Appendix G Facility Requirements Supplemental Data
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Gulfstream GV / GV-SP (G500/G550) / GIV-X (G450/G350)
Gulfstream EASA-OSD-FC-GV Series-GAC-001, Basic Issue Document Reference # Operational Suitability Data (OSD) Flight Crew Gulfstream GV / GV-SP (G500/G550) / GIV-X (G450/G350) 21 May 2015 Operational Suitability Data – Flight Crew G-V Gulfstream GV / GV-SP (G500/G550) / GIV-X (G450/G350) Operational Suitability Data (OSD) – Flight Crew This OSD document is provided on behalf of Gulfstream Aerospace. It is made available to users in accordance with paragraph 21.A.62 of Part-21. Users should verify the currency of this document. Revision Record Rev. No. Content Date JOEB Report JOEB report Gulfstream GV / GV-SP (G500/G550) 15 Jun 2006 Rev. 7 / GIV-X (G450/G350) OSD FC Replaces and incorporates the JOEB report for the Gulfstream GV / GV-SP (G500/G550) / GIV-X 21 May 2015 Original (G450/G350) OSD FC G-V – Original 21 May 2015 Page 2 of 37 Operational Suitability Data – Flight Crew G-V Contents Revision Record ........................................................................................................................... 2 Contents ...................................................................................................................................... 3 Acronyms ..................................................................................................................................... 5 Preamble ..................................................................................................................................... 7 1. Introduction ............................................................................................................... -
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. -
2020 Annual Noise Contour Report
Minneapolis St. Paul International Airport (MSP) 2020 Annual Noise Contour Report Comparison of the 2020 Actual and the 2007 Forecast Noise Contours February 2021 MAC Community Relations Office and HNTB Corporation MSP 2020 Annual Noise Contour Report Metropolitan Airports Commission Table of Contents ES EXECUTIVE SUMMARY .................................................................................................. 1 ES.1 BACKGROUND ...................................................................................................................... 1 ES.2 AIRPORT NOISE LITIGATION AND CONSENT DECREE .............................................................. 1 ES.3 MSP 2020 IMPROVEMENTS EA/EAW ..................................................................................... 2 ES.4 THE AMENDED CONSENT DECREE ......................................................................................... 2 ES.5 2020 NOISE CONTOURS ......................................................................................................... 3 ES.6 AMENDED CONSENT DECREE PROGRAM ELIGIBILITY ............................................................. 3 ES.7 AMENDED CONSENT DECREE PROGRAM MITIGATION STATUS ............................................. 3 1. INTRODUCTION AND BACKGROUND ................................................................................. 8 1.1 CORRECTIVE LAND USE EFFORTS TO ADDRESS AIRCRAFT NOISE ............................................ 8 1.2 2007 FORECAST CONTOUR ................................................................................................. -
Cessna 172 in Flight 1964 Cessna 172E 1965 Cessna F172G
Cessna 172 in flight 1964 Cessna 172E 1965 Cessna F172G 1971 Cessna 172 The 1957 model Cessna 172 Skyhawk had no rear window and featured a "square" fin design Airplane Cessna 172 single engine aircraft, flies overhead after becoming airborne. Catalina Island airport, California (KAVX) 1964 Cessna 172E (G- ASSS) at Kemble airfield, Gloucestershire, England. The Cessna 172 Skyhawk is a four-seat, single-engine, high-wing airplane. Probably the most popular flight training aircraft in the world, the first production models were delivered in 1957, and it is still in production in 2005; more than 35,000 have been built. The Skyhawk's main competitors have been the popular Piper Cherokee, the rarer Beechcraft Musketeer (no longer in production), and, more recently, the Cirrus SR22. The Skyhawk is ubiquitous throughout the Americas, Europe and parts of Asia; it is the aircraft most people visualize when they hear the words "small plane." More people probably know the name Piper Cub, but the Skyhawk's shape is far more familiar. The 172 was a direct descendant of the Cessna 170, which used conventional (taildragger) landing gear instead of tricycle gear. Early 172s looked almost identical to the 170, with the same straight aft fuselage and tall gear legs, but later versions incorporated revised landing gear, a lowered rear deck, and an aft window. Cessna advertised this added rear visibility as "Omnivision". The final structural development, in the mid-1960s, was the sweptback tail still used today. The airframe has remained almost unchanged since then, with updates to avionics and engines including (most recently) the Garmin G1000 glass cockpit. -
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. -
FCM Aircraft Operations That Generated Complaints July 2015
FCM Aircraft Operations that Generated Complaints July 2015 Complaints FCM FCM FCM Helicopter FCM Regarding Complaints Complaints Aircraft Types Nighttime FCM Submitted Submitted via Complaints Complaints Complaints Run-ups via Internet Phone Unknown 184 6 7 2 184 0 Beechcraft King Air 200 46 0 30 0 46 0 Raytheon Beechjet 400 15 0 9 0 15 0 Cessna Citation Jet 560XL 15 1 4 0 15 0 Beechcraft King Air 90 13 1 6 1 13 0 Cirrus SR-22 9 0 2 0 9 0 Cessna Skyhawk 172 8 0 0 0 8 0 Cessna Citation Jet 525 7 0 3 0 7 0 Beechcraft King Air 350 6 0 2 0 6 0 Learjet 45 6 0 1 0 6 0 Cessna 310 Twin 5 0 0 0 5 0 Cessna Skywagon 185 5 0 0 0 4 1 Piper Malibu Meridian 4 0 0 0 4 0 Hawker 125 Jet 4 0 1 0 4 0 Piper Malibu 4 0 1 0 4 0 Pilatus PC-12 4 0 1 0 4 0 Cessna Citation Jet 560 4 0 1 0 4 0 Cessna 340 Twin 3 0 0 0 3 0 Beechcraft King Air 300 3 0 2 0 3 0 Cessna Corsair 425 2 0 0 0 2 0 Cessna 206 2 0 0 0 2 0 Experimental 2 0 1 0 2 0 Cessna Citation Jet 750 2 0 2 0 2 0 Socata TBM 700 2 0 0 0 2 0 Cessna Golden Eagle 421 2 0 0 0 2 0 Cessna Centurion 210 2 0 0 0 2 0 Cessna Skylane 182 2 0 0 0 2 0 Piper Cherokee 2 0 0 0 2 0 T-6 TEXAN 2 0 0 0 2 0 Rockwell Turbo Commander 900 2 0 0 0 2 0 Cessna Citation Mustang 2 0 0 0 2 0 Boeing 737-900 1 0 1 0 1 0 Report Generated: 09/30/2015 15:36 Page 1 Complaints FCM FCM FCM Helicopter FCM Regarding Complaints Complaints Aircraft Types Nighttime FCM Submitted Submitted via Complaints Complaints Complaints Run-ups via Internet Phone Piper Navajo Twin 1 0 0 0 1 0 Mitsubishi MU-2 1 0 0 0 1 0 Beechcraft Debonair/Bonanza 1 0 1 0 1 0 -
The Years of Change
The Years of Change In early January of 1993 all the B-2 structural tests were successfully completed. The static load tests were taken to failure to 161% of maximum stress, and the durability test completed more than 2 lifetimes, which represented 20,000 design flight hours. January 1993 confidence was high for the $4-billion PAMPA Program as the company prepared to complete its first flight evaluation aircraft. However, the realities of the “post-cold war” era forced management to gear up for a tough year as the battle of the defense budget continued in Washington. The ailing commercial aviation industry presented additional challenges for the company. Boeing cut production on all their programs, and 1993 looked very gloomy. The company announced plans for down-sizing up to 1,500 people by the end of the year. Vought president Gordon Williams streamlined the management team to help the company ride out the business downturn, and still continue to meet its customer requirements. He stated that “business will be smaller but stronger.” In March 1993 Vought shipped its last engine nacelle for the Canadair business jet while continuing production on the regional jet nacelles. The 500th horizontal stabilizer for the Boeing 767 was shipped during March, and 141 employees elected to retire. In the meantime, Loral Corporation formed a new missiles group by combining Loral Vought Systems and Loral Aeronutronic during the month. At the end of April, 104 employees elected to retire. McDonnell Douglas certified Vought’s business processes in early May, which was another milestone on the way to becoming a preferred supplier for McDonnell Douglas. -
Aviation Activity Forecasts BOWERS FIELD AIRPORT AIRPORT MASTER PLAN
Chapter 3 – Aviation Activity Forecasts BOWERS FIELD AIRPORT AIRPORT MASTER PLAN Chapter 3 – Aviation Activity Forecasts The overall goal of aviation activity forecasting is to prepare forecasts that accurately reflect current conditions, relevant historic trends, and provide reasonable projections of future activity, which can be translated into specific airport facility needs anticipated during the next twenty years and beyond. Introduction This chapter provides updated forecasts of aviation activity for Kittitas County Airport – Bowers Field (ELN) for the twenty-year master plan horizon (2015-2035). The most recent FAA-approved aviation activity forecasts for Bowers Field were prepared in 2011 for the Airfield Needs Assessment project. Those forecasts evaluated changes in local conditions and activity that occurred since the previous master plan forecasts were prepared in 2000, and re-established base line conditions. The Needs Assessment forecasts provide the “accepted” airport-specific projections that are most relevant for comparison with the new master plan forecasts prepared for this chapter. The forecasts presented in this chapter are consistent with Bowers Field’s current and historic role as a community/regional general aviation airport. Bowers Field is the only airport in Kittitas County capable of accommodating a full range of general aviation activity, including business class turboprops and business jets. This level of capability expands the airport’s role to serve the entire county and the local Ellensburg community. The intent is to provide an updated set of aviation demand projections for Bowers Field that will permit airport management to make the decisions necessary to maintain a viable, efficient, and cost-effective facility that meets the area’s air transportation needs. -
EVB Runway 7-25 Alternatives DRAFT 7 22 2019
NEW SNEW SMSMMMYRNAYRNA BEACH MUNICIPAL AIRPORT Runway 7/25 Runway Safety Area Alternatives City of New Smyrna Beach DRAFT Prepared By: July 2019 New Smyrna Beach Municipal Airport Runway 7/25 Alternatives Table of Contents 1. Introduction ......................................................................................................................... 1 2. Florida Department of Transportation Airport Inspection Report .......................................... 2 3. C&S Companies Report ...................................................................................................... 3 4. 2018 Airport Master Plan Update ........................................................................................ 4 5. Airport Layout Plan ............................................................................................................. 6 6. FAA Versus FDOT Safety Area Requirements .................................................................... 6 7. Departure Surfaces ............................................................................................................. 7 8. Published Departure and Landing Distances ...................................................................... 7 9. Typical Aeronautical Insurance Policies .............................................................................. 8 10. Typical Airport Leases at the Airport ................................................................................ 9 11. Wetlands at the Ends of the Runway .............................................................................. -
Name of Plan Wing Span Details Source Area Price Ama Ff Cl Ot Scale Gas Rubber Electric Other Glider 3 View Engine Red. Ot C
WING NAME OF PLAN DETAILS SOURCE AREA PRICE AMA POND RC FF CL OT SCALE GAS RUBBER ELECTRIC OTHER GLIDER 3 VIEW ENGINE RED. OT SPAN COMET MODEL AIRPLANE CO. 7D4 X X C 1 PURSUIT 15 3 $ 4.00 33199 C 1 PURSUIT FLYING ACES CLUB FINEMAN 80B5 X X 15 3 $ 4.00 30519 (NEW) MODEL AIRPLANE NEWS 1/69, 90C3 X X C 47 PROFILE 35 SCHAAF 5 $ 7.00 31244 X WALT MOONEY 14F7 X X X C A B MINICAB 20 3 $ 4.00 21346 C L W CURLEW BRITISH MAGAZINE 6D6 X X X 15 2 $ 3.00 20416 T 1 POPULAR AVIATION 9/28, POND 40E5 X X C MODEL 24 4 $ 5.00 24542 C P SPECIAL $ - 34697 RD121 X MODEL AIRPLANE NEWS 4/42, 8A6 X X C RAIDER 68 LATORRE 21 $ 23.00 20519 X AEROMODELLO 42D3 X C S A 1 38 9 $ 12.00 32805 C.A.B. GY 20 BY WALT MOONEY X X X 20 4 $ 6.00 36265 MINICAB C.W. SKY FLYER PLAN 15G3 X X HELLDIVER 02 15 4 $ 5.00 35529 C2 (INC C130 H PLAMER PLAN X X X 133 90 $ 122.00 50587 X HERCULES QUIET & ELECTRIC FLIGHT INT., X CABBIE 38 5/06 6 $ 9.00 50413 CABIN AEROMODELLER PLAN 8/41, 35F5 X X 20 4 $ 5.00 23940 BIPLANE DOWNES CABIN THE OAKLAND TRIBUNE 68B3 X X 20 3 $ 4.00 29091 COMMERCIAL NEWSPAPER 1931 Indoor Miller’s record-holding Dec. 1979 X Cabin Fever: 40 Manhattan Cabin. -
Cessna 340 Page 1 of 14
Cessna 340 Page 1 of 14 Volume 34 • Number 2 • February 2004 Cessna 340 A fast, pressurized cabin-class twin that’s an excellent step-up from a Avionics Report high performance single. Used Aircraft Guide Maintenance Matters Accessories Although airplanes are often sold as Misc. business and transportation tools, the reality of ownership falls short of the ideal. They either lack the range, the carrying capacity or the ability to deal with real-world weather, thus an airline or a charter outfit gets the call. Still, there are plenty of pilot/businessmen who couldn’t function without an airplane. These owners typically start with single- The Cessna 340 is a standout thanks to engine airplanes and quickly outgrow payload/fuel flexibility and near 200-knot cruise them for the reasons stated above. A speeds. Pressurization is an added plus. serious business airplane needs a decent cabin, credible speed and the ability to hack it when there’s ice or thunder in the forecast. Pressurization is nice since the clients don’t want to spend several hours with a plastic hose stuck up their noses. Enter the Cessna 340. Owners looking to step-up from a high-performance single will inevitably make a pass or two through the 340 classified section. And well they should. Although not without its shortcomings—most notably certain loading limitations and an overly complex fuel system—the 340 is nevertheless an impressive, flexible and capable airplane that meets the business mission well and can do double duty as a family airplane. Model History The 340 owes its existence to the boom days of general aviation during the late 1960s and early 1970s. -
Aerodynamic Analysis and Design of a Twin Engine Commuter Aircraft
28TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES AERODYNAMIC ANALYSIS AND DESIGN OF A TWIN ENGINE COMMUTER AIRCRAFT Fabrizio Nicolosi*, Pierluigi Della Vecchia*, Salvatore Corcione* *Department of Aerospace Engineering - University of Naples Federico II [email protected]; [email protected], [email protected] Keywords: Aircraft Design, Commuter Aircraft, Aerodynamic Analysis Abstract 1. Introduction The present paper deals with the preliminary design of a general aviation Commuter 11 seat Many in the industry had anticipated 2011 to be aircraft. The Commuter aircraft market is today the year when the General Aviation characterized by very few new models and the manufacturing industry would begin to recover. majority of aircraft in operation belonging to However, the demand for business airplanes and this category are older than 35 years. Tecnam services, especially in the established markets of Aircraft Industries and the Department of Europe and North America, remained soft and Aerospace Engineering (DIAS) of the University customer confidence in making purchase of Naples "Federico II" are deeply involved in decision in these regions remained weak. This the design of a new commuter aircraft that inactivity, nonetheless, was offset in part by should be introduced in this market with very demand from the emerging markets of China good opportunities of success. This paper aims and Russia. While a full resurgence did not take to provide some guidelines on the conception of place in 2011, the year finished with signs of a new twin-engine commuter aircraft with recovery and reason of optimism. GAMA eleven passengers. Aircraft configuration and (General Aviation Manufacturer Association) cabin layouts choices are shown, also compared 2011 Statistical Databook & Industry Outlook to the main competitors.