Leading the Charge We Put TBM 940 Speedster Through Its Paces for NBAA
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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 ............................................................................................ -
A “Short Course” on Ice and the TBM
A “Short Course” on Ice and the TBM. Icing is topical at the present time as a result of a recent accident in a TBM. I have had a number of conversations with pilots who I would consider knowledgeable and it is apparent that there is a lot of confusion surrounding this subject. Also noting on line posts this confusion is not limited to owner pilots. I have had occasion to be a victim of my own stupidity in a serious icing condition years ago and I can vouch that icing is a deadly serious situation in more ways than one. Before going on with the subject we want to stipulate that the data we are about to provide is a summary of information that is to be found on line, along with narrative and data provided from knowledgeable instructors, if any of the data provided conflicts with anything you have been taught we urge you to satisfy yourself as to which data is correct. TBM operators fly in the same airspace where we find Part 25 aircraft (Commercial Category) aircraft. There is a big difference in how these two categories of aircraft are affected by icing conditions. A 767 will often be climbing at over 300 kts and 4000+ ft/min at typical icing altitudes. This creates two very distinct advantages for the 767: first, their icing exposure time may be less than 1/3 of ours. Second, icing conditions are a function of TAT (Total Air Temperature), not SAT (static air temp). TAT is warmer than SAT because of the effects of compressibility as the airplane operates at faster and faster speeds. -
Cessna Owner Magazine Article, October 2017
The following article appeared in the October 2017 edition of CESSNA OWNER magazine, the official publication of the Cessna Owner Organization. Whether for business or pleasure, the Official Publication of the Cessna Owner Organization Since 1975 Cessna Owner Organization is dedicated to assisting CESSNA>> October 2017 aircraft owners in OWNER MAGAZINE their continual pursuit to become better, TKS smarter and safer ROTECTION owners and pilots. ICE P Since 1975, the Liquid Armor for the collective knowledge War on Icing and experience of its members has saved owners countless hours of downtime and thousands of dollars in operational expenses. www.cessnaowner.org www.facebook.com/ CessnaOwnerOrganization Est. 1975 Not a member? Learn more at www.CessnaOwner.org TKS Ice Protection Liquid Armor for the War on Icing By Scott Sherer here are many people out accumulation before launching. I wind is strong and the wind chill there who really like snow also have a heavy-duty tug for get- is very low. The winter cloud in Tsports; things like skiing, ting my bird in and out of the han- Wisconsin is dark and grey. (I say snowboarding, ice skating, hockey, gar quickly, and the Janitrol fur- “cloud” and not “clouds” because we snowmobiling and all of those other nace, along with an assortment of seem to have only one cloud here sports that you typically see during other engine and interior warming and it covers the entire state from the winter Olympics. I’m sure that contraptions, helps to get my plane November well into January!) many aviators enjoy some of these warm and ready fast. -
LORD Flight Control Equipment
LORD Flight Control Equipment ELECTROMECHANICAL SOLUTIONS LORD provides customers innovative offerings globally with best-in-class cockpit controls • Inceptors to convert pilot inputs into flight control system commands • Force feedback optimized for pilot effectiveness • Electromechanical actuators for deployment of doors, landing gear, vents and control surfaces • Worldwide distribution, repair and overhaul network with AOG stock, servicing OEMs and end users Typical Applications: Benefits: • Cockpit Controls/ • Enable safer flights Inceptors Flight Controls for Business and Commercial Aircraft • Reduce pilot workload • Actuators • Reduce aircraft weight • Sensors • Optimize drag of wings • Dampers Side Stick • Enhance pilot comfort Throttle Control Flaps and Spoiler Levers Electric Pedals Actuator Systems for Aircraft and Helicopters • Door Systems • Flight Control Systems • Force Feel Systems • Locking Systems Our extensive experience in commercial fixed wing flight control systems and our innovative active vibration control systems in helicopters combine to make us a great partner for providing advanced flight control interfaces for aerospace applications. Cockpit Control Solutions LORD inceptors provide functional and ergonomic interfaces between pilots and various aircraft systems. Our Cockpit Control solutions are compact and lightweight and can be seamlessly integrated into cockpit designs. LORD flight control inceptors can be tailored to sidestick or yoke based cockpit layouts. Pilot Interface with: Modular Inceptor Components: • Flight Control Systems • Force Feel Dampers • Engine Control Systems • RVDT Transducer Units • Landing Gear Systems • Force Transducer Units Integrated Inceptors: • Auto Throttle Control Unit • Speed Brake Control Unit • Flap and Slat Control Unit • Nose Wheel Steering Hand Wheel • Side Stick (or Yoke) • Rudder and Brake Pedals Electromechanical Actuators Current aircraft primarily use hydraulic actuators to move surfaces and manage the landing gear operations. -
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 -
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. -
F-117A Accident During Air Show Flyover Caused by Omission of Fasteners in Wing-Support Structure
FLIGHT SAFETY FOUNDATION Aviation Mechanics Bulletin SEPTEMBER–OCTOBER 1998 F-117A Accident during Air Show Flyover Caused by Omission of Fasteners in Wing-support Structure FLIGHT SAFETY FOUNDATION Aviation Mechanics Bulletin Dedicated to the aviation mechanic whose knowledge, craftsmanship and integrity form the core of air safety. Robert A. Feeler, editorial coordinator September–October 1998 Vol. 46 No. 5 F-117A Accident during Air Show Flyover Caused by Omission of Fasteners in Wing-support Structure.......................................................... 1 Maintenance Alert ...................................................................................... 9 News & Tips ............................................................................................... 13 AVIATION MECHANICS BULLETIN Copyright © 1998 FLIGHT SAFETY FOUNDATION INC. ISSN 0005-2140 Suggestions and opinions expressed in FSF publications belong to the author(s) and are not necessarily endorsed by Flight Safety Foundation. Content is not intended to take the place of information in company policy handbooks and equipment manuals, or to supersede government regulations. Staff: Roger Rozelle, director of publications; Wayne Rosenkrans, senior editor; Mark Lacagnina, senior editor; John D. Green, copyeditor; Rick Darby, editorial consultant; Karen K. Ehrlich, production coordinator; Ann L. Mullikin, assistant production coordinator; and David Grzelecki, librarian, Jerry Lederer Aviation Safety Library. Subscriptions: US$35 (U.S.-Canada-Mexico), US$40 Air Mail (all other countries), six issues yearly. • Include old and new addresses when requesting address change. • Flight Safety Foundation, Suite 300, 601 Madison Street, Alexandria, VA 22314 U.S. • Telephone: (703) 739-6700 • Fax: (703) 739-6708 We Encourage Reprints Articles in this publication, in the interest of aviation safety, may be reprinted, in whole or in part, in all media, but may not be offered for sale or used commercially without the express written permission of Flight Safety Foundation’s director of publications. -
Evaluation of Two Unique Side Stick Controllers in a Fixed-Base Flight Simulator
NASA/TM-2003-212042 Evaluation of Two Unique Side Stick Controllers in a Fixed-Base Flight Simulator Jann Mayer and Timothy H. Cox NASA Dryden Flight Research Center Edwards, California December 2003 The NASA STI Program Office…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 Office plays a key or other meetings sponsored or cosponsored part in helping NASA maintain this by NASA. important role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program Office is operated by technical, or historical information from Langley Research Center, the lead center for NASA programs, projects, and mission, NASA’s scientific and technical information. often concerned with subjects having The NASA STI Program Office provides access substantial public interest. to the NASA STI Database, the largest collection of aeronautical and space science STI in the • TECHNICAL TRANSLATION. English- world. The Program Office is also NASA’s language translations of foreign scientific institutional mechanism for disseminating the and technical material pertinent to results of its research and development activities. NASA’s mission. These results are published by NASA in the NASA STI Report Series, which includes the Specialized services that complement the STI following report types: Program Office’s diverse offerings include creating custom thesauri, building customized databases, organizing and publishing research • TECHNICAL PUBLICATION. Reports of results…even providing videos. completed research or a major significant phase of research that present the results of For more information about the NASA STI NASA programs and include extensive data Program Office, see the following: or theoretical analysis. -
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. -
Kc-10A, T/N 83-0080 9Th Air Refueling Squadron 60Th Air Mobility Wing Travis Air Force Base, California
UNITED STATES AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION BOARD REPORT KC-10A, T/N 83-0080 9TH AIR REFUELING SQUADRON 60TH AIR MOBILITY WING TRAVIS AIR FORCE BASE, CALIFORNIA LOCATION: NEAR MOUNTAIN HOME AFB, IDAHO DATE OF ACCIDENT: 1 NOVEMBER 2016 BOARD PRESIDENT: COL PERRY M. LONG III Conducted IAW Air Force Instruction 51-503 ACTION OF THE CONVENING AUTHORITY 1 0 JUL 2117 The report of the accident investigation board, conducted under the provisions of AFI 51-503, that investigated the 1 November 2016 mishap that occurred near Mountain Home Air Force Base, Idaho, involving KC-10A, T/N 83-0080, assigned to the 60th Air Mobility Wing, Travis Air Force Base, California, complies with applicable regulatory and statutory guidance and on that basis is approved. \\signed\\ fHOMA^J; Major General, U| Vice Commander United States Air Force Accident Investigation Board Report Class A Mishap, Near Mountain Home AFB, ID EXECUTIVE SUMMARY UNITED STATES AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION KC-10A, T/N 83-0080 NEAR MOUNTAIN HOME AFB, IDAHO 1 NOVEMBER 2016 On 1 November 2016, at 1546 hours Zulu time (Z), a United States Air Force KC-10A Extender, tail number 83-0080, the mishap aircraft, assigned to the 60th Air Mobility Wing, departed from its home station of Travis Air Force Base (AFB), California, on a training mission in support of two flights of F-15s and a C-17. The scheduled flight profile was a formation departure from Travis AFB, refueling for approximately one hour with the F-15s, refueling training for approximately 1 hour 15 minutes with the C-17, and approximately one half hour of approach training before landing at Travis AFB. -
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. -
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.