Decision 2009/016/R 01/12/2009 Annex I
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79952 Federal Register / Vol
79952 Federal Register / Vol. 75, No. 244 / Tuesday, December 21, 2010 / Rules and Regulations Unsafe Condition DEPARTMENT OF TRANSPORTATION 1601 Lind Avenue, SW., Renton, (d) This AD was prompted by an accident Washington 98057–3356; telephone and the subsequent discovery of cracks in the Federal Aviation Administration (425) 227–1137; fax (425) 227–1149. main rotor blade (blade) spars. We are issuing SUPPLEMENTARY INFORMATION: 14 CFR Part 39 this AD to prevent blade failure and Discussion subsequent loss of control of the helicopter. [Docket No. FAA–2009–0864; Directorate We issued a supplemental notice of Compliance Identifier 2008–NM–202–AD; Amendment 39–16544; AD 2010–26–05] proposed rulemaking (NPRM) to amend (e) Before further flight, unless already 14 CFR part 39 to include an AD that done: RIN 2120–AA64 would apply to the specified products. (1) Revise the Limitations section of the That supplemental NPRM was Airworthiness Directives; DASSAULT Instructions for Continued Airworthiness by published in the Federal Register on AVIATION Model Falcon 10 Airplanes; establishing a life limit of 8,000 hours time- July 27, 2010 (75 FR 43878). That Model FAN JET FALCON, FAN JET in-service (TIS) for each blade set Remove supplemental NPRM proposed to FALCON SERIES C, D, E, F, and G each blade set with 8,000 or more hours TIS. correct an unsafe condition for the Airplanes; Model MYSTERE-FALCON (2) Replace each specified serial-numbered specified products. The MCAI states: 200 Airplanes; Model MYSTERE- blade set with an airworthy blade set in During maintenance on one aircraft, it was accordance with the following table: FALCON 20–C5, 20–D5, 20–E5, and 20– F5 Airplanes; Model FALCON 2000 and discovered that the overpressure capsules were broken on both pressurization valves. -
Decision 2005/07/R
DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to Regulation (EC) No 1592/2002 of 15 July 2002 on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency1 (hereinafter referred to as the “Agency”), and in particular Articles 13 and 14 thereof. Having regard to the Commission Regulation (EC) No 2042/2003 of 28 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.2 Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. -
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. -
DASSAULT AVIATION Model Falcon 10 Airplanes
43878 Federal Register / Vol. 75, No. 143 / Tuesday, July 27, 2010 / Proposed Rules Applicability New Requirements of This AD: Actions Bulletin SBF100–27–092, dated April 27, (c) This AD applies to Fokker Services B.V. (h) Within 30 months after the effective 2009; and Goodrich Service Bulletin 23100– Model F.28 Mark 0100 airplanes, certificated date of this AD, do the actions specified in 27–29, dated November 14, 2008; for related in any category, all serial numbers. paragraphs (h)(1) and (h)(2) of this AD information. concurrently. Accomplishing the actions of Issued in Renton, Washington, on July 21, Subject both paragraphs (h)(1) and (h)(2) of this AD 2010. (d) Air Transport Association (ATA) of terminates the actions required by paragraph Jeffrey E. Duven, America Code 27: Flight Controls. (g) of this AD. (1) Remove the tie-wrap, P/N MS3367–2– Acting Manager, Transport Airplane Reason 9, from the lower bolts of the horizontal Directorate, Aircraft Certification Service. (e) The mandatory continuing stabilizer control unit, in accordance with the [FR Doc. 2010–18399 Filed 7–26–10; 8:45 am] airworthiness information (MCAI) states: Accomplishment Instructions of Fokker BILLING CODE 4910–13–P Two reports have been received where, Service Bulletin SBF100–27–092, dated April during inspection of the vertical stabilizer of 27, 2009. F28 Mark 0100 aeroplanes, one of the bolts (2) Remove the lower bolts, P/N 23233–1, DEPARTMENT OF TRANSPORTATION that connect the horizontal stabilizer control of the horizontal stabilizer control unit and unit actuator with the dog-links was found install bolts, P/N 23233–3, in accordance Federal Aviation Administration broken (one on the nut side & one on the with the Accomplishment Instructions of Goodrich Service Bulletin 23100–27–29, head side). -
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. -
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. -
Outlook V37 N2 March 2021 Draft Portrait
Outlook / AHSA News Vol. 37 No. 3 June 2021 Outlook A.H.S.A. AHSA News Vol. 37 No. 3 June 2021 This edi�on of Outlook comes to readers in the middle of winter - and this photograph of Anse�-ANA’s Douglas DC-6B VH-INU (c/n 44694-558) from the Peter Kelly collec�on was taken on an overcast and wet day, typical of what might be expected in a Melbourne winter. But in fact the photograph was taken at Essendon on December 15th 1966. Newsletter of the Website: Aviation Historical www.ahsa.org.au Society of Australia, Inc. A0033653P Facebook Group: ARBN 092-671-773 www.facebook.com/groups/AHSAustPage 1 Outlook / AHSA News Vol. 37 No. 3 June 2021 Avia�on Historical Society of Australia Inc. What’s Inside? President’s Comment 2 Our 2020/21 Commi�ee: AHSA news 3 President: Dave Prossor Civil Avia�on Centenary Update 6 [email protected] Civil Avia�on Snippets 6 RAAF Centenary Update 10 Vice-President: Derek Buckmaster [email protected] Military Avia�on Snippets 12 Australian Industry News Snippets 15 Secretary: Mark Pilkington Coming Avia�on Events 16 [email protected] Museum News 16 Treasurer: Robert Van Woerkom New books on Australian Avia�on History 18 [email protected] Research Corner 20 Membership David Knight Secretary: [email protected] President’s Comment Commi�ee Members: For a start I would like to think that AHSA readers enjoyed the GPCAPT David Fredericks last issue of the newsle�er. A different style and content being Dion Makowski driven by the current commi�ee. -
Computer and Information Science, ISSN 1913-8989, Vol. 1, No. 1
Vol. 1, No. 1 Computer and Information Science Mapping of Power Transmission Lines on Malaysian Highways Using UPM-APSB’s AISA Airborne Hyperspectral Imaging System Hj. Kamaruzaman Jusoff Forest Geospatial Information & Survey Lab, Lebuh Silikon Faculty of Forestry, Universiti Putra Malaysia Serdang 43400 Selangor, Malaysia Tel: +60-3-8946 7176 E-mail: [email protected] Norsuzila Ya’acob Faculty of Electrical Engineering, Universiti Teknologi MARA UiTM 40450 Shah Alam, Malaysia Tel: +60-3-5544 2000 E-mail: [email protected] Abstract Power transmission lines routes mapping is an important technique for locating power transmission line routes and towers on mountain/hilltops to assist viewing of their impacts on the environment, operations and allocation of public utilities. A study was therefore conducted to map the power transmission lines within Bukit Lanjan PLUS highway. The main objective of this study is to assess the capability of airborne hyperspectral sensing for mapping of power transmission. By using ENVI software, the airborne hyperspectral imaging data was enhanced using convolution filtering technique using band 3 which produced a gray scale image which appeared clearer and sharper. The spectral reflectance curves were acquired for each power line which showed the same spectrum characteristics in curve or the reflectance energy. This is because of the same power lines composition material for all power lines. Ground verification was done by comparing the UPM-APSB’s AISA Global Positioning System (GPS) coordinates readings with ground GPS coordinates readings of the power transmission lines footings. The ground verification result from the two matching power transmission line footings showed that the accuracy of power lines identification was acceptable. -
Falco Builders Letter
Falco Builders Letter A Visit with Frati If anybody ever suggests you go visit Frati “in Milan,” as Alfred Scott did when he heard I was going to be in Italy writing about the Piaggio Avanti turboprop, here’s my suggestion: get Alfred to pay the cabfare. If you can’t do that, buy a car. A small Fiat will do, and it’ll prob- ably be cheaper than a cab. I leapt off the train from Genoa at Milan’s central station and plunged straight into a waiting taxi. “Via Trieste Vente-Quat- tro,” I said in my best non-Italian, and about $15 later, that’s exactly where he took me—24 Via Trieste. Quiet urban residential street... relatively upscale... odd place for an airplane factory.... Actually, there was no number 24. We found a phone booth, and my cabbie Jim and Gail Martin's Falco is the 17th Sequoia Falco to fly. was nice enough to tackle the Italian telephone system on my behalf. He First Flight: Around the Falco called Frati’s number, and I knew I was in trouble when I saw him perform the Jim and Gail Martin Patch classic application of heel of hand smartly Jim and Gail Martin’s Falco flew for Luciano Nustrini came to Oshkosh as to forehead, as though trying to jar loose a the first time on August 13th in But- planned, but not via Europe as he had subdural hematoma: the Via Trieste that ler, Pennsylvania, making it the 17th intended. There was a change in plans, I wanted, it turned out—a street that ap- Sequoia Falco to fly. -
Simulation Programs Using Concurrent Computer Systems
SIMULATION PROGRAMS USING CONCURRENT COMPUTER SYSTEMS US AIR FORCE PROGRAMS US NAVY PROGRAMS OTHER GOVERNMENT PROGRAMS JAPAN FIGHTER AIRCRAFT Coast Guard HH-60 Jayhawk Active Phased Array Radar FIGHTER AIRCRAFT F-117A Nighthawk AH-1S Cobra F-14B/A Tomcat NASA Space Shuttle SMS F-15 Eagle C-1 Trader F/A-18 Hornet NASA X-29 US101 Helicopter C-130 Hercules BOMBER AIRCRAFT ATTACK AIRCRAFT F-15J WST INTERNATIONAL MILITARY PROGRAMS B-1B Lancer ERS A-6E Intruder FS-X/F-2 Avionics Development B-2 Spirit ATD Crew Trainer AUSTRALIA JSDF Anti-aircraft Artillery ELECTRONIC WARFARE B-52 Stratofortress WST Collins-class Submarine CCS OH-1 Ninja EA-6B Prowler F-111 Aardvark Avionics Development P-3C Orion NEWTS Patriot Missile Defense ATTACK AIRCRAFT CZECKOSLOVAKIA P-3C Orion SH-60K Sea Hawk A-10 Thunderbolt L-159 ALCA S-3 Viking T-4 Trainer AC-130U Gunship FRANCE Agusta 129 Helicopter T-5 Trainer RESEARCH T-90 Tank MISSILES LEAP Program Airbus A400M CALCM Cruise E-2C Hawkeye TC-90 Trainer U-125A Peace Krypton HELICOPTERS Eurocopter US-1A Kai CARGO AIRCRAFT CH-46 Sea Knight Exocet Missile KOREA C-12F Huron CH-53 Sea Stallion Mirage 2000 Fighter F-16K Avionics Development C-130 Hercules MH-60R LAMPS Mistral Missile Hawk 60 Trainer C-17 Globemaster III SURFACE/SUBSURFACE Rafale Fighter KC-135 Stratotanker NETHERLANDS AGSS class sub GERMANY F-16 Eagle AGG2 Gepard Tank Tomahawk ACM Missile SAUDI ARABIA ELECTRONIC WARFARE C-160 Transall E-2C AWACS F-5 Tiger GENERAL TRAINERS CH-53G Helicopter EC-135 Looking Glass SINGAPORE 20F16 Tactical Command E-3A AWACS -
AIN 2014 Product Support Survey
required tooling and material to to shape connectivity solutions. reliability challenge. Honeywell 2014 Engine rescue an AOG,” the company “When these pilot advisors on has had success in these types Survey Rules told AIN. our Global Customer Committee of location with hydrodynamic Manufacturer Ratings (GCC) told us they needed bet- carbon seal designs and has & Methodology Overall Overall Overall Williams International ter access to Honeywell’s techni- recently introduced them to Average Average Average As with AIN Publications’ previ- “We have been focusing on cal resources, we responded. The the TFE731-20/40/50/60 acces- 2014 2013 2013-2014 ous annual Product Support Surveys, ensuring owners have no worries new Honeywell Pilot Gateway sory gearboxes.” Turbofan the objective this year was to obtain when operating our engines.” To (http://pilots.honeywell.com) Honeywell has drawn on from the users of business jets, accomplish this, Williams intro- is a one-stop shop for our techni- human-factor design principles Rolls-Royce 8.0 7.8 0.2 turboprop airplanes and turbine- duced “significant enhancements cal publications, pilot guides and to reduce the number of tools Williams 8.0 8.1 -0.1 powered helicopters statistically to our Total Assurance Program familiarization videos, all orga- required to perform mainte- Honeywell 7.9 7.8 0.1 valid information about the product (TAP). We created TAP Blue, nized by aircraft make, model nance tasks on the HTF7000. CFE 7.6 7.3 0.3 support provided by engine manu- which provides an unlimited- and system type.” The tool also Historically, more than 30 dif- GE 7.6 7.9 -0.3 facturers over the last year and to duration warranty with coverage allows pilots to provide feed- ferent hand tools were required P&WC 7.6 7.7 -0.1 report this information to our read- beyond that offered anywhere back, report technical problems to perform maintenance tasks Turboprops ers.