A Review and Analysis of Precision Approach and Landing System (PALS) Certification Procedures
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Navair 00-80T-104 Signal Officer
THE LANDING NAVAIR 00-80T-104 SIGNAL OFFICER THE LSO WORKSTATION NORMAL NATOPS PROCEDURES LANDING SIGNAL OFFICER EMERGENCY MANUAL PROCEDURES EXTREME WEATHER CONDITION OPERATIONS THIS PUBLICATION SUPERSEDES NAVAIR 00-80T-104 DATED 1 NOVEMBER 1997 AND CHANGED 15 AUGUST 1998. COMMUNICATIONS NATOPS EVAL, PILOT PERFORMANCE RECS, A/C MISHAP STATEMENTS DISTRIBUTION STATEMENT C — Distribution authorized to U.S. Government Agencies and their contractors to protect publications required for official use or for administrative or operational purposes only determined on 1 May 1992. Other requests for this document shall be referred to Commanding Officer, Naval Air Technical Data and Engineering Service Command, Naval Air Station, North Island, P.O. Box 357031, Building 90, Distribution, San Diego, CA 92135–7031. DESTRUCTION NOTICE — For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document. ISSUED BY AUTHORITY OF THE CHIEF OF NAVAL OPERATIONS AND UNDER THE DIRECTION OF THE COMMANDER, NAVAL AIR SYSTEMS COMMAND. INDEX 1 (Reverse Blank) 15 DECEMBER 2001 2 NAVAIR 00-80T-104 15 December 2001 LETTER OF PROMULGATION 1. The Naval Air Training and Operating Procedures Standardization (NATOPS) Program is a posi- tive approach toward improving combat readiness and achieving a substantial reduction in the aircraft mishap rate. Standardization, based on professional knowledge and experience, provides the basis for development of an efficient and sound operational procedure. The standardization program is not planned to stifle individual initiative, but rather to aid the commanding officer in increasing the unit’s combat potential without reducing command prestige or responsibility. 2. This manual standardizes ground and flight procedures but does not include tactical doctrine. -
Pilot Stories
PILOT STORIES DEDICATED to the Memory Of those from the GREATEST GENERATION December 16, 2014 R.I.P. Norm Deans 1921–2008 Frank Hearne 1924-2013 Ken Morrissey 1923-2014 Dick Herman 1923-2014 "Oh, I have slipped the surly bonds of earth, And danced the skies on Wings of Gold; I've climbed and joined the tumbling mirth of sun-split clouds - and done a hundred things You have not dreamed of - wheeled and soared and swung high in the sunlit silence. Hovering there I've chased the shouting wind along and flung my eager craft through footless halls of air. "Up, up the long delirious burning blue I've topped the wind-swept heights with easy grace, where never lark, or even eagle, flew; and, while with silent, lifting mind I've trod the high untrespassed sanctity of space, put out my hand and touched the face of God." NOTE: Portions Of This Poem Appear On The Headstones Of Many Interred In Arlington National Cemetery. TABLE OF CONTENTS 1 – Dick Herman Bermuda Triangle 4 Worst Nightmare 5 2 – Frank Hearne Coming Home 6 3 – Lee Almquist Going the Wrong Way 7 4 – Mike Arrowsmith Humanitarian Aid Near the Grand Canyon 8 5 – Dale Berven Reason for Becoming a Pilot 11 Dilbert Dunker 12 Pride of a Pilot 12 Moral Question? 13 Letter Sent Home 13 Sense of Humor 1 – 2 – 3 14 Sense of Humor 4 – 5 15 “Poopy Suit” 16 A War That Could Have Started… 17 Missions Over North Korea 18 Landing On the Wrong Carrier 19 How Casual Can One Person Be? 20 6 – Gardner Bride Total Revulsion, Fear, and Helplessness 21 7 – Allan Cartwright A Very Wet Landing 23 Alpha Strike -
Ship Suitability Testing – Preparing for the Future
Ship Suitability Testing – Preparing for the Future Mr. Ronald J. Harney Senior T&E Engineer for Ship Suitability Naval Air Warfare Center, Aircraft Division 21950 Nickles Rd, Bldg 2649, Rm 207C Patuxent River, MD, 20670 USA [email protected] ABSTRACT In support of the United States Navy Sea Power 21 initiative, ship suitability test and evaluation personnel are preparing to support a large number of test and evaluation programs. The pillars of Sea Power 21, which include Sea Basing, Sea Shield, and Sea Strike call for a diverse set of new and modified aircraft and air capable ships. Ship compatibility testing may be required on aircraft ranging from the two variants of the Joint Strike Fighter to the Firescout unmanned helicopter; and from C-130 cargo aircraft to small unmanned seaplanes. Additionally, aircraft compatibility testing will be required on ships ranging from the Littoral Combat Ship to the DDX destroyer, and from a new amphibious assault ship to the latest in nuclear carrier technology, CVN-21, which will incorporate all new electric catapult and arresting gear equipment. The precision approach landing systems group is already testing enabling technologies for a new GPS-based Joint Precision Approach and Landing System, which will significantly change the air traffic control environment, enable all aircraft to have precision approach capability, and provide the means to operate fighter-sized Unmanned Combat Air Vehicles on aircraft carriers. These aircraft/ship test and evaluation programs will require the development of new methodology. They will also require the testers to research and modify test techniques that have not been used for decades. -
Instruction and Technical Manual for Prototype Landing Signal Officer's Display System
NBSIR 74-589R Instruction and Technical Manual for Prototype Landing Signal Officer's Display System Charles C. Gordon Measurement Engineering Division Institute for Applied Technology National Bureau of Standards Washington, D. C. 20234 November 1974 Interim Report Sponsored by: Commander Naval Air System Command Code 53722 Department of Navy Washington, D. C. 20361 r I 1 NBSIR 74-'589R INSTRUCTION AND TECHNICAL MANUAL FOR PROTOTYPE LANDING SIGNAL OFFICER'S DISPLAY SYSTEM Charles C. Gordon Measurement Engineering Division Institute for Applied Technology National Bureau of Standards Washington, D. C. 20234 November 1974 Interim Report Sponsored by; Commander Naval Air System Command Code 53722 Department of Navy Washington, D. C. 20361 U. S. DEPARTMENT OF COMMERCE, Frederick B. Dent, Secretary NATIONAL BUREAU OF STANDARDS. Richard W. Roberts. Director Table of Contents Page 1.0 Introduction 1 1.1 Specifications 6 1.1.1 Displays 6 1.1.2 Head-Up Displays ^> 1.1.3 Intercom Unit 7 1.1. ^ Power Required 7 2.0 Console Display and Controls 7 2.1 Console Mount and Controls 7 2.2 Displays and Controls 7 2.2.1 Intercom and PLAT 7 2.2.2 Pointer Displays 7 2.2.2a Airspeed 12 2.2.2b Rate of Descent 12 2.2.2c Range 12 2. 2. 2d Ramp Motion 12 2.2.3 Deck Open and Closed and LSO Wave-Off ... 12 2.2. n Aircraft Type 13 2.2.5 ACLS Status 13 2.2.6 V/ind Angle and Speed 13 2.2.7 MOVLAS 13 2.3 Head-Up Display 13 2.3.1 Airspeed 1^ 2.3.2 Ramp Motion 1^ 2.3.3 Aircraft Range 14 2.3.4 Glide-Slope Line Up 14 3.0 Console Operation 14 4.0 Console Storage , IH Technical Details of the Equipment ..... -
Vpa Report 2002-12-05
UNCLASSIFIED NAVAL AIR WARFARE CENTER AIRCRAFT DIVISION PATUXENT RIVER, MARYLAND TECHNICAL REPORT REPORT NO: NAWCADPAX/TR-2002/71 REVIEW OF THE CARRIER APPROACH CRITERIA FOR CARRIER-BASED AIRCRAFT PHASE I; FINAL REPORT by Thomas Rudowsky Stephen Cook Marshall Hynes Robert Heffley Melvin Luter Thomas Lawrence CAPT Robert Niewoehner Douglas Bollman Page Senn Dr. Wayne Durham Henry Beaufrere Michael Yokell Albert Sonntag Approved for public release; distribution is unlimited. UNCLASSIFIED DEPARTMENT OF THE NAVY NAVAL AIR WARFARE CENTER AIRCRAFT DIVISION PATUXENT RIVER, MARYLAND NAWCADPAX/TR-2002/71 REVIEW OF THE CARRIER APPROACH CRITERIA FOR CARRIER-BASED AIRCRAFT - PHASE I; FINAL REPORT by Thomas Rudowsky Stephen Cook Marshall Hynes Robert Heffley Melvin Luter Thomas Lawrence CAPT Robert Niewoehner Douglas Bollman Page Senn Dr. Wayne Durham Henry Beaufrere Michael Yokell Albert Sonntag NAWCADPAX/TR-2002/71 REPORT DOCUMENTATION PAGE Form Approved 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 instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing this 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 Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. -
Outer-Loop Control Factors for Carrier Aircraft
Robert Heffley Engineering 349 First Street, Los Altos, CA 94022, USA Telephone: (650) 949-1747 FAX: (650) 949-1243 RHE-NAV-90-TR-1 OUTER-LOOP CONTROL FACTORS FOR CARRIER AIRCRAFT Robert K. Heffley 1 December 1990 CONTRACT SUMMARY REPORT Distribution authorized to U. S. Government agencies and their contractors; (Critical technology). Other requests for this document will be referred to the Naval Air Systems Command (AIR-5301). Prepared for: Naval Air Systems Command Department of the Navy Washington DC 20361 This report was prepared under Contract N00019-89-C-0259 which was competitively awarded for a total cost of $52,998. THIS PAGE IS INTENTIONALLY BLANK UNCLASSIFIED Page i SECURITY CLASSIFICATION OF THIS PAGE REPORT DOCUMENTATION PAGE 1a. REPORT SECURITY CLASSIFICATION 1b. RESTRICTIVE MARKINGS UNCLASSIFIED 2a. SECURITY CLASSIFICATION AUTHORITY 3. DISTRIBUTION/AVAILABILITY OF REPORT Distribution authorized to U. S. Government agencies and their 2b. DECLASSIFICATION/DOWNGRADING SCHEDULE contractors; (Critical technology). Other requests for this document will be referred to the Naval Air Systems Command (AIR-5301). 4. PERFORMING ORGANIZATION REPORT NUMBER(S) 5. MONITORING ORGANIZATION REPORT NUMBER(S) RHE-NAV-90-TR-1 6a. NAME OF PERFORMING ORGANIZATION 6b. OFFICE SYMBOL 7a. NAME OF MONITORING ORGANIZATION Robert Heffley Engineering (I f applicable) Department of the Navy Naval Air Systems Command, AIR-5301 6c. ADDRESS (City, State, and ZIP Code) 7b. ADDRESS (City, State, and ZIP Code) 349 First Street Los Altos, CA 94022 Washington, DC 20361 8a. NAME OF FUNDING/SPONSORING 8b. OFFICE SYMBOL 9. PROCUREMENT INSTRUMENT IDENTIFICATION NUMBER ORGANIZATION (If applicable) Contract N00019-89-C-0259 Naval Air Systems Command AIR-5301 8c. -
F35C Joint Strike Fighter Additive Manufacturing Tailhook Redesign
F35C Joint Strike Fighter Additive Manufacturing Tailhook Redesign 4/24/16 Submitted to Lockheed Martin Representative Team EDSGN 100, Section: 23 Group 4: Kiran Judd, James Harris, Madeline Woody, and Zach Ceneviva Abstract: The objective for the project was to design, prototype, and manufacture an effective redesign of the Lockheed Martin F35C tailhook, utilizing additive manufacturing. The F35C tailhook, like many other subtractive manufactured parts, suffers from a waste of excess material and limitations when creating advanced designs. The main question relating to the current process is how does one eliminate the total amount of material used, while still retaining the original strength? For this reason, when designing the prototype material reduction, affordability, accessibility in the field, effectiveness, and durability were treated with the utmost importance with respect to design criteria. After the printing of the prototype, it was necessary to test the design criteria in order to see if the efficiency and reliability met the desired goals for the tailhook. The tailhook prototype did not pass all of the set criteria for its design, but performed especially well when compared to the set criteria for the durability. Although the initial prototype performed well during the durability test, it did not perform as well as hoped within the material reduction, affordability, and effectiveness categories. These areas proved to be lacking, leading to corrections which would later lead to the improved second prototype, created by the team. Following the improvements implemented within the second prototype, an effective, durable tailhook was created utilizing additive manufacturing processes. Table of Contents Introduction Pg. -
F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings
University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Masters Theses Graduate School 5-2007 F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings Brian T. Schrum University of Tennessee - Knoxville Follow this and additional works at: https://trace.tennessee.edu/utk_gradthes Part of the Navigation, Guidance, Control and Dynamics Commons Recommended Citation Schrum, Brian T., "F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings. " Master's Thesis, University of Tennessee, 2007. https://trace.tennessee.edu/utk_gradthes/323 This Thesis is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by Brian T. Schrum entitled "F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the equirr ements for the degree of Master of Science, with a major in Aviation Systems. Robert B. Richards, Major Professor We have read this thesis and recommend its acceptance: Peter Solies, Rodney Allison Accepted for the Council: Carolyn R. Hodges Vice Provost and Dean of the Graduate School (Original signatures are on file with official studentecor r ds.) To the Graduate Council: I am submitting herewith a thesis written by Brian T. -
Research Article Modeling and Simulation of Arresting Gear System with Multibody Dynamic Approach
Hindawi Publishing Corporation Mathematical Problems in Engineering Volume 2013, Article ID 867012, 12 pages http://dx.doi.org/10.1155/2013/867012 Research Article Modeling and Simulation of Arresting Gear System with Multibody Dynamic Approach Wenhou Shen,1,2 Zhihua Zhao,1 Gexue Ren,1 and Jiapeng Liu1 1 Tsinghua University, Beijing 100084, China 2 Naval Aviation Institute, Huludao 125001, China Correspondence should be addressed to Wenhou Shen; [email protected] Received 17 July 2013; Revised 19 September 2013; Accepted 19 September 2013 Academic Editor: Song Cen Copyright © 2013 Wenhou Shen et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. The arresting dynamics of the aircraft on the aircraft carrier involves both a transient wave propagation process in rope and a smooth decelerating of aircraft. This brings great challenge on simulating the whole process since the former one needs small time-step to guarantee the stability, while the later needs large time-step to reduce calculation time. To solve this problem, this paper proposes a full-scale multibody dynamics model of arresting gear system making use of variable time-step integration scheme. Especially, a kind of new cable element that is capable of describing the arbitrary large displacement and rotation in three-dimensional space is adopted to mesh the wire cables, and damping force is used to model the effect of hydraulic system. Then, the stress of the wire ropes during the landing process is studied. Results show that propagation, reflection, and superposition of the stress wave between the deck sheaves contribute mainly to the peak value of stress. -
Table of Contents Next Page
, SERVICE PUBLICATION OF OCKHEED-GEORGIA COMPANY / DIVISION OF OCKHEED CORPORATION Editor: Don H. Hungate Associate Editors: Charles I. Gale, James A. Loftin, Arch McCleskey, Patricia Thomas Art Direction and Production: Anne G. Anderson This summer marks the 25th anniversary of the first flight of the Lockheed Hercules; a Volume 6, No. 3, July - September 1979 quarter century of service to nations throughout the world! Over 1,550 Hercules (C-130s Vol. 6, No. 3, July. September 1979 and L-100) have been delivered to 44 countries. We at Lockheed are very proud of this Contents: record and the reputation the Hercules has earned. It is a reputation built on depend- ability, versatility, and durability. 2 Focal Point The Hercules is a true workhorse. Many developing countries depend on it to carry all types of cargo, from lifesaving food to road-building equipment. They carry these cargoes to remote areas that are not easily accessible by any other mode of transporta- 3 tion. An additional advantage is its ability to land and take off in incredibly short 3 Crew Door Rigging distances, even on unpaved clearings. The tasks the Hercules is capable of accomplishing are almost limitless; from hunting hurricanes, to flying mercy relief missions. It is the universal airborne platform. And it is 14 Royal Norwegian Air Force energy-efficient, using only about half the fuel a comparable jet aircraft would require. 15 One of the more interesting aspects of these 25 years is that while the external design of 15 Hydraulic Pressure Drop the aircraft has changed very little, constant improvements in systems and avionics equip- ment have made the world’s outstanding cargo airplane also among the world’s most modern. -
Natops Landing Signal Officer Manual
THE LANDING NAVAIR 00-80T-104 SIGNAL OFFICER THE LSO WORKSTATION NATOPS NORMAL LANDING SIGNAL PROCEDURES OFFICER MANUAL EMERGENCY PROCEDURES EXTREME WEATHER CONDITION OPERATIONS THIS PUBLICATION SUPERSEDES NAVAIR 00-80T-104 DATED 1 MAY 2007. COMMUNICATIONS NATOPS EVAL, PILOT PERFORMANCE RECS, A/C MISHAP STATEMENTS DISTRIBUTION STATEMENT C — Distribution authorized to U.S. Government Agencies and their contractors to protect publications required for official use or for administrative or operational purposes only, effective (01 May 2009). Other requests for the document shall be referred to COMNAVAIRSYSCOM, ATTN: NATOPS Officer, Code 4.0P, 22244 Cedar Point Rd, BLDG 460, Patuxent River, MD 20670−1163 DESTRUCTION NOTICE — For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document. ISSUED BY AUTHORITY OF THE CHIEF OF NAVAL OPERATIONS AND UNDER THE DIRECTION OF THE COMMANDER, NAVAL AIR SYSTEMS COMMAND. INDEX 0800LP1097834 1 (Reverse Blank) 1 MAY 2009 NAVAIR 00-80T-104 DEPARTMENT OF THE NAVY NAVAL AIR SYSTEMS COMMAND RADM WILLIAM A. MOFFETT BUILDING 47123 BUSE ROAD, BLDG 2272 PATUXENT RIVER, MD 20670-1547 1 May 2009 LETTER OF PROMULGATION 1. The Naval Air Training and Operating Procedures Standardization (NATOPS) Program is a positive approach toward improving combat readiness and achieving a substantial reduction in the aircraft mishap rate. Standardization, based on professional knowledge and experience, provides the basis for development of an efficient and sound operational procedure. The standardization program is not planned to stifle individual initiative, but rather to aid the Commanding Officer in increasing the unit’s combat potential without reducing command prestige or responsibility. -
Supercarrier Operations Guide]
Operations Guide Updated 24 May 2020 DCS [Supercarrier Operations Guide] Contents LATEST CHANGES ........................................................................................................................................................................... 4 QUICKSTART GUIDE ....................................................................................................................................................................... 5 How do I install this module? ....................................................................................................................................................... 6 How do I know the module is installed? ....................................................................................................................................... 6 How do I select a Supercarrier mission? ..................................................................................................................................... 7 Creating Your Own Mission ......................................................................................................................................................... 8 Catapult Start .............................................................................................................................................................................11 Taxi to Catapult ..........................................................................................................................................................................12 Returning