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PROMOTION REQUIREMENTS for CAP Members
PROMOTION REQUIREMENTS for CAP Members BY JOHN W. TALBOTT, Lt Col, CAP NEBRASKA WING Developed on 03/15/02 Update on 26 February 2006 AIR FORCE OFFICER RANKS Colonel (O-6) (Col) Second Lieutenant (O-1) (2nd Lt) st Brigadier General (O-7) (Brig Gen) First Lieutenant (O-2) (1 Lt) Captain (O-3) (Capt) Major General (08) (Maj Gen) Major (O-4) (Maj) Army Air Corps Lieutenant Colonel (O-5) (Lt Col) AIR FORCE NCO RANKS Chief Master Sergeant (E-9) (CMsgt) Senior Master Sergeant (E-8) (SMsgt) Master Sergeant (E-7) (Msgt) Technical Sergeant (E-6) (Tsgt) Staff Sergeant (E-5) (Ssgt) CAP Flight Officers Rank Flight Officer: Technical Flight Officer Senior Flight Officer NOTE: The following is a compilation of CAP Regulation 50-17 and CAP 35-5. It is provided as a quick way of evaluating the promotion and training requirements for CAP members, and is not to be treated as an authoritative document, but instead it is provided to assist CAP members in understanding how the two different regulations are inter-related. Since regulations change from time to time, it is recommended that an individual using this document consult the actual regulations when an actual promotion is being evaluated or submitted. Individual section of the pertinent regulations are included, and marked. John W. Talbott, Lt Col, CAP The following are the requirements for various specialty tracks. (Example: promotion to the various ranks for senior Personnel, Cadet Programs, etc.) members in Civil Air Patrol (CAP): For promotion to SFO, one needs to complete 18 months as a TFO, (See CAPR 35-5 for further details.) and have completed level 2: (Attend Squadron Leadership School, complete Initially, all Civil Air Patrol the CAP Officer course ECI Course 13 members who are 18 years or older are or military equivalent, and completes the considered senior members, (with no requirements for a Technician rating in a senior member rank worn), when they specialty track (this is completed for join Civil Air Patrol. -
NSIAD-91-54 Flying Hours: Overview of Navy and Marine Corps Flight Operations
United States General Accountinr! Office Report to the Chairman, Subcommittee GAO on Defense, Committee on Appropriations, U.S. Senate April 1991 FLYING HOURS Overview of Navy and Marine Corps Flight Operations WIll143694IllI llll1 GAO,‘NSIAD-91-54 i , i ’ United States General Accounting Office GAO Washington, D.C. 20648 National Security and International Affairs Division B-241707 April 12,199l The Honorable Daniel K. Inouye Chairman, Subcommittee on Defense Committee on Appropriations United States Senate Dear Mr. Chairman: As you requested, we reviewed the Navy’s flying hour program to determine l what types of aviators are flying carrier-based aircraft, l the types and amounts of flying performed by such aviators, and . the relevancy of the flying to operations and training. We focused on the A-6, F-14, and F/A-18 carrier-based aircraft, although we also reviewed the flying hour program as it relates to other carrier-based aircraft. The information pertains to naval aviation prior to the commencement of Operations Desert Shield and Desert Storm. While the concepts discussed in the report and the prior years data presented are still relevant, the fiscal year 1991 budget data do not reflect the commencement of the air war in January 1991. The Navy and Marine Corps need well-trained, highly skilled aviators to Background effectively and successfully accomplish their aviation missions. The skills demanded of an adept aviator include the ability to strike naval and land targets, protect ships from air threats, and take off from and land on aircraft carriers. An aviator’s primary means of gaining and maintaining proficiency is through hands-on training funded by the flying hour program. -
USNA Service Assignment
USNA Service Assignment Annual Parent Club Officer Conference October 30th, 2020 CAPT W. Scott Switzer, USN Deputy Commandant for Professional Development 1 Service Assignment Philosophy • Process Goal: match qualifications, talent, aptitudes, and desires with Navy and USMC accession requirements to provide Midshipmen fleet with best qualified Officers Midshipmen Performance & Preferences • Aptitude Our mission: BEST FIT assignments •USNA is the Navy’s premier source for Unrestricted Line warfare officers (URL) Needs of Navy & USMC 95% of the class will be assigned URL or USMC Analogous to Fleet Detailing 2 Service Communities Unrestricted Line Officers Restricted Line Officers (95% of Class) (5% of Class) • Surface Warfare Officer (SWO) • Medical/Dental ― Nuclear SWO • Aviation Maintenance Duty Officer ― SWO Options (Engineering Duty Officer, • Civil Engineering Corps Intelligence, Oceanography, Information Professional, Cryptologic Warfare) • Supply Corps • Pilot • Information Warfare Community • Naval Flight Officer (NFO) ― Intelligence Officer ― Oceanography Officer • Submarine ― Information Professional • USMC (up to 25% of class) ― Cryptologic Warfare Officer ― Ground ― Cyber Warfare Engineer ― Pilot ― Cyber Operations 3 Midshipmen to Fleet/USMC Officers – Career Information/Training Program 1/C Year 1/C, 2/C, 3/C, 4/C Service Assignment Career Information - Briefs - Community/Service Specific Screening - Briefs Preference Entry - Junior Officer Forum Commissioning - Community/Service Assignment Boards - Career Interest Survey - -
Adventures in Low Disk Loading VTOL Design
NASA/TP—2018–219981 Adventures in Low Disk Loading VTOL Design Mike Scully Ames Research Center Moffett Field, California Click here: Press F1 key (Windows) or Help key (Mac) for help September 2018 This page is required and contains approved text that cannot be changed. NASA STI Program ... in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part in or other meetings sponsored or co- helping NASA maintain this important role. sponsored by NASA. The NASA STI program operates under the • SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information technical, or historical information from Officer. It collects, organizes, provides for NASA programs, projects, and missions, archiving, and disseminates NASA’s STI. The often concerned with subjects having NASA STI program provides access to the NTRS substantial public interest. Registered and its public interface, the NASA Technical Reports Server, thus providing one of • TECHNICAL TRANSLATION. the largest collections of aeronautical and space English-language translations of foreign science STI in the world. Results are published in scientific and technical material pertinent to both non-NASA channels and by NASA in the NASA’s mission. NASA STI Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing • TECHNICAL PUBLICATION. Reports of specialized research announcements and feeds, completed research or a major significant providing information desk and personal search phase of research that present the results of support, and enabling data exchange services. -
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Armed Forces Equivalent Ranks Order Men Women Royal New Zealand New Zealand Army Royal New Zealand New Zealand Naval New Zealand Royal New Zealand Navy: Women’s Air Force: Forces Army Air Force Royal New Zealand New Zealand Royal Women’s Auxilliary Naval Service Women’s Royal New Zealand Air Force Army Corps Nursing Corps Officers Officers Officers Officers Officers Officers Officers Vice-Admiral Lieutenant-General Air Marshal No equivalent No equivalent No equivalent No equivalent Rear-Admiral Major-General Air Vice-Marshal No equivalent No equivalent No equivalent No equivalent Commodore, 1st and Brigadier Air Commodore No equivalent No equivalent No equivalent No equivalent 2nd Class Captain Colonel Group Captain Superintendent Colonel Matron-in-Chief Group Officer Commander Lieutenant-Colonel Wing Commander Chief Officer Lieutenant-Colonel Principal Matron Wing Officer Lieutentant- Major Squadron Leader First Officer Major Matron Squadron Officer Commander Lieutenant Captain Flight Lieutenant Second Officer Captain Charge Sister Flight Officer Sub-Lieutenant Lieutenant Flying Officer Third Officer Lieutenant Sister Section Officer Senior Commis- sioned Officer Lieutenant Flying Officer Third Officer Lieutenant Sister Section Officer (Branch List) { { Pilot Officer Acting Pilot Officer Probationary Assistant Section Acting Sub-Lieuten- 2nd Lieutenant but junior to Third Officer 2nd Lieutenant No equivalent Officer ant Navy and Army { ranks) Commissioned Officer No equivalent No equivalent No equivalent No equivalent No equivalent No -
Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
Helicopter Safety July-August 1991
F L I G H T S A F E T Y F O U N D A T I O N HELICOPTER SAFETY Vol. 17 No. 4 For Everyone Concerned with the Safety of Flight July/August 1991 The Philosophy and Realities of Autorotations Like the power-off glide in a fixed-wing aircraft, the autorotation in a helicopter must be used properly if it is to be a successful safety maneuver. by Michael K. Hynes Aviation Consultant In all helicopter flying, there is no single event that has a In the early years of airplane flight, the fear of engine greater impact on safety than the autorotation maneuver. failure, or that the airplane might have structural prob- The mere mention of the word “autorotation” at any lems during flight, was very strong. If either of these gathering of helicopter pilots, especially flight instruc- events took place, the pilot’s ability to get the airplane tors, will guarantee a long and lively discussion. safely on the ground quickly was important. The time it took to get the airplane on the ground was directly in There are many misconceptions about autorotations and proportion to the altitude at which the airplane was being they contribute to the accident rate when an autorotation flown. It is therefore logical that all early flights were precedes a helicopter landing accident. One approach to flown at low altitudes, often at less than 500 feet above a discussion of autorotations is to look at the subject the ground (agl). from three views: first, the philosophy of the subject; second, the reality of the circumstances that require au- At these low altitudes, the pilot did not always have the torotations; and third, the execution of the maneuver. -
DYNAMIC MODELING of AUTOROTATION for SIMULTANEOUS LIFT and WIND ENERGY EXTRACTION by SADAF MACKERTICH B.S. Rochester Institute O
DYNAMIC MODELING OF AUTOROTATION FOR SIMULTANEOUS LIFT AND WIND ENERGY EXTRACTION by SADAF MACKERTICH B.S. Rochester Institute of Technology, 2012 A thesis submitted in partial fulfilment of the requirements for the degree of Master of Science in the Department of Mechanical and Aerospace Engineering in the College of Engineering and Computer Science at the University of Central Florida Orlando, Florida Spring Term 2016 Major Professor: Tuhin Das c 2016 Sadaf Mackertich ii ABSTRACT The goal of this thesis is to develop a multi-body dynamics model of autorotation with the objective of studying its application in energy harvesting. A rotor undergoing autorotation is termed an Autogyro. In the autorotation mode, the rotor is unpowered and its interaction with the wind causes an upward thrust force. The theory of an autorotating rotorcraft was originally studied for achieving safe flight at low speeds and later used for safe descent of helicopters under engine failure. The concept can potentially be used as a means to collect high-altitude wind energy. Autorotation is inherently a dynamic process and requires detailed models for characterization. Existing models of autorotation assume steady operating conditions with constant angu- lar velocity of the rotor. The models provide spatially averaged aerodynamic forces and torques. While these steady-autorotation models are used to create a basis for the dynamic model developed in this thesis, the latter uses a Lagrangian formulation to determine the equations of motion. The aerodynamic effects on the blades that produce thrust forces, in- plane torques, and out-of-plane torques, are modeled as non-conservative forces within the Lagrangian framework. -
Development of a Helicopter Vortex Ring State Warning System Through a Moving Map Display Computer
Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 1999-09 Development of a helicopter vortex ring state warning system through a moving map display computer Varnes, David J. Monterey, California. Naval Postgraduate School http://hdl.handle.net/10945/26475 DUDLEY KNOX LIBRARY NAVAL POSTGRADUATE SCHOOL MONTEREY CA 93943-5101 NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS DEVELOPMENT OF A HELICOPTER VORTEX RING STATE WARNING SYSTEM THROUGH A MOVING MAP DISPLAY COMPUTER by David J. Varnes September 1999 Thesis Advisor: Russell W. Duren Approved for public release; distribution is unlimited. 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. REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED 1. agency use only (Leave blank) September 1999 Master's Thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS DEVELOPMENT OF A HELICOPTER VORTEX RING STATE WARNING SYSTEM THROUGH A MOVING MAP DISPLAY COMPUTER 6. AUTHOR(S) Varnes, David, J. 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) PERFORMING ORGANIZATION Naval Postgraduate School REPORT NUMBER Monterey, CA 93943-5000 10. -
Tuskegee Airmen Chronology Daniel L. Haulman Organizational
TUSKEGEE AIRMEN CHRONOLOGY DANIEL L. HAULMAN ORGANIZATIONAL HISTORY BRANCH AIR FORCE HISTORICAL RESEARCH AGENCY MAXWELL AFB, AL 36112-6424 14 November 2011 1 TUSKEGEE AIRMEN CHRONOLOGY Dr. Daniel L. Haulman Chief, Organization History Division Air Force Historical Research Agency Expanded Edition: 30 September 2011 27 June 1939: Congress passed the Civilian Pilot Training Act. (Robert J. Jakeman, The Divided Skies.) September-October 1939: The Civil Aeronautics Administration received Tuskegee Institute’s application to be a civilian pilot training institution, and after Tuskegee obtained permission to use the Montgomery Airport as a facility, the application was approved. (Robert J. Jakeman, The Divided Skies) Late February 1940: The Civil Aeronautics Authority approved Tuskegee’s Kennedy Field for Civilian Pilot Training, after improvements to the field, eliminating Tuskegee Institute’s need to use the Montgomery Airport. (Robert J. Jakeman, The Divided Skies) 25 March 1940: George A. Wiggs arrived in Tuskegee to administer the standard written examination required of all Civilian Pilot Training students. Every student who took the examination passed, surpassing the passing rate of other schools in the South. (Robert J. Jakeman, The Divided Skies.) 16 September 1940: Congress passed a Selective Service Act which required all the armed services to enlist “Negroes”. On the same day, the War Department announced that the Civil Aeronautics Authority, in cooperation with the U.S. Army, would start the development of “colored personnel” for the aviation service. (Public Law 783, 16 September 1940; War Department Press Release, 16 September 1940; 99th Fighter Squadron summary history in the lineage and honors folder of the 99th Flying Training Squadron at the Air Force Historical Research Agency (AFHRA), Maxwell AFB, AL) Late October 1940: In a press release, President Franklin D. -
CAP Grade Abbreviations – As Per CAPR 35-5 and CAPR 52-16 Air
CAP Grade Abbreviations – as per CAPR 35-5 and CAPR 52-16 For use in internal CAP communications and correspondence NOTE: Spell out the grade the first time you use it in your release/article then use the correct abbreviation after that. Senior Member Grades Cadet Member Grades Senior Member SM Cadet Basic C/AB Staff Sergeant SSgt Cadet Airman C/Amn Technical Sergeant TSgt Cadet Airman First Class C/A1C Master Sergeant MSgt Cadet Senior Airman C/SRA Senior Master Sergeant SMSgt Cadet Staff Sergeant C/SSgt Chief Master Sergeant CMSgt Cadet Technical Sergeant C/TSgt Flight Officer FO Cadet Master Sergeant C/MSgt Technical Flight Officer TFO Cadet Senior Master Sergeant C/SMSgt Senior Flight Officer SFO Cadet Chief Master Sergeant C/CMSgt Second Lieutenant 2d Lt Cadet Second Lieutenant C/2d Lt First Lieutenant 1st Lt Cadet First Lieutenant C/1st Lt Captain Capt Cadet Captain C/Capt Major Maj Cadet Major C/Maj Lieutenant Colonel Lt Col Cadet Lieutenant Colonel C/Lt Col Colonel Col Cadet Colonel C/Col Brigadier General Brig Gen Major General Maj Gen Air Force (CAP) Grades as per the AP Style Guide For use in Public Affairs Products NOTE: Spell out the grade the first time you use it in your release/article then use the correct abbreviation after that. Note: The AP Style guide does not give guidance for cadet grades so spell out “Cadet” before the appropriate abbreviation to denote the appropriate cadet grade. Flight Officer grades are not reflected in the guide so by analogy, we suggest the abbreviations below. -
Supplement to the London Gazette, Ist July 1969 6793
SUPPLEMENT TO THE LONDON GAZETTE, IST JULY 1969 6793 ENGINEER BRANCH MEDICAL TECHNICIAN BRANCH Promotion (MEDICAL SECTION) Flying Officer to Flight Lieutenant : Retirement M. P. KEITCH (684988). 26th Jun. 1969. Squadron Leader J. A. H. RUSSELL (522815). G. L. PERRY, B.Sc., A.C.G.I. (507682). 30th 14th Jun. 1969. Jun. 1969. EDUCATION BRANCH Retirement Promotion Wing Commander K. F. VENN, D.C.Ae., C.Eng., A.F.R.Ae.S., A.M.B.I.M. (49526) (at own request). Flight Lieutenant to Squadron Leader : 31st May 1969. B. O'HARE, B.Com. (506119). 30th Jun 1969. Squadron Leaders : PROVOST BRANCH J. T. C. BYRNE, C.Eng., M.I.Mech.E. (44587) Promotion (at own request). 30th May 1969. H. R. PORTER, CEng., A.F.R.Ae.S. (50059). 26th Flying Officer to Flight Lieutenant : Jun. 1969. A. C. P. SEYMOUR (4335200). 28th Jun. 1969. Flight Lieutenant A. C. FIFE (563648). 20th CATERING BRANCH Jun. 1969. Retirement Flying Officer C. G. CHURCH (195362), (on ENGINEER (PHOTOGRAPHY) BRANCH account of medical unntness for Air Force service). Transfer to the General List 30th Jun. 1969. The undermentioned Squadron Leaders are trans- ferred to the General List from 1st Jul. 1969: PHYSICAL FITNESS BRANCH W. H. P. BROWN (4036978). Transfer to the General List W. J. COLE (3025154). Squadron Leader F. W. LAST, D.Phys.Ed. Promotion (504847) is transferred to the General List from 1st Jul. 1969. Flying Officer to Flight Lieutenant: G. J. BROWN (4253831). 27th Jun. 1969. Promotion Flying Officer to Flight Lieutenant : EQUIPMENT BRANCH E. W. WAGHORN (3032427).