7‚000 lbs Useful Load* 2‚450 kg 5‚500 lbs *NOTE: Basic Empty Weight & Useful Load are approximate; actual weights will be aircraft specific. Exhibit A Page 3 of 17 Dimensions Wing Span (floats up) 15.5 m 50.9ft Span (floats down) 14.6 m 47.9 ft Area (not including floats) 35.8 m3 385 sq ft Length (overall) 12.1 m 39.6 ft Height (wheels down‚ aircraft level) 4.6 m 15.0 ft Fuselage Cabin Height (maximum) 170 cm 67 in Width (maximum) 137 cm 54 in Length (maximum) 33 cm
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Analysis and Design Project “GOWN RENTAL MANAGEMENT AND INFORMATION SYSTEM” Presented to the Faculty of Gordon College Olongapo City In Partial FulfilmentoftheRequirements for the Degree ASSOCIATE IN COMPUTER TECHNOLOGY By: JUNNIEFER C. SABILE MARK JOSEPH L. PEREZ March 14‚ 2013 Republic of the Philippines Gordon College Olongapo City College of Computer Studies APPROVAL SHEET A System Analysis and Design Project entitled“GOWN RENTAL MANAGEMENT AND INFORMATION SYSTEM”prepared
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Aircraft Incidents Attributable to Human Factors On June 10th 1990‚ a British Airways BAC 1-11 suffered a catastrophic decompression in mid flight‚ resulting in Captain Tim Lancaster being partially sucked out of the aircraft. Only the quick reactions of flight attendant‚ Nigel Ogden‚ who managed to secure the captains legs and feet‚ meanwhile the co-pilot Alastair Atchison fought to descend the aircraft from 17‚500ft to a safe altitude and eventually touch down safely on runway 02 at Southampton
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OBJECTIVE To ensure and guarantee the safety of flight‚ the materials in an aircraft used is an important element. This includes small parts like nuts‚ bolts and screw. The materials are chosen because they must have a certain features like light and extremely strong This project looks into the parts of an airplane mainly the wing. The wing of an aircraft comprises of skin‚ spar‚ ribs and stringer. We will further discuss into the properties‚ test standards and factors of the materials being chose
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Aircraft Solutions: Security Assessments And Recommendations Ruth Garcia Session: March 2012 Security in Computing Professor: Randy Strauber BACKGROUND Aircraft Solutions (AS) located in beautiful southern California has become a recognized leader in the electronics‚ commercial‚ defense and aerospace industries. This is due their design and fabrication of component products and services available to their customers in the various industries. What set Aircraft
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Cebu Pacific Aircraft Accidents in the Philippines Executive Summary The purpose of this study is to provide the information and solution programs in providing quality service. CAAP (Civil Aviation Authority of the Philippines) is one that provides airlines the legal authority to participate in improving work-related tasks and services in aviation industry. One of the most pressing issues facing most airline industry locally today is the need to improve their quality service in terms of communication
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Case Study of “Beacon Car Rental” Henry was the senior vice president of operations. Tony was the chief marketing officer‚ and they were talking about Beacon’s latest acquisition—VillageCar. But they seemed to have different opinions on it. The most important thing was—could an auto rental company fully integrate its car-sharing start-up without losing customers? A week later Henry went to Tony’s office and set a paper down on his desk; it was an article from the Journal of Consumer Research which
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Aircraft continuing airworthiness record system At the completion of any maintenance‚ the certificate of release to service required by point M.A.801 or point 145.A.50 shall be entered in the aircraft continuing airworthiness records. Each entry shall be made as soon as practicable but in no case more than 30 days after the day of the maintenance action. The aircraft continuing airworthiness records shall consist of: • an aircraft logbook‚ engine logbook(s) or engine module log cards
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@AIRBUS A320 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING AC The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied‚ nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for
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SFTY 435 Aircraft Crash Survival Analysis and Design Final Examination Return completed exam to instructor by 10:00 PM on 11 December 2012. Send to email: Name: Provide an essay type answer for the following questions. 1. Describe the effect plowing can have on crash forces when the impact surface is soft soil. Earth gouging and scooping of soil occur when the structure makes initial contact with the ground which minimize the acceleration and force levels to which the structure
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