Descent and Approach Profile Management
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Enhancing Flight-Crew Monitoring Skills Can Increase Flight Safety
Enhancing Flight-crew Monitoring Skills Can Increase Flight Safety 55th International Air Safety Seminar Flight Safety Foundation November 4–7, 2002 • Dublin, Ireland Captain Robert L. Sumwalt, III Chairman, Human Factors and Training Group Air Line Pilots Association, International Captain Ronald J. Thomas Supervisor, Flight Training and Standards US Airways Key Dismukes, Ph.D. Chief Scientist for Aerospace Human Factors NASA Ames Research Center To ensure the highest levels of safety each flight crewmember must carefully monitor the aircraft’s flight path and systems, as well as actively cross-check the actions of each other.1 Effective crew monitoring and cross-checking can literally be the last line of defense; when a crewmember can catch an error or unsafe act, this detection may break the chain of events leading to an accident scenario. Conversely, when this layer of defense is absent the error may go undetected, leading to adverse safety consequences. Following a fatal controlled flight into terrain (CFIT) approach and landing accident (ALA) involving a corporate turbo-prop the surviving pilot (who was the Pilot Not Flying) told one of the authors of this paper, “If I had been watching the instruments I could have prevented the accident.” This pilot’s poignant statement is quite telling; in essence, he is stating that if he had better monitored the flight instruments he could have detected the aircraft’s descent below the minimum descent altitude (MDA) before it struck terrain. This pilot’s statement is eerily similar to a conclusion reached by the U.S. National Transportation Safety Board (NTSB) after an airliner descended through the MDA and impacted terrain during a nighttime instrument approach. -
Aircraft Engine Performance Study Using Flight Data Recorder Archives
Aircraft Engine Performance Study Using Flight Data Recorder Archives Yashovardhan S. Chati∗ and Hamsa Balakrishnan y Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA Aircraft emissions are a significant source of pollution and are closely related to engine fuel burn. The onboard Flight Data Recorder (FDR) is an accurate source of information as it logs operational aircraft data in situ. The main objective of this paper is the visualization and exploration of data from the FDR. The Airbus A330 - 223 is used to study the variation of normalized engine performance parameters with the altitude profile in all the phases of flight. A turbofan performance analysis model is employed to calculate the theoretical thrust and it is shown to be a good qualitative match to the FDR reported thrust. The operational thrust settings and the times in mode are found to differ significantly from the ICAO standard values in the LTO cycle. This difference can lead to errors in the calculation of aircraft emission inventories. This paper is the first step towards the accurate estimation of engine performance and emissions for different aircraft and engine types, given the trajectory of an aircraft. I. Introduction Aircraft emissions depend on engine characteristics, particularly on the fuel flow rate and the thrust. It is therefore, important to accurately assess engine performance and operational fuel burn. Traditionally, the estimation of fuel burn and emissions has been done using the ICAO Aircraft Engine Emissions Databank1. However, this method is approximate and the results have been shown to deviate from the measured values of emissions from aircraft in operation2,3. -
E6bmanual2016.Pdf
® Electronic Flight Computer SPORTY’S E6B ELECTRONIC FLIGHT COMPUTER Sporty’s E6B Flight Computer is designed to perform 24 aviation functions and 20 standard conversions, and includes timer and clock functions. We hope that you enjoy your E6B Flight Computer. Its use has been made easy through direct path menu selection and calculation prompting. As you will soon learn, Sporty’s E6B is one of the most useful and versatile of all aviation computers. Copyright © 2016 by Sportsman’s Market, Inc. Version 13.16A page: 1 CONTENTS BEFORE USING YOUR E6B ...................................................... 3 DISPLAY SCREEN .................................................................... 4 PROMPTS AND LABELS ........................................................... 5 SPECIAL FUNCTION KEYS ....................................................... 7 FUNCTION MENU KEYS ........................................................... 8 ARITHMETIC FUNCTIONS ........................................................ 9 AVIATION FUNCTIONS ............................................................. 9 CONVERSIONS ....................................................................... 10 CLOCK FUNCTION .................................................................. 12 ADDING AND SUBTRACTING TIME ....................................... 13 TIMER FUNCTION ................................................................... 14 HEADING AND GROUND SPEED ........................................... 15 PRESSURE AND DENSITY ALTITUDE ................................... -
GFC 700 AFCS Supplement
GFC 700 AFCS Supplement GFC 700 AFCS Supplement Autopilot Basics Flight Director vs. Autopilot Controls Activating the System Modes Mode Awareness What the GFC 700 Does Not Control Other Training Resources Automation Philosophy Limitations Modes Quick Reference Tables Lateral Modes Vertical Modes Lateral Modes Roll Hold Heading Select (HDG) Navigation (NAV) Approach (APR) Backcourse Vertical Modes Pitch Hold Altitude Hold (ALT) Glidepath (GP) Glideslope (GS) Go Around (GA) Selected Altitude Capture (ALTS) Autopilot Procedures Preflight Takeoff / Departure En Route Arrival/Approach Approaches Without Vertical Guidance Approaches With Vertical Guidance Revised: 02/08/2021 Missed Approach Autopilot Malfunctions/Emergencies Annunciations Cautions (Yellow) Warnings (Red) Emergency Procedures Manual Electric Trim Control Wheel Steering C172 w/ GFC700 Autopilot Checklist Piper Archer w/ GFC700 Autopilot Checklist Supplement Profile Addenda Autopilot Basics Flight Director vs. Autopilot ATP’s newer Cessna 172s and Piper Archers come factory-equipped with the GFC 700 Automatic Flight Control System (AFCS). The GFC 700 AFCS, like most autoflight systems, includes both a flight director (FD) and an autopilot (AP). The FD calculates the pitch and bank angles needed to fly the desired course, heading, altitude, speed, etc., that the pilot has programmed. It then displays these angles on the primary flight display (PFD) using magenta command bars. The pilot can follow the desired flight path by manipulating the control wheel to align the yellow aircraft symbol with the command bars. Alternately, the pilot can activate the AP, which uses servos to adjust the elevators, ailerons, and elevator trim as necessary to follow the command bars. Controls The AFCS is activated and programmed using buttons on the left bezel of the PFD and the multifunction display (MFD). -
Design and Analysis of Advanced Flight: Planning Concepts
NASA Contractor Report 4063 Design and Analysis of Advanced Flight: Planning Concepts Johri A. Sorerisen CONrRACT NAS1- 17345 MARCH 1987 NASA Contractor Report 4063 Design and Analysis of Advanced Flight Planning Concepts John .A. Sorensen Analytical Mechanics Associates, Inc. Moantain View, California Prepared for Langley Research Center under Contract NAS 1- 17345 National Aeronautics and Space Administration Scientific and Technical Information Branch 1987 F'OREWORD This continuing effort for development of concepts for generating near-optimum flight profiles that minimize fuel or direct operating costs was supported under NASA Contract No. NAS1-17345, by Langley Research Center, Hampton VA. The project Technical Monitor at Langley Research Center was Dan D. Vicroy. Technical discussion with and suggestions from Mr. Vicroy, David H. Williams, and Charles E. Knox of Langley Research Center are gratefully acknowledged. The technical information concerning the Chicago-Phoenix flight plan used as an example throughout this study was provided by courtesy of United Airlines. The weather information used to exercise the experimental flight planning program EF'PLAN developed in this study was provided by courtesy of Pacific Southwest Airlines. At AMA, Inc., the project manager was John A. Sorensen. Engineering support was provided by Tsuyoshi Goka, Kioumars Najmabadi, and Mark H, Waters. Project programming support was provided by Susan Dorsky, Ann Blake, and Casimer Lesiak. iii DESIGN AND ANALYSIS OF ADVANCED FLIGHT PLANNING CONCEPTS John A. Sorensen Analytical Mechanics Associates, Inc. SUMMARY The Objectives of this continuing effort are to develop and evaluate new algorithms and advanced concepts for flight management and flight planning. This includes the minimization of fuel or direct operating costs, the integration of the airborne flight management and ground-based flight planning processes, and the enhancement of future traffic management systems design. -
The Difference Between Higher and Lower Flap Setting Configurations May Seem Small, but at Today's Fuel Prices the Savings Can Be Substantial
THE DIFFERENCE BETWEEN HIGHER AND LOWER FLAP SETTING CONFIGURATIONS MAY SEEM SMALL, BUT AT TODAY'S FUEL PRICES THE SAVINGS CAN BE SUBSTANTIAL. 24 AERO QUARTERLY QTR_04 | 08 Fuel Conservation Strategies: Takeoff and Climb By William Roberson, Senior Safety Pilot, Flight Operations; and James A. Johns, Flight Operations Engineer, Flight Operations Engineering This article is the third in a series exploring fuel conservation strategies. Every takeoff is an opportunity to save fuel. If each takeoff and climb is performed efficiently, an airline can realize significant savings over time. But what constitutes an efficient takeoff? How should a climb be executed for maximum fuel savings? The most efficient flights actually begin long before the airplane is cleared for takeoff. This article discusses strategies for fuel savings But times have clearly changed. Jet fuel prices fuel burn from brake release to a pressure altitude during the takeoff and climb phases of flight. have increased over five times from 1990 to 2008. of 10,000 feet (3,048 meters), assuming an accel Subse quent articles in this series will deal with At this time, fuel is about 40 percent of a typical eration altitude of 3,000 feet (914 meters) above the descent, approach, and landing phases of airline’s total operating cost. As a result, airlines ground level (AGL). In all cases, however, the flap flight, as well as auxiliarypowerunit usage are reviewing all phases of flight to determine how setting must be appropriate for the situation to strategies. The first article in this series, “Cost fuel burn savings can be gained in each phase ensure airplane safety. -
N87- 19393 CE Bith Ab AUTCEETIC TESMINAL EM (BASA) 21 P CSCL 17Ti Unclas H1/06 43501 NASA Tech Ni Ca I Paper 2669
) A SIPSCLATICL EVALUATION GP A N87- 19393 CE bITH Ab AUTCEETIC TESMINAL EM (BASA) 21 p CSCL 17ti Unclas H1/06 43501 NASA Tech ni ca I Paper 2669 1987 A Simulation Evaluation of a Pilot Interface With an Automatic Terminal Approach System David A. Hinton Langley Research Center Hampt o n, Virginia National Aeronautics and Space Administration Scientific and Technical Information Branch Summary with a high potential for mistakes and has limited time to detect and correct any errors. A successful A piloted-simulation study was performed to arrival depends on the correct interpretation of ap- evaluate the pilot interface with an automatic termi- proach chart details, the correct setting of numerous nal approach system (ATAS). The ATAS was con- cockpit controls, and precise aircraft guidance near ceived as a concept for improving the pilot inter- the ground. face with high levels of automation. It consists of Automation in the form of an autopilot has been instrument approach data storage, automatic radio used to reduce pilot work load and improve pilot tuning, autopilot, autothrottle, and annunciation of performance in the terminal area. Research studies These components allow the ATAS flight status. (ref. 2) and airplane accident and incident reports to automatically execute instrument approaches, in- suggest, however, that the probability of pilot error cluding procedure turns, altitude changes, missed actually increases with an increase in automation, approaches, and holding patterns, without requir- partially because of design limitations of the pilot- ing the pilot to set up navigation radios or change machine interface. Conventional autopilot interfaces autopilot modes. provide the pilot with many opportunities to make The results show that fewer pilot blunders were errors because of the requirements to change radio made during approaches when using the ATAS than frequencies and autopilot modes as the approach when using a baseline, heading-select autopilot. -
Initiating a Missed Approach Below Mda
Issue No. 9 INITIATING A MISSED APPROACH BELOW MDA So there you are, on approach, inside the FAF and below MDA. You saw the runway and began descent, but it is raining, visibility is marginal and things are murky and scuddy (technical terms). Wind is directly across the runway at 11G18 and you are crabbing down, passengers are nervous. But you are holding the CDI in the center and maintaining control. Over the runway you go into your wing-low sideslip for the crosswind landing, things are going pretty well and then whoops a big gust destabilizes you so you abort the landing. Now what do you do, go missed or go around for another landing attempt? To provide some context, let’s attach the scenario to an interesting little airport, Andrews- Murphy Airport, NC (KRHP). The instrument approach procedure (IAP) and the takeoff minima and obstacle departure procedure are shown here. This airport is nestled in a scenic valley surrounded by mountains, which are quite close on the north. A topo map can be viewed here or just go to the TopoZone website and search for Andrews, NC, or go to the airport lat/long of 3512N/08352W. You will notice that the MDA is 2329 feet above the runway. Now remember that obstacle protection on a missed approach procedure is based on going missed at the MAP at MDA with a minimum climb gradient of 200 feet per nautical mile. No obstacle protection is assured when you go missed below MDA or past the MAP. In fact, you are not assured of obstacle protection even above MDA if the missed is initiated below MDA or after the MAP. -
Emergency Procedures C172
EMERGENCY PROCEDURES NON CRITICAL ACTION June 2015 1. Maintain aircraft control. Table of Contents 2. Analyze the situation and take proper action. C 172 3.Land as soon as conditions permit NON CRITICAL ACTION PROCEDURES E-2 GROUND OPERATION EMERGENCIES GROUND OPERATION EMERGENCIES E-2 Emergency Engine Shutdown on the Ground Emergency Engine Shutdown on the Ground E-2 1. FUEL SELECTOR -------------------------------- OFF Engine Fire During Start E-2 2. MIXTURE ---------------------------- IDLE CUTOFF TAKEOFF EMERGENCIES E-2 3. IGNITION ------------------------------------------ OFF Abort E-2 4. MASTER SWITCH ------------------------------- OFF IN-FLIGHT EMERGENCIES E-3 Engine Failure Immediately After T/O E-3 Engine Fire during Start Engine Failure In Flt - Forced Landing E-3 If Engine starts Engine Fire During Flight E-4 1. POWER ------------------------------------- 1700 RPM Emergency Descent E-4 2. ENGINE -------------------------------- SHUTDOWN Electrical Fire/High Ammeter E-4 If Engine fails to start Negative Ammeter Reading E-4 1. CRANKING ----------------------------- CONTINUE Smoke and Fume Elimination E-5 2. MIXTURE --------------------------- IDLE CUT-OFF Oil System Malfunction E-4 3 THROTTLE ----------------------------- FULL OPEN Structural Damage or Controllability Check E-5 4. ENGINE -------------------------------- SHUTDOWN Recall E-6 FUEL SELECTOR ------ OFF Lost Procedures E-6 IGNITION SWITCH --- OFF Radio Failure E-7 MASTER SWITCH ----- OFF Diversions E-8 LANDING EMERGENCIES E-9 TAKEOFF EMERGENCIES Landing with flat tire E-9 ABORT E-9 LIGHT SIGNALS 1. THROTTLE -------------------------------------- IDLE 2. BRAKES ----------------------------- AS REQUIRED E-2 E-1 IN-FLIGHT EMERGENCIES Engine Fire During Flight Engine Failure Immediately After Takeoff 1. FUEL SELECTOR --------------------------------------- OFF 1. BEST GLIDE ------------------------------------ ESTABLISH 2. MIXTURE------------------------------------ IDLE CUTOFF 2. FUEL SELECTOR ----------------------------------------- OFF 3. -
Takeoff and Landing Weather Minimums
Federal Aviation Administration, DOT § 121.651 field elevation for 15 minutes upon VFR weather minimums of § 91.155 of reaching an ETOPS Alternate Airport this chapter apply at those locations. and then conduct an instrument ap- [Doc. No. 6258, 29 FR 19222, Dec. 31, 1964 as proach and land. amended by Amdt. 121–39, 33 FR 4097, Mar. 2, (3) Fuel to account for APU use. If an 1968; Amdt. 121–206, 54 FR 34331, Aug. 18, 1989; APU is a required power source, the Amdt. 121–226, 56 FR 65663, Dec. 17, 1991] certificate holder must account for its fuel consumption during the appro- § 121.651 Takeoff and landing weather priate phases of flight. minimums: IFR: All certificate hold- ers. [Doc. No. FAA–2002–6717, 72 FR 1882, Jan. 16, 2007, as amended by Amdt. 121–348, 75 FR (a) Notwithstanding any clearance 12121, Mar. 15, 2010] from ATC, no pilot may begin a takeoff in an airplane under IFR when the § 121.647 Factors for computing fuel weather conditions reported by the required. U.S. National Weather Service, a Each person computing fuel required source approved by that Service, or a for the purposes of this subpart shall source approved by the Administrator, consider the following: are less than those specified in— (a) Wind and other weather condi- (1) The certificate holder’s operations tions forecast. specifications; or (b) Anticipated traffic delays. (2) Parts 91 and 97 of this chapter, if (c) One instrument approach and pos- the certificate holder’s operations sible missed approach at destination. specifications do not specify takeoff (d) Any other conditions that may minimums for the airport. -
Aic France a 31/12
TECHNICAL SERVICE ☎ : +33 (0)5 57 92 57 57 AIC FRANCE Fax : +33 (0)5 57 92 57 77 ✉ : [email protected] A 31/12 Site SIA : http://www.sia.aviation-civile.gouv.fr Publication date: DEC 27 SUBJECT : Deployment of CDO (continuous descent operations) on the French territory 1 INTRODUCTION After a trial and assessment period, the DSNA (French Directorate for Air Navigation Services) would now like to deploy continuous descent operations all across the French territory. When well performed by pilots, continuous descent reduces the effects of aircraft noise on the residential areas near airports and CO2 emissions. Continuous descent approach performance indicators for the residential community (reduction of noise linked to the elimination of superfluous sound levels) are or shall soon be available for all large French airports. The gains in CO2 shall be included in national greenhouse gas emission monitoring indicators. The DSNA will use this AIC to provide a set of recommendations and procedures on how to create, deploy and use this type of operation at national level, in order to help airlines perform successful CDO. Both the applications of the internationally standardized general principles and the French choices for fields which are not yet standardized are described in this AIC. 2 DEFINITION CDO (Continuous Descent Operations) is a flight technique which enables aircraft to have optimized flight profiles, either linked to instrument approach procedures and adapted airspace structures or air control techniques, by using reduced engine power and whenever possible, configurations limiting aerodynamic drag, in order to decrease the following: - noise nuisance in the areas surrounding the aerodromes, - emissions of gases into the atmosphere, - consumption of aircraft fuel. -
Aircraft Performance (R18a2110)
AERONAUTICAL ENGINEERING – MRCET (UGC Autonomous) AIRCRAFT PERFORMANCE (R18A2110) COURSE FILE II B. Tech II Semester (2019-2020) Prepared By Ms. D.SMITHA, Assoc. Prof Department of Aeronautical Engineering MALLA REDDY COLLEGE OF ENGINEERING & TECHNOLOGY (Autonomous Institution – UGC, Govt. of India) Affiliated to JNTU, Hyderabad, Approved by AICTE - Accredited by NBA & NAAC – ‘A’ Grade - ISO 9001:2015 Certified) Maisammaguda, Dhulapally (Post Via. Kompally), Secunderabad – 500100, Telangana State, India. AERONAUTICAL ENGINEERING – MRCET (UGC Autonomous) MRCET VISION • To become a model institution in the fields of Engineering, Technology and Management. • To have a perfect synchronization of the ideologies of MRCET with challenging demands of International Pioneering Organizations. MRCET MISSION To establish a pedestal for the integral innovation, team spirit, originality and competence in the students, expose them to face the global challenges and become pioneers of Indian vision of modern society . MRCET QUALITY POLICY. • To pursue continual improvement of teaching learning process of Undergraduate and Post Graduate programs in Engineering & Management vigorously. • To provide state of art infrastructure and expertise to impart the quality education. [II year – II sem ] Page 2 AERONAUTICAL ENGINEERING – MRCET (UGC Autonomous) PROGRAM OUTCOMES (PO’s) Engineering Graduates will be able to: 1. Engineering knowledge: Apply the knowledge of mathematics, science, engineering fundamentals, and an engineering specialization to the solution