Fuel Reduction for the Mobility Air Forces

Total Page:16

File Type:pdf, Size:1020Kb

Fuel Reduction for the Mobility Air Forces Research Report Fuel Reduction for the Mobility Air Forces Christopher A. Mouton, James D. Powers, Daniel M. Romano, Christopher Guo, Sean Bednarz, Caolionn O’Connell C O R P O R A T I O N For more information on this publication, visit www.rand.org/t/RR757 Library of Congress Control Number: 2015931912 ISBN: 978-0-8330-8765-2 Published by the RAND Corporation, Santa Monica, Calif. © Copyright 2015 RAND Corporation R® is a registered trademark. Limited Print and Electronic Distribution Rights This document and trademark(s) contained herein are protected by law. This representation of RAND intellectual property is provided for noncommercial use only. Unauthorized posting of this publication online is prohibited. Permission is given to duplicate this document for personal use only, as long as it is unaltered and complete. Permission is required from RAND to reproduce, or reuse in another form, any of its research documents for commercial use. For information on reprint and linking permissions, please visit www.rand.org/pubs/permissions.html. The RAND Corporation is a research organization that develops solutions to public policy challenges to help make communities throughout the world safer and more secure, healthier and more prosperous. RAND is nonprofit, nonpartisan, and committed to the public interest. RAND’s publications do not necessarily reflect the opinions of its research clients and sponsors. Support RAND Make a tax-deductible charitable contribution at www.rand.org/giving/contribute www.rand.org Preface The Department of Defense (DoD) is the largest U.S. government user of energy, typically accounting for about 80 percent of the total government energy consumption. In particular, aviation fuel accounts for about half of DoD’s total energy use. In the context of significant fuel price increases—DoD spending on petroleum rose 381 percent between fiscal year (FY) 2005 and FY 2011 whereas DoD’s petroleum use decreased 4 percent over the same period—the current Air Force Energy Plan aims to reduce the consumption of aviation fuel 10 percent from a 2006 baseline by 2015. As of March 2013, the Air Force had already exceeded that goal, achieving a 12 percent reduction. To help achieve this goal, energy efficiency and conservation measures have been implemented during this time, and additional initiatives are being considered as a way to further reduce fuel consumption. These measures include technology improvements (aerodynamics, aircraft weight, propulsion, etc.) and fleet, flight, and ground operations optimization. This report provides a detailed analysis of the fuel and cost savings potential of fuel efficiency initiatives being considered by Air Mobility Command (AMC), the biggest consumer of aviation fuel in DoD. A summary of this report is also available: Christopher A. Mouton, James D. Powers, Daniel M. Romano, Christopher Guo, Sean Bednarz, and Caolionn O’Connell, Fuel Reduction for the Mobility Air Forces: Executive Summary, Santa Monica, Calif.: RAND Corporation, RR-757/1-AF, 2015. The research reported here was commissioned by the AMC Director of Operations and conducted within the Resource Management Program of RAND Project AIR FORCE as part of a project entitled “Reducing Mobility Air Forces (MAF) Energy Costs: Best Practices in Aviation Operations and Training.” It should be of interest to mobility air operations planners and those concerned with energy use within DoD. RAND Project AIR FORCE RAND Project AIR FORCE (PAF), a division of the RAND Corporation, is the U.S. Air Force’s federally funded research and development center for studies and analyses. PAF provides the Air Force with independent analyses of policy alternatives affecting the development, employment, combat readiness, and support of current and future air, space, and cyber forces. Research is conducted in four programs: Force Modernization and Employment; iii Manpower, Personnel, and Training; Resource Management; and Strategy and Doctrine. The research reported here was prepared under contract FA7014-06-C-0001. Additional information about PAF is available on our website: http://www.rand.org/paf/ iv Contents Preface ............................................................................................................................................ iii Figures............................................................................................................................................ ix Tables ............................................................................................................................................. xi Summary ...................................................................................................................................... xiii Acknowledgments ........................................................................................................................ xxi Abbreviations ............................................................................................................................. xxiii 1. Introduction ................................................................................................................................. 1 Background ........................................................................................................................................... 1 Purpose .................................................................................................................................................. 2 Analysis Approach ................................................................................................................................ 2 Key Assumptions ............................................................................................................................. 2 Flight Modeling ............................................................................................................................... 4 Annualized Costs ............................................................................................................................. 5 Fleet Retirements ............................................................................................................................. 5 Cost-to-Carry ................................................................................................................................... 7 Caveats ............................................................................................................................................. 8 Observations .......................................................................................................................................... 8 Fuel Reduction Potential .................................................................................................................. 8 Fuel Reduction Options ................................................................................................................... 9 How This Report Is Organized ............................................................................................................ 11 2. Fuel Efficiency in Commercial Aviation .................................................................................. 13 Background ......................................................................................................................................... 13 Information Sources ............................................................................................................................ 14 Differences Between Commercial Aviation and the Air Force .......................................................... 15 Technological Improvements .............................................................................................................. 16 Propulsion ...................................................................................................................................... 16 Aerodynamics ................................................................................................................................ 17 Weight Reduction .......................................................................................................................... 18 Operational Improvements .................................................................................................................. 20 Ground Efficiencies ....................................................................................................................... 20 Airborne Efficiencies ..................................................................................................................... 23 Fleet Efficiencies ........................................................................................................................... 24 Implementation .................................................................................................................................... 26 v Information System ........................................................................................................................ 27 Integrating Fuel Conservation into Company Culture ................................................................... 28 Conclusion ........................................................................................................................................... 29 3. Cost-Effective Options for Reducing Fuel Use ........................................................................ 31 Engine-Out Taxiing ............................................................................................................................
Recommended publications
  • Technical Supplements
    Technical Supplements S1 The IG JAS Investment In this Technical Supplement the JAS 39 Gripen product concept is outlined, the procurement process documented, the Industry Group IG JAS presented and the critical role of the competent public procurement agency, the FMV, highlighted. S1.1 The Procurement of the JAS 39 Gripen Aircraft with Swing-Role Capabilities The JAS 39 Gripen multirole combat aircraft (J stands for fighter, A for Attack and S for Surveillance/reconnaissance) is a fourth generation aircraft that entered operational service in 1997. It replaced the Viggen, the last of which was taken out of service in 2006. JAS 39 Gripen is a combat aircraft with swing-role capabilities that can change mission in flight. This swing-role capability was unique when Gripen was launched but has later been introduced on the French Rafale and the Eurofighter. Other competing multirole aircraft first have to land to reconfigure its information, guidance, and weapons systems for a new role. Gripen was the first “unstable” aircraft in the world which meant that in order for the aircraft to be stable at all speeds and in all maneuvers many more navigation surfaces are needed than the pilot can possibly control himself to minimize air friction at each moment. He needs incredibly sophisticated computer systems support to maneuver the aircraft effectively and safely. Competing fourth generation combat aircraft are F-35/JSF (the USA, not yet (2009) delivered to market), the Eurofighter Typhoon (the UK, etc.) and Rafale (Dassault, France). JAS 39 Gripen also competes with upgraded versions of the third generation aircraft of Lockheed Martin F-16 (the USA, first delivered in 1978), Boeing F/A18 Hornet (the USA, first delivered in 1983), Dassault Mirage 2000 (France, first delivered in 1983), and Mig-29 (the former Soviet Union, first delivered in 1977).
    [Show full text]
  • Design and Analysis of Advanced Flight: Planning Concepts
    NASA Contractor Report 4063 Design and Analysis of Advanced Flight: Planning Concepts Johri A. Sorerisen CONrRACT NAS1- 17345 MARCH 1987 NASA Contractor Report 4063 Design and Analysis of Advanced Flight Planning Concepts John .A. Sorensen Analytical Mechanics Associates, Inc. Moantain View, California Prepared for Langley Research Center under Contract NAS 1- 17345 National Aeronautics and Space Administration Scientific and Technical Information Branch 1987 F'OREWORD This continuing effort for development of concepts for generating near-optimum flight profiles that minimize fuel or direct operating costs was supported under NASA Contract No. NAS1-17345, by Langley Research Center, Hampton VA. The project Technical Monitor at Langley Research Center was Dan D. Vicroy. Technical discussion with and suggestions from Mr. Vicroy, David H. Williams, and Charles E. Knox of Langley Research Center are gratefully acknowledged. The technical information concerning the Chicago-Phoenix flight plan used as an example throughout this study was provided by courtesy of United Airlines. The weather information used to exercise the experimental flight planning program EF'PLAN developed in this study was provided by courtesy of Pacific Southwest Airlines. At AMA, Inc., the project manager was John A. Sorensen. Engineering support was provided by Tsuyoshi Goka, Kioumars Najmabadi, and Mark H, Waters. Project programming support was provided by Susan Dorsky, Ann Blake, and Casimer Lesiak. iii DESIGN AND ANALYSIS OF ADVANCED FLIGHT PLANNING CONCEPTS John A. Sorensen Analytical Mechanics Associates, Inc. SUMMARY The Objectives of this continuing effort are to develop and evaluate new algorithms and advanced concepts for flight management and flight planning. This includes the minimization of fuel or direct operating costs, the integration of the airborne flight management and ground-based flight planning processes, and the enhancement of future traffic management systems design.
    [Show full text]
  • Market Report a Publication of Saab Aircraft Leasing
    Issue 27 December 2011 MARKET REPORT A PUBLICATION OF SAAB AIRCRAFT LEASING DARWIN DEVELOPS EUROPEAN NETWORK PlottING A NEW COURSE GULFSTREAM INTERNATIONAL ADDS SAAB 340Bplus AIRCRAFT AND BECOMES SILVER AIRWAYS messaGE FROM CONTENTS Michael Magnusson Golden Air shines as niche Swedish carrier ......................... 3-5 Reflecting on 2011 activity and Darwin develops European network .................................... 6-9 readying for next year’s priorities Flying to the finish line. .................................................... 10-12 Pinnacle positions .................................................................13 As 2011 draws to a close, we can look back over a busy year during which Lakeshore luxury ..................................................................13 we transacted business on many Saab Plotting a new course 340Bplus aircraft. As we have taken Gulfstream International adds Saab 340Bplus aircraft aircraft back from Mesaba, we have found and becomes Silver Airways ........................................... 14-16 new homes for them with both old and new customers. The 30-seat turboprop Saab 340 operators in Thailand expand regional airline service ...........................................................17 continues to be a perfect regional aircraft choice on many regional routes. Saab Destination: Scatsta Airport, Shetland – Scotland. ......18 We are especially pleased that a revitalized Gulfstream International Airlines in Saab 340 Global Operators Conference set for 2012 ...........19 Florida, soon
    [Show full text]
  • Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft
    Air s.Pace ELectric Innovative Commuter Aircraft D2.1 Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft Name Function Date Author: Maximilian Spangenberg (ASP) WP2 Co-Lead 31.03.2020 Approved by: Markus Wellensiek (ASP) WP2 Lead 31.03.2020 Approved by: Dr. Qinyin Zhang (RRD) Project Lead 31.03.2020 D2.1 Economic Feasibility Study page 1 of 81 Clean Sky 2 Grant Agreement No. 864551 © ELICA Consortium No export-controlled data Non-Confidential Air s.Pace Table of contents 1 Executive summary .........................................................................................................................3 2 References ........................................................................................................................................4 2.1 Abbreviations ...............................................................................................................................4 2.2 List of figures ................................................................................................................................5 2.3 List of tables .................................................................................................................................6 3 Introduction ......................................................................................................................................8 4 ELICA market study ...................................................................................................................... 12 4.1 Turboprop and piston engine
    [Show full text]
  • 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.
    [Show full text]
  • CRUISE FLIGHT OPTIMIZATION of a COMMERCIAL AIRCRAFT with WINDS a Thesis Presented To
    CRUISE FLIGHT OPTIMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS _______________________________________ A Thesis presented to the Faculty of the Graduate School at the University of Missouri-Columbia _______________________________________________________ In Partial Fulfillment of the Requirements for the Degree Master of Science _____________________________________________________ by STEPHEN ANSBERRY Dr. Craig Kluever, Thesis Supervisor MAY 2015 The undersigned, appointed by the dean of the Graduate School, have examined the thesis entitled CRUISE FLIGHT OPTMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS presented by Stephen Ansberry, a candidate for the degree of Master of Science, and hereby certify that, in their opinion, it is worthy of acceptance. Professor Craig Kluever Professor Roger Fales Professor Carmen Chicone ACKNOWLEDGEMENTS I would like to thank Dr. Kluever for his help and guidance through this thesis. I would like to thank my other panel professors, Dr. Chicone and Dr. Fales for their support. I would also like to thank Steve Nagel for his assistance with the engine theory and Tyler Shinn for his assistance with the computer program. ii TABLE OF CONTENTS ACKNOWLEDGEMENTS………………………………...………………………………………………ii LIST OF FIGURES………………………………………………………………………………………..iv LIST OF TABLES…………………………………………………………………………………….……v SYMBOLS....................................................................................................................................................vi ABSTRACT……………………………………………………………………………………………...viii 1. INTRODUCTION.....................................................................................................................................1
    [Show full text]
  • May 31, 2004 5 - 1
    Airports Authority of India Manual of Air Traffic Services – Part 1 CHAPTER 5 SEPARATION METHODS AND MINIMA 5.1 Provision for the separation of Whenever, as a result of failure or controlled traffic degradation of navigation, communications, altimetry, flight control or other systems, 5.1.1 Vertical or horizontal separation shall aircraft performance is degraded below the be provided: level required for the airspace in which it is a) between IFR flights in Class D and E operating, the flight crew shall advise the airspaces except when VMC climb or ATC unit concerned without delay. Where the descent is involved under the failure or degradation affects the separation conditions specified in para 5.5.6; minimum currently being employed, the b) between IFR flights and special VFR controller shall take action to establish flights; [and another appropriate type of separation or c) between special VFR flights separation minimum. 5.1.2 No clearance shall be given to execute any manoeuvre that would reduce 5.2 Reduction in separation minima the spacing between two aircraft to less than the separation minimum applicable in the 5.2.1 In the vicinity of aerodromes circumstances. In the vicinity of aerodromes, the separation 5.1.3 Larger separations than the specified minima may be reduced if: minima should be applied whenever a) adequate separation can be provided exceptional circumstances such as unlawful by the aerodrome controller when each interference or navigational difficulties call for aircraft is continuously visible to this extra precautions. This should be done with controller; or due regard to all relevant factors so as to b) each aircraft is continuously visible to avoid impeding the flow of air traffic by the flight crews of the other aircraft application of excessive separations.
    [Show full text]
  • Ec-130 Employment ______Compliance with This Instruction Is Mandatory
    BY ORDER OF THE COMMANDER AFSOC INSTRUCTION 11-202, VOLUME 17 AIR FORCE SPECIAL OPERATIONS COMMAND 1 JUNE 1997 Flying Operations EC-130 EMPLOYMENT ____________________________________________________________________________________ COMPLIANCE WITH THIS INSTRUCTION IS MANDATORY. This instruction implements AFPD 11-2, Flight Rules and Procedures. It establishes employment procedures for AFSOC EC-130 aircraft and aircrew. It applies to all AFSOC EC-130 aircrews. It applies to the Air National Guard (ANG) when published in the ANGIND 2. OPR: HQ AFSOC/DOVF (Capt Wallace), 193 SOW/OGV (Maj McCarthy) Certified by: HQ AFSOC/DOV (Col Garlington) Pages: 33 Distribution: F; X Chapter 1 -- E-130E Employment Procedures Paragraph Section A -- Employment Concept General .........................................................................................................................1.1 Mission .........................................................................................................................1.2 Communications and Operations Security (COMSEC and OPSEC) ...............................1.3 Crew Rest .....................................................................................................................1.4 Checklists/Inflight Guides..............................................................................................1.5 Definitions ....................................................................................................................1.6 Section B -- Mission Planning and Employment Procedures
    [Show full text]
  • The Connection
    The Connection ROYAL AIR FORCE HISTORICAL SOCIETY 2 The opinions expressed in this publication are those of the contributors concerned and are not necessarily those held by the Royal Air Force Historical Society. Copyright 2011: Royal Air Force Historical Society First published in the UK in 2011 by the Royal Air Force Historical Society All rights reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording or by any information storage and retrieval system, without permission from the Publisher in writing. ISBN 978-0-,010120-2-1 Printed by 3indrush 4roup 3indrush House Avenue Two Station 5ane 3itney O72. 273 1 ROYAL AIR FORCE HISTORICAL SOCIETY President 8arshal of the Royal Air Force Sir 8ichael Beetham 4CB CBE DFC AFC Vice-President Air 8arshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-8arshal N B Baldwin CB CBE FRAeS Vice-Chairman 4roup Captain J D Heron OBE Secretary 4roup Captain K J Dearman 8embership Secretary Dr Jack Dunham PhD CPsychol A8RAeS Treasurer J Boyes TD CA 8embers Air Commodore 4 R Pitchfork 8BE BA FRAes 3ing Commander C Cummings *J S Cox Esq BA 8A *AV8 P Dye OBE BSc(Eng) CEng AC4I 8RAeS *4roup Captain A J Byford 8A 8A RAF *3ing Commander C Hunter 88DS RAF Editor A Publications 3ing Commander C 4 Jefford 8BE BA 8anager *Ex Officio 2 CONTENTS THE BE4INNIN4 B THE 3HITE FA8I5C by Sir 4eorge 10 3hite BEFORE AND DURIN4 THE FIRST 3OR5D 3AR by Prof 1D Duncan 4reenman THE BRISTO5 F5CIN4 SCHOO5S by Bill 8organ 2, BRISTO5ES
    [Show full text]
  • Saab 340 the VERSATILE TURBOPROP Saab 340 > the Versatile TURBOPROP
    SAAB 340 THE VERSATILE TURBOPROP SAAB 340 > THE VERSATILE TURBOPROP 2 SAAB 340 > THE VERSATILE TURBOPROP ”WE ARE A NICHE MARKET operator...THE SAAB 340 IS A WORKHORSE AIRCRAFT AND very RELIABLE.” GEORG POMMER ROBIN HOOD Aviation CEO THE FLEXIBLE PERFORMER To safeguard against today’s rapidly changing environment and improve profitability, successful airlines must choose an aircraft that minimizes risk and is adaptable to an ever-changing market environment. In addition, passengers demand comfort and service similar to that offered by major carriers. The Saab 340 is a favorite among airline passengers due to its flexibility, comfort and reliable performance. With about half the operating costs of a regional jet, the Saab 340 can offer service in a variety of markets, large or small. RELIABILITY IN A VARIETY OF OPERATIONS The cost-effective Saab 340 consistently generates profits for a wide range of regional air transport services. With the right blend of technologies, the Saab 340 combines high productivity with dependability. THE “FACTS” @ 4Q – 2009 • 25-year track record • best selling 30-seat turboprop • more than 410 operational aircraft found on six continents and in 30 countries • over 13 million hours flown and an estimated 250 million passengers • consistent 99% dispatch reliability • award winning customer support services 3 SAAB 340 > THE VERSATILE TURBOPROP THE BIG AIRLINE CHOICE 4 SAAB 340 > THE VERSATILE TURBOPROP WORLD’S LARGEST 340BPLUS OPERATOR ”...OUR OVERALL OBJECTIVE IS TO PROVIDE A SEAMLESS The red, white and blue Delta livery is replacing Northwest colors service PRODUCT TO OUR on all aircraft and airport signage as the newly merged airline is passengers.
    [Show full text]
  • Planning Horizons
    3 F R To properly plan for the future of Coolidge facilities will be evaluated in Chapter Four Municipal Airport, it is necessary to trans- to determine the most cost-effective and late forecast aviation demand into the efficient means for implementation. specific types and quantities of facilities that can adequately serve this identified demand. This chapter uses the results of the PLANNING HORIZONS forecasts conducted in Chapter Two, as well as established planning criteria, to The cost-effective, efficient, and orderly determine the airside (i.e., runways, development of an airport should rely more taxiways, navigational aids, marking and upon actual demand at an airport than on a lighting) and landside (i.e., terminal build- time-based forecast figure. In order to ing, hangars, aircraft parking apron, and develop a Master Plan that is demand-based automobile parking) facility requirements. rather than time-based, a series of planning horizon milestones have been established The objective of this effort is to identify, in for Coolidge Municipal Airport that take general terms, the adequacy of the existing into consideration the reasonable range of airport facilities, outline what new facilities aviation demand projections prepared in the may be needed, and when these may be previous chapter. needed to accommodate forecast demands. Having established these facility require- ments, alternatives for providing these 3-1 It is important to consider that the ac- airport to develop facilities according tual activity at the airport may be to need generated by actual demand higher or lower than projected activity levels. The demand-based schedule levels. By planning according to activ- provides flexibility in development, as ity milestones, the resulting plan can development schedules can be slowed accommodate unexpected shifts, or or expedited according to actual de- changes, in the area’s aviation de- mand at any given time during the mand.
    [Show full text]
  • Aircraft Part Number Manufacturer Nomenclature Aerospace Bae 146
    Aircraft Part Number Manufacturer Nomenclature Aerospace BAe 146 114.054 Kratos Ammeter Aerospace BAe 146 114.056 Kratos Voltmeter Aerospace BAe 146 114.058 Kratos Fuel Temperature Indicator Aerospace BAe 146 114.059 Kratos Duct Temperature Aerospace BAe 146 114.062 Kratos Battery Condition Aerospace BAe 146 114.063 Kratos Fuel Quantity Indicator Aerospace BAe 146 114.063-1 Kratos Fuel Quantity Indicator Aerospace BAe 146 114.065 Kratos Spoiler Position Indicator Aerospace BAe 146 114.158 Kratos Indicator Aerospace BAe 146 115.024 Kratos Cabin Temp. Indicator Aerospace BAe 146 115.026 Kratos Hydraulic Pressure Indicator Aerospace BAe 146 115.033 Kratos Voltmeter DC Indicator Aerospace BAe 146 115.034 Kratos Voltmeter AC Indicator Aerospace BAe 146 124.183 Kratos Outside Air Temp Ind Aerospace BAe 146 2594860-901 Sperry Directional Gyroscope Aerospace BAe 146 4034559-901 Honeywell Distance Bearing Indicator Aerospace BAe 146 DB-100 Honeywell Distance Bearing Indicator Aerospace BAe 146 WL651RSA5 Smith Industries N2 Percent RPM Indicator Aerospace BAe 146 WL702RSA1 Smith Industries N1 Percent RPM Indicator Aerospace BAe 146 WL706RSA4 Ametek/GE Turbine Gas Temp Indicator Aerospace BAe 146 WL719RSA1 Smith Industries N1 Percent RPM Indicator AH-1 2587451-2 Sperry Directional Gyroscope AH-1 2587451-3 Sperry Directional Gyroscope AH-1 50015 Flightline Systems Directional Gyroscope AH-1 50015-1 Flightline Systems Directional Gyroscope AH-1 CN-998(B) Sperry Directional Gyroscope AH-1 CN-998-ASN-43 Sperry Directional Gyroscope AH-1 CN-998B/ASN-43
    [Show full text]