PC-21 Brochure
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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 ............................................................................................ -
MASAD-83-22 Air Force and Navy Trainer Aircraft Acquisition Programs
/-Gr - Y 4 , +Asl+H., c BY THECOMPTROLLER GENERAL ’ eport To The Congress8 z THEUNITED STATES r Force And Navy Trainer rcraft Acquisition Programs G41 examined the status of one Navy and tvAir Force Programs to acquire 1,184 tri ler aircraft costing an estimated $10.8 bi In over the next decade. GAO found th *The Department of Defense needs to firm up its plans to acquire T-45 aircraft for training Navy pilots. In doing so, the Navy should be directed to consider extending use of its present aircraft. -The Air Force’s T-46A has experienced some cost growth. Its accelerated en- ginadevelopment and concurrent test- ing and production are areas of poten- tial concern. -The Air Force planned to begin develop- ment of the Tanker-Transport-Bomber Training System in fiscal year 1983, but tha Congress did not authorize’ appropriations for the program in that! y@ar. The Air Force has applied for\\ fiscal year 1984 approval. \ 121798 GAO/MA#AD-82-22 &LY &I983 Request for copies of GAO reports should be sent to: U.S. General Accounting Off ice Document Handling and Information Services Facility P.O. Box 6015 Gaithersburg, Md. 20760 Telephone (202) 2756241 The first five copies of individual reports are free of charge. Additional copies of bound audit reports are $3.25 each. Additional copies of unbound report (i.e., letter reports) and most other publications are $1.00 each. There will be a 26% discount on all orders for 100 or more copies mailed to a single address. Salk orders must be prepaid on a cash, check, or money order basis. -
EWIS Practices Job Aid 2.0
Aircraft EWIS Practices Job Aid 2.0 Federal Aviation Administration Aircraft Electrical Wiring Interconnect System (EWIS) Best Practices Job Aid Revision: 2.0 This job aid covers applicable 14 CFR part 25 aircraft (although it is also widely acceptable for use with other types of aircraft such as military, small airplanes, and rotorcraft). This job aid addresses policy; industry EWIS practices; primary factors associated with EWIS degradation; information on TC/STC data package requirements; EWIS selection and protection; routing, splicing and termination practices; and EWIS maintenance concepts (including how to perform a EWIS general visual inspection). The job aid also includes numerous actual aircraft EWIS photos and examples. UNCONTROLLED COPY WHEN DOWNLOADED 1 Aircraft EWIS Practices Job Aid 2.0 Additional Notes • This presentation contains additional speaker notes for most slides • It’s advisable to read these notes while viewing the slide presentation Aircraft EWIS Best Practices Job Aid 2.0 Federal Aviation 2 Administration UNCONTROLLED COPY WHEN DOWNLOADED 2 Aircraft EWIS Practices Job Aid 2.0 Printing the Additional Notes To print the slides and accompanying speaker notes: – Navigate back to the FAA Aircraft Certification job aids web page – Open and print Printable Slides and Notes Aircraft EWIS Best Practices Job Aid 2.0 Federal Aviation 3 Administration UNCONTROLLED COPY WHEN DOWNLOADED 3 Aircraft EWIS Practices Job Aid 2.0 Background • Why the need for EWIS best practices Job Aid? – Accident/Incident Service History – Aging Transport Systems Rulemaking Advisory Committee (ATSRAC) – Enhanced Airworthiness Program for Airplane System (EAPAS) – EAPAS Rule Making Aircraft EWIS Best Practices Job Aid 2.0 Federal Aviation 4 Administration Historically, wiring and associated components were installed without much thought given to the aging aspects: • Fit and forget. -
We Listen to Make It Right. We Stay to Make It Real
RUAG at a glance We listen to make it right. We stay to make it real. A promise you can trust. One strategy – Combining civil and Focusing on International military applications core business growth three key areas To ensure it is strongly positioned in the face Space Space Switzerland of international competition – both now Civil Aero- structures and in the future – RUAG is pursuing its tried Air Europe and tested corporate strategy based on Aviation America three key areas: “Combining civil and Ammotec Military military applications”, “Focusing on core Land Asia / Pacific business” and “International growth”. Defence Market Divisions segments Brand promise We listen to make it right. We stay to make it real. A promise you can trust. Corporate values Collaboration – High performance – Visionary thinking Corporate purpose Ensuring the Swiss Armed Forces are properly equipped Competencies in aerospace, Net sales by market security and defence Switzerland 37 % 37 % RUAG develops trailblazing innovations and swiftly and professionally. Among other 0 % 20 % 40 % 60 % 80 % 100 % internationally sought-after cutting-edge things, clients benefit from RUAG’s vast technology in the aerospace sector as well expertise in security issues and from the Abroad 63 % as in security and defence. In 2016, RUAG expansion of its cyber-security, space and 63 % posted net sales of CHF 1,858 million, of aerostructure activities 0 % 20 % 40 % 60 % 80 % 100 % which 63 % was earned outside the Swiss home market. To continually meet the demand among its Civil and military applications customers and partners for unusual inno- The civil and military sectors are closely vations, RUAG invests roughly 9 % of sales Civil 57 % bound up with each other at RUAG. -
Leading the Charge We Put TBM 940 Speedster Through Its Paces for NBAA
15-21 October 2019 I flightglobal.com FLIGHT TEST Leading the charge We put TBM 940 speedster through its paces for NBAA £3.90 Wow, how? ACES high 42 Questions remain over defunct US Air Force boosts Collins Icelandic carrier’s comeback 13 with ejection seat deal 20 9 770015 371310 FLIGHT TEST Power of one Turboprop-single family has been a market success since launch in 1988, amassing sales of more than 900 units across three variants Daher has delivered a compelling offer for owner-flyers, with a range of enhancements on the TBM 940 providing an edge over the piston-twin segment. We put it through its paces MICHAEL GERZANICS POMPANO BEACH have allowed single-engined designs to make to be efficient. Airspace congestion, however, inroads into the twin-turbine segment. can make reaching optimum altitudes for jets he single-engined turboprop market The growth of the single-engined turbo- problematic, so their real-world range can be is populated by numerous aircraft of prop segment is based on the near-bulletproof shorter. Jets also have higher direct operating varying configurations. In broad reliability and scalability of the PT6 family. costs, however. T strokes, it can be broken down into This paradigm shift from piston-twins to tur- Runway performance and training require- two segments: fast, low-winged aircraft and bine-singles is conceptually on par with ex- ments are also two factors that fuel the single- slower, more spacious high-winged designs. tended twin-engine operations authorisations engined turboprop segment, because runway In the West, these diverse offerings share a all but killing off three- and four-engined civil length for turboprops is shorter than that single critical component – their engine. -
Pilatus Aircraft Ltd Annual Report 2017 Facts and Figures Key Figures at a Glance
PILATUS AIRCRAFT LTD ANNUAL REPORT 2017 FACTS AND FIGURES KEY FIGURES AT A GLANCE EBIT (CHF million) Total Sales (CHF million) 300 1500 250 1250 200 1000 150 750 100 500 EBIT AND TOTAL SALES (CHF MILLION) OF THE PILATUS GROUP 50 250 EBIT EBIT before R&D 0 0 Total Sales 2013 2014 2015 2016 2017 KEY INDICATORS OF THE PILATUS GROUP 2013 2014 2015 2016 2017 Total Sales (CHF million) 1014 1174 1122 821 986 Aircraft in Net Sales 112 127 121 117 115 Orders Received (CHF million) 410 561 1367 1087 1422 Order Book Value (CHF million) 1817 1226 1470 1744 2167 EBIT (CHF million) 145 200 191 89 135 EBIT as % of Sales 14.3 17.0 17.0 10.8 13.7 Cash Flow (net profit plus depreciation, CHF million) 143 195 178 95 133 Cash Flow as % of Sales 14.1 16.6 15.9 11.6 13.5 Investments in Fixed Assets (CHF million) 18 36 42 49 54 Investments in R&D (CHF million) 83 97 107 101 107 EBIT before R&D (CHF million) 228 297 298 190 242 EBIT before R&D as % of Sales 22.5 25.3 26.6 23.1 24.5 Net Assets (CHF million) 163 210 324 398 534 Inventories (CHF million) 688 754 639 485 647 Customer Advances (CHF million) 654 758 497 204 238 Pilatus Aircraft Ltd | Annual Report 2017 Number of Full- time Equivalents 2200 2100 2000 1900 1800 1700 1600 1500 EMPLOYEE GROWTH OF 1400 THE PILATUS GROUP Number of Full-time 1300 Equivalents 1200 1100 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017 1000 Number of Full-time 1363 1330 1395 1441 1576 1752 1882 1905 1961 2113 Equivalents 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017 BALANCE SHEET EXTRACT OF THE PILATUS GROUP 2013 2014 2015 2016 2017 Current Assets (CHF million) 1457 1768 1646 1259 1255 Long-term Assets (CHF million) 117 140 173 214 349 Total Assets (CHF million) 1574 1908 1819 1473 1604 Liabilities (CHF million) 929 1113 870 520 541 Equity (CHF million) 645 795 949 953 1063 Total Liabilities and Equity (CHF million) 1574 1908 1819 1473 1604 Equity Ratio in % 1 41.0 41.7 52.2 64.7 66.3 1 The PoC accruals and the customer advances are disclosed using the gross method (PoC = Percentage of Completion). -
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. -
Structural Integrity for Aging Airplanes
STRUCTURAL INTEGRITY FOR AGING AIRPLANES Michel Guillaume Zurich University of Applied Sciences, Centre for Aviation Keywords: Fatigue, Aging Airplanes, Structural Integrity Abstract is still considered to be critical based on the current review. Following the current risk assessment which The intense usage of Swiss military was based on ICAO standard, recommendations airplanes has a significant impact on fatigue were made to fly the P-3 till 5’000 flight hours life. The Swiss design life based on the OEM with no constraints but beyond 5’000 flight design goal is reduced. As a result, special hours further engineering investigation program has to be implemented to ensure the (damage tolerance analysis) and inspections are structural integrity over the aircrafts’ lifespan. definitely needed. The P-3 has real potential for An important task was to perform a full scale longer usage in civil conditions as the result of fatigue test that reflects the Swiss usage the less severe usage compared to the spectrum. The life of the Swiss military conservative original design spectrum from airplanes could thus be extended to meet the Pilatus. economic life goals – using fatigue tests – by more than 10 years for the Venom De Haviland DH-112 and the Mirage III. 1 Introduction Today former military planes like the Pilatus P3 (trainer), Venom, Vampire, Hunter and Mirage Up to 1958 no formal fatigue requirements III are civil registered. During operations in exist only static strength considerations plus military service, these planes had strict safety factors were expected to preclude fatigue requirements regarding inspection, mainte- damages. In 1954 two Comet I De Havilland nance and life time. -
Pilatus Wins Pc-21 Follow-Up Order from the Swiss Air Force
MEDIA RELEASE Stans, December 17, 2010 PILATUS WINS PC-21 FOLLOW-UP ORDER FROM THE SWISS AIR FORCE Pilatus Aircraft Ltd is delighted that the Swiss Air Force is to expand its successful PC-21 Jet Pilot Training System (JEPAS) with a follow-up order for two further PC-21 turboprop training aircraft with logistics and engineering services, plus another debriefing system. The contract with armasuisse, the Procurement and Technology Unit of the Swiss Federal Department of Defence, Civil Protection and Sport (DDPS), was signed in Stans on 17 December 2010, and is worth some 30 million Swiss francs. Delivery is scheduled for the first half of 2012. The Swiss Air Force took delivery of a fleet of six Pilatus PC-21 training aircraft in summer 2008. Since 2009, young Swiss Air Force pilots transfer directly to the F/A-18 fighter jet after basic training on the NCPC-7 and thorough instruction on the PC-21 Jet Pilot Training System (JEPAS). The PC-21's state-of- the-art cockpit is designed to simulate the functionalities of a modern combat aircraft and enables the operator to train pertinent skills at a very early stage of training. As a result, trainee pilots can safely bypass the expensive jet trainer phase. Oscar J. Schwenk, CEO and Chairman of the Board of Directors, comments as follows on the contract: "The Swiss Air Force has achieved its main goal in purchasing the PC- 21s, which is to train future military pilots to a higher standard in a shorter timeframe with the help of a high-performance, cost-effective training system designed to allow a direct transfer to the F/A-18 fighter jet. -
FAA-H-8083-3A, Airplane Flying Handbook -- 3 of 7 Files
Ch 04.qxd 5/7/04 6:46 AM Page 4-1 NTRODUCTION Maneuvering during slow flight should be performed I using both instrument indications and outside visual The maintenance of lift and control of an airplane in reference. Slow flight should be practiced from straight flight requires a certain minimum airspeed. This glides, straight-and-level flight, and from medium critical airspeed depends on certain factors, such as banked gliding and level flight turns. Slow flight at gross weight, load factors, and existing density altitude. approach speeds should include slowing the airplane The minimum speed below which further controlled smoothly and promptly from cruising to approach flight is impossible is called the stalling speed. An speeds without changes in altitude or heading, and important feature of pilot training is the development determining and using appropriate power and trim of the ability to estimate the margin of safety above the settings. Slow flight at approach speed should also stalling speed. Also, the ability to determine the include configuration changes, such as landing gear characteristic responses of any airplane at different and flaps, while maintaining heading and altitude. airspeeds is of great importance to the pilot. The student pilot, therefore, must develop this awareness in FLIGHT AT MINIMUM CONTROLLABLE order to safely avoid stalls and to operate an airplane AIRSPEED This maneuver demonstrates the flight characteristics correctly and safely at slow airspeeds. and degree of controllability of the airplane at its minimum flying speed. By definition, the term “flight SLOW FLIGHT at minimum controllable airspeed” means a speed at Slow flight could be thought of, by some, as a speed which any further increase in angle of attack or load that is less than cruise. -
Handley Page, Lachmann, Flow Control and Future Civil Aircraft
Handley Page, Lachmann, flow control and future civil aircraft John Green ABSTRACT Frederick Handley Page and Gustav Lachmann independently developed and patented the concept of the slotted wing as a means of increasing maximum lift. Subsequently they co-operated on the project and Lachmann joined Handley Page Ltd. The Handley Page slotted wing became used worldwide, generating substantial income for the company from use of the patent, and its descendents can be found on all modern transport aircraft. In the years following World War II, Lachmann led research at Handley Page to reduce drag by keeping the boundary layer laminar by surface suction. Handley Page led this field in the UK and developed a number of aircraft concepts, none of which came to fruition as full scale projects. However, looking to the future, the basic concept of laminar flow control holds out arguably the greatest potential of all technologies for reducing the fuel burn and environmental impact of future civil aircraft. 1. INTRODUCTION This is the story of two men of genius, Frederick Handley Page and Gustav Lachmann, Figs. 1 and 2. They were brought together by chance, as a result of having independently, and unknown to each other, invented and patented the same aerodynamic concept. During World War I they had been on opposite sides. Handley Page, who had been 28 at the outbreak of hostilities, established his company’s reputation as the designer of the large biplane bombers, the ‘bloody paralysers’ sought by the Royal Navy in 1914, that made a great contribution to the war effort in 1917 and 1918.