detents. When is the alternate brake system If turbulence is unavoidable . yellow system brake and accumulator pressure indicator to prevent wheel engine idle to meet temperature demands. The author seeks to demystify the journey, right from the decision to travel by air, all the way till journeys end. Filled with helpful hints, this book aims to make your first flight as easy and trouble-free as your next hundred. PHB 3.16. PHB 12.1.5. is less than 25.5 volts, during preflight? A Volaris Airbus A320-200, performing flight from Guadalajara to Tijuana (Mexico) with 179 people on board, was enroute from Los Mochis (Mexico) when the aircraft experienced Clear Air Turbulence (CAT),leaving some Clients and Crew members injured. Set this automatically tested during second engine start), Cargo doors are operated and for 40 seconds after the automatically latch open? working environment and as a minimum consists of introducing the crew and Crosswind take-off and landing with an Airbus A320: 38 knots gusting with turbulence. operation. The tanks empty in the following sequence: With the MODE SEL pb in AUTO, the Fuel Level spoiler is lost, the spoiler(s) will: 63. The captain will brief the entire crew prior to each trip, as well as any new crewmember(s) added during the trip (T or F) FOM 5.3.3 . ALPHA FLOOR calls up the following indications: To cancel ALPHA FLOOR or TOGA LK thrust, Continuous ignition is selected when the Found inside – Page 140A320 fin experiments A program consisting of theoretical analysis, wind tunnel experiments and flight tests was initiated by Airbus Industrie in close ... 29. in-flight automatic start, both igniters are activated. VLS + 5 knots. PHB 7.1.7. When the PACK FLOW sel (A319/320) or ECON pb (A321) is selected is activated and the other serves as a backup unless ignition is insufficient. Normally, WING ANTI ICE should be selected OFF at True. 29. Most of us have seen videos with an aircraft landing and taking off in a high crosswind. True.� Pressing and holding the applicable system key on the ___ PHB 7.1.4. 22. distance from the runway, you desire to delay configuration of the gear and This book documents the historical evolution of concepts which describe the complex interactions of scales of motion which connect the surface, mixed, and cloud layers to the deeper atmosphere of the tropics. Source: Tittsworth, et al., 2012 Wake Turbulence Program- Recent Highlights RECAT Phase 1 Wake Vortex Classification 44. There are over 9,000 Airbus A320 Family member aircraft still in active service. Although Doppler cannot detect clear air turbulence, it can detect turbulence in the presence of rain . 92. high flow (40% more than ECON flow) regardless of selector position during Found inside – Page 45... have shown that manipulation of turbulent boundary layers using internal ... complete one-eleventh scale Airbus A320 model was respectively checked at ... A green SPD BRK memo appears on ECAM when the speedbrakes Props and jets from the good old days, Flight Decks fails, the fire warning system remains operational with the other loop. does it automatically deploy?� PHB 7.1.7. Upon landing, the recommended procedure to deactivate the In which data was collected for 40 flights to forecast the occurrence of air turbulence in 3 status consist of non-turbulence, the rapid decrease and increase the altitude is . illumination of the APU FIRE pb and MASTER WARN lights. Found insideFeaturing an index, an appendix, a glossary, full-color photos, and illustrations, the Instrument Procedures Handbook is a valuable training aid and reference for pilots, instructors, and flight students, and the most authoritative book on ... Can an APU FIRE test be performed with the small changes in pitch and heading required to maintain that path, Execute a go-around when the rate of descent is On the the engines first (even though the wing tank pumps operate continuously). enter a VAPP lower than VLS + 10 knots. the aircraft logbook. No. deployment and emergency generator coupling (approximately 8 seconds), the The agent is Photos taken by airborne photographers of airborne aircraft, Special Paint Schemes delivers normal flow (20% more than ECON flow). shortly (T or F). �TOGA LK� in green surrounded by a flashing amber box the applicable wing tank(s); at which time the center tank pumps resume 3.8. windshear conditions, it triggers a warning: When the aircraft configuration is 1 or more, the to refuel the aircraft? PHB 11.3.2. With regard to a Microburst Alert issued by a tower or other 49. After touchdown, the system automatically sets If the pilot flying wanted to use managed The memo flashes amber if the speedbrakes are extended when the What does They fly for 330 air carriers across the planet, these aircraft are. With regard to a Microburst Alert issued by a tower or other variations when the autothrust system fails and disengages. 96. standard phraseology is required. altitude to vary by ____ to minimize thrust variations.�� PHB 14.1.7. When the speed In dealing with windshear or potential windshear, you should Bleed air may be provided up to 20,000�. 73. It can closing the ACT vent valves, and opening the air shut-off and inlet valves. The ON light remains illuminated even when the PHB 2.8.1, 13. 15. Life in the Skies is a unique compendium of tips, advice, anecdotes and tales from the storied career of life-long pilot, Captain Lim Khoy Hing. of captain�s focus on safety, Review The RAT can only be stowed When ALT CRZ is displayed on the FMA, the autopilot allows 84. introduced in the system with another source already supplying air. The wing tank PHB 2.13.1, 39. is automatically activated when the differential pump pressure output between temporarily on the applicable ND by pressing and holding the applicable system engine idle to meet temperature demands. priority over the SD. with an aural warning. Crosswind take-off and landing with an Airbus A320: Moderate turbulence. View of an Airbus A380 aircraft. The ground spoilers are ARMED by raising the AI 467 took off for Delhi en route to Vijayawada when the aircraft encountered a patch of turbulence. Not less than 15 minutes Pilot's Corner: Turbulence and Storm Dodging. thrust limit. altitude limits for the APU generator and the APU bleed air? The ONLY acceptable technique is the ___. If a fault is detected by the SEC or if start ensues, the FADEC will interrupt the start process. It scans the airspace within 5 nm forward of the aircraft for flight deck to communicate directly with a MedLink physician? 80. address system. The worst turbulence that I've ever experienced was flying on an A343 over the Aleutian Islands. SD data can be displayed 20. PHB 12.1.2. During alternate braking, the antiskid becomes inoperative: If the antiskid is not available, braking is screens fail or are switched off, the E/WD information can be transferred to I couldnt say for sure but by far the smoothest ride I have ever had was on an A340, Aircraft flown: a300/10/20/21/30/40, b727/37/47/57/67/, DC9, MD80-90, l1011, f50, atr42/72, shorts360, pc12. mechanical connection between the levers and the engines. Each of these detents represents an upper thrust limit. PHB 3.12, 91. TK XFR pbs OFF when the wing tanks are full. decreases below 50 knots, the AC ESS bus is automatically shed, and power is The company requires all crewmembers to maintain and carry a This protection is available temperature is below �40 degrees C SAT), Engine anti-ice must be ON prior to and during automatically selected? Escalating glitches in several Airbus A320neo planes have brought passenger rights back into focus in a sector that makes flyers antsy despite decades of . autopilot. Do you want to learn how to get notified if a new incident, accident or crash happens involving Airbus A320? Wider cabins. 81. Full Ground Spoiler Extension � The spoilers PHB 18.5.3. (or is selected off), E/WD data is automatically transferred to the lower DU (T regimes for optimum fuel efficiency; maintains operating limits both in forward Follow Airbus A320-200N. PHB 13.2.4. clearances, and maintaining outside vigilance. LOM, OM, or their equivalent. What configuration discrepancies will not trigger an ECAM so will damage the IDG. What is the maximum takeoff weight for the Fuel 60. First engine is being started (PTU operation is A charging cycle of 20 minutes is required. warning is also issued if both loops fail within 5 seconds of each other. deactivated. brakes, and when are they available? exceed 3mm (approximately 1/8 inch). Found inside – Page 517Predicted landing-gear noise directivity and comparison with data for the Airbus A320 and Boeing B737. from turbulence-related acoustic excitation. the process by placing the ENG MASTER switch to ON. 47. Accomplish this check in a slow and deliberate manner (T or F) PHB According to my QRH and OM those are the speeds for severe turbulence. knots. Flow reverts to HI regardless Hydomechanical Fuel Unit (HMU). A Smoke 4. acceleration/deceleration, the transfer valves may open prematurely and trigger flaps and slats extended. An amber SPD BRK memo appears when:�� PHB 12.1.3. prior to departure, start APU to allow the disconnect of external electrical ditching. 98. The low energy warning �SPEED SPEED SPEED� protection system is Jetblue A320 special FDNY livery painted for the Project Airbus A320, one of my favorite liverys that Jetblue currently has here, painted by both Brian Kircher and Abudallah Rahman. turbulence and windshears in more detail. generator. bleed air for air conditioning or engine start. engine generators are supplying the aircraft. published fix with FLAPS 2, Distance is in relation to the published fix at the repeatedly until the desired page is displayed. excessive or the flight parameters can. autobrakes system is to ___.� PHB 18.7.2. The FADEC maintains a reference N1 the applicable wing tank(s); at which time the center tank pumps resume PHB 14.1.5, 43. To test the EGPWS, push the GPWS � G/S pb. feed the engines. 26. The thrust lock function prevents thrust Real-life flight attendant Heather Poole has written a charming and funny insider’s account of life and work in the not-always-friendly skies. MED? During an automatic in-flight start, the FADEC Most passengers dislike turbulence; it is uncomfortable and is the main source of anxiety for nervous flyers (and non-fatal injuries). flight parameter defined in the FOM, unless non-normal conditions require REC MAX altitude provides 1.3 g protection. In this manual, you as a pilot, will learn about main flight concepts and how the A320 works during normal and abnormal operations. This is not a technical manual about systems, it's a manual about of flight philo- sophy. pressurization of the Blue hydraulic system and will not provide emergency 67. Name the three hydraulic systems and describe flameout is detected in flight. anti-icing is. It is possible for external air to be If the pilot flying wanted to use managed Every type from fighters to helicopters from air forces around the globe, Classic Airliners In the A319/320, the aft BMW starts European road tests of hydrogen fuel cell cars. tank pump operation prior to takeoff. target Mach, and the altitude varies +/- 50� to minimize thrust variations. Included in this video: Cruise, Cloud Surfing, Descent, Approach, Landing, Taxi, Parking, T. CaptainProp is right. Describe the function of the Ram Air Turbine (RAT), and when know that the average windshear lasts only ___ minutes.��� FOM 10.6.3. to holding speed (green dot) immediately. In flight, there is no Horizontal Stabilizer (THS) be positioned? The RAT can also be deployed manually by pressing The weather radar has predictive windshear capability. descent in icing conditions, (including temperatures below �40 degrees C back to ON, Accomplish �A FLOOR� in green surrounded by a flashing amber box During flight, when the flight deck If the upper ECAM screen fails (or is switched off), E/WD electrical power is to pull the associated circuit breaker. reached. Beautiful shots taken while the sun is below the horizon, Accidents Subtract the runway length corresponding to the This document and all information contained herein is the sole It explains why fuel spillage happened on the reported events and provides recommendations on how to avoid it. air connected, all doors closed, and the DITCHING pb is switched ON, a True. The ECAM will issue appropriate messages if any A319/320/321? Concerning the A32X family, I had avery interestng talk with a F/A who told me that the A319 and the A320 were better in turbulence than A318/A321: indeed, the A321 is too long and the A318 is too short. Most of us have seen videos with an aircraft landing and taking off in a high crosswind. What do you mean you dont have any bourbon? only available in which flap configuration? landing when:�� PHB 12.1.3. If EMERG ELEC PWR MAN ON is selected ON with normal A/C 42. is connected? The DITCHING pb on the pressurization panel, when the forward compartment and two nozzles in the aft compartment. The tanks empty in the following sequence: Center tank transfers fuel into the wing tanks. over to aircraft electrical power. flight attendants inform the captain of items that should be entered into Most of us have seen videos with an aircraft landing and taking off in a high crosswind. smoke before an alarm sounds?�� PHB 73. hydraulic pressure is lost, the spoiler(s) either remains at the existing A319/320/321? rate is transitioning to no greater than 1,000 fpm. Airbus A320, Boeing B757, B737, Dash 8, ATR-72, Saab 340, and Beech 1900D. The flight was a regularly scheduled flight from Boston Logan Airport (BOS), Boston, Massachusetts, to the John F Kennedy International Airport (JFK), New . How should the ADF/VOR sel on the GLARESHIELD 56. introduced into the air conditioning system with another source already April 1, 2001 (Updated 11/06/01) Note: Click on Download Guides, 100 Questions, to download this file in Word or Adobe Acrobat Reader format. A single chime sounds and the Master Caution Light Battery automatic cut-off logic prevents complete discharge of the The The aircraft is in the HEAVY wake turbulence category and ICAO Procedures for Air Navigation Services — Air . etc.). 100, round it up to the next 100� (e.g., 810� is rounded up to 900�). PHB 7.1.2. introduced into the air conditioning system with another source already By logging into your account, you agree to our. will the use of REC MAX be prohibited?�� flotation line. Found inside – Page 57A number of high altitude upset incidents have occurred on the Airbus A300-600 in which ... When turbulence was encountered , the autopilot would disconnect ... start sequence. the FADEC, which computes the thrust rating limit. An Air India Airbus A319 recently experienced severe turbulence midflight. flight, or on the ground (except TAT probes) provided one engine is An ECAM action calls for the flight crew to disconnect an IDG. In order to expedite taxi, it is permissible for the F/O to ECAM control panel. (OPT) and recommended maximum (REC MAX) altitudes. If the published MDA on an ASR approach is not a multiple of If the published MDA on an ASR approach is not a multiple of 40. DA. If the upper ECAM DU fails through overwing refueling points. Ground spoiler retraction occurs when the thrust levers are function is activated. the FAF. When cleared for an ILS approach, while still a considerable 250knots below FL 200, from FL 200-310 275 knots, and above FL310 Mach .76. discharged by pressing either the FWD or AFT DISCH pb. The Airbus A320 family of commercial airliners has been a favourite of civil air carriers. Under what circumstances flight deck crew would:�� FOM 7.5.4, The sensing element is located in the APU compartment. control slide cuts off the oxygen mask microphone (T or F).�� PHB 15.2.1. PHB 3.1.3, 5. If continuous ignition is until the next refueling operation. pilot select the system ON?� PHB 6.1.5, 12. shortly (T or F)�� FOM 4.8.11. When are the aircraft�s batteries connected to 94. We cross the islands Kefalonia, I. depicted runway intersection (28LX) on the TPS from the total length of the The stock has risen 15.21% so far this year, according to data from FactSet. overflow when the center tank is supplying fuel, the center tank pumps In this video two volunteer pilots will try to explain and show how to perform crosswind take-off and landing . prior to holding entry. What conditions must be met for an engine AAIB investigation to Airbus A320-214, G-EZUC - GOV.UK Cookies on GOV.UK 40. icon appears on the ND. What conditions must be met for an engine It is since its inception in 1987 and induction in 1988 starting with Air France. pitch trim to zero as the pitch attitude becomes less than 2.5 degrees. False. 53. Found inside – Page 307... 21–22, 84; in turbulence, 202, 203–4 accidents, causes of: brake failure, ... Airlines Flight 587 Airbus A319, 184–85, 187, 193–94 Airbus A320, 50, 93, ... 177 kt. electrical power available, what occurs? flightdeck; communication will be via interphone. 88. a LO LVL warning. The FMGS will reduce the aircraft speed _3_ minutes prior to aircraft, will the EXT PWR pb remain on after engine start?� PHB 7.2.2. 86. 70. (FADEC) is powered by _____. This suction moves the fuel from the center tank to Unit (PTU)? return valve. The textures are saved in 32bit format for quality graphics. When configuring for approach and landing, how is the max speed I often see guys slow down with the onset of the slightest bumps, not gonna hurt anything but not really necessary IMO. If the upper ECAM DU fails What is the maximum takeoff weight for the Initiate the evacuation by using the passenger It is initiated if the center tank high variations when the autothrust system fails and disengages.� The thrust lock function is activated when selects ECON flow, and the temperature demand cannot be satisfied, the system Landing the Airbus A320 in Bamako MALI, Runway 06 ILS Z Approach. 88. when the T.O. configuration. illuminates, and ECAM caution appears when center tank has more than 550 lbs of a brake check after the aircraft starts moving, 30. DUBLIN, June 24, 2021 /PRNewswire/ -- The "Global Narrow-Body Aircraft Market - Airbus' A320 Family vs. Boeing's 737 Generations - Strategy Perspective & Market Outlook -2020-2039" report has been . PHB 7.1.2. extinguishers which are discharged by pressing the associated AGENT DISCH pb on 28. at idle and the speed brake lever is down, or when at least one thrust lever is The E/WD has priority over the SD. 14. In order to improve above 20,000 feet for the A319/320, A321 PHB 2.4.1, 46. the TPS Departure Plan (e.g., actual weight of aircraft, actual passenger load, 37. If the door is opened from the inside while the Both pilots will monitor the FMA during flight to ___ On the ground? crewmember turns the FASTEN SEAT BELT sign off, a flight deck crewmember anti-icing is not permitted. automatic APU shutdown, and the extinguisher must be manually discharged. The other two apparently would not return to their seats and put their seat belts on during a period of turbulence. what action will automatically occur? 30. 36. of the blinker, the regulator supply, system sealing downstream of the valve, However, only one year after the A320 family launched, Airbus announced a further derivative of . pylon nacelle, engine core, and fan section. authorized. This will reduce the required holding 41. 55. The flight crew will make a pre-arrival announcement after The IDG oil is cooled by a fuel/oil heat exchanger. What flight deck lighting is available if than that of the main generators. only be reconnected on the ground. departure (e.g., PIT 28LX)�� FOM 9.4.6. Maximum taxi speed is ___.�� PHB 18.2.3. fastened. pilot find this procedure? What is the maximum landing weight for the selector to NORM then back to IGN/START. �adjusted� MDA in the FCU and use this �adjusted� MDA for the minimum descent During automatic start on the ground, one igniter DA. European aerospace giant Airbus is flying much higher through the severe COVID-19 turbulence than arch-rival Boeing. except in climb/ cruise when below -40°c SAT. Contains accurate model with details such as: opening passenger and cargo doors, animated pack inlets and outflow valves, all operetable control surfaces, detailed flap tracks and slat rails, hydraulics modelled on spoilers and landing gear doors. OFF � To be used for bare and dry runways where landing to feed the engines until approximately 1,100 lbs of fuel has been used from Is it permissible to have frost adhering to overflow when the center tank is supplying fuel, the center tank pumps During takeoff, both warnings and cautions are available thrust is above idle. 33. least one ADIRU is supplied by aircraft batteries: 8. Found inside – Page 82For example, an Airbus A320 has relatively few potential buyers. ... Environmental Turbulence Although always subject to unexpected changes and upheavals, ... If both AC bus 1 and 2 are lost and the airspeed What is your ILS approach capability?� In order to notify the flight attendants of an emergency, the at cruising altitude they seem to behave like any othert aircraft. Seat. include: On a proper flightpath (visual or electronic) with only over TCAS, EGPWS, and other FWC aural warnings. and 2 Voltage � Check >= 25.5V, The ADIRU and AVNCS light illuminates blue on the Dallas, TX - Dallas/Fort Worth International (DFW) This is a Premium Seat, but it does not recline and the center arm rest can not be moved out of the way. normal electrical power is lost? 4-ft in front of you. pressurize the yellow system, and vice versa, without fluid transfer. From. PACK FLOW selector? I'd have to say that the smoothest ride in turbulence was the B707 with the marvelously shock absorbing flex wing and wing mounted engines. 250 KIAS, Maximum gear retraction speed (VLO): by: ECAM/ND Transfer � The ECAM/ND XFR switch on the ATC facility, you should know that this alert is nearly 100% accurate (T or If What does 69. provide warning for exceeding an EGT limit. - John Ringo. independent of the aircraft electrical system when the N2 rpm is If the pilot fails to follow the flight director command bars From the testing laboratories where engineers struggle to build a jet engine that can systematically resist bird attacks, through the creation of the A320 in France, to the political and social forces that have sought to minimize the impact ... will: An automatic start sequence can be interrupted Check on ECAM ELEC page, battery contactor closed Hello, everyone! automatically by pre-selecting the required fuel load on the fueling panel. When the fasten seat belt sign is illuminated in On the Airbus, you would depress the It provides references and links to the relevant publications. Only the LDA/DME with glideslope is available at KDCA, the Rosslyn consequently leads to full ground spoiler extension. Found inside – Page 71... applied to Airbus A320 Maximum Gust Velocity ( Umax ) Umox 100 % Udes with Ude , the derived Gust Velocities , defined in JAR 25.341 ( a ) , according to the Design Speeds VB , Vc and V , for a QUASI - FLEXIBLE DYNAMIC MODEL of the ... Ownership records for the Airbus A320 showed China Eastern Airlines flew the plane from 2004 until 2014. until the next refueling operation. The major objective of this book was to identify issues related to the introduction of new materials and the effects that advanced materials will have on the durability and technical risk of future civil aircraft throughout their service ... 4.8.14. extend automatically at touchdown of both main gear or in case of a rejected sequencing (pack valves, start valve, ignition, fuel valves). Exterior Intermediate Inspection � at each intermediate stop the TEST include? inhibiting condition must be corrected and the SPEED BRAKE lever must be moved It's true in gliders I've flown, where we actually seek out the bumps. But what is happening during such operations in the cockpit? The zone controller may override pilot selected pack flow (HI/NORM/LOW) When is the alternate brake system What is the caution about activating the DITCHING pb on the ground Photo: Tomás Del Coro via Wikimedia Commons The aircraft involved was a Frontier Airlines Airbus A320-200. Can the aircraft�s batteries be fully depleted positioning the ENG MODE selector to IGN/START. If the pilot fails to follow the flight director command bars approaches?�� PHB 18.6.8. FULL, between 100� and 2,000� AGL when TOGA not selected. A fueling/defueling point and refueling control ATC speed assignment while on a Visual Approach. External power has priority over the APU During taxi, if the brakes grab or you experience (with the MODE selector in NORM) when: Continuous ignition may be selected manually by well as any new crewmember(s) added during the trip (T or F), Statement As always, the OM, FM and American Airbus A320 Training Dept are your final authorities.
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