Backup Flight Instruments: They Stand up When Standards Stand Down

Total Page:16

File Type:pdf, Size:1020Kb

Backup Flight Instruments: They Stand up When Standards Stand Down PILOT’S GUIDE A Buyer’s Guide: Standalone Instruments Backup Flight Instruments: They Stand Up When Standards Stand Down By Dave Hig D o n ost pilots remember sig- curs: For pilots in IMC, loss of the atic spinning-iron gyros and suc- nificant events in their AI, for whatever cause, too often tion pumps. Mflying lives: their first solo; results in an unhappy outcome. Still, the Federal Aviation their first cross-country flight; The odds-on favorite for such a Administration requires modern check rides; and flights significant problem is the dry-air vacuum digital electronic panels to employ because they don’t fit the desir- pump dominant among aircraft a backup set of instruments able description of “uneventful.” suction systems. — often a compact, but old style, A newly minted instrument The related parallel failure of spinning-mass attitude indicator, pilot’s first trip in actual instrument the directional gyro (DG) adds to plus an airspeed indicator and meteorological conditions (IMC) the pressure of partial-panel fly- altimeter. Typically, the standby usually stays with him. And few ing in IMC. The single-point loss AI is electric and the aircraft events imprint as strongly as the of the DG, in contrast, doesn’t sports a secondary source of first time a primary instrument threaten attitude control to the electrical power. fails while flying inside the egg- degree of a loss of attitude indi- Owners of older aircraft have shell. Flying IMC, pretty much any cation; ditto for the turn direction options for adding attitude-indica- failure of a primary system or pri- and rate information delivered by tion redundancy to their panels, mary instrument makes the flight the electrically driven turn gyro, regardless of whether it’s a stan- “eventful.” whether a turn coordinator or turn dard six-pack panel, all glass or a Instrument pilots learn to use indicator. hybrid of glass and analog. the so-called “standard six-pack” Outside the ultimate IMC failure For the instrument pilot, incor- of instruments dominant in our crisis, that of an engine, no other porating standby instruments can predominantly analog panels component loss stresses pilot- help ensure an instrument failure — three of them gyro indicators ing skills and compounds the risk in IMC remains validly described — to successfully execute instru- equation of instrument flight like as “uneventful.” Several manu- ment flight. the loss of attitude indication in facturers offer standby instrument Most of our success hinges on IMC or, a close second, in night equipment created to relieve at our ability to become competent VMC. least the stress of an instrument by trusting a mechanical attitude failure. indicator (AI) in defiance of and Partial Panel: Some pilots opt to add a sec- ignoring completely the attitude Points for Difficulty ondary suction source to their air- indications of our inner-ear mech- One of the benefits of modern plane, a relatively low-cost option anisms. Loss of this AI, the most glass cockpits spins off, if you offering the dual benefit of keep- primary of our primary instrument will, from the shift to solid-state, ing the DG and the AI functioning. flight tools, greatly challenges our no-moving-parts sensors and Many pilots have added both a odds of success in IMC. electronic displays with miniscule secondary suction source and The track record from both real failure rates. These technologies a secondary, standby electricity life and objective research con- allow the elimination of problem- source to provide maximum sys- - 46 - P ilot ’ S G One of the benefits of modern glass cockpits spins off, if you A Buyer’s Guide: Standalone Instruments uide will, from the shift to solid-state, no-moving-parts sensors and electronic displays with miniscule failure rates. tem redundancy to their cockpits. driven AI a minor change — but power to maintain the integral But only a secondary indicator of it’s a minor piece of work with a battery’s charge. For standby attitude information can give an huge implication for the instrument instruments lacking the ability to instrument pilot the fullest hedge pilot facing the failure of a primary self-power, be sure you either against the possibly catastrophic AI. can shed load to keep the instru- outcome of a primary AI failure. The cockpit also must have an ment running until you’re down or In recognizing the lower prior- inclinometer — the trusty old slip/ that it’s on a standby buss to give ity of turn gyros in the instrument skid ball — to comply with the AC. it power priority. And don’t let a cockpit, the FAA issued Advisory By adding a second, alterna- shortage of mounting space hold Circular 91-75 several years ago tively powered AI — regardless of you back. to make adding redundant atti- whether or not it replaces a turn The industry has advisory tude indication easier than ever. gyro — the pilot essentially keeps circular AC 91-75, in large part, In essence, according to AC a full panel to work with in instru- because of the long-term efforts of 91-75, aircraft weighing no more ment conditions. Sporty’s founder Hal Shevers. He than 12,500 pounds, use a sec- Some important issues require petitioned the FAA for nearly two ond AI in place of a turn gyro, consideration when planning an decades to allow replacement of either an AI powered electrically upgrade to add standby instru- the turn coordinator with a backup or an air-powered unit with an ments to the panel. One of the pri- electric attitude indicator. available standby suction source mary considerations is, whenever In 2003, Shevers’ efforts finally — not as appealing a change as adding an instrument or system bore fruit with the issuance of AC going to an electric secondary AI. that increases electrical need, be 91-75, which in turn makes find- sure your generating system can ing space for a backup AI as easy StanDing By with meet this need. as replacing the turn coordinator Standby inStrumentS Independent power for standby or moving it to another location, In this “Buyer’s Guide,” we instruments provides the greatest allowing for a much safer panel examine equipment designed pri- redundancy, allowing the instru- layout in case of vacuum failure or marily to serve in a backup role ment or box to function for some failure of the primary AI. in today’s general aviation panel. limited time in the event of an Shevers’ efforts also helped In some cases, the products electrical-system failure — this is launch production of an electric described can serve as the pri- time a pilot needs to either find attitude indicator with inclinom- mary, allowing the aircraft owner visual conditions or on the ground eter, which was redesigned with to move older instruments else- as quickly as possible using the improvements and helped drive where in the panel and adding a nearest practical instrument- development of other standby layer of redundancy differently. approach option. products. Because turn gyros typically Even with its own standalone employ electric power, AC 91-75 power source, a self-powering makes swapping in an electrically standby device still needs ship’s Continued on following page… - 47 - STANDALONE INSTRUMENTS And company elements now Continued from page 47 incorporated into L-3 long have offered some of the industry stan- dards in standby instruments: J.E.T. standby AIs; AIM Gyros; and the GH-3000 series for busi- ness-turbine aircraft. Kelly manufaCturing Co. rC allen rCa 2600 CaStleBerry Digital horizon inStrumentS Introduced in April 2009 dur- model 300-14el ing the annual AEA International This is the attitude indicator Convention & Trade Show, this Sporty’s revived in Hal Shevers’ brand-new, digital-display horizon/ quest to convince the FAA that an attitude indicator allows the addi- electric AI was a safer choice than tion of an optional inclinometer, the turn coordinator found in stan- making it a candidate to replace trilogy eSi-1000 dard IFR panels. a turn gyro to serve as an electric L-3’s Trilogy ESI-1000, the first After the issuance of the AC, backup unit to a standard suction- solid-state integrated standby Shevers found no competitively powered AI. system created specifically for priced, high-value options that Designed around an all-solid- Part 23 aircraft, is designed as a would convince pilots to make the state digital sensor system, the backup for glass cockpit avionics. safer choice. RCA 2600 fits in the same stan- So complete in its capabilities, After combing the manufacturing dard 3-inch opening, or in a small- it’s easy to imagine some aircraft community with his specifications er opening for the 2-inch model. owners considering the Trilogy for and committing the marketing The RCA 2600 works on any a compact conversion to a glass power of Sporty’s, Shevers con- voltage from 9 to 32, and it draws primary flight display — defined vinced Castleberry Instruments a fraction of the current required these days as an electronic sys- to update and produce this AI. for conventional spinning-mass tem essentially serving to provide Sporty’s initial commitment was for electric gyros. all the information of the entire 1,000 units, which sold out almost Kelly’s newest RC Allen AI also standard six-pack in an IFR panel. immediately. weighs a fraction of a traditional The name, Trilogy, comes from Castleberry found the enterprise electric gyro, at 16 ounces for the the instrument’s integration of all launch profitable enough to con- 3-inch and 8.5 ounces for the 2- three functions the FAA requires tinue building the 300-14EL as a inch.
Recommended publications
  • Pitot-Static System Blockage Effects on Airspeed Indicator
    The Dramatic Effects of Pitot-Static System Blockages and Failures by Luiz Roberto Monteiro de Oliveira . Table of Contents I ‐ Introduction…………………………………………………………………………………………………………….1 II ‐ Pitot‐Static Instruments…………………………………………………………………………………………..3 III ‐ Blockage Scenarios – Description……………………………..…………………………………….…..…11 IV ‐ Examples of the Blockage Scenarios…………………..……………………………………………….…15 V ‐ Disclaimer………………………………………………………………………………………………………………50 VI ‐ References…………………………………………………………………………………………….…..……..……51 Please also review and understand the disclaimer found at the end of the article before applying the information contained herein. I - Introduction This article takes a comprehensive look into Pitot-static system blockages and failures. These typically affect the airspeed indicator (ASI), vertical speed indicator (VSI) and altimeter. They can also affect the autopilot auto-throttle and other equipment that relies on airspeed and altitude information. There have been several commercial flights, more recently Air France's flight 447, whose crash could have been due, in part, to Pitot-static system issues and pilot reaction. It is plausible that the pilot at the controls could have become confused with the erroneous instrument readings of the airspeed and have unknowingly flown the aircraft out of control resulting in the crash. The goal of this article is to help remove or reduce, through knowledge, the likelihood of at least this one link in the chain of problems that can lead to accidents. Table 1 below is provided to summarize
    [Show full text]
  • Use of the MS Flight Simulator in the Teaching of the Introduction to Avionics Course
    Session 1928 Use of the MS Flight Simulator in the teaching of the Introduction to avionics course Iulian Cotoi, Ruxandra Mihaela Botez Ecole de technologie supérieure Département de génie de la production automatisée 1100 Notre Dame Ouest Montréal, Qué., Canada, H3C 1K3 Introduction The course Introduction to avionics GPA-745 is an optional course in the Aerospace program given in the Department of Automated Production Engineering at École de technologie supérieure in Montreal, Canada. The main objectif of this course is the study of electronic avionics instrumentation installed in aircraft. In this course, the following chapters are presented : History of avionics, Methods of navigation and orientation, Pilot cockpit and board instrumentation, Communication systems, Radio-navigation systems, Landing systems, Engine signalization instruments, Central alarm systems, Maintenance systems and Warning systems. The presentation of the course in the class to the students is shown on PowerPoint slides and videos on modern aircraft such as Airbus and Boeing. Also, regarding the pilot induced oscillations a video film is provided from Bombardier Aerospace. However, the presentation of the course in the class may be improved and become more efficient grace to the use of MS Flight Simulator. The main idea of this paper is to show how the participation of the students in the class will be increased by use of the MS Flight Simulator. The use of the systems and the electronic board instrumentation will be shown with the help of the new flight simulations modules realized within the MS Flight Simulator. For each instrument, one module will be created and presented in the class, which will result in a more interesting course presentation, stimulating and dynamical from pedagogical point of view, than the theory of the course by use of PowerPoint.
    [Show full text]
  • Module-7 Lecture-29 Flight Experiment
    Module-7 Lecture-29 Flight Experiment: Instruments used in flight experiment, pre and post flight measurement of aircraft c.g. Module Agenda • Instruments used in flight experiments. • Pre and post flight measurement of center of gravity. • Experimental procedure for the following experiments. (a) Cruise Performance: Estimation of profile Drag coefficient (CDo ) and Os- walds efficiency (e) of an aircraft from experimental data obtained during steady and level flight. (b) Climb Performance: Estimation of Rate of Climb RC and Absolute and Service Ceiling from experimental data obtained during steady climb flight (c) Estimation of stick free and fixed neutral and maneuvering point using flight data. (d) Static lateral-directional stability tests. (e) Phugoid demonstration (f) Dutch roll demonstration 1 Instruments used for experiments1 1. Airspeed Indicator: The airspeed indicator shows the aircraft's speed (usually in knots ) relative to the surrounding air. It works by measuring the ram-air pressure in the aircraft's Pitot tube. The indicated airspeed must be corrected for air density (which varies with altitude, temperature and humidity) in order to obtain the true airspeed, and for wind conditions in order to obtain the speed over the ground. 2. Attitude Indicator: The attitude indicator (also known as an artificial horizon) shows the aircraft's relation to the horizon. From this the pilot can tell whether the wings are level and if the aircraft nose is pointing above or below the horizon. This is a primary instrument for instrument flight and is also useful in conditions of poor visibility. Pilots are trained to use other instruments in combination should this instrument or its power fail.
    [Show full text]
  • Instrument and Equipment
    PCAR PART 7 Republic of the Philippines CIVIL AVIATION REGULATIONS (CAR) PART 7 INSTRUMENT AND EQUIPMENT July 2021 Edition i U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 INTENTIONALLY LEFT BLANK PAGE July 2021 Edition ii U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition iii U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition iv U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 July 2021 Edition v U N C O N T R O L L E D C O P Y W H E N D O W N L O A D E D PCAR PART 7 RECORD OF AMENDMENTS Amendment No. Date Subject Incorporated By Original Issue 23 June 2008 Ruben F. Ciron First Amendment 21 March 2011 1. 7.2.9 Navigation Equipment Ramon S. Gutierrez Second Amendment 01 August 2013 Inserted vertical bars on the LT GEN William K previous amendments Hotchkiss III AFP (Ret) Third Amendment 31 October 2013 1.
    [Show full text]
  • FAA-H-8083-15, Instrument Flying Handbook -- 1 of 2
    i ii Preface This Instrument Flying Handbook is designed for use by instrument flight instructors and pilots preparing for instrument rating tests. Instructors may find this handbook a valuable training aid as it includes basic reference material for knowledge testing and instrument flight training. Other Federal Aviation Administration (FAA) publications should be consulted for more detailed information on related topics. This handbook conforms to pilot training and certification concepts established by the FAA. There are different ways of teaching, as well as performing, flight procedures and maneuvers and many variations in the explanations of aerodynamic theories and principles. This handbook adopts selected methods and concepts for instrument flying. The discussion and explanations reflect the most commonly used practices and principles. Occasionally the word “must” or similar language is used where the desired action is deemed critical. The use of such language is not intended to add to, interpret, or relieve a duty imposed by Title 14 of the Code of Federal Regulations (14 CFR). All of the aeronautical knowledge and skills required to operate in instrument meteorological conditions (IMC) are detailed. Chapters are dedicated to human and aerodynamic factors affecting instrument flight, the flight instruments, attitude instrument flying for airplanes, basic flight maneuvers used in IMC, attitude instrument flying for helicopters, navigation systems, the National Airspace System (NAS), the air traffic control (ATC) system, instrument flight rules (IFR) flight procedures, and IFR emergencies. Clearance shorthand and an integrated instrument lesson guide are also included. This handbook supersedes Advisory Circular (AC) 61-27C, Instrument Flying Handbook, which was revised in 1980.
    [Show full text]
  • Study of the Pilot's Attention in the Cabin During the Flight Auxiliary Devices Such As Variometer, Turn Indicator with Crosswise Or Other
    Journal of KONES Powertrain and Transport, Vol. 25, No. 3 2018 ISSN: 1231-4005 e-ISSN: 2354-0133 DOI: 10.5604/01.3001.0012.4309 STUDY OF THE PILOT’S ATTENTION IN THE CABIN DURING THE FLIGHT Mirosław Adamski, Mariusz Adamski, Ariel Adamski Polish Air Force Academy, Department of Aviation Dywizjonu 303 Street 35, 08-521 Deblin, Poland tel.: +48 261 517423, fax: +48 261 517421 e-mail: [email protected] [email protected], [email protected] Andrzej Szelmanowski Air Force Institute of Technology Ksiecia Boleslawa Street 6, 01-494 Warsaw, Poland tel.: +48 261 851603, fax: +48 261 851646 e-mail: [email protected] Abstract The pilot, while performing certain tasks or being in the battlefield environment works in a time lag. He is forced to properly interpret the information and quickly and correctly take action. Therefore, the instruments in the cabin should be arranged in such a way that they are legible and the operator have always-easy access to them. Due to the dynamics of the aircraft and the time needed to process the information by the pilot, a reaction delay occurs, resulting in the plane flying in an uncontrolled manner even up to several hundred meters. This article discusses the VFR and IFR flight characteristics, the pilot’s attention during flight, cabin ergonomics, and the placement of on-board instruments having a significant impact on the safety of the task performed in the air. In addition, tests have been carried out to determine exactly what the pilot’s eye is aimed at while completing the aerial task.
    [Show full text]
  • Flight Instruments - Rev
    Flight Instruments - rev. 9/12/07 Ground Lesson: Flight Instruments Objectives: 1. to understand the flight instruments, and the systems that drive them 2. to understand the pitot static system, and possible erroneous behavior 3. to understand the gyroscopic instruments 4. to understand the magnetic instrument, and the short comings of the instrument Justification: 1. understanding of flight instruments is critical to evaluating proper response in case of failure 2. knowledge of flight instruments is required for the private pilot checkride. Schedule: Activity Est. Time Ground 1.0 Total 1.0 Elements Ground: • overview • pitot-static instruments • gyroscopic instruments • magnetic instrument Completion Standards: 1. when the student exhibits knowledge relating to flight instruments including their failure symptoms 1 of 3 Flight Instruments - rev. 9/12/07 Presentation Ground: pitot-static system 1. overview (1) pitot-static system uses ram- air and static air measurements to produce readings. (2) pressure and temperature effect the altimeter i. remember - “Higher temp or pressure = Higher altitude” ii. altimeters are usually adjustable for non-standard temperatures via a window in the instrument (i) 1” of pressure difference is equal to approximately 1000’ of altitude difference 2. components (1) static ports (2) pitot tube (3) pitot heat (4) alternate static ports (5) instruments - altimeter, airspeed, VSI gyroscopic system 1. overview (1) vacuum :system to allow high-speed air to spin certain gyroscopic instruments (2) typically vacuum engine-driven for some instruments, AND electrically driven for other instruments, to allow back-up in case of system failure (3) gyroscopic principles: i. rigidity in space - gyroscopes remains in a fixed position in the plane in which it is spinning ii.
    [Show full text]
  • ASA Ch 3 the Instrument - Workbook Questions
    ASA Ch 3 The Instrument - Workbook Questions 1. The flight instruments are commonly grouped into basic categories based on the a. physical properties they rely on to work. b. whether they are used on the ground or in flight. c. Library of Congress catalog system, Dewey Decimal. 2. The basis of a conventional attitude indicator is a self-erecting a. vertical card mounted on a swivel. b. attitude flag arranged on a diagonal. c. gyroscope spinning on a vertical axis. 3. If the spin axis of the attitude indicator gyroscope moves off the vertical for some reason, the internal mechanism will realign it at a rate of approximately a. 3 degrees per second. b. 3 degrees per minute. c. 3 degrees per hour. 4. Occasionally, the miniature airplane on the attitude indicator may require repositioning while in level flight, due to changes in a. altitude (and corresponding air density). b. pitch attitude (associated with airspeed changes). c. the Earth’s gravitational forces. 5. If the attitude indicator experiences a failure of the power source, it will a. be unusable. b. continue to function if you maintain the same heading. c. still be a valid source of bank attitude. 6. Acceleration of the aircraft may cause the gyroscope to move off vertical, moving the horizon line a. toward the pilot. b. in the direction of the turn. c. to an incorrect position. 7. During a rapid acceleration, the horizon line will move down and the attitude indicator will indicate a false climb. a. True b. False 8. To avoid false indications when speeding up or slowing down, a pilot should increase the instrument scan rate a.
    [Show full text]
  • First Air Flight 6560 Struck a Hill About 1 Nautical Mile East of the Runway
    AVIATION INVESTIGATION REPORT A11H0002 CONTROLLED FLIGHT INTO TERRAIN BRADLEY AIR SERVICES LIMITED (FIRST AIR) BOEING 737-210C, C-GNWN RESOLUTE BAY, NUNAVUT 20 AUGUST 2011 The Transportation Safety Board of Canada (TSB) investigated this occurrence for the purpose of advancing transportation safety. It is not the function of the Board to assign fault or determine civil or criminal liability. Aviation Investigation Report A11H0002 Controlled flight into terrain Bradley Air Services Limited (First Air) Boeing 737-210C, C-GNWN Resolute Bay, Nunavut 20 August 2011 Summary On 20 August 2011, the Boeing 737-210C combi aircraft (registration C-GNWN, serial number 21067), operated by Bradley Air Services Limited under its business name First Air, was being flown as First Air charter flight 6560 from Yellowknife, Northwest Territories, to Resolute Bay, Nunavut. At 1642 Coordinated Universal Time (1142 Central Daylight Time), during the approach to Runway 35T, First Air flight 6560 struck a hill about 1 nautical mile east of the runway. The aircraft was destroyed by impact forces and an ensuing post-crash fire. Eight passengers and all 4 crew members sustained fatal injuries. The remaining 3 passengers sustained serious injuries and were rescued by Canadian military personnel, who were in Resolute Bay as part of a military exercise. The accident occurred during daylight hours. No emergency locator transmitter signal was emitted by the aircraft. Ce rapport est également disponible en français. Table of contents 1.0 Factual information ..................................................................................
    [Show full text]
  • Cirrus Airplane Maintenance Manual Model Sr22
    CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22 ATTITUDE AND DIRECTION 1. DESCRIPTION This section contains information pertaining to those portions of the system which use magnetic, gyro- scopic, and inertia forces. Included is the magnetic compass, turn coordinator, attitude indicator, and mag- netometer. (See Figure 34-001) For information pertaining to the horizontal situation indicator (HSI), see Dependent Position Determining. (Refer to 34-50) • Magnetic Compass The magnetic compass, mounted to the fuselage above the windshield, contains a circular compass card, visible through the compass case window, suspended in alcohol solution. The compass is equipped with compensating magnets and has two adjusting set screws, one for North-South adjust- ment and one for East-West adjustment. These set screws are located behind the access plate on the compass face. Light is integral and controlled by the instrument light rheostat on the bolster switch panel. • Turn Coordinator The turn coordinator is an electrically driven rate gyro and slip/skid coordinator which provides roll axis information to the pilot and autopilot. The turn coordinator is mounted either in the instrument panel to the left of the HSI (Serials 0002 thru 0434, 0435 thru 0820 w/o PFD) or behind the RH bolster panel (Serials 0435 thru 0820 w/ PFD, 0821 & subs). 28 VDC for roll rate gyro operation is supplied through the 2-amp TURN COORD #1 circuit breaker on the Essential Bus and the 2-amp TURN COORD #2 circuit breaker on the Main Bus 2. • Attitude Indicator The attitude indicator is an electrically driven gyro that displays a pictorial horizon and provides the pilot with a visual indication of the airplane’s pitch and roll attitude by sensing pitching and rolling movements about the airplane’s lateral and longitudinal axis.
    [Show full text]
  • G5 Electronic Flight Instrument Pilot's Guide for Certified Aircraft Blank Page SYSTEM OVERVIEW
    G5 Electronic Flight Instrument Pilot's Guide for Certified Aircraft Blank Page SYSTEM OVERVIEW FLIGHT INSTRUMENTS AFCS ADDITIONAL FEATURES INDEX Blank Page © 2017 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 5.00 or later. 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. Garmin AT, Inc.,2345 Turner Road SE, Salem, OR 97302, U.S.A. Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, Hampshire SO40 9LR U.K. Garmin Corporation, No. 68, Zhangshu 2nd Road, Xizhi District, New Taipei City, Taiwan 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. Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries. This trademark may not be used without the express permission of Garmin. December, 2017 190-01112-12 Rev. A Printed in the U.S.A.
    [Show full text]
  • Airplane Attitude Instrument Flying Using Analog Instrumentation
    Chapter 6, Section I Airplane Attitude Instrument Flying Using Analog Instrumentation Introduction Attitude instrument flying is defined as the control of an aircraft’s spatial position by using instruments rather than outside visual references. Today’s aircraft come equipped with analog and/or digital instruments. Analog instrument systems are mechanical and operate with numbers representing directly measurable quantities, such as a watch with a sweep second hand. In contrast, digital instrument systems are electronic and operate with numbers expressed in digits. Although more manufacturers are providing aircraft with digital instrumentation, analog instruments remain more prevalent. This section acquaints the pilot with the use of analog flight instruments. 6-1 Any flight, regardless of the aircraft used or route flown, Control Instruments consists of basic maneuvers. In visual flight, aircraft attitude The control instruments display immediate attitude and power is controlled by using certain reference points on the indications and are calibrated to permit those respective aircraft with relation to the natural horizon. In instrument adjustments in precise increments. In this discussion, the flight, the aircraft attitude is controlled by reference to term “power” is used in place of the more technically correct the flight instruments. Proper interpretation of the flight term “thrust or drag relationship.” Control is determined instruments provides essentially the same information that by reference to the attitude and power indicators. Power outside references do in visual flight. Once the role of each indicators vary with aircraft and may include manifold instrument in establishing and maintaining a desired aircraft pressure, tachometers, fuel flow, etc.[Figure 6-1] attitude is learned, a pilot is better equipped to control the aircraft in emergency situations involving failure of one or Performance Instruments more key instruments.
    [Show full text]