DOCSLIB.ORG

Aerospace and Propulsion A

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Aerospace and Propulsion A Commerce Control List Supplement No. 1 to Part 774 Category 9—page 1 CATEGORY 9 - AEROSPACE AND turbine engines which meet all of the following: PROPULSION a. Certified by the civil aviation authority in a country listed in Supplement No. 1 to Part 743; A. “END ITEMS,” “EQUIPMENT,” and “ACCESSORIES,” “ATTACHMENTS,” “PARTS,” “COMPONENTS,” AND b. Intended to power non-military manned “SYSTEMS” “aircraft” for which any of the following has been issued by a Wassenaar Arrangement N.B.: For propulsion systems designed or Participating State listed in Supplement No. 1 to rated against neutron or transient ionizing Part 743 for the “aircraft” with this specific radiation, see the U.S. Munitions List, 22 CFR engine type: part 121. b.1. A civil type certificate; or 9A001 Aero gas turbine engines having any of b.2. An equivalent document recognized the following (see List of Items Controlled). by the International Civil Aviation Organization (ICAO). License Requirements Note 2: 9A001.a does not apply to aero Reason for Control: NS, MT, AT gas turbine engines for Auxiliary Power Units (APUs) approved by the civil aviation authority Country Chart in a Wassenaar Arrangement Participating State Control(s) (See Supp. No. (see Supplement No. 1 to part 743 of the EAR). 1 to part 738) NS applies to entire entry NS Column 1 b. Designed to power an “aircraft” designed to MT applies to only to those MT Column 1 cruise at Mach 1 or higher, for more than 30 engines that meet the minutes. characteristics listed in 9A101 AT applies to entire entry AT Column 1 9A002 ‘Marine gas turbine engines’ designed List Based License Exceptions (See Part 740 for to use liquid fuel and having all of the a description of all license exceptions) following (see List of Items Controlled), and “specially designed” assemblies and LVS: N/A “components” therefor. GBS: N/A License Requirements List of Items Controlled Reason for Control: NS, AT Related Controls: See also 9A101 and 9A991 Related Definitions: N/A Country Chart Items: Control(s) (See Supp. No. 1 to part 738) a. Incorporating any of the “technologies” NS applies to entire entry NS Column 2 controlled by 9E003.a, 9E003.h, or 9E003.i; or AT applies to entire entry AT Column 1 Note 1: 9A001.a does not control aero gas Export Administration Regulations Bureau of Industry and Security March 29, 2021 Commerce Control List Supplement No. 1 to Part 774 Category 9—page 2 List Based License Exceptions (See Part 740 for (See Supp. No. 1 a description of all license exceptions) to part 738) NS applies to entire entry NS Column 2 LVS: $5000 AT applies to entire entry AT Column 1 GBS: N/A List Based License Exceptions (See Part 740 for List of Items Controlled: a description of all license exceptions) Related Controls: N/A LVS: $5000 Related Definition: N/A GBS: N/A Items: List of Items Controlled a. Maximum continuous power when operating in “steady state mode” at standard Related Controls: N/A reference conditions specified by ISO 3977- Related Definition: N/A 2:1997 (or national equivalent) of 24,245 kW or Items: more; and a. Controlled by 9A001; or b. ‘Corrected specific fuel consumption’ not exceeding 0.219 kg/kWh at 35% of the b. Whose design or production origins are either maximum continuous power when using liquid not from a Wassenaar Participating State (see fuel. Supplement No. 1 to part 743 of the EAR) or unknown to the manufacturer. Note: The term ‘marine gas turbine engines’ includes those industrial, or aero-derivative, gas turbine engines adapted for a ship’s electric 9A004 Space launch vehicles and “spacecraft,” power generation or propulsion. “spacecraft buses”, “spacecraft payloads”, “spacecraft” on-board systems or equipment, Technical Note: For the purposes of 9A002, terrestrial equipment, and air-launch ‘corrected specific fuel consumption’ is the platforms, as follows (see List of Items specific fuel consumption of the engine corrected Controlled). to a marine distillate liquid fuel having a net specific energy (i.e., net heating value) of 42 License Requirements MJ/kg (ISO 3977-2:1997). Reason for Control: NS and AT 9A003 “Specially designed” assemblies or Country Chart “components,” incorporating any of the Control(s) (See Supp. No. 1 “technologies” controlled by 9E003.a, 9E003.h to part 738) or 9E003.i, for any of the following aero gas NS applies to 9A004.g, NS Column 1 turbine engines (see List of Items Controlled). .u, .v, .w and .x AT applies to 9A004.g, AT Column 1 License Requirements .u, .v, .w, .x and .y Reason for Control: NS, AT License Requirement Note: 9A004.b through .f, and .h are controlled under ECCN Control(s) Country Chart 9A515. Export Administration Regulations Bureau of Industry and Security March 29, 2021 Commerce Control List Supplement No. 1 to Part 774 Category 9—page 3 Note: For the purpose of 9A004.e.2, List Based License Exceptions (See Part 740 for ‘payload data handling’ includes payload data a description of all license exceptions) management, storage, and processing. LVS: N/A e.3. ‘Attitude and orbit control’; GBS: N/A Note: For the purpose of 9A004.e.3, List of Items Controlled ‘attitude and orbit control’ includes sensing and actuation to determine and control the position Related Controls: (1) See also 9A104, and orientation of a “spacecraft”. 9A515, and 9B515. (2) See ECCNs 9E001 (“development”) and 9E002 N.B.: Equipment specially designed for (“production”) for technology for items military use is “subject to the ITAR”. See 22 CFR controlled by this entry. (3) See USML parts 120 through 130. Categories IV for the space launch vehicles and XV for other spacecraft that are f. Terrestrial equipment specially designed for “subject to the ITAR” (see 22 CFR parts “spacecraft”, as follows: 120 through 130). Related Definition: N/A f.1. Telemetry and telecommand equipment Items: “specially designed” for any of the following data processing functions: a. Space launch vehicles; f.1.a. Telemetry data processing of b. “Spacecraft”; frame synchronization and error corrections, for monitoring of operational status (also known as c. “Spacecraft buses”; health and safe status) of the “spacecraft bus”; or d. “Spacecraft payloads” incorporating items f.1.b. Command data processing for specified by 3A001.b.1.a.4, 3A002.g, 5A001.a.1, formatting command data being sent to the 5A001.b.3, 5A002.c, 5A002.e, 6A002.a.1, “spacecraft” to control the “spacecraft bus”; 6A002.a.2, 6A002.b, 6A002.d, 6A003.b, 6A004.c, 6A004.e, 6A008.d, 6A008.e, 6A008.k, f.2. Simulators “specially designed” for 6A008.l or 9A010.c; ‘verification of operational procedures’ of “spacecraft”. e. On-board systems or equipment, specially designed for “spacecraft” and having Technical Note: For the purposes of any of the following functions: 9A004.f.2, ‘verification of operational procedures’ is any of the following: e.1. ‘Command and telemetry data handling’; 1. Command sequence confirmation; 2. Operational training; Note: For the purpose of 9A004.e.1, 3. Operational rehearsals; or ‘command and telemetry data handling’ includes 4. Operational analysis. bus data management, storage, and processing. g. “Aircraft” “specially designed” or modified to e.2. ‘Payload data handling’; or be air-launch platforms for space launch vehicles; h. “Sub-orbital craft”. Export Administration Regulations Bureau of Industry and Security March 29, 2021 Commerce Control List Supplement No. 1 to Part 774 Category 9—page 4 designed” for liquid rocket propulsion i. through t. [RESERVED] systems. (These items are “subject to the ITAR.” See 22 CFR parts 120 through 130.) u. The James Webb Space Telescope (JWST) being developed, launched, and operated under the supervision of the U.S. National Aeronautics 9A007 Solid rocket propulsion systems. and Space Administration (NASA). (These items are “subject to the ITAR.” See 22 CFR parts 120 through 130.) v. “Parts,” “components,” “accessories” and “attachments” that are “specially designed” for the James Webb Space Telescope and that are 9A008 “Components” “specially designed” not: for solid rocket propulsion systems. (These items are “subject to the ITAR.” See 22 CFR v.1. Enumerated or controlled in the USML; parts 120 through 130.) v.2. Microelectronic circuits; 9A009 Hybrid rocket propulsion systems. v.3. Described in ECCN 7A004 or 7A104; or (These items are “subject to the ITAR.” See 22 CFR parts 120 through 130.) v.4. Described in an ECCN containing “space-qualified” as a control criterion (See ECCN 9A515.x.4). 9A010 “Specially Designed” “Parts”, “Components”, Systems and Structures, for w. The International Space Station being Launch Vehicles, Launch Vehicle Propulsion developed, launched, and operated under the Systems or “Spacecraft”. (See Related supervision of the U.S. National Aeronautics and Controls paragraph.) Space Administration. List of Items Controlled x. “Parts,” “components,” “accessories” and “attachments” that are “specially designed” for Related Controls: (1) See USML Category the International Space Station. IV of the International Traffic in Arms Regulations (ITAR) (22 CFR parts 120 y. Items that would otherwise be within the scope through 130) and ECCN 9A604 for of ECCN 9A004.v or .x but that have been paragraphs 9A010.a, .b and .d. (2) See identified in an interagency-cleared commodity USML Category XV of the ITAR and classification (CCATS) pursuant to § 748.3(e) as ECCN 9A515 for paragraph 9A010.c. warranting control in 9A004.y. (3) See Supplement No. 4 to part 774, Order of Review for guidance on the process for determining classification of 9A005 Liquid rocket propulsion systems items. containing any of the systems or Related Definitions: N/A “components,” controlled by 9A006. (These Items: items are “subject to the ITAR.” See 22 CFR parts 120 through 130.) a.
Load more

Recommended publications
  • FAA Order 8130.2H, February 4, 2015
    U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADM INISTRATION ORDER 8130.2H 02/04/2015 National Policy SUBJ: Airworthiness Certification of Products and Articles This order establishes procedures for accomplishing original and recurrent airworthiness certification ofaircraft and related products and articles. The procedures contained in this order apply to Federal Aviation Administration (FAA) manufacturing aviation safety inspectors (ASI), to FAA airworthiness AS Is, and to private persons or organizations delegated authority to issue airworthiness certificates and related approvals. Suggestions for improvement of this order may be submitted using the FAA Office of Aviation Safety (AVS) directive feedback system at http://avsdfs.avs.faa.gov/default.aspx, or FAA Form 1320-19, Directive Feedback Information, found in appendix I to this order. D G!JD Cf1 · ~ David Hempe Manager, Design, Manufacturing, & Airworthiness Division Aircraft Certification Service Distribution: Electronic Initiated By: AIR-1 00 02/04/2015 8130.2H Table of Contents Paragraph Page Chapter 1. Introduction 100. Purpose of This Order .............................................................................. 1-1 101. Audience .................................................................................................. 1-1 102. Where Can I Find This Order .................................................................. 1-1 103. Explanation of Policy Changes ................................................................ 1-1 104. Cancellation ............................................................................................
    [Show full text]
  • Leading the Charge We Put TBM 940 Speedster Through Its Paces for NBAA
    15-21 October 2019 I flightglobal.com FLIGHT TEST Leading the charge We put TBM 940 speedster through its paces for NBAA £3.90 Wow, how? ACES high 42 Questions remain over defunct US Air Force boosts Collins Icelandic carrier’s comeback 13 with ejection seat deal 20 9 770015 371310 FLIGHT TEST Power of one Turboprop-single family has been a market success since launch in 1988, amassing sales of more than 900 units across three variants Daher has delivered a compelling offer for owner-flyers, with a range of enhancements on the TBM 940 providing an edge over the piston-twin segment. We put it through its paces MICHAEL GERZANICS POMPANO BEACH have allowed single-engined designs to make to be efficient. Airspace congestion, however, inroads into the twin-turbine segment. can make reaching optimum altitudes for jets he single-engined turboprop market The growth of the single-engined turbo- problematic, so their real-world range can be is populated by numerous aircraft of prop segment is based on the near-bulletproof shorter. Jets also have higher direct operating varying configurations. In broad reliability and scalability of the PT6 family. costs, however. T strokes, it can be broken down into This paradigm shift from piston-twins to tur- Runway performance and training require- two segments: fast, low-winged aircraft and bine-singles is conceptually on par with ex- ments are also two factors that fuel the single- slower, more spacious high-winged designs. tended twin-engine operations authorisations engined turboprop segment, because runway In the West, these diverse offerings share a all but killing off three- and four-engined civil length for turboprops is shorter than that single critical component – their engine.
    [Show full text]
  • CF-18 Fighter Demonstration Manual
    FIGHTER DEMONSTRATION MANUAL Version 4.0 Issued under the Authority of Commander 1 Canadian Air Division Custodian: OC FSET March 2019 Endorsed by: Approved by: Recoverable Signature Recoverable Signature X A DComd FG Col Luc Girou... X BGen I.H. Huddleston MGen J.H.C Drouin Deputy Commander Force Generation Commander 1 Canadian Air Division Signed by: GIROUARD, LUC 607 Signed by: BOYLE, SEAN 627 Fighter Demonstration Manual Record of Amendments Amend DATE DETAILS DONE BY # 0 XX Mar 19 Capt Thys R.G.T. This document is issued on the authority of the OC Fighter Standards and Evaluation Team (FSET) and contains information specific to the employment and role of the Fighter Demonstration Team. Inquiries and suggestions for changes shall be forwarded through Special Events Coord and OC FSET for review and submission to SSO Fighters for the approval of the Commander 1 Canadian Air Division. Table of Contents FIGHTER DEMONSTRATION MANUAL .................................................... 1 Chapter 1: PREPARATION ........................................................................ 8 101. TEAM SELECTION ........................................................... 8 102. AIRSHOW ROUTINE ........................................................ 9 103. FIGHTER DEMONSTRATION TRAINING ........................ 9 104. ACCEPTANCE SHOW ...................................................... 9 Chapter 2: OPERATIONAL CONSIDERATIONS .................................... 11 201. CONFIGURATION .......................................................... 11
    [Show full text]
  • This Annex to EASA TCDS IM.A.636 Was Created to Publish Selected
    Explanatory Note to TCDS No.: EASA.IM.A.636 – M3000 Date: 06/03/2020 Issue: 03 This annex to EASA TCDS IM.A.636 was created to publish selected special conditions / deviations / equivalent safety findings that are part of the applicable certification basis: CONTENTS B-02 High Speed Characteristics 2 B-52 Human Factor – Integrated Avionics Systems 12 C-03 Speed Margin 18 C-04 Yawing Manoeuvre 21 C-106 Emergency landing dynamic conditions - HIC 22 C-107 Emergency landing dynamic conditions - lumbar loads 24 D-01 Take-off Warning System 26 D-02 Extension and Retraction Systems 27 D-03 Wheels 28 D-04 Brakes and Braking System 29 D-05 Doors / Canopy 32 D-06 Bird Strike 35 D-102 Canopy Fracturing System 36 D-103 Ejection Seats 44 D-105 Emergency Evacuation Provisions 52 D-106 Fire Extinguisher 53 D-107 Cabin Pressure Altitude Warning Indication 54 E-101 Digital Electronic engine/propeller control PMU 55 E-114 Suction Defuel 56 E-115 Single Power Control Lever 57 E-116 Digital Propeller Tachometer and Markings 58 E-117 Digital Propeller Tachometer and Markings 59 F-02 Hydraulic System 60 F-52 Protection from Effects of HIRF 61 F-54 Protection from Effects of Lightning Strike, Indirect Effects 65 F-101 On Board Oxygen Generator System - OBOGS 66 F-103 Electronic Standby Direction Indicator (Compass) 71 F-104 HUD Certification 72 ESF 23.841-01 Cabin rate of climb indicator removal 74 ESF 23.1555 Use of Yellow and Black Emergency Markings 75 Disclaimer – This document is not exhaustive and it will be updated gradually.
    [Show full text]
  • Design and Development of Ejection Seat Mechanism in Aircraft
    International Journal of Innovative Technology and Exploring Engineering (IJITEE) ISSN: 2278-3075, Volume-8 Issue-11, September 2019 Design and Development of Ejection Seat Mechanism in Aircraft R. Rajaprasanna, A. Rajendra Prasad, T. Vignesh, M. C. Anand Chakaravarthi, Priyadarshi Dutt appropriate to fly an air ship. For moving of seats it need high Abstract: This research manages the discharge framework that fuel and cost of such carriers would be essentially astronomic. can be actualized in a common air ship. It is significant for a In the contender flying machines at the hour of launch the flying machine to have a launch situate in the event that the plane shade is first opened and the discharge seat is rescued with the meets a mishap in a fight or during experimental drill and the pilot, this framework can be additionally utilized in the pilot needs to rescue to spare their life. The component includes common plane to rescue the pilot, yet as by the common lifting of the pilot to a protected good ways from the air ship and after that sending the parachute. As there is increment in air airplane laws, the pilot is in charge of the security of the traffic, this discharge framework gives extra security measures to travelers. Simultaneously the travelers can't be catapulted like the life of travelers. By this strategy alongside the pilot, the group in the contender planes since we can't open the top of the individuals and the travelers can be spared. This discharge plane and can't discharge huge number of travelers one after framework comprises of an exceptionally made ejector cushion, another.
    [Show full text]
  • Ejection Seat Mechanism in Civil Aircraft Richard Johnson Abstract—This Paper Deals with the Ejection System That Can Be Implemented in a Civil Aircraft
    International Journal of Scientific & Engineering Research, Volume 3, Issue 10, October-2012 1 ISSN 2229-5518 Ejection Seat Mechanism in Civil Aircraft Richard Johnson Abstract—this paper deals with the ejection system that can be implemented in a civil aircraft. It is important for an aircraft to have an ejection seat in case the plane meets an accident in a battle or during test flight and the pilot has to bail out to save his or her life. The mechanism involves lifting of the pilot to a safe distance away from the aircraft and then deploying the parachute. As there is increase in air traffic, this ejection system provides additional safety measures to the life of passengers. By this method along with the pilot, the crew members and the passengers can be saved. This ejection system consists of a specially made ejector pad, track system and parachute. The ejection system is governed by a timing sensor which ensures that the movement of the passenger seat take place in equal interval of time to avoid collision between two consecutive seats. Index Terms- Bail, ejector pad, track system, ejection, hydraulic, propulsion, stability. —————————— —————————— empty weight. Instead of high propulsive power, simple 1 INTRODUCTION spring mechanism is implemented. To avoid the collisions the 1.1 Problem statement timing system, sequence and equal interval of ejection is Ejection seats have been traditionally fitted in military included. aircraft from the late 1940’s and onwards. But it was not used In this method there is no need to open the roof of the in the civil aircrafts because of the following reasons.
    [Show full text]
  • Legal and Engineering Aspects of Deployable Black Boxes with Video Recording Capability
    IJMS 2016 vol. 4 (1): International Journal of Multidisciplinary Studies (IJMS) Volume 4, Issue 1, 2017 Legal and Engineering Aspects of Deployable Black Boxes with Video Recording Capability Abeysekara Thusitha B1 and Abimani Menuwansala Peiris H2 1Department of Civil Law, Faculty of Law, General Sir John Kotelawala Defence University, Sri Lanka 2Department of Aeronautical Engineering, Faculty of Engineering, General Sir John Kotelawala Defence University, Sri Lanka ABSTRACT Black box is a compilation of data produced by on-board and ground communications, specifically and inherently in digital nature; therefore it is a digital database and part of a discussion on protection of digital databases. The Existing Black box technology used in Commercial Aircraft is accommodated with Affixed type black boxes. However, if the Deployable black boxes are implemented with fixed black boxes as a dual combined recorder system, the discovery of crash location can be determined with more effectually than the present technology. The lives of the survivors, initiation of aircraft accident and investigation progression obtain safety recommendations to avoid similar happenstances will depend upon the accessibility to the crash location immediately by search and rescue organizations with the reliable information they achieved through satellite communications. Deployable Recorders will provide a backup source of flight data other than the fixed black box data; assist the investigators to carry out their investigations with more trustworthy information while implementing the video recording capability. A new idea has been introduced in this research to implement a mechanism to deploy a parachute with the ejection of the deployable recorder from the aircraft to minimize the impact during its dwindling to the ground.
    [Show full text]
  • L-39 Albatros: Own and Fly a Fighter Jet
    FOR THE PILOTS OF OWNER-FLOWN, CABIN-CLASS AIRCRAFT FEBRUARY 2019 $3.95 US VOLUME 23 NUMBER 2 L-39 Albatros: Own and Fly a Fighter Jet Return to Service Checklist Crosswinds and Contamination Meet a Worldwide Ferry Pilot More Tech for Your Tow February 2019 TWIN & TURBINE • 1 B/E Aerospace Inc. 4/C Ad www.winner-aviation.com mail to: [email protected] 2 • TWIN & TURBINE February 2019 2 2019 Optimism FEBRUARY2019 • VOL. 23, NO. 2 by Rebecca Groom Jacobs Contents 3 Airmail 4 Return to Service Checklist by Dianne White 6 When the Rubber 6 Doesn’t Meet the Road by Joe Casey Jet Journal 10 L-39 Albatros: Own and Fly a Fighter Jet by Dan Greenwald 10 16 Cheap at Any Price by Kevin Ware 22 Five on the Fly Five Questions with Ferry Pilot 16 Guido Warnecke by Rebecca Groom Jacobs 24 Best Tugs: Advanced Towing by Rich Pickett From the Flight Deck 22 28 Gettin’ Hitched: Saying ‘I Do’ to DIY Aircraft Towing by Kevin Dingman En Route 30 Ice Shield Reduces Downtime with New Wing B/E Aerospace Inc. 24 Boot Application 4/C Ad AeroSearcher: A New Way to Search for Aviation Products www.winner-aviation.com On Final mail to: [email protected] 32 How to Train an Astronaut by David Miller Twin & Turbine (ISSN 1945-6514), USPS 24432 is published monthly by Village Press, Inc. with advertising offices located at 2779 EDITOR ADVERTISING DIRECTOR Aero Park Drive, Traverse City, Michigan Rebecca Groom Jacobs John Shoemaker 49686. Telephone (231) 946-3712.
    [Show full text]
  • Martin-Baker)
    TM 55-1680-308-24 TECHNICAL MANUAL ORGANIZATIONAL, DS AND GS MAINTENANCE MANUAL EJECTION SEAT, MODEL MK-J5D (MARTIN-BAKER) PART NUMBER 134AB80000 This copy is a reprint which includes current pages from Changes 1 through 10. TM 55-1680-308-24, dated 13 December 1974, rescinded by DA Pam 310-1, is now reinstated for active Army and is available through normal supply channels. HEADQUARTERS, DEPARTMENT OF THE ARMY 13 DECEMBER 1974 This manual is published for the use of all concerned. By Order of the Secretary of the Army FRED C. WEYAND Official General. United States Army VERNE L. BOWERS Chief of Staff Major General, United States Army The Adjutant General DISTRIBUTION: To be distributed in accordance with DA Form 12-31 Organizational Maintenance Requirements for OV-1A, B and C, and OV-1D aircraft. TM 55-1680-308-24 URGENT C 10 CHANGE HEADQUARTERS DEPARTMENT OF THE ARMY NO. 10 } WASHINGTON, D.C., 14 May 1991 ORGANIZATIONAL, DS AND GS MAINTENANCE MANUAL EJECTION SEAT, MODEL MK-J5D (MARTIN-BAKER) PART NUMBER 134AB80000 TM 55-1680-308-24, 13 December 1974, is changed as follows: 1. Remove and insert pages as indicated below. New or changed text material is indicated by a vertical bar in the margin. An illustration change is indicated by a miniature pointing hand. Remove pages Insert pages i and ii i and ii 1-1 and 1-2 1-1 and 1-2 3-1 and 3-2 3-1 and 3-2 4-47 and 4-48 4-47 and 4-48 4-48A/4-48B 4-48A/4-48B 2.
    [Show full text]
  • Evaluation of Aircraft Ejection Seat Safety When Using Advanced Helmet Sensors
    Report No. DODIG‑2015‑090 U.S. Department of Defense InspectorMARCH 9, 2015 General Evaluation of Aircraft Ejection Seat Safety When Using Advanced Helmet Sensors INTEGRITY EFFICIENCY ACCOUNTABILITY EXCELLENCE INTEGRITY EFFICIENCY ACCOUNTABILITY EXCELLENCE Mission Our mission is to provide independent, relevant, and timely oversight of the Department of Defense that supports the warfighter; promotes accountability, integrity, and efficiency; advises the Secretary of Defense and Congress; and informs the public. Vision Our vision is to be a model oversight organization in the Federal Government by leading change, speaking truth, and promoting excellence—a diverse organization, working together as one professional team, recognized as leaders in our field. Fraud, Waste & Abuse HOTLINE Department of Defense dodig.mil/hotline|800.424.9098 For more information about whistleblower protection, please see the inside back cover. Evaluation of Aircraft Ejection Seat Safety When Using ResultsAdvanced Helmet in SensorsBrief March 9, 2015 Findings (cont’d) Objective Handbook,” October 1998, has not been revised or updated as required by DoD Manual 4120.24, We are issuing this report in response to a “Defense Standardization Program (DSP), Policies request from Congress through the National and Procedures.” Defense Authorization Act (NDAA) for Fiscal Year 2015. We determined whether Furthermore, our evaluation concluded that the overall risk DoD aircraft ejection seats meet aircrew of ejection is remote. Also, the addition of HMDs and/or survivability and equipment airworthiness NVGs does not significantly increase the risk of major injury requirements for pilots and aircrew wearing during ejection if the aircrew is following proper ejection helmet -mounted displays (HMDs), night procedures described in the Naval Air Training and Operating vision goggles (NVGs), or both during Procedures (NATOPS) or the Air Force flight manuals.
    [Show full text]
  • B-177166 In-Flight Escape Systems for Helicopters Should Be
    .J REPORT TO THE CONGRESS I In-Flight Escape Systems For Helicopters Should Be Developed To Prevent Fatalities 6a777766 Department of Defense BY THE COMPTROLLER GENERAL OF THE UNITED STAT GOMPTROLLER GENERAL OFTHE UNITED STATES WASHINGION DC 20648 B-177166 To the President of the Senate and the 4 Speaker of the House of Representatives / We are reporting that In-flight escape systems for helicopters should be developed to prevent fatalltles. We made our review pursuant to the Budget and AC- countxng Act, 1921 (31 U s.c 531, and the Accounting and Auditing Act of 1950 (31 U S.C 67). We are sending copies of this report to the Director, Office of Management and Budget, the Secretary of Defense, the Secretary of the Army, and the Secretary of the Navy, Comptroller General of the United States Contents Page DIGEST 1 CHAPTER 1 INTRODUCTION 5 2 URGENTNEED FOR HELICOPTER IN-FLIGHT ESCAPESYSTEMS 6 3 EFFORTS TO DEVELOPA CAPSULE IN-FLIGHT ESCAPESYSTEM 9 Technlcal feaslblllty demonstrated 9 Appllcatlon to operational helicopters 9 Development efforts 13 4 EFFORTS TO DEVELOPAN INDIVIDUAL IN-FLIGHT ESCAPESYSTEM 15 Indlvldual in-flight escape systems 1.5 DOD emergency funds requested for the Cobra 18 No provision for an in-flight escape system In the advanced attack helicopter 19 5 CONCLUSIONSAND RECOMMENDATIONS 20 Recommendations to the Secretary of Defense 20 Agency comments and our evaluation 21 Matters for conslderatlon by the Congress 23 APPENDIX I Letter of November 29, 1972, from the Director of Defense Research and Engineering 25 II Principal
    [Show full text]
  • A Historical Perspective of Aircrew Systems Effects on Aircraft Design
    NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS A HISTORICAL PERSPECTIVE OF AIRCREW SYSTEMS EFFECTS ON AIRCRAFT DESIGN by David O. Bauer September, 1996 Thesis Advisor: Conrad F. Newberry Approved for public release; distribution is unlimited. DUDLEY KNOX LIBRARY NAVAL POSTGRADUATE. SCHOOl MONTEREY CA 93943-5101 Form Approved REPORT DOCUMENTATION PAGE OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget. Paperwork Reduction Project (0704-0188) Washington DC 20503. 1. AGENCY USE ONLY (leave bank) REPORT DATE 3. REPORT TYPE AND DATES COVERED September 1996 Master's Thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS A HISTORICAL PERSPECTIVE OF AIRCREW SYSTEMS EFFECTS ON AIRCRAFT DESIGN 6. AUTHOR(S) David O. Bauer 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION Naval Postgraduate School REPORT NUMBER Monterey CA 93943-5000 9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSORING/MONITORING AGENCY REPORT NUMBER 11. SUPPLEMENTARY NOTES The views expressed in this thesis are those of the author and do not reflect the official policy or position of the Department of Defense or the U. S. Government.
    [Show full text]