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Use of Rudder on Boeing Aircraft
12ADOBL02 December 2011 Use of rudder on Boeing aircraft According to Boeing the Primary uses for rudder input are in crosswind operations, directional control on takeoff or roll out and in the event of engine failure. This Briefing Leaflet was produced in co-operation with Boeing and supersedes the IFALPA document 03SAB001 and applies to all models of the following Boeing aircraft: 707, 717, 727, 737, 747, 757, 767, 777, 787, DC-8, DC-9, DC-10, MD-10, md-11, MD-80, MD-90 Sideslip Angle Fig 1: Rudder induced sideslip Background As part of the investigation of the American Airlines Flt 587 crash on Heading Long Island, USA the United States National Transportation Safety Board (NTSB) issued a safety recommendation letter which called Flight path for pilots to be made aware that the use of “sequential full opposite rudder inputs can potentially lead to structural loads that exceed those addressed by the requirements of certification”. Aircraft are designed and tested based on certain assumptions of how pilots will use the rudder. These assumptions drive the FAA/EASA, and other certifica- tion bodies, requirements. Consequently, this type of structural failure is rare (with only one event over more than 45 years). However, this information about the characteristics of Boeing aircraft performance in usual circumstances may prove useful. Rudder manoeuvring considerations At the outset it is a good idea to review and consider the rudder and it’s aerodynamic effects. Jet transport aircraft, especially those with wing mounted engines, have large and powerful rudders these are neces- sary to provide sufficient directional control of asymmetric thrust after an engine failure on take-off and provide suitable crosswind capability for both take-off and landing. -
Comprehensive Guide
Comprehensive Guide 2014 Edition Portrait Of An Outstanding Performer................................... 4 1. TBM 900 Overview....................................................... 22 2. Technical Description................................................... 32 3. Fly in Style.................................................................. 46 4. Master of Performance................................................... 50 5. TBM vs Competitors........................................................ 56 6. Range Finder................................................................. 62 7. World Class Support....................................................... 70 8. Insuring your TBM.......................................................... 80 9. Testimonials.................................................................. 84 10. Contacts..................................................................... 92 TBM 900 A new TBM. Ahead of the firewall, everything is new: a redesigned cowling with more efficient inlet, a simplified plenum to improve airflow, easy nozzle access, inertial separator up to VMO and more. Everything is new... except the engine. The TBM 900 is still powered by the industry standard PT6A, but with all the other improvements, you get the equivalent of 80 more horsepower without increasing fuel consumption. And thanks to the new torque limiter, you can use all 850 horses right from takeoff. When you add this to Hartzell’s new composite five-blade propeller, the TBM 900’s sea-level standard takeoff distance improves -
Top Turboprop Series: We Compare Popular Pre-Owned Models
FOR THE PILOTS OF OWNER-FLOWN, CABIN-CLASS AIRCRAFT SEPTEMBER 2019 $3.95 US VOLUME 23 NUMBER 9 Top Turboprop Series: We Compare Popular Pre-Owned Models Five Questions The Latest on One Pilot’s with Corporate the Cessna Denali Introduction Angel Network & SkyCourier to Aerobatics Jet It US One year $15.00, two years $29.00 Canadian One year $24.00, two years $46.00 Overseas One Year $52.00, Two Years $99.00 Single copies $6.50 PRIVATE. FAST. SMART. EDITOR Rebecca Groom Jacobs SEPTEMBER2019 • VOL. 23, NO. 9 (316) 641-9463 Contents [email protected] EDITORIAL OFFICE 2779 Aero Park Drive 4 Traverse City, MI 49686 Editor’s Briefing Phone: (316) 641-9463 E-mail: [email protected] 2 A Career Shaped by Turboprops PUBLISHER by Rebecca Groom Jacobs Dave Moore PRESIDENT Position Report Dave Moore 4 What Makes a Turboprop CFO Safer? Answer: You Rebecca Mead PRODUCTION MANAGER by Dianne White Mike Revard PUBLICATIONS DIRECTOR Jake Smith GRAPHIC DESIGNER Marci Moon 6 TWIN & TURBINE WEBSITE 6 Top Turboprop Series: www.twinandturbine.com Pre-Owned Piper Meridian ADVERTISING DIRECTOR and Daher TBM 700C2 John Shoemaker Twin & Turbine by Joe Casey 2779 Aero Park Drive Traverse City, MI 49686 12 Five on the Fly with Phone: 1-800-773-7798 Corporate Angel Network Fax: (231) 946-9588 [email protected] by Rebecca Groom Jacobs ADVERTISING ADMINISTRATIVE COORDINATOR & REPRINT SALES 14 The Latest on the Betsy Beaudoin Cessna Denali and Phone: 1-800-773-7798 [email protected] SkyCourier ADVERTISING ADMINISTRATIVE by Rich Pickett ASSISTANT Jet It Erika Shenk 22 Intro to Aerobatics Phone: 1-800-773-7798 by Jared Jacobs [email protected] SUBSCRIBER SERVICES Rhonda Kelly Diane Smith Jamie Wilson Molly Costilow 22 Kelly Adamson P.O. -
2021 AOPA Turbine Pilot June
Farm to Capital First Year Only New Twice DC AERIAL PHOTOS p. 60 REAL-LIFE TURBINE LESSONS p. T-11 FACTORY-FRESH CESSNA 150 p. 50 TURBINE EDITION The Voice of General Aviation aopa.org/pilot | June 2021 | $10.95 June 2021 Beyond Chart Tabs PRECISE FIELD PERFORMANCE p. T-6 Wx Watch FAR-OUT FORECASTS p. 76 TBM Spot Landing Contests | Beyond Chart Tabs | Far-Out Forecasts | Far-Out Chart Tabs | Beyond Contests TBM Spot Landing TBM OWNERSHIP Fast Friends THE ORIGINAL TURBINE SINGLE SPEEDSTER p. T-14 FUN AND SAFETY AT SPOT LANDING CONTESTS p. T-16 aopa.org + Redefining Flight Safety and Performance Photo: Chris Rose The Daher TBM 940 sets the standard for performance, while also taking safety to new levels. After incorporating envelope protection and autothrottle to make loss of control virtually impossible, we have now introduced HomeSafeTM, the emergency autoland system that automatically returns the plane to a runway if the pilot becomes incapacitated. Not to mention the most reliable turboprop in its class, built-in engine safeguards and automatic transmission of critical engine data back to the manufacturer after each flight. Daher, where safety comes first. Speak to a Daher expert: TBM (Americas) (954) 993-8477 (Internaitonal) +33 5 62 41 77 88 www.tbm.aero SAFE TURBINE PILOT QUICK LOOK Daher TBM 700 Fast, efficient personal travel machine BY PETER A. BEDELL DAHER/SOCATA’S TBM 700 is now 30 years old and, despite being the first pressurized turbine single, it’s still the reign- ing speed champ of its category. The 900-series TBMs in production today top out at 330 KTAS. -
Runway Excursions Study
NLR-CR-2010-259 Executive summary A STUDY OF RUNWAY EXCURSIONS FROM A EUROPEAN PERSPECTIVE Report no. NLR-CR-2010-259 Author(s) G.W.H. van Es Report classification UNCLASSIFIED Date May 2010 Knowledge area(s) ) Vliegveiligheid (safety & security) Problem area on the European context. The Vliegoperaties Safety statistics show that study was limited to civil Luchtverkeersmanagement(A runway excursions are the most transport type of aircraft (jet and TM)- en luchthavenoperaties common type of accident turboprop) involved in Descriptor(s) reported annually, in the commercial or business Runway safety European region and worldwide. transport flights. Overrun Veeroff Description of work Results and conclusions Runway friction Causal and contributory factors The final results are used to RTO that may lead to a runway define preventive measures for excursion are identified by runway excursions. analysing data of runway excursions that occurred during the period 1980-2008. The scope of this report includes runway excursions that have taken place globally with a focus UNCLASSIFIED NLR-CR-2010-259 NLR Air Transport Safety Institute Anthony Fokkerweg 2, 1059 CM Amsterdam, UNCLASSIFIED P.O. Box 90502, 1006 BM Amsterdam, The Netherlands Telephone +31 20 511 35 00, Fax +31 20 511 32 10, Web site: http://www.nlr-atsi.nl NLR-CR-2010-259 A STUDY OF RUNWAY EXCURSIONS FROM A EUROPEAN PERSPECTIVE G.W.H. van Es This report may be cited on condition that full credit is given to NLR, the author and EUROCONTROL. This report has also been published as a EUROCONTROL report. This document has been given an NLR report identifier to facilitate future reference and to ensure long term document traceability. -
National Transportation Safety Board Aviation Accident Final Report
National Transportation Safety Board Aviation Accident Final Report Location: Morristown, NJ Accident Number: ERA12FA115 Date & Time: 12/20/2011, 1005 EST Registration: N731CA Aircraft: SOCATA TBM 700 Aircraft Damage: Destroyed Defining Event: Loss of control in flight Injuries: 5 Fatal Flight Conducted Under: Part 91: General Aviation - Personal Analysis Although the pilot filed an instrument flight rules flight plan through the Direct User Access Terminal System (DUATS), no evidence of a weather briefing was found. The flight departed in visual meteorological conditions and entered instrument meteorological conditions while climbing through 12,800 feet. The air traffic controller advised the pilot of moderate rime icing from 15,000 feet through 17,000 feet, with light rime ice at 14,000 feet. The controller asked the pilot to advise him if the icing worsened, and the pilot responded that he would let them know and that it was no problem for him. The controller informed the pilot that he was coordinating for a higher altitude. The pilot confirmed that, while at 16,800 feet, "…light icing has been present for a little while and a higher altitude would be great." About 15 seconds later, the pilot stated that he was getting a little rattle and requested a higher altitude as soon as possible. About 25 seconds after that, the flight was cleared to flight level 200, and the pilot acknowledged. About one minute later, the airplane reached a peak altitude of 17,800 feet before turning sharply to the left and entering a descent. While descending through 17,400 feet, the pilot stated, "and N731CA's declaring…" No subsequent transmissions were received from the flight. -
G1000® Are Registered Trademarks of Garmin Ltd
® G1000 Integrated Flight Deck Cockpit Reference Guide System Software 0719.03 or later FLIGHT INSTRUMENTS ENGINE & AIRFRAME SYSTEMS NAV/COM/TRANSPONDER/AUDIO PaNEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES ABNORMAL OPERATION ANNUNCIATIONS & ALERTS APPENDIX INDEX Copyright © 2007-2008 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0719.03 or later for the Socata TBM 850. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138 Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. Tel: 44/0870.8501241 Fax: 44/0870.8501251 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099 Web Site Address: www.garmin.com Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. -
The Influence of Wing Loading on Turbofan Powered Stol Transports with and Without Externally Blown Flaps
https://ntrs.nasa.gov/search.jsp?R=19740005605 2020-03-23T12:06:52+00:00Z NASA CONTRACTOR NASA CR-2320 REPORT CXI CO CNI THE INFLUENCE OF WING LOADING ON TURBOFAN POWERED STOL TRANSPORTS WITH AND WITHOUT EXTERNALLY BLOWN FLAPS by R. L. Morris, C. JR. Hanke, L. H. Pasley, and W. J. Rohling Prepared by THE BOEING COMPANY WICHITA DIVISION Wichita, Kans. 67210 for Langley Research Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • NOVEMBER 1973 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA CR-2320 4. Title and Subtitle 5. Reoort Date November. 1973 The Influence of Wing Loading on Turbofan Powered STOL Transports 6. Performing Organization Code With and Without Externally Blown Flaps 7. Author(s) 8. Performing Organization Report No. R. L. Morris, C. R. Hanke, L. H. Pasley, and W. J. Rohling D3-8514-7 10. Work Unit No. 9. Performing Organization Name and Address The Boeing Company 741-86-03-03 Wichita Division 11. Contract or Grant No. Wichita, KS NAS1-11370 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Contractor Report National Aeronautics and Space Administration Washington, D.C. 20546 14. Sponsoring Agency Code 15. Supplementary Notes This is a final report. 16. Abstract The effects of wing loading on the design of short takeoff and landing (STOL) transports using (1) mechanical flap systems, and (2) externally blown flap systems are determined. Aircraft incorporating each high-lift method are sized for Federal Aviation Regulation (F.A.R.) field lengths of 2,000 feet, 2,500 feet, and 3,500 feet, and for payloads of 40, 150, and 300 passengers, for a total of 18 point-design aircraft. -
PDF Version August September 2010
IDWEST FLYERAUGUST/SEPTEMBER 2010 M AGAZINE Published For & By The Midwest Aviation Community Since 1978 midwestflyer.com Turbine Comfort Zone If you want to stay in your comfort zone, but while cruising at 31,000 feet and with an approach speed slow enough to land on most runways, the TBM 850 from DAHER-SOCATA is for you. Nearly as quick as a light jet, but at a fraction of the cost, the TBM 850 offers substantially more payload and range. Featuring outstanding dependability and ease of handling, the TBM 850 is powered by the Pratt & Whitney PT6A turbine engine and equipped with state-of-the-art Garmin G1000 avionics. The TBM 850’s luxuriously-appointed cabin and distinctive European styling raise the bar even further. We invite you to take the controls for an unforgettable experience, flight after flight. Contact your nearest TBM 850 distributor: www.tbm850.com Tel: (954) 893-1400 (USA) +33 5 62 41 73 01 (International) Delivering performance since 1911 AD OSHKOSH.indd 1 09/07/10 20:17 H ONDAJET MIDWEST Turbine Comfort Zone If you want to stay in your comfort zone, but while cruising at 31,000 feet and with an approach speed slow enough to land on most runways, the TBM 850 from DAHER-SOCATA is for you. Nearly as quick as a light jet, but at a fraction of the cost, the TBM 850 offers substantially more payload and range. Featuring outstanding dependability and ease of handling, the TBM 850 is powered by the Pratt & Whitney PT6A turbine engine and equipped with state-of-the-art Garmin G1000 avionics. -
Crosswind Landings What Could Possibly Go Wrong? by STEVE KROG
STEVE KROG COMMENTARY / THE CLASSIC INSTRUCTOR Crosswind Landings What could possibly go wrong? BY STEVE KROG CROSSWIND LANDINGS CONTINUE to cause sweaty palms and mild SETTING THE STAGE cases of indigestion whenever discussed among the local gang of We began our flights working from the turf hangar pilots. As many of you have heard me say before, hours of runway, which provided us with a good pleasure flying are missed by many due to a fear of crosswinds. starting point from which to establish a base I recently was working on crosswind landings with a longtime and to measure progress. Other than experi- pilot who was relatively new to tailwheel flying. He had contacted encing a few bounces during the three-point me expressing a desire to become a better, more relaxed, and confi- landing, all went well. The wheel landings dent tailwheel pilot, as he was experiencing a lot of anxiety were equally safe and smooth. His ability to whenever he flew his recently acquired Cub. handle the Cub safely on turf was evident, especially with no crosswind. Then it was time to switch runways and CROSSWIND LANDINGS begin tackling crosswind landings, in this case a crosswind from left to right at approx- imately 30 degrees and 10 mph. It was immediately apparent that his anxiety was WIND building at the mention of a crosswind land- ing. A method I like to use in this situation is to do a crosswind takeoff and closely observe the pilot’s control inputs. He made all the right control movements, but they were very stiff and almost always a split-second behind the aircraft when they were needed. -
2014-05 Flyer
FLIGHT TEST FLIGHT TEST Daher-Socata TBM 900 Daher-Socata TBM 900 Jacques Callies reports on the Tarbes-based manufacturer’s secret project: a complete aerodynamic makeover of the already successful TBM 850. The new TBM 900 is set to become the company’s sole model hree years ago, in the utmost secrecy, the founder of DynAero, known for his creative Daher-Socata gave its design office a talent and mastery of composite materials, which challenge: look at how to improve on the he had demonstrated when manufacturing TBM 850. No need to start from scratch lighter aircraft. Twhen you already have a high-performance We knew that the jet evaluation had served aeroplane which is loved by its pilots and owners, only to confirm that it was not the path to go and which continues to enjoy healthy sales. The down, but that was about it. So on 6 March we result is the new TBM 900. And while the name were quite taken aback to discover that a team of doesn’t mean that the engine develops 900hp, its 125 people had worked on a very different performance in comparison with the TBM 850 project: improving the TBM 850 to make it a might make you think otherwise, as we shall see. more efficient and spectacular aircraft on several Despite regular visits to the factory in Tarbes, in levels, namely performance, handling, noise and the foothills of the Pyrenees, the secret was well carbon footprint. kept. Everyone thought that Daher-Socata was It’s tempting to make a comparison with the working on a completely different aircraft. -
AVIATION WEEK Pilot Report: Daher Socata TBM 900 We Fly the Fastest Civil Single-Engine Turboprop May 22, 2014 Fred George | Shownews
AVIATION WEEK Pilot Report: Daher Socata TBM 900 We fly the fastest civil single-engine turboprop May 22, 2014 Fred George | ShowNews A 325-kt cruise speed may seem slow by light jet standards, but it’s pretty impressive when the aircraft you’re flying only is burning 400 lb. per hour. Daher-Socata’s TBM 900, the latest iteration of the TBM 700, is at least 14 kt faster than TBM 850, based on our flying both aircraft back-to-back. It also needs less runway and climbs faster, plus it uses less fuel and is quieter both inside and outside. Last Thursday, we strapped into the left seat of TBM 900 S/N 1014 with Daher- Socata’s chief pilot Stéphane Jacques at the firm’s plant in Tarbes, France, for a two- hour evaluation of the myriad improvements wrapped into the new model. The preflight walk-around revealed much about what makes the aircraft faster and quieter than its predecessor. Most obvious are the aircraft’s new composite Hartzell five- blade prop and winglets. The Hartzell five-blade incorporates the latest 3-D aero computer modeling, one that analyzes the airflow of the prop around the nose of the aircraft. Socata officials say they looked closely at an advanced prop from MT-Propeller but opted for the Hartzell because the aircraft cruises 3 to 5 kt faster. The winglets were designed in-house at Socata. Their principal benefit is drag reduction at the higher angles of attack encountered during takeoff and climb. They also were added for aesthetic value.