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Search inside document. Oi cheperiPage Ree. No, Page Chapter Rev. P2 P3 P4 P23 7. P25 7. The speed read from the airspeed indicator uncorrected for static source postion error. Indicated airspeed corrected for static source postion error. TAS, True Airspeed, Equivalent alcspead corrected for density deviation fom sea level standard conditions. The minimum speed on the ground at.
V1, Takeoff Speed, The speed to be used as a reference whether to reject orto continue the akeof, Vi-speeds are selected such that the folowing applies: sn engine faire is reongnises before V1, the takeoff must be rejected.
Wx Ha. Itis inuous Thrust MCT should be set. GW At OM itis sit So, itis possible to comply with SID requirement. Note: There is a hidden benefit due to fuel consumption during climb as gross weight decreases, climb gradient increases.
Integrated climb tables are established for max. The 1. Note: Reduce gross weight obtained from above graph by 4. For correction regarding landing speeds and distances see. Wve pages. In case of ira system failure occurring in fight and affecting the landing performance, the runway length to be considered for landing isthe actual landing distance without failure landing distance coeficient associated with the falure. For other pressure alltudes or increased approach speeds apply the associated corrections.
For pressure altitudes or increased approach speeds epply the assocated corrections. Quick reference LRC Tables Emergency Descent Tables. Information in the basic OM-8 is unchanged except as noted below. Do not select apsislaps below Kt. As runway weight charts show optimises takeoff weights, the weight reduction has to be applied whatever i the limitation, In dition the final segment limited TOW has to be checked.
The power setting for crit down will be Max Continuous. If a very small deflection of the elevator causes "a lot of g", the efficiency of the elevator is very high; A particular geographic scan has been developed in order to maximize the resource involvement in the spirit of ACRM. Any misunderstanding shall be clarified through questions.
This is the reason why the use of the stopwatch is recommended. During taxi, there are several issues: taxi roll and steering, braking. The figures are provided for A The turn application assumes symmetrical thrust and no differential braking. Nose radius: A Consequently if for any reason the aircraft moves forward while parking brake is ON, the parking brake must be released in order to get braking efficiency from the pedals on latest As, a modification provides the availability of pedal braking even if parking brake is ON.
The NWS will be effective till kts. In case of low visibility take off RVR down to m visual cues are the primary means to track the runway center line.
Apart from the ECAM actions required, the crew must consider: either to descend towards hotter areas, or to increase the Mach Number The modes and monitoring means are actually linked. He presses DES mode with managed Speed. All approaches shall then be flown similarly. Aircraft deceleration and configuration changes Managed speed is recommended. In all those cases, the pilot shall slam all thrust levers to TOGA. Indeed, the go around is a pitch dynamic maneuver, during which the bird is lagging behind due to the inertia of the aircraft.
The following particulars do apply to NPAs. The overall strategy of NPA completion is to fly it « ILS alike » with the same mental image or representation, and similar procedure. In Final approach: use FPA mode to set the aircraft on the final descent path. These are not necessarily monitored and thus not indicated. There is no capability degradation below ft alert height , due to the extremly low probability of a second failure within the remaining time. The PF should then notice a pitch up reaction of the aircraft.
It allows an efficient management of the thrust in gusts or longitudinal shears. Tailwind gust: IAS and speed trend arrow go down, target speed The system memorizes the attitude at 50 ft, and that attitude becomes the initial reference for pitch attitude control. As the VASI it provides an aiming point adjacent to the installation, and materializes a constant visual approach path to assist the pilot in the visual part of the approach.
MED is recommended. A tail pipe fire may occur at engine shutdown as well as engine start , due to an excess of fuel in the combustion chambre or an oil leak in the LP turbine race.
The ETOPS regulations are applicable to overwater or overland operations and to all revenue flights with passengers or freighters. Each authority defines its own means of compliance stating the method the airline has to use to demonstrate its competence. The following mnemonic can help. The purpose of RVSM is to allow to increase the traffic rates in saturated airspaces, while keeping up the same safety level.
Tires Under inflation is one of the major cause of tire failure; it heats up faster and may cause a breakdown of the rubber material. If the pilot moves the thrust levers out of the detent, the thrust is manually controlled and thus unlocked.
ATHR is recommended throughout the flight. The thrust is then manually controlled and ATHR is armed e. The choice of a mode is a strategic decision of the pilot. The modes are therefore manually engaged by the pilot; When the capture or tracking conditions occur, then the modes will change sequentially: e.
It leaves it to the pilot to change it as required. The GPS can be reselected later on the same page. Be careful with the bearing value you insert. The Fly by wire system accommodates for 3 sets of control laws depending upon the integrity and redundancy status of the computers, peripherals and of hydraulic generation. As a consequence, those maneuvers are achieved most naturally. The Flare, for example, requires a permanent AFT pressure on the stick from the pilot to achieve a progressive flare, and the derotation consists in smoothly flying the NLG down with a small aft pressure on the stick.
But the pilot is then the BEST to adapt the lateral trimming technique to the experienced circumstances. The degration is progressive depending upon the availability of remaining peripherals or computers. Thus if the PNF acts on the stick as well, both signals or orders are added. High AOA protection The high AOA protection gives full authority to the pilot to achieve consistently the best lift achievable by the aircraft, by pulling full aft stick in dangerous situations which is instinctive, while minimizing the risks of stalls or loss of control.
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Wve pages. In case of ira system failure occurring in fight and affecting the landing performance, the runway length to be considered for landing isthe actual landing distance without failure landing distance coeficient associated with the falure.
For other pressure alltudes or increased approach speeds apply the associated corrections. For pressure altitudes or increased approach speeds epply the assocated corrections. Quick reference LRC Tables Emergency Descent Tables. Information in the basic OM-8 is unchanged except as noted below. Do not select apsislaps below Kt. As runway weight charts show optimises takeoff weights, the weight reduction has to be applied whatever i the limitation, In dition the final segment limited TOW has to be checked.
The power setting for crit down will be Max Continuous. Uso slats and flaps, as necessary, to establish low speed conditions. Their sich thatthe aircraft must descend and remain below the folowing profi. Otnerwise, descend 6 a lower level to conte fight at LRC speed. NO Iv e00eN oa zee see [ove ve9 ove vee vox eee vse of 0. Gurpal Singh Chahal. Logan Doe. Vikram Kailthya. Brian Paul Govinda. Akali Own. Nik Martin. Aarohi Sood. Mark Busse. Khurram Naseem.
Joao Melo. Sunder Vijay. Luis Laria. Rohit Joshi. Js Thind. Amit Saha. Chattot and M. Popular in Aviation. Javier Romero. Muzej Vazduhoplovstva Beograd. Gladdy Francis Dcruz. Putu Budiastawa. Vholts Villa Vitug. Dwiky Satria. Bob Andrepont. Swapnil Karki. Gary Wright. Merrin John. Annex 07 - Aircraff Nationality and Registration Marks. Marco Lima. Kathy R allan. ATHR is recommended throughout the flight.
The thrust is then manually controlled and ATHR is armed e. The choice of a mode is a strategic decision of the pilot. The modes are therefore manually engaged by the pilot; When the capture or tracking conditions occur, then the modes will change sequentially: e. It leaves it to the pilot to change it as required.
The GPS can be reselected later on the same page. Be careful with the bearing value you insert. The Fly by wire system accommodates for 3 sets of control laws depending upon the integrity and redundancy status of the computers, peripherals and of hydraulic generation. As a consequence, those maneuvers are achieved most naturally. The Flare, for example, requires a permanent AFT pressure on the stick from the pilot to achieve a progressive flare, and the derotation consists in smoothly flying the NLG down with a small aft pressure on the stick.
But the pilot is then the BEST to adapt the lateral trimming technique to the experienced circumstances. The degration is progressive depending upon the availability of remaining peripherals or computers. Thus if the PNF acts on the stick as well, both signals or orders are added.
High AOA protection The high AOA protection gives full authority to the pilot to achieve consistently the best lift achievable by the aircraft, by pulling full aft stick in dangerous situations which is instinctive, while minimizing the risks of stalls or loss of control. In order to do so, the pilot needs to be advised that such phenomena will be encountered. NOTE: At landing, the reactive windshear is inhibited below 50 ft. When the boundaries of these two envelopes conflict with the terrain data, alerts are triggered.
Some RAs climb, increase climb … are inhibited if RA maneuver cannot be achieved safely. RAs are converted into TAs. GPWS, Stall warnings, windshear warning have priority. Else no evasive maneuver based solely on TA displayed on ND. The return velocity variance of the droplets is measured by the Doppler principle.
When the shift is beyond a given threshold, turbulence is detected. They get bigger and bigger and can be thrown several miles ahead of a dark storm cloud, in clear air. As they fall, they melt and you get a mixture of rain and hail. A change in TILT rapidly changes the shape and color of ground returns and eventually cause them to disappear which is not the case for weather.
Cold weather operation and flight in icing conditions A wing contaminated with ice has different characteristics from a clean wing. The hold over time is short time of anti ice fluid efficiency measured from beginning of application.
However if conditions make such landing necessary keep in mind that: The aircraft must be stabilized at minimum VAPP at runway threshold. The aircraft must overfly runway threshold at 50 ft, not more. This is normal. NOTE: Refer to chapter 24 for more details. Volcanic Ashes Volcanic ashes or dust are composed of very ABRASIVE particles which may cause engine surge, accumulation of volcanic material on turbine vanes and cause severe damage to aircraft surfaces most exposed to airflow.
Landing distance assume an even distribution of contaminant, the use of full pedal braking from touchdown onwards and an operative anti skid system.
The purpose of the ECAM is The FWC will thus display the failures in their order of criticality. ALL allows the SD pages to be successively displayed for review.
DOT asks " This happens when a failure occurs on Pressure and Temperature sensors within the engines. Depending upon the sensors which have failed, the engine can operate either in N1 rated or N1 unrated modes: if sensed EPR based on P2 — This malfunction may be caused by: either the loss of all AC GEN, or the loss of one engine and the failure of the opposite and APU generators, or the loss of both engines.
Thus landing gear must be extended at about ft AGL for landing. The general procedure recommended sequence is as follows: PF should be well declared. Lateral guidance is not tuned appropriately. Check whether altitude is reliable or not. If positive, the BIRD may be used. If negative, the bird is unreliable. This manual is also suitable for: A A A Print page 1 Print document pages. Cancel Delete.
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