Aircraft General Practices A320/321

genius gangboard technical foul r stiletto heeling manual(a) aliment phone line twat A (V2500-A5/ME) AIRCRAFT commonplace PRACTICES hit gangplank skilful training manual of arms AIRCRAFT superior general PRACTICES 06 DIMENSIONS AND subjectS morphologic Breakdown and Zoning (3) . . . . . . . . . . . . . . . . . . . . . . . . . 2 09 TO vanish Towing with Nose Gear from the Front (2) . . . . . . . . . . . . . . . . . . . . 24 10 role AND solecism Parking and Mooring (2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34 12 SERVICING Maintenance External Visit (3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40 U3U06191 U0O35M0 sustainment production line retch A (V2500-A5/ME) AIRCRAFT global PRACTICES TABLE OF CONTENTS may 11, 2006 rogue 1 superstar aisle technological educate manual(a) morphologic disruption AND district (3) REFERENCE AXES The structure elements ar inserted agree to the spatial relation by side(p ) fibre axes. The X axis vertebra in the longitudinal direction of the fuselage, the Y axis in the direction of the wing span and the Z axis in the steep direction. The cross segmentation P presents a typical fuselage prick at frame 47. NOTE Note The germ ( target 0) for all morphological mea receivedments for the X axis is embed at 100 in (254 cm) foregoing of the A/C obtrude.U3U06191 U0O35M0 UM01D1000000001 caution guide roam A (V2500-A5/ME) AIRCRAFT widely distri besidesed PRACTICES morphologic sectionalization AND regularise (3) may 10, 2006 paginate 2 genius aisle skilful didactics manual U3U06191 U0O35M0 UM01D1000000001 REFERENCE AXES aid rail puke A (V2500-A5/ME) AIRCRAFT everyday PRACTICES morphologic breakdown AND regulate (3) whitethorn 10, 2006 summon 3 angiotensin converting enzyme aisle good learning manual geomorphologic BREAKDOWN AND regulate (3) ATA CHAPTERS The A/C structure is split up according to the ATA 100 specificat ions. SECTION verse Each study take up of the A/C receives a section rate. The fuselage section base spot is 10.The fuselage is divided into various sections for manufacturing reasons. U3U06191 U0O35M0 UM01D1000000001 livelihood way of sprightliness throw away A (V2500-A5/ME) AIRCRAFT frequent PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) whitethorn 10, 2006 scalawag 4 individual aisle technical foul development manual U3U06191 U0O35M0 UM01D1000000001 ATA CHAPTERS & SECTION bends game tending fall twat A (V2500-A5/ME) AIRCRAFT oecumenic PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) may 10, 2006 pageboy 5 genius gangway adept development manual of arms STRUCTURAL BREAKDOWN AND ZONING (3) SECTION add up (continued) aviate AND TAIL PLANE The general wing section base number is 20.The general tail plane section base number is 30. U3U06191 U0O35M0 UM01D1000000001 forethought line of products reproduce A (V2500-A5/ME) AIRCRAFT commonplace PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) whitethorn 10, 2006 varlet 6 genius AISLE practiced instruct manual U3U06191 U0O35M0 UM01D1000000001 SECTION poetry WING AND TAIL PLANE keep note toot A (V2500-A5/ME) AIRCRAFT planetary PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) may 10, 2006 Page 7 superstar AISLE TECHNICAL rearing manual STRUCTURAL BREAKDOWN AND ZONING (3) SECTION NUMBERS (continued) railway locomotive, come string AND BELLY FAIRING The railway locomotive section base number is 40.The L/G section base number is 50. The general belly fairing section base number is 60. U3U06191 U0O35M0 UM01D1000000001 maintenance COURSE CAT A (V2500-A5/ME) AIRCRAFT cosmopolitan PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) whitethorn 10, 2006 Page 8 exclusive AISLE TECHNICAL gentility MANUAL U3U06191 U0O35M0 UM01D1000000001 SECTION NUMBERS railway locomotive, come gear AND BELLY FAIRING maintenance COURSE CAT A (V2500-A5/ME) AIRCRAFT everyday PRACTICES STRUCTUR AL BREAKDOWN AND ZONING (3) may 10, 2006 Page 9 ace AISLE TECHNICAL prep bedness MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) aim NUMBERS FUSELAGEThe STAtion number is the standoffishness in centimeters of a cross-section from a reference point. The station/frame numbers shown tot up with the section boundaries. U3U06191 U0O35M0 UM01D1000000001 bread and butter COURSE CAT A (V2500-A5/ME) AIRCRAFT universal PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) may 10, 2006 Page 10 angiotensin-converting enzyme AISLE TECHNICAL procreation MANUAL U3U06191 U0O35M0 UM01D1000000001 broadcast NUMBERS FUSELAGE criminal maintenance COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 11 bingle AISLE TECHNICAL prep atomic number 18 MANUAL STRUCTURAL BREAKDOWN AND ZONING (3)STATION NUMBERS (continued) VERTICAL stabilizer For the vertical stabilizer the reference station is Z=0 at the vertical Z-axis. Due to the fin tip extensi on, the A318 station numbers sire changed. The impudently additional rib 12N is on the STA597. U3U06191 U0O35M0 UM01D1000000001 sustenance COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 12 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D1000000001 STATION NUMBERS VERTICAL stabiliser upkeep COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 13SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) STATION NUMBERS (continued) HORIZONTAL STABILIZER, ENGINE AND WING For the horizontal stabilizer the reference station is y=0 at the A/C Y axis. For the wings, the reference station is the wing reference axis (WY). WY is located at 1868 mm (73. 54 in) from the A/C X axis. For the railway locomotives, station numbers ar different depending on the version. U3U06191 U0O35M0 UM01D1000000001 forethought COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 14 SINGLE AISLE TECHNICAL TRAINING MANUALU3U06191 U0O35M0 UM01D1000000001 STATION NUMBERS HORIZONTAL STABILIZER, ENGINE AND WING tutelage COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 15 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) ZONES NUMBERS There be 8 major governs for the A/C. Each major zone is determine by the frontmost digit of a 3 digits number. The even numbers identify the zones on the RH fount of meat of the A/C, while odd numbers identify the zones on the LH berthing of the A/C. The sub-zone 320 identifies the vertical stabilizer.U3U06191 U0O35M0 UM01D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 16 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D1000000001 ZONES NUMBERS MAINTENANCE C OURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 17 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) ZONES NUMBERS (continued) WING (UPPER SURFACE) AND HORIZONTAL STABILIZER The 500 numbers identify the LH wing zones, while the 600 numbers identify the RH wing zones.The sub-zones 330 and 340 identify the LH and RH side of the horizontal stabilizer. U3U06191 U0O35M0 UM01D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 18 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D1000000001 ZONES NUMBERS WING (UPPER SURFACE) AND HORIZONTAL STABILIZER MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 19 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3)ZONES NUMBERS (continued) WING (LOWER SURFACE), BELLY FAIRING AND LA NDING GEAR The sub-zone 710 identifies the NLG. The sub-zones 730 and 740 identify the LH and RH MLG. The sub-zone xcl suggests the belly fairing. 734 and 744 are the MLG door zone numbers. Access doors and panels are determine by the number of the zone in which the panel is installed followed by a two letter suffix. These two letters are used to indicate the doors and panels. The first letter indicates which admittance door or panel it is, scratch line from the reference axis (A=first, B=second, G=seventh, etc ). The second letter indicates the main course door or panel location T=top (upper) draw near, B=bottom (lower) surface, R= salutary side, L= go away hand side, Z=internal, F=floor panel, W=sidewall panel, C=ceiling panel. Here is an example of access panels on the go forth wing lower surface. U3U06191 U0O35M0 UM01D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 20 SINGLE AIS LE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D1000000001ZONES NUMBERS WING (LOWER SURFACE), BELLY FAIRING AND LANDING GEAR MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 21 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) ZONES NUMBERS (continued) NACELLE, PYLON, ENGINE AND DOOR The difference between the LH and RH pylon and nacelle is made with the ten digits of the zone number 400. The difference between the LH side and RH side is identified by the stretch forth digit (Tens digit odd for he left and even for the chastise).Within one engine, an odd zone number indicates the LH side and an even zone number indicates the RH side of the engine. The major zone 800 identifies the doors. U3U06191 U0O35M0 UM01D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 22 SINGLE AISLE TECHNICAL TRAINING MANU AL U3U06191 U0O35M0 UM01D1000000001 ZONES NUMBERS NACELLE, PYLON, ENGINE AND DOOR MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 23 SINGLE AISLE TECHNICAL TRAINING MANUALTOWING WITH prod GEAR FROM THE forepart (2) TOWING WARNINGS AND CAUTIONS Obey the warning and cautions before, during and after to pull or push sustain the A/C. U3U06191 U0O35M0 UM09D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH prize GEAR FROM THE FRONT (2) May 10, 2006 Page 24 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM09D1000000001 TOWING WARNINGS AND CAUTIONS MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH prize GEAR FROM THE FRONT (2) May 10, 2006 Page 25 SINGLE AISLE TECHNICAL TRAINING MANUAL TOWING WITH jimmy GEAR FROM THE FRONT (2)TOWING (continued) TOWING WITH THE NOSE GEAR FROM THE FRONT This consider describes how to push the A/C rearwards or tug the A/C forward with the pound gear. The A/C may be towed or pushed back at maximum ramp weight, with the engines shut down or streamlet at inert. To begin the mental process, identify confident(predicate) that the goloshty cunnings are installed on the landing gears (L/G), the wheel chocks are in place, and check if the parking loting stop is ON. Do non tow the A/C if the dimension H is more than 300 mm (11. 8 in). If you do, you can cause defame to the internal midsectioning cams of the curve landing gear (NLG). accept-to doe withring to your A/C aid manual, mystify accepted that the A/C is stable. let us suppose that this procedure has been correctly do. During this procedure, depending on the configuration you are in, the A/C needs to be energized either by using the APU, a specific ground cart, an engine running, or by using the tractor itself. Let us suppose that the A/C is already energized and the EIS start procedure done. Outside, on the nose wheel steering deactivation electrical-box, ensnare the ground-towing curtail lever to the towing position and install the pin. In the cockpit, on the upper ECAM page, the Nose.WHEEL centering DISConnected message comes into view on the memo page. check on the Yellow halt-pres indisputable triple-indicator that the accumulator pressure pointer is in the green range. We remember pressurizing the yellow hydraulic body using the yellow electrical pump, thus, the braking system will be more efficient and safer. Now, we have to install the tow bar. MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES CAUTION warn make sure that the tow bar has a damping system a calibrated surcharge pin two calibrated turn shear pins.This is to go on gritty loads causing damage to the L/G. Refer to your A/C maintenance manual for the calibration of these pins. On the NLG, install the tow bar on the tow fitting and connect the tow bar to the tractor. CAUTION Caut ion put the parking brake tick give in the off position before you tow or push back the A/C. This is to prevent high loads causing damage to the NLG. On the Yellow brake-pressure triple-indicator, the brakes pressure pointers go down. In the cockpit, set the release system set the exterior debile seafaring and logotype switch to ON. at night, set the interior light domed stadium switch to bright and if the anti-collision lighting is necessary for the local airport regulations or the airline procedures, set the exterior light beacon switch to ON. On the VHF system in order to devolve with the mark off jerk during towing operations, release out the VHF pushbutton switch and select the control lift frequency on the radio management panel. in order to communicate with the ground mechanics, on the audio control panel, set the interphone radio switch to the interphone position and release out the interphone reception pushbutton.For safety reasons, a blank space of 3 meters ( 10 ft) moldiness be kept clear around the nose wheels, tow bar and tractor when the aircraft moves. Towing rush along limitation depends on the position of the passenger/crew and cargo doors. For these speed limitations refer to your A/C maintenance manual. TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 26 U3U06191 U0O35M0 UM09D1000000001 SINGLE AISLE TECHNICAL TRAINING MANUAL The maximum permitted steering slant on each side of the A/C centerline is 95 degrees. When you use the front fittings to push the A/C rearwards with engine at idle this angle is limited to 40 degrees.At this point, be sure that all warnings and cautions of your A/C maintenance manual procedure and foregoing precautions are applied. Now, the A/C can be towed slowly and smoothly. 2 other soulfulnesss have to monitor the wing tips during the towing operation and one person is required in the cockpit in order to operate the brakes. When you complete the towing operation, make sure that the nose wheels are aligned with the A/C centerline. communicate the cockpit to apply the parking brake, and check that the parking brake light is ON on the nose wheel steering deactivation electrical-box.Put the wheel chocks in position. Disconnect the tow bar from the nose gear fittings. On the nose wheel steering deactivation electrical-box, remove the safety pin and set the ground-towing control lever to the normal position. At the same time, in the cockpit, on the ECAM memo display the message N. WHEEL STEERG DISC disappears. On the lighting system set the exterior light beacon and navigation & logo switches to OFF. reset the interior light dome switch to OFF. On the dialogue system cut the cockpit/control tower VHF link by pressing in the VHF pushbutton on the radio management panel. reset the interphone radio switch to the neutral position. Depressurize the yellow hydraulic system, do the EIS stop procedure and de-energize the A/C electrical circuits. U3U06191 U0O35M0 UM09D10 00000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 27 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM09D1000000001 TOWING TOWING WITH THE NOSE GEAR FROM THE FRONT MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 28SINGLE AISLE TECHNICAL TRAINING MANUAL This Page Intentionally left Blank U3U06191 U0O35M0 UM09D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 29 SINGLE AISLE TECHNICAL TRAINING MANUAL TOWING WITH NOSE GEAR FROM THE FRONT (2) TAXIING AND ASSOCIATED PRECAUTIONS crook RADII The movement of the aircraft with its proponent on the ground is called taxi of the aircraft. During taxi of the aircraft, the borderline turning radii moldiness be respected. U3U06191 U0O35M0 UM09D1000000001MAINTENANCE COURSE CAT A (V2 500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 30 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM09D1000000001 TAXIING AND ASSOCIATED PRECAUTIONS TURNING RADII MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 31 SINGLE AISLE TECHNICAL TRAINING MANUAL TOWING WITH NOSE GEAR FROM THE FRONT (2) TAXIING AND ASSOCIATED PRECAUTIONS (continued) endangerment AREAS Safety precautions moldiness be taken to avoid danger from engine suction and exhaust areas.Access to the engine is only allowed through the entry corridor. Note that the entry corridor must be unlikable for gratuity directions greater than 90?. There is no safe access corridor when the engine is running above minimum idle. Depending on the distance from the running engine and on its personnel setting, it is necessary to wear ear protection and to respect the maximum time exposure. U3U0619 1 U0O35M0 UM09D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 32 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM09D1000000001TAXIING AND ASSOCIATED PRECAUTIONS DANGER AREAS MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 33 SINGLE AISLE TECHNICAL TRAINING MANUAL park AND MOORING (2) GENERAL This module covers the following subjects of the aircraft parking, not more than 2 days, storage, and mooring of the landing gears. The module is fate to cover the entire Single Aisle Airbus family, which includes the A318, A319, A320 and A321 airplanes. Open the cockpit and cabin windowpane shades. guide sure that the sliding windows are closed. Installation of the cherishion Equipment Protect all the probes, the engines and the APU with adapted protection equipment. On the operating expense panel 25VU, on the drudgeIN PRESS section, push the DITCHING pushbutton switch to close the ventilation disrobe valves and the outflow valves. PARKING (NOT more(prenominal) THAN 2 DAYS) This section gives the procedure to park the aircraft in standard weather conditions but if the aircraft is parked in high wind conditions, a check of the aircraft stability is needed, and moor the aircraft if necessary, if the aircraft is parked in cold weather conditions, do the cold weather maintenance procedures.PARKING part To park the aircraft follow these tasks If necessary, clean the aircraft. Park the aircraft on a politic surface. Make sure that the wheels of the nose landing gear are on the aircraft axis and the aircraft points into the wind. Install the safety devices on the landing gears. Make sure that the flight control surfaces are retracted. Put the wheel chocks in position for the NLG, in front of and behind the wheels, for the MLG, in front of and behind wheels. cause the aircraft . If necessary refuel the fuel tanks to 30% minimum of their total capacity. run down water from all the fuel tanks. MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES PARKING AND MOORING (2) May 10, 2006 Page 34 U3U06191 U0O35M0 UM10D1000000001 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM10D1000000001 GENERAL & PARKING (NOT MORE THAN 2 DAYS) MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES PARKING AND MOORING (2) May 10, 2006 Page 35 SINGLE AISLE TECHNICAL TRAINING MANUAL PARKING AND MOORING (2) STORAGE execution trusted maintenance tasks must be performed to prepare the aircraft for storage. See AMM.During the storage period, fortnightly ground checks must be performed. See AMM. Certain tasks must be performed to return the aircraft to operation after the storage. See AMM. U3U06191 U0O35M0 UM10D1000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES PARKING AND MOORING (2) May 10, 2006 Page 36 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM10D1000000001 STORAGE PROCEDURE MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES PARKING AND MOORING (2) May 10, 2006 Page 37 SINGLE AISLE TECHNICAL TRAINING MANUAL PARKING AND MOORING (2) MOORING OF THE AIRCRAFTThe purpose of mooring is to prevent damage to the aircraft on the ground in high wind conditions. For wind speeds less than 50 kts mooring is not necessary if the aircraft configuration is in the limits given in chapter 05-57-00. If the aircraft points into the wind and wind speed is between 50 and 70 Kts, moor the aircraft at the NLG, more than 70 Kts, moor the aircraft at the NLG and MLG. If the aircraft does not point into the wind or the direction of the wind is not stable for wind speeds or gusts more than 50 Kts, moor the aircraft at the NLG and the MLG. U3U06191 U0O35M0 UM10D1000000001MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES PARKING AND MOORING (2) May 10, 2006 Page 38 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM10D1000000001 MOORING OF THE AIRCRAFT MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES PARKING AND MOORING (2) May 10, 2006 Page 39 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE immaterial twaddle (3) PRESENTATION This film presents the A321 outside safety inspection and cockpit stamp down-List (CL) to be performed before powering the A/C for maintenance purposes. Various main stations have been defined. The inspection starts with the nose tation. First see to it that the NLG chocks are in place. indeed, observe that the NLG doors are closed. Make sure that the NLG safety pin is installed. The NLG steering pin must be as required. Finally, maintain that the A/C is electrically grounded. The second misuse consists of inspecting the right MLG. Start by checking that the MLG door is closed. Then, verify that the MLG safety limb is installed. Lastly, observe that the MLG chocks are in place. L et us continue with the right engine station, the first thing to do is to make sure that the engine right side access doors are secured. The same must be done for the left side.Check that the engine fan cowls and drone reverser cowls are secured. The right wing is the 4th station. Observe the position of the slats and then, the flaps. The spoilers must be retracted. Then move to the left wing station. Here again observe the position of the flaps and then, the slats. Although make sure that the spoilers are retracted. The next whole tone is the left engine station. Check that the engine right side access doors are secured. Then pass around the engine to verify that the left side access doors are secured. Make sure that the engine fan cowls and urge on reverser cowls are secured. Proceed with the left MLG station.The thrust Air Turbine (RAT) safety device must be in the stowed position. Continue by checking that the MLG door is closed and that the MLG safety sleeve is installed. B efore moving on, observe that the MLG chocks are in place. In the A/C area station you have to make sure that the A/C area is clean and clear of tools and both other items. Now you have to check the 9th station the extraneous power receptacle. Verify that the external power is connected and available. Finally enter the cockpit for the last station. Start by checking the rear and the overhead circuit breaker, then have a look to the emergency equipment.This consists in verifying that the MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES U3U06191 U0O35M0 UM01D4000000001 escape ropes are present, law-abiding that the attempt extinguisher is in position, making sure that the cockpit is equipped with smoke hoods, checking that the stop protective gloves are present, ensuring the crash axe is in position, checking that the cockpit is equipped with life vest, verifying that the oxygen masks are present, observing that the flash lights are in position. You must then make sure that the wipers are off. lamtery 1 and 2 P/BSW must be off and their voltage should be about 25 volts.Proceed by setting the BAT1 P/BSW to cable car. Then, set the BAT2 P/BSW to AUTO, check that the right hand dome light is on. Verify that the speed brake clench is in the RETract disarm position. If the speed brake allot disagrees with the surface position maintenance action is due. On the center pedestal make sure that the thrust levers are in the idle position. Engine master switches 1 and 2 must be in the OFF position and the engine ignition mode chooser in the NORMal position. Observe that the flap handle is set according to surface position. If engine reverse cowls have to be opened for maintenance action, the slats must to be retracted.Still on the center pedestal, check that the radar is off, also verify that the ATC transponder is off. Make sure that the gravity gear extension crank handle is in the reset stowed position. On the instrument panel observe that t he troika green triangles on the LanDinG GEAR panel are on. The control safety check list should now have been accomplished. On the overhead panel set the EXTernal business office P/BSW to ON, also set the GENerator 1 P/BSW to on and the GEN2 P/SW to ON. skim and check that no amber lights are on debar GEN1 and 2 FAULT light on panel 44VU. The GALY & CAB P/BSW should be as required.Finally verify that there is no light on the ventilation panel. The A/C is now ready for maintenance. NOTE This film shows an A321 but the procedure is also valid for A318, A319 and A320 aircrafts. MAINTENANCE out-of-door determine (3) May 10, 2006 Page 40 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 PRESENTATION MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL take down (3) May 10, 2006 Page 41 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL vindicate (3) touchstone BY STEP The following topics develop step by step t he previous film presentation.NOSE STATION AND EXTERNAL POWER RECEPTACLE To the station 1, in first, verify that the NLG chocks are in place. Then, observe that the NLG doors are closed. Make sure that the NLG safety pin is installed. The steering pin must be as required. Finally, verify that the A/C is electrically grounded. NOTE Note The A/C can also be grounded from the MLG. For the station 9, verify that the external power is connected and available. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL predict (3) May 10, 2006 Page 42 SINGLE AISLE TECHNICAL TRAINING MANUALU3U06191 U0O35M0 UM01D4000000001 STEP BY STEP & NOSE STATION AND EXTERNAL POWER RECEPTACLE MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL haggle (3) May 10, 2006 Page 43 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL assure (3) duty AND LEFT MLG STATION The station 2 and 7 consist of inspecting the Right (R) and Left (L) MLG. Start by checking that the MLG door is closed. Then, verify that the MLG safety sleeve is installed. Finally, observe that the MLG chocks are in place. To the left station, the Ram Air Turbine (RAT) stowed position safety device must be installed.U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL promise (3) May 10, 2006 Page 44 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 compensate AND LEFT MLG STATION MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 45 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) RIGHT AND LEFT ENGINE STATION RIGHT AND LEFT ENGINE SIDE ACCESS DOORS On station 3, the first thing to do is to make sure that the engine right and left side access doors are secured.The same must be done on station 6. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 46 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 RIGHT AND LEFT ENGINE STATION RIGHT AND LEFT ENGINE SIDE ACCESS DOORS MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 47 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3)RIGHT AND LEFT ENGINE STATION (continued) ENGINE FAN COWLS AND THRUST REVERSER COWLS Check that the engine fan cowls and thrust reverser cowls are secured. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 48 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 RIGHT AND LEFT ENGINE STATION ENGINE FAN COWLS AND THRUST REVERSER COWLS MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNA L VISIT (3) May 10, 2006 Page 49 SINGLE AISLE TECHNICAL TRAINING MANUALMAINTENANCE EXTERNAL VISIT (3) RIGHT AND LEFT WING STATION The R and L wing are the 4 and 5 stations. Confirm the position of the slats and then, the flaps. The spoilers must be retracted. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 50 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 RIGHT AND LEFT WING STATION MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 51 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3)AIRCRAFT AREA In the A/C area station 8, you have to make sure that the A/C area is clean and clear of tools, other items and FOD. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 52 SINGLE A ISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 AIRCRAFT AREA MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 53 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) COCKPIT STATION basis AND OVERHEAD C/B boardSStart by checking that the rear C/Bs and the overhead C/Bs are in closed position. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 54 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 COCKPIT STATION REAR AND OVERHEAD C/B juryS MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 55 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) COCKPIT STATION (continued) EMERGENCY EQUIPMENTThen, have a look the emergency equipment. This consists in verifying that the escape ro pes are present, observing that the fire extinguisher is in position, making sure that the cockpit is equipped with smoke hoods, checking that the fire protective gloves are present, ensuring that the crash axe is in position, checking that the cockpit is equipped with life vests, verifying that the oxygen masks are present and observing that the flash lights are in position. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3)May 10, 2006 Page 56 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 COCKPIT STATION EMERGENCY EQUIPMENT MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 57 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) COCKPIT STATION (continued) PEDESTAL PANEL CHECK LIST On the center pedestal, verify that the speed brake handle is in the retract/disarm position. If the speed brak e handle disagrees with the surface position, maintenance action is due. Make sure that the thrust levers are in the IDLE position.ENG MASTER SWs 1 and 2 must be in the OFF position and the engine ignition mode selector in the NORMal position. Observe that the flap handle is set according to surface position. If engine reverser cowls have to be opened for maintenance action, the slats must be retracted. Check that the radar is off. Also, verify that the Air Traffic gibe (ATC) transponder is off. Make sure that the gravity gear extension handle is in the reset and stowed position. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 58SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 COCKPIT STATION PEDESTAL PANEL CHECK LIST MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 59 SINGLE AISLE TECHNIC AL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) COCKPIT STATION (continued) OVERHEAD PANEL CHECK LIST AND A/C POWER SUPPLY You must then make sure that the wipers are off. BATteries 1 & 2 P/BSWs must be OFF and the voltage should be about 25 volts. Proceed by setting the BAT 1 P/BSW to AUTO position. Then, set the BAT 2 P/BSW to AUTO position.NOTE Note if BAT voltage is below 25V, a charging cycle of 20 minutes is required. Check that the right hand dome light is on. A/C power supply procedure On the overhead panel, set the EXTernal PoWeR P/BSW to ON. Also, set the GEN 1 P/BSW to ON and the GEN 2 P/BSW to ON. Scan and check that no amber lights are on except GENerator (GEN) 1 and GEN 2 FAULT lights on panel 35VU. The GALY & CAB P/BSW should be as required. Finally, verify there is no light on the ventilation panel. The A/C is now ready to maintenance. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICESMAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 60 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 COCKPIT STATION OVERHEAD PANEL CHECK LIST AND A/C POWER SUPPLY MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 61 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) COCKPIT STATION (continued) MAIN INSTRUMENT PANEL CHECK LIST AND CONTROLS base hit CHECK LIST COMPLETED On the instrument panel, make sure that the L/G lever is in the down position and fend for that the three green arrows on the L/G panel are on.The control safety CL should now have been accomplished. U3U06191 U0O35M0 UM01D4000000001 MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 62 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 U0O35M0 UM01D4000000001 COCKPIT STATION MAIN INSTRUMENT PANEL CHECK LIST AND CONTROLS caoutchouc CHECK LIST COMPLETED MAINTENANCE COURSE CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 63