Flight International Test Pilot Peter on the Beechcraft King Air 350, Which Is Only Collins Flew This Model in 2008, Commenting: 1.24M X 1.32M

Total Page:16

File Type:pdf, Size:1020Kb

Flight International Test Pilot Peter on the Beechcraft King Air 350, Which Is Only Collins Flew This Model in 2008, Commenting: 1.24M X 1.32M FLIGINTERNHTAT IONAL 7-13 JUNE 2016 FLIGHT TEST PRECISION APPROACH Pilatus makes its Swiss army knife of the sky an even sharper ride FIN_070616_301.indd 1 29/06/2016 11:58 COVER STORY UPGRADED PC-12 POWERS AHEAD Pilatus launched its turboprop single in 1991 with modest sales expectations, but a quarter of a century and a string of updates later it is still in high demand; now, with engine update and other subtle but potent enhancements, its NG is sharper than ever MICHAEL GERZANICS DENVER more than 1,400 of the type have been sold. I flew this variant in 2004, and noted its As with most long-running serial produc- flight deck reminded me of early model Boe- hen the PC-12 was announced tion aircraft, the PC-12 has benefited from nu- ing 737-300s. Small screen electronic primary in 1989, manufacturer Pilatus merous improvements since launch. The first flight and horizontal situation displays were anticipated a market for PC-12 (SN101-400) had a Pratt & Whitney installed, but conventional round-dial air- approximately 200 aircraft. But Canada PT6A-67B, a conventional round-dial speed, altimeter and vertical velocity indica- Wwhile many were convinced it would be a cockpit and a maximum take-off weight tors remained. A Honeywell Bendix/King niche product, the versatile PC-12 has become (MTOW) of 4,100kg (9,030lb), later increased KMD-850 multi-function display and LCD one of the most successful turboprop singles to 4,500kg. The first major advance came with engine instrument system made it a poor in history; since its first flight in May 1991, SN401, which featured an updated cockpit. man’s glass cockpit. FIN_070616_026-030.indd 26 29/06/2016 11:50 PC-12NG FLIGHT TEST a composite five-bladed scimitar propeller. Pilatus has sold more Aside from giving the big single a rakish than 1,400 PC-12s appearance, it shortens the PC-12’s time to since first flight in 1991 climb by about 10%. Numerous minor aero- dynamic refinements help the PC-12 cleanly slice through the air. The propeller and aero tweaks combine in equal measure, according to Pilatus’s chief US pilot Jed Johnson, to give the aircraft a maximum cruise speed of 285KTAS (527km/h). The 5kt speed bump, Jon Youngblut/Pilatus over the previous model, slightly closes the Gerzanics (left) and Johnson: more glass and gap with the smaller and less cavernous more horsepower never go out of fashion Daher TBM900, which boasts a maximum cruise speed of 330KTAS. The blades are very thin, designed to have a Another notable upgrade was to the Primus uniform thrust/lift distribution along the Apex flight deck. Build 10 of the software span. If this sounds vaguely familiar, thank improved system functionality and capabili- the elliptical wing of Supermarine’s Spitfire. ties. One particularly useful addition is an The straight wing has an aspect ratio of FMS altitude temperature compensation approximately 10.27, with large fowler flaps capability. This allows vertical navigation that extend inward from the wing root under- approaches at extreme temperatures – more neath the fuselage. Pilatus made the flaps as than a nice-to-have if your destination is only large as possible to reduce stall speed. For served by GPS-based approaches. single-engined aircraft, US federal aviation Johnson was the safety pilot for my regulations dictate a stall speed of 61KIAS, to preview flight out of Rocky Mountain make a crash more survivable, but even with Metropolitan airport (KBJC) to and from the large flaps, the PC-12NG’s is 67KIAS (at Pagosa Springs (KPSO). He has been associat- MTOW). So, to attain certification, the US ed with Pilatus for nearly 20 years, and has Federal Aviation Administration allowed the distinction of having sold more than 150 Pilatus to use an equivalent level of safety PC-12s, amassing nearly 8,000h on the type. (ELOS): a 26g cockpit and 19g cabin seats, During the pre-flight safety inspection he which would dissipate energy in the event of pointed out NG features. To counter propeller- a forced landing. induced “P-factor,” the engine is mounted canted, 3° to the right and 3° downwards. CABIN CLASS COMFORT Vibrations from the PT6A-67P are dampened After we rounded the right wing tip, with its by polymer mounting bushings. As can be 10” radar pod, Johnson pointed out some of Jon Youngblut/Pilatus expected, these bushings get a workout, and the aerodynamic tweaks that helped boost the there are dedicated NACA ducts on the cowl- PC-12NG’s top end. Gap seals were added to With SN684, Pilatus increased the weight ing to direct cooling air to them. the trailing edge of the wing. Flap fairings to 4,700kg and made refinements to the flight Engine oil is checked through a sight gauge, were refined and external antennas moved control system. Production of this variant with an electronic level sensor relaying infor- and oriented to reduce drag. As with all ended with SN880. mation to the system’s multi-function display. PC-12s, flush rivets are employed forward of In 2008, Pilatus fielded the PC-12NG (Next The PT6 has proven to be an extremely relia- the fuselage’s aft pressure bulkhead. Rivets aft Generation), with production starting at ble engine, with an inflight shutdown rate of of the bulkhead have exposed heads as they SN1001. This was the most significant update are in an area of turbulent flow. On the left to the now well-established “niche” aircraft. The current NG is no doubt a side of the aircraft was a most impressive fea- The flight deck received a well-deserved better aircraft than the one I ture, the 1.35m x 1.32m (height x width) cargo makeover with the installation of a door that opens into the 9.34m3 cabin. The Honeywell Primus Apex glass flight deck. had flown 11 years earlier PC-12’s cargo door is larger than that available Fellow Flight International test pilot Peter on the Beechcraft King Air 350, which is only Collins flew this model in 2008, commenting: 1.24m x 1.32m. Its cabin is also taller and “The Apex system makes for a modern, well less than one every 651,126h (on a 12-month wider than the much more expensive type. laid-out, uncluttered cockpit.” Under the rolling average). The number-one cause of The King Air’s cabin, however, is 0.78m long- cowling, a more powerful PT6A-67P turbine engine failure has been oil starvation, fre- er than the PC-12’s and has a volume of 10m3. was installed, improving runway and cruise quently the result of an improperly closed oil While few PC-12 customers cross shop the performance. The Swiss are not renowned for fill cap – though Johnson says the -67P’s cap is King Air, the relative cabin size illustrates just being fashion leaders, but more glass and nearly impossible to install incorrectly. how big the PC-12 is. more horsepower are two things that will Should the statistically nearly impossible After closing the electrically actuated cargo never go out of style. happen, the PT6A-67P’s oil filler check valve door, we rounded the left wing and entered will prevent oil from being syphoned from an the aircraft via the forward door. The manual- PC-12NG IMPROVED open filler. ly-operated counterbalanced cabin entry door For 2016, Pilatus has further sharpened the While not as aggressively shaped as the has four integral steps and features LED light- Swiss army knife of aircraft. The biggest and propellers on the Airbus A400M, the PC-12’s ing. Opposite the entry door is a small cabinet most obvious enhancement is the addition of five-bladed prop was fascinating to look at. with a chemical flush toilet. With an endur- ❯❯ FIN_070616_026-030.indd 27 29/06/2016 11:51 COVER STORY PC-12NG SPECIFICATIONS a versatile utility vehicle. Up to nine standard hand and was intuitive to operate. Four but- seats can be fitted, and in the combi configura- tons on the multi-function controller, or a side Crew 2* tion nearly two-thirds of the cabin is available tap of the scroll wheel on the CCD, changed Passengers 9 max for cargo aft of four standard seats. The versa- the “active” window. The CCD allowed Wing span 16.28m tility of the PC-12 is further highlighted by its graphical flight plan changes en route to and Length 14.40m growing use as an air ambulance. According from KPSO, a capability I first experienced in Height 4.26m to Tom Aniello, vice-president of marketing Dassault’s EASy and Gulfstream’s PlaneView MTOW 4,740kg for Pilatus, there are approximately 125 PC- flight decks. The second was the wireless Engine 1 x P&WC PT6A-67P 12s in dedicated air ambulance service. In the capability resident in Apex Build 10. While Power 1,200shp (SL to ISA +35ºC) medical evacuation configuration, two litter not demonstrated during my visit, databases Take-off distance 793m patients can be carried in pressurised comfort. and canned flight plans can be updated rap- idly without a hard connection while on the Ceiling 30,000ft PRIMUS APEX FORWARD ground. A vertical situation display was a Range (HSC) 3,417km (MTOW, VFR reserves) The flight deck of my preview aircraft was handy addition to the flight deck displays. Landing distance 661m (MLW, SL, ISA) very similar to the one flown by Collins in The fourth and final feature that stood out was * SOURCE: Pilatus single pilot certificated 2008, but Pilatus and Honeywell have im- the Smartview synthetic vision system.
Recommended publications
  • Epic Performance for Tнe Entire King Air 200 Family
    BEECHCRAFT KING AIR B200GT EPIC PERFORMANCE FOR THE B200 ENTIRE KING AIR 200 FAMILY... 200 ...utilizing Swept Blade Technology Simply more of what you bought your King Air for! THE ELEMENTS OF RAISBECK’S 200-SERIES EPIC PERFORMANCE PACKAGE (Elements available separately) SWEPT BLADE TURBOFAN PROPELLERS RAM AIR RECOVERY SYSTEM ENHANCED PERFORMANCE LEADING EDGES DUAL AFT BODY STRAKES HIGH FLOTATION GEAR DOORS OPTIONAL CROWN WING LOCKERS Diaphragm Seal Particle Separator with flap Ice Shedder Turning Vane Flap Bypass Door Seal Benefits Benefits Benefits Benefits Benefits Benefits • Stunning ramp presence • Significantly increases climb and cruise • Cruise speeds and range are increased • Passenger ride quality is improved • Climb and cruise performance of standard- • FAA-certified to carry 600 pounds total cargo in • Quiet and virtually vibrationless operation performance in both normal and anti-ice • Stall speeds and characteristics are improved • Pilot control and handling qualities are gear King Airs is restored 17 cubic feet of luggage space from takeoff to touchdown operating modes • Air conditioning and cooling are more efficient enhanced • Cruise speed is increased 8 to 12 knots • Returns your cabin to your passengers • Certified around the world to meet the most • Protects against FOD—deployable for all • Outboard wing fatigue life is inherently • Air Minimum Control Speed is inherently depending on altitude • Handles skis, snowboards, camping and stringent regulations and noise requirements ground, takeoff and landing operations
    [Show full text]
  • Using an Autothrottle to Compare Techniques for Saving Fuel on A
    Iowa State University Capstones, Theses and Graduate Theses and Dissertations Dissertations 2010 Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft Rebecca Marie Johnson Iowa State University Follow this and additional works at: https://lib.dr.iastate.edu/etd Part of the Electrical and Computer Engineering Commons Recommended Citation Johnson, Rebecca Marie, "Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft" (2010). Graduate Theses and Dissertations. 11358. https://lib.dr.iastate.edu/etd/11358 This Thesis is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Graduate Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. Using an autothrottle to compare techniques for saving fuel on A regional jet aircraft by Rebecca Marie Johnson A thesis submitted to the graduate faculty in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Major: Electrical Engineering Program of Study Committee: Umesh Vaidya, Major Professor Qingze Zou Baskar Ganapathayasubramanian Iowa State University Ames, Iowa 2010 Copyright c Rebecca Marie Johnson, 2010. All rights reserved. ii DEDICATION I gratefully acknowledge everyone who contributed to the successful completion of this research. Bill Piche, my supervisor at Rockwell Collins, was supportive from day one, as were many of my colleagues. I also appreciate the efforts of my thesis committee, Drs. Umesh Vaidya, Qingze Zou, and Baskar Ganapathayasubramanian. I would also like to thank Dr.
    [Show full text]
  • Aircraft Service Manual
    Propeller Technical Manual Jabiru Aircraft Pty Ltd JPM0001-1 4A482U0D And 4A484E0D Propellers Propeller Technical Manual FOR 4A482U0D and 4A484E0D Propellers DOCUMENT No. JPM0001-1 DATED: 1st Feb 2013 This Manual has been prepared as a guide to correctly operate & maintain Jabiru 4A482U0D and 4A484E0D propellers. It is the owner's responsibility to regularly check the Jabiru web site at www.jabiru.net.au for applicable Service Bulletins and have them implemented as soon as possible. Manuals are also updated periodically with the latest revisions available from the web site. Failure to maintain the propeller, engine or aircraft with current service information may render the aircraft un-airworthy and void Jabiru’s Limited, Express Warranty. This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled. Should you have any questions or doubts about the contents of this manual, please contact Jabiru Aircraft Pty Ltd. This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled. ISSUE 1 Dated : 1st Feb 2013 Issued By: DPS Page: 1 of 32 L:\files\Manuals_For_Products\Propeller_Manuals\JPM0001-1_Prop_Manual (1).doc Propeller Technical Manual Jabiru Aircraft Pty Ltd JPM0001-1 4A482U0D And 4A484E0D Propellers 1.1 TABLE OF FIGURES ............................................................................................................................................. 3 1.2 LIST OF TABLES .................................................................................................................................................
    [Show full text]
  • Boeing 737 Postmaintenance Test Flight Encounters Uncommanded Roll-And-Yaw Oscillations
    FLIGHT SAFETY FOUNDATION Accident Prevention Vol. 55 No. 5 For Everyone Concerned with the Safety of Flight May 1998 Boeing 737 Postmaintenance Test Flight Encounters Uncommanded Roll-and-yaw Oscillations Fluid leaking from the cabin onto the yaw-damper coupler in the electronic-and-equipment bay affected electronic signals transmitted to the yaw-damper actuator and caused a dutch-roll oscillation. FSF Editorial Staff On Oct. 22, 1995, a Boeing 737-236 Advanced was • “Sufficiently conductive contaminant paths in straight-and-level flight at Flight Level (FL) 200 between certain adjacent pins had affected the (20,000 feet), at an indicated airspeed of 290 knots phase and magnitude of the signals transmitted when roll-and-yaw oscillations began. The flight crew to the yaw-damper actuator, thereby stimulating disengaged the autopilot, autothrottles and yaw a forced dutch-roll mode of the aircraft; damper, but the uncommanded roll-and-yaw oscillations continued. • “The location of the E&E bay — beneath the cabin floor in the area of the aircraft doors, galleys The crew declared an emergency and descended to and toilets — made it vulnerable to fluid ingress 7,000 feet. The oscillations stopped when airspeed was from a variety of sources; [and,] reduced to about 250 knots. After a satisfactory check of the aircraft’s low-speed handling characteristics, the • “The crew actions immediately following the crew returned to London (England) Gatwick Airport onset of the dutch-roll oscillations did not result and landed without further incident. in the disengagement of the malfunctioning yaw- damper system.” The U.K. Air Accidents Investigation Branch (AAIB), in its final report on the incident, identified four causal factors: The B-737, operated by British Airways, was built in 1980 and had accumulated 37,871 hours in service.
    [Show full text]
  • 1976 Cessna T210L Turbo Centurion II for Sale
    1976 Cessna T210L Turbo Centurion II Wolfe Aviation Business Aircraft Acquisitions, Appraisals, Sales and Service Verlyn Wolfe, PSCA ASA Accredited Senior Aircraft Appraiser Wolfe Aviation Stockton Metropolitan Airport (KSCK) 2050 East Sikorsky Street, Hangar 7 Stockton, California 95206 P.O. Box 31592, Stockton, California 95213-1592 Telephone: (209) 983-0117 Ext. 233 Cellular: (209) 607-9804 Email: [email protected] Wolfe Aviation believes the following information to be accurate but does not warrant nor guarantee the information accordingly; purchasers should rely upon their own inspection of the aircraft. There shall be no agreement between parties unless set forth in a written contract signed by buyer and seller. 1 Details: • Registration: N2803S • Serial Number: 21061049 • Airframe Time: 2,983 Hours total time since new • Engine: Teledyne Continental Motors TSIO-520-H4B sn: 217325-R; 285 HP 1,005 Hours since factory remanufacture; 1,400 hour TBO Compressions at last annual: #1 68, #2 75, #3 72, #4 68, #5 62, #6 60 Remanufactured by Teledyne Continental Motors 08/30/1994 Turbo overhauled by Main Turbo Systems, Inc. 08/08/2019 @ 83 hours ago 500 Hour magneto inspections c/w 01/26/2018 @ 86 hours ago Knisley Welding exhaust system installed 08/08/2018 • Propeller: Hartzell PHC-J3YF-1RF/F7691 three blade Scimitar propeller 27 Hours since new propeller installed; 2,000 hour TBO Propeller manufactured new by Hartzell Propeller 2018 New McCauley Propeller governor installed 10/21/2019 @ 24 hours ago • Inspection: Annual inspection
    [Show full text]
  • 11ADOBL04 December 2010
    11ADOBL04 December 2010 Use of rudder on Airbus A300-600/A310 (extracted from former FCOM Bulletin N°15/1 – Subject N°40) Reason for issue On February 8th, 2002, the National Transportation Safety Board (NTSB), in cooperation with the French Bureau d'Enquêtes et d'Analyses (BEA), issued recommendations that aircraft manufacturers re-emphasize the structural certification requirements for the rudder and vertical stabilizer, showing how some maneuvers can result in exceeding design lim- its and even lead to structural failure. The purpose of this Bulletin is to re-emphasize proper operational use of the rudder, highlight certification requirements and rud- der control design characteristics. Yaw control General In flight, yaw control is provided by the rudder, and directional stability is provided by the vertical stabilizer. The rudder and vertical stabilizer are sized to meet the two following objectives: Provide sufficient lateral control of the aircraft during crosswind takeoffs and landings, within the published crosswind limits (refer to FCOM Operating Limitations chapter). Provide positive aircraft control under conditions of engine failure and maximum asymmetric thrust, at any speed above Vmcg (minimum control speed - on ground). The vertical stabilizer and the rudder must be capable of generating sufficient yawing moments to maintain directional control of the aircraft. The rudder deflection, necessary to achieve these yawing moments, and the resulting sideslip angles place significant aerodynamic loads on the rudder and on the vertical stabilizer. Both are designed to sustain loads as prescribed in the JAR/FAR 25 certification requirements which define several lateral loading conditions (maneuver, gust loads and asymmetric loads due to engine failure) leading to the required level of structural strength.
    [Show full text]
  • B737-800 FTD System Failures
    IOS B737 FTD System Failures 0 Welcome The information contained within this document is believed to be accurate at the time of publication. However, it is subject to change without notice and does not represent a commitment on the part of Multi Pilot Simulations (MPS). Multi Pilot Simulations assumes no responsibility or liability for any errors or inaccuracies that may appear in this document. Boeing, Boeing 737 and Boeing 737NG are registered trademarks of Boeing Company. Airbus, Airbus A320 are registered trademarks of Airbus. All other trademarks mentioned herein are the property of their respective owners. All rights reserved. No rights or claims can be derived from data in this document. WELCOME-1 FSTD: B737 FTD 1 Index Applicability: - Failures marked with a @-sign in the failure title are available on FNPT II/MCC and FTD1/FTD2 FSTDs - Failures without a @-sign are available on FTD1/FTD2 FSTDs only 0 WELCOME .................................................................................................................................. 1 CONTACT INFORMATION ................................................................................................................................ 1 DOCUMENT OWNER ....................................................................................................................................... 1 REVISION HISTORY ......................................................................................................................................... 1 1 INDEX ...................................................................................................................................
    [Show full text]
  • Commercial Aftermarket Services About Moog
    Commercial Aftermarket Services About Moog Moog Inc. is a worldwide designer, manufacturer, and integrator of precision motion control products and systems. Over the past 60 years, we have developed a reputation for delivering innovative solutions for the most challenging motion control applications. As a result, we have become a key supplier to the world’s leading aircraft manufacturers and are positioned on virtually every platform in the marketplace – supplying reliable actuation systems that are highly supportable and add significant value for our customers. A key element of our success has been our customer focus. With Moog, you will find a team of people ready to deliver quality products and support services, all while being flexible and responsive to your needs. Our superior products and services directly reflect the creativity, work ethic and remarkable attention to purpose of our people. We exhibit our commitment by supporting our products throughout the life cycle of a platform, from idea conception and design of original parts, to aftermarket support and 24/7 service. With Moog, you will find a wide spectrum of products, services and support from a dedicated and trustworthy organization. Our culture, coupled with our commitment to our customers, process control and product innovation, will continue to drive the success of our company and yours. 2 Moog Products & Services Moog is the world’s premier supplier of high performance products and support services for commercial, military and business jet aircraft. We offer a complete range of technologies, an extensive heritage in systems integration, and stand behind our products with an unparalleled global customer support network.
    [Show full text]
  • National Transportation Safety Board Washington, Dc 20594 Aircraft
    PB99-910401 ‘I NTSB/AAR-99/01 DCA94MA076 NATIONAL TRANSPORTATION SAFETY BOARD WASHINGTON, D.C. 20594 AIRCRAFT ACCIDENT REPORT UNCONTROLLED DESCENT AND COLLISION WITH TERRAIN USAIR FLIGHT 427 BOEING 737-300, N513AU NEAR ALIQUIPPA, PENNSYLVANIA SEPTEMBER 8, 1994 6472A Abstract: This report explains the accident involving USAir flight 427, a Boeing 737-300, which entered an uncontrolled descent and impacted terrain near Aliquippa, Pennsylvania, on September 8, 1994. Safety issues in the report focused on Boeing 737 rudder malfunctions, including rudder reversals; the adequacy of the 737 rudder system design; unusual attitude training for air carrier pilots; and flight data recorder parameters. Safety recommendations concerning these issues were addressed to the Federal Aviation Administration. The National Transportation Safety Board is an independent Federal Agency dedicated to promoting aviation, raiload, highway, marine, pipeline, and hazardous materials safety. Established in 1967, the agency is mandated by Congress through the Independent Safety Board Act of 1974 to investigate transportation accidents, study transportation safety issues, and evaluate the safety effectiveness of government agencies involved in transportation. The Safety Board makes public its actions and decisions through accident reports, safety studies, special investigation reports, safety recommendations, and statistical reviews. Recent publications are available in their entirety at http://www.ntsb.gov/. Other information about available publications may also be obtained from the Web site or by contacting: National Transportation Safety Board Public Inquiries Section, RE-51 490 L’Enfant Plaza, East, S.W. Washington, D.C. 20594 Safety Board publications may be purchased, by individual copy or by subscription, from the National Technical Information Service.
    [Show full text]
  • Speed, Power and Control Depend on Innovation
    Discover Speed, Power and Control Depend on Innovation he latest innovation from Lancair is a new T2-seat “little brother” to the groundbreaking Mako — the Barracuda. Establishing a new standard for value, Barracuda offers high per- formance, operational economy and Lancair’s trademark aerodynamic style in a cost-effective package for two. nnounced at EAA AirVenture 2018, Barracuda is the latest design from Lancair’s legendary innovators. AA beautiful 2-place composite single with exceptional performance and style at an affordable price point. Speed, Power and Control Barracuda Specifications Start with Innovation. Base Engine Continental IO-550-N Horsepower 310 Power to climb. Speed to take you to new places. Innovation that Hartzell Propeller 3-blade “Scimitar” only Lancair can bring you. Three decades after revolutionizing the Landing Gear (Base Configuration) Fixed Mains, Retractable Nose world of two-seat aircraft, a rich history of unparalleled innovation Useable Fuel 65 gal and record-setting performance continues with the Lancair Gross Weight (lb) 2200 Barracuda. Updated and optimized from tip to tail, Barracuda is Empty Weight (lb) 1450 faster, more agile and quicker to build than its predecessors. Useful Load (lb) 750 Full Fuel Payload (lb) 360 It’s All About The Options. Glass Panel G3X Touch AmSafe Seat Belts optional You’ll enjoy a wealth of options to customize your Barracuda. Speed Brakes optional Speed Brakes from Precise Flight, Wheel Brakes from Beringer and Built-in Oxygen optional convenient access to the baggage area via an openable rear window Wingspan 25.5 ft are just a sample. Choose a Hartzell 3-blase ‘Scimitar’ propeller to Length 22 ft boost performance.
    [Show full text]
  • Flight Deck Solutions, Technologies and Services Moving the Industry Forward Garmin Innovation Brings Full Integration to Business Flight Operations and Support
    FLIGHT DECK SOLUTIONS, TECHNOLOGIES AND SERVICES MOVING THE INDUSTRY FORWARD GARMIN INNOVATION BRINGS FULL INTEGRATION TO BUSINESS FLIGHT OPERATIONS AND SUPPORT From web-based flight planning, fleet scheduling and tracking services to integrated flight display technology, head-up displays, advanced RNP navigation, onboard weather radar, Data Comm datalinks and much more — Garmin offers an unrivaled range of options to help make flying as smooth, safe, seamless and reliable as it can possibly be. Whether you operate a business jet, turboprop or hard-working helicopter, you can look to Garmin for industry-leading solutions scaled to fit your needs and your cockpit. The fact is, no other leading avionics manufacturer offers such breadth of capability — or such versatile configurability — in its lineup of flight deck solutions for aircraft manufacturers and aftermarket upgrades. When it comes to bringing out the best in your aircraft, Garmin innovation makes all the difference. CREATING A VIRTUAL REVOLUTION IN GLASS FLIGHT DECK SOLUTIONS By presenting key aircraft performance, navigation, weather, terrain routings and so on. The map function is designed to interface with a and traffic information, in context, on large high-resolution color variety of sensor inputs, so it’s easy to overlay weather, lightning, traffic, displays, today’s Garmin glass systems bring a whole new level of terrain, towers, powerlines and other avoidance system advisories, as clarity and simplicity to flight. The screens offer wide viewing angles, desired. These display inputs are selectable, allowing the pilot to add advanced backlighting and crystal-sharp readability, even in bright or deselect overlays to “build at will” the map view he or she prefers for sunlight.
    [Show full text]
  • Hondajet Model HA-420
    Honda Aircraft Company PILOT’S OPERATING MANUAL HondaJet Model HA-420 Original Issue: December 10, 2015 Revision B2: March 3, 2017 This Pilot’s Operating Manual is supplemental to the current FAA Approved Airplane Flight Manual, HJ1-29000-003-001. If any inconsistencies exist between this Pilot’s Operating Manual and the FAA Approved Airplane Flight Manual, the FAA Approved Airplane Flight Manual shall be the governing authority. These commodities, technology, or software were exported from the United States in accordance with the Export Administration Regulations. Diversion contrary to U.S. law is prohibited. P/N: HJ1-29000-005-001 Copyright © Honda Aircraft Company 2016 FOR TRAINING PURPOSES ONLY Honda Aircraft Company Copyright © Honda Aircraft Co., LLC 2016 All Rights Reserved. Published by Honda Aircraft Company 6430 Ballinger Road Greensboro, NC 27410 USA www.hondajet.com Copyright © Honda Aircraft Company 2016 FOR TRAINING PURPOSES ONLY Honda Aircraft Company LIST OF EFFECTIVE PAGES This list contains all current pages with effective revision date. Use this list to maintain the most current version of the manual: Insert the latest revised pages. Then destroy superseded or deleted pages. Note: A vertical revision bar in the left margin of the page indicates pages that have been added, revised or deleted. MODEL HA-420 PILOT’S OPERATING MANUAL Title Page ...................................................................... March 3, 2017 Copyright Page ............................................................. March 3, 2017 List of Effective Pages .................................................. March 3, 2017 Record of Revisions ..................................................... March 3, 2017 Record of Temporary Revisions ................................... March 3, 2017 List of Service Bulletins ............................................... March 3, 2017 Documentation Group .................................................. March 3, 2017 SECTION 1 – SYSTEMS DESCRIPTION Pages 1 – 232 ..........................................................
    [Show full text]