A330B2 for quiz.docx

The manufacturing is a Trans- national process, structured around key manufacturing units; each unit is responsible for producing a complete section of the aircraft The A340 and A330 use the same assembly line since most of the A/C systems are similar. The popular widebody Airbus A330 Family is a m...

The manufacturing is a Trans- national process, structured around key manufacturing units; each unit is responsible for producing a complete section of the aircraft The A340 and A330 use the same assembly line since most of the A/C systems are similar. The popular widebody Airbus A330 Family is a modern, versatile and highly efficient product line that includes the latest state-of-the- art technology. Airbus is powering this jetliner family into the future with the A330neo (new engine option) - continuing a reputation for ongoing innovation by incorporating new Rolls-Royce Irent 7000 engines along with Sharklet wingtip devices. On- board, passengers benefit from the smart and modern Airspace by Airbus design, which provides more personal space and comfort in a quiet environment. The A/C general information presentation is divided into: ⁃ the reference axes. ⁃ the A C dimensions ⁃ the section and station numbers ⁃ the zone presentation ⁃ the access panels The structure elements are identified according to the following reference axes. The reference (station 0) for all structural measurements in the X- avis are installed FWD of the A C nose. These are the major A C reference axes. Each major part of the AC, related to the production sharing, receives a section number. Here the fuselage sections are shown. The station number is the distance in centimeters of a cross section from a reference point. Here are the fuselage station numbers, which are the section boundaries The A/C is divided into zones in order to make easy the maintenance and the component location. Each area is identified by major zones hundreds). The A/C is divided into 8 major zones: - 100: Lower Fuselage -200: Upper Fuselage, - 300: Stabilizers -400: Nacelles/Pylons - 500: Left Wing - 600: Right Wing. - 700: Landing Gear, - 800: Doors. ATA 05 of the AMM lists the zonal inspection requirements for the AC. An identification is given to the items below- ⁃ Access doors for the maintenance, ⁃ Service doors, ⁃ Fairings. ⁃ Removable access panels of the radio rack. ⁃ Removable floor panels ⁃ Removable partition panels ⁃ Removable ceiling panels, ⁃ Removable sidewall panels NOTE: Electrical panels are not included here since a special rule applies to them. UIZ IAl The first three digits identify the smallest zone in which the door/panel is found. The first letter or identifier shows the position of the access doors and panels in a logical sequence: ⁃ Forward to aft, for the fuselage ⁃ Inboard to outboard, for the wing and horizontal stabilizer, ⁃ Bottom to top, for the vertical stabilizer. The second letter or locator identifies the access door or panel in its relation to the aircraft:: T =TOP (upper surface),. B= Bottom (lower surface), An identification is given to the items below: ⁃ Access doors for the maintenance, ⁃ Service doors, -Fairings ⁃ Removable access panels of the radio rack, -Removable floor panels, -Removable partition panels ⁃ Removable ceiling panels, ⁃ Removable side wall panels NOTE: Electrical panels are not included here since a special rule ap to them. The first three digits identify the smallest zone in which the door/panel is found The first letter or identifier shows the position of the access doors and panels in a sequence: ⁃ Forward to aft, for the fuselage ⁃ Inboard to outboard, for the wing and horizontal stabilizer ⁃ Bottom to top, for the vertical stabilizer. The second letter or locator identifies the access door or panel in its relation to the aircraft:: MAJOR ZONE I = TOP (upper surface). B =Bottom (lower surface), L=Left hand. R=Right hand ⁃ Internal. F Floor panel. W= Sidewall panel. C- Ceiling panel diadards When all the letters of the alphabet have been used up for the first letter (identifier) sequence starts again with letter A and the other letters below are used for the locator. I = TOP (upper surface),. B =Bottom (lower surface), L=Left hand, R=Right hand. Z-Internal F= Floor panel W= Sidewall panel C= Ceiling panel When all the letters of the alphabet have been used up for the first letter (identifier). the sequence starts again with letter A and the other letters below are used for the locator U=Top (upper surface), D-Bottom (lower surface), P=Lef hand S =Right hand G = Floor panel, X = Sidewall panel, Y = Ceiling panel. NOTE: The letters I and 0 are not used. Special Identification Rules: Passenger/crew doors, cargo doors, landing gear doors: only the zone number is used since each is a zone in itself. Blow-out doors and vents have no identification number. MA I Access doors and panels in the fuselage centerline have the identification of the LH zone. Similar doors on opposite sides of the aircraft have the same letter identifier even though zone numbers will be different, he placards and mark A door on a zone limit is identified with the number of the zone from which it is removed. If an access door or panel is in more than one zone, the lowest zone number applicable is used. The three jacks have to be operated together. As soon as the jacking operation is finished, position the tail safety stay to stabilize the aircraft. The three jacking points, when equipped with jacking pads, are used to lift the aircraft. The forward jacking point is located forward of the Nose Landing Gear (NLG). The wing jacking points are located outboard of the Main Landing Gear (MLG). You can lift the aireraft at the forward jacking point only, with the main wheels on the ground. A tail safety stay can be positioned at the rear of the aireraft after jacking to stabilize the aircraft landing gear has jacking points: ⁃ 2 jacking points located on each MLG - 1 jacking point located on the NLG. The open air jacking operation is limited if the wind velocity exceeds permissible values which depend on aurcratt gross weight and center of gravity position, In any condition. the aircraft must be pointing upwind. There are two main procedures to level the aircraft: ⁃ Quick leveling with Air Data Inertial Reference System (ADIRS), ⁃ Quick leveling with a spirit level in cabin or cargo compartment You can weigh the aircraft with ⁃ The aircraft on jacks ⁃ The aircraft on its wheels ⁃ The aircraft on landing gear jacks Before towing the aircraft. ⁃ Make sure that the safety devices are installed on the landing gears ⁃ Make sure that the dimension H of the Nose Landing Gear (NLG) is never greater than 310 mm. ⁃ On the nose wheel steering deactivation electrical box, set the ground towing control lever to the towing position and install the pin NOTE: Towing the aircraft is possible either with the NLG front device or the NLG aft device. Commercial transport areratt have a large number of markings and placards on their external surface and in the cabin. Their fnction is to: ⁃ Give warnings about dangers ⁃ Give instructions ⁃ Give the location of equipment Markings and placards are written for targeted populations, which can be from different cultures and with different skills The internal instructions are given as written markings. Placards that use pictograms help to: ⁃ Prevent the problem of accurate translation for many languages ⁃ Remove ambiguities in verbal phrases and their interpretation ⁃ Decrease the work to keep placards and manuals consistent. ⁃ Get a fleet-wide commonality ⁃ Decrease training for crews because of the similarity with non- aviation symbols ⁃ Make new placards not necessary after operator change ⁃ Give aid to dyslexic people to get the information ⁃ Make placards easier to read at a distance and in bad lighting conditions. This chapter includes the following SF sections: \- scheduled maintenance tasks and checks. \- unscheduled maintenance checks. unscheduled maintenance checks are necessary. \- HARD OVERWEIGHT LANDING \- L/G DOWN LIMIT SPEED EXCEEDE \- FLAP / SLAT LIMIT SPEED EXCEEDED ) - BIRD OR HAIL STRIKE \- TIRE BURST / TREAD THROW \- BRAKE EMERG. APPLIED / OHVT \- FLT IN EXCESSIVE TURBULENCE \- FLT WITH VMO EXCEEDED \- LIGHTNING STRIKE /STATICDISCHARGE - TAIL RUNWAY IMPACT \- FLT THROUGH DUST STORM / DUST CONTAMINATION ON GROUND \- FLT THROUGH VOLCANO ASH / ASH CONTAMINATION ON GROUND \- MERCURY SPILLAGE \- ABNORMAL PAX / CREW DOOR MOVEMENT \- NOSE LG STEERING ANGLE EXCEEDED