the European Union European Aviation Safety Agency NPA 2018-13 Table of contents Table of contents 1. -
Annex III to Decision 2015/029/R
AMC/GM TO ANNEX III (PART-66) TO REGULATION (EU) No 1321/2014 APPENDICES TO AMC TO PART-66 APPENDICES TO AMC TO PART-66 APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCES The following aircraft type ratings should be used to ensure a common standard throughout the Member States. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Regulation (EC) No 216/2008 and its Implementing Rules; this list is only intended for maintenance purposes. In order to keep this list current and the type ratings consistent, such information should be first passed on to the Agency using the Rulemaking Enquiry form (http://easa.europa.eu/webgate/rulemaking-enquiry/) in case a Member State needs to issue a type rating that is not included in this list. Notes on when the licences should be modified: When a modification is introduced by this Decision to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the Aircraft Maintenance Licences (AMLs) may be modified at the next renewal or when the licence is reissued, unless there is an urgent reason to modify the licence. Notes on aircraft modified by Supplemental Type Certificate (STC): — This Appendix I intends to include the type ratings of aircraft resulting from STCs for installation of another engine. These STCs are those approved by the Agency and those approved by the Member States before 2003 and grandfathered by the Agency. -
Military Vehicle Options Arising from the Barrel Type Piston Engine
Journal of Power Technologies 101 (1) (2021) 22–33 Military vehicle options arising from the barrel type piston engine Pawe l Mazuro1 and Cezary Chmielewski1,B 1Warsaw University of Technology B [email protected] Abstract in terms of efficiency, meaning that piston engines can deliver enhanced range and endurance. This is benefi- The article reviews knowledge about requirements for engines in cial in missions requiring a stopover for refueling and state-of-the-art unmanned aerial vehicles and tanks. Analysis of particularly useful for unmanned supply, observation design and operational parameters was carried out on selected and maritime missions. turboshaft and piston engines generating power in the range of 500 - 1500 kW (0.5 - 1.5 MW). The data was compared In contrast, land combat vehicles have significantly with the performance of innovative, barrel type piston engines, different drive unit requirements. High mobility en- which are likely to become an alternative drive solution in the ables the vehicle to rapidly change location after de- target vehicle groups. tection. To this end, the torque curve as a function of the rotational speed of the shaft is of decisive im- portance. Keywords: military UAV, tanks, turboshaft engines, piston engines, barrel type piston engines The complexity of tank engines adds an additional layer of requirements, impacting the reliability and durability of the power unit, and they come with re- 1 Introduction lated manufacturing and operating costs. In military land vehicles, the engine should be as small This article consolidates knowledge on options and as possible; the space saved can be used for other capabilities arising from use of the barrel type piston purposes. -
This Is a Quick Guide for the IL76
Ilyushin IL-76 About the airplane: 1 Country of origin: Russia Powerplants: 4 x 117.7kN (26,455 lb) Aviadvigatel Soloviev D30KP turbofans. The IL-76MF is powered by 4 x 156.9kN (35,275 lb) Aviadvigatel PS90ANs. Performance: IL-76T - Max speed 850km/h (460 kts), cruising speed 750 to 800 km/h (405 to 430 kts). Max range with reserves 6700 km (3615 nm), range with 40 ton (88,185 lb) payload 5000 km (2700 nm). IL-76TD - Speeds same. Range with max payload 3650 km (1970 nm), with 20 ton (44,090 lb) payload 7300 km (3940 nm). IL-76MF - Cruising speed range 750 to 780 km/h (405 to 420 kts). Range with 40 ton (88,185 lb) payload 5200 km (2805 nm). Weights: lL-76T - Max takeoff weight: 170,000 kg (374,785 lb). IL-76TD - Max takeoff weight: 190,000 kg (418,875 lb). IL-76MF - Operating empty weight: 101,000 kg (222,665 lb), max payload: 52,000kg (114,640 lb), max takeoff weight: 200,000 kg (440,925 lb). Dimensions: Wing span: 50.50 m (165ft 8 in), length: 46.59 m (152 ft 10 in), height: 14.76m (48 ft 5 in). Wing area: 300.0 m2 (3229.2 ft2). Il-76MF - Same except for length which is approx. 53 m (174 ft). Capacity: Flight crew of five members including two pilots, flight engineer, navigator and radio operator, plus two freight handlers. IL-76MP firefighting conversion can carry 44 ton (97,000lb) of fire retardant in two tanks. Production: Over 900 IL-76s of all models built, most for the Russian military, but over 300 are in service with Aeroflot and other civilian operators. -
Aerospace Short Courses Catalog
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Economic Growth in the Governance of the Cold War Divide Mikoyan's
Economic Growth in the Governance of the Cold War Divide Mikoyan’s Encounter with Japan, Summer 1961 ✣ Oscar Sanchez-Sibony Noguchi Yoshio had written to him after all. Anastas Mikoyan had been re- tired for ten years. The year was 1975, and to mark Mikoyan’s 80th birthday, Noguchi had sent the retired Soviet official a souvenir.1 He was not the only one to remember Mikoyan in his retirement. Writing in 1972 on the occasion of his oil company’s 60th anniversary, the redoubtable Idemitsu Sazo sent to Mikoyan—in the somewhat bewildered words of then-Soviet ambassador to Japan Oleg Troyanovskii—a “piece of cloth.”2 Matsubara Yosamatsu, presi- dent of the industrial and shipbuilding conglomerate Hitachi Zosen, chose a more personal note. In his letter, he recounted to Mikoyan the first time they met in August 1961 during Mikoyan’s tour of the corporation’s shipyard in Sakurajima, as well as their encounter a year later when Matsubara headed a delegation of Japanese businessmen in Moscow. “Ten years have passed since then,” he wistfully wrote to the Old Bolshevik. “And in that time, economic relations between our two countries strengthen with every year as trade rela- tions develop between our countries even more greatly.”3 Meanwhile, Prime Minister Sato Eisaku also recalled that fateful year, writing in his personal letter to Mikoyan: “I am sincerely glad that relations between Japan and the Soviet Union, especially after your visit to Japan in 1961, continue to develop 1. Mikoyan’s thank-you note dates from 1 December 1975 and is stored in Russian State Archive of Sociopolitical History (RGASPI), Fond (F.) 84, Opis’ (Op.) 3, Delo (D.) 108, List (L.) 43.