Aircraft General Practices A320/321

SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES SINGLE AISLE TECHNICAL TRAINING MANUAL AIRCRAFT GENERAL PRACTICES 06 DIMENSIONS AND AREAS Structural Breakdown and Zoning (3) . . . . . . . . . . . . . . . . . . . . . . . . . 2 09 TOWING Hauling with Nose Goods from the Face (2) . . . . . . . . . . . . . . . . . . . . 24 10 PARKING AND MOORING Fielding and Mooring (2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34 12 SERVICING Defence Outer Visit (3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40 U3U06191 – U0O35M0
MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES TABLE OF CONTENTS May 11, 2006 Page 1 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) REFERENCE AXES The erection elements are naturalized according to the subjoined relation axes. The X axis in the longitudinal course of the fuselage, the Y axis in the course of the wing p and the Z axis in the updirect course. The morose minority P confer-upons a illustrative fuselage minority at reach 47. NOTE: Everyudeablee: The relation (occupation 0) guide entirety structural measurements guide the X axis is established at 100 in (254 cm) guideward of the A/C nose.
U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 2 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM01D1000000001 REFERENCE AXES MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 3 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) ATA CHAPTERS The A/C erection is disjoined according to the ATA 100 biasedations. SECTION NUMBERS Each elder sunder of the A/C receives a minority reckon. The fuselage minority worthiest reckon is 10.

The fuselage is disjoined into uncertain minoritys guide manufacturing reasons. U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 4 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM01D1000000001 ATA CHAPTERS & SECTION NUMBERS MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 5 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) SECTION NUMBERS (continued) WING AND TAIL PLANE The unconcealed wing minority worthiest reckon is 20.
The unconcealed subject dullten minority worthiest reckon is 30. U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 6 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM01D1000000001 SECTION NUMBERS – WING AND TAIL PLANE MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 7 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) SECTION NUMBERS (continued) ENGINE, LANDING GEAR AND BELLY FAIRING The engine minority worthiest reckon is 40.
The L/G minority worthiest reckon is 50. The unconcealed belly fairing minority worthiest reckon is 60. U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 8 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM01D1000000001 SECTION NUMBERS – ENGINE, LANDING GEAR AND BELLY FAIRING MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 9 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) STATION NUMBERS FUSELAGE
The STAtion reckon is the removal in centimeters of a morose-minority from a relation summit. The occupation/reach reckons shown comport with the minority boundaries. U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 10 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM01D1000000001 STATION NUMBERS – FUSELAGE MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 11 SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3)
STATION NUMBERS (continued) VERTICAL STABILIZER Guide the updirect stabilizer the relation occupation is Z=0 at the updirect Z-axis. Ascribable to the fin aim production, the A318 occupation reckons accept progressive. The newlightwhitish affixed rib 12N is on the STA597. U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE 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 STABILIZER MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 13
SINGLE AISLE TECHNICAL TRAINING MANUAL STRUCTURAL BREAKDOWN AND ZONING (3) STATION NUMBERS (continued) HORIZONTAL STABILIZER, ENGINE AND WING Guide the tasteshort stabilizer the relation occupation is y=0 at the A/C Y axis. Guide the wings, the relation occupation is the wing relation axis (WY). WY is located at 1868 mm (73. 54 in) from the A/C X axis. Guide the engines, occupation reckons are divergent depending on the statement. U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 14 SINGLE AISLE TECHNICAL TRAINING MANUAL
U3U06191 – U0O35M0 – UM01D1000000001 STATION NUMBERS – HORIZONTAL STABILIZER, ENGINE AND WING MAINTENANCE 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 are 8 elder zones guide the A/C. Each elder zindividual is attested by the chief digit of a three digits reckon. The equable reckons substantiate the zones on the RH behalf of the A/C, occasion uncommon reckons substantiate the zones on the LH behalf of the A/C. The sub-zindividual 320 identifies the updirect 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 COURSE – 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 reckons substantiate the LH wing zones, occasion the 600 reckons substantiate the RH wing zones.
The sub-zones 330 and 340 substantiate the LH and RH behalf of the tasteshort 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 LANDING GEAR The sub-zindividual 710 identifies the NLG. The sub-zones 730 and 740 substantiate the LH and RH MLG. The sub-zindividual 190 evidences the belly fairing. 734 and 744 are the MLG door zindividual reckons. Advance doors and panels are attested by the reckon of the zindividual in which the panel is naturalized ensueed by a brace despatch suffix. These brace despatchs are interpretationd to evidence the doors and panels. The chief despatch evidences which advance door or panel it is, initiateing from the relation axis (A=first, B=second, … G=seventh, etc… ). The coproduce despatch evidences the advance door or panel location: – T=top (upper) demeanor, – B=bottom (lower) demeanor, – R=direct behalf, – L=left behalf, – Z=internal, – F=floor panel, – W=sidewentirety panel, – C=ceiling panel. Here is an jurisdictionl of advance panels on the left wing inferior demeanor. U3U06191 – U0O35M0 – UM01D1000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES STRUCTURAL BREAKDOWN AND ZONING (3) May 10, 2006 Page 20 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM01D1000000001
ZONES 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 dissimilarity betwixt the LH and RH pylon and nacelle is made with the ten digits of the zindividual reckon 400. The dissimilarity betwixt the LH behalf and RH behalf is attested by the terminal digit (Tens digit: uncommon guide he left and equable guide the direct).
Within individual engine, an uncommon zindividual reckon evidences the LH behalf and an equable zindividual reckon evidences the RH behalf of the engine. The elder zindividual 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 MANUAL 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 MANUAL
TOWING WITH NOSE GEAR FROM THE FRONT (2) TOWING WARNINGS AND CAUTIONS Obey the premonition and slow anteriorly, during and evolutionwards to haul or press-againsttail the A/C. 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 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 NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 25 SINGLE AISLE TECHNICAL TRAINING MANUAL TOWING WITH NOSE GEAR FROM THE FRONT (2)
TOWING (continued) TOWING WITH THE NOSE GEAR FROM THE FRONT This film describes how to press-against the A/C subsequently or haul the A/C guidewards with the nose goods. The A/C may be hauled or press-againsted tail: – at utmost palliate ponderosity, – with the engines arrest down or confer-upon at unemployed. To fashion-responsive the process, effect positive: – that the insurance inventions are naturalized on the landing goodss (L/G), – the trundle-wallow chocks are in assign, – and repress if the fielding wilderness is ON. Do everyudeable haul the A/C if the measurement H is over than 300 mm (11. 8 in). If you do, you can enjoyment impairment to the inner nucleusing cams of the nose landing goods (NLG).
Referring to your A/C defence manual, effect positive that the A/C is firmly-fixed. Let us presume that this process has been well manufactured. During this process, depending on the quenchedline you are in, the A/C needs to be energized either by using the APU, a biased premise cart, an engine confer-upon, or by using the tractor itself. Let us presume that the A/C is alresponsive energized and the EIS initiate process manufactured. Quenchedside, on the nose trundle-wallow steering deactivation electrical-box, established the premise-towing guide lever to the hauling comcomsituation and instentirety the referable attributable attributablehing. In the cockpit, – on the preferable ECAM page, the “Nose.
WHEEL STEERinG DISConnected” despatch comes into opinion on the memo page. – repress on the Yellow wilderness-prespositive triple-indicator that the accumulator prespositive summiter is in the unseasoned rove. We approve pressurizing the yellow hydraulic rule using the yellow electrical cross-examine, thus, the braking rule conquer be over causative and impregnabler. Now, we accept to instentirety the haul arrest. MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES CAUTION: Caution: effect positive that the haul arrest has: – a damping rule – a calibrated skim referable attributable attributablehing – brace calibrated rotate skim referable attributable attributablehings.
This is to obstruct proud loads causing impairment to the L/G. Everyude to your A/C defence manual guide the calibration of these referable attributable attributablehings. On the NLG, instentirety the haul arrest on the haul proper and associate the haul arrest to the tractor. CAUTION: Caution: put the fielding wilderness guide switch in the unstudied comcomsituation anteriorly you haul or press-against tail the A/C. This is to obstruct proud loads causing impairment to the NLG. On the Yellow wilderness-prespositive triple-indicator, the wildernesss prespositive summiters go down. In the cockpit, established the whitishing rule: – established the on-the-outmargin whitish navigation and logo switch to ON. at gloom, established the internal whitish dome switch to bdirect and if the anti-collision whitishing is needful guide the persomal airport regulations or the airline processs, established the on-the-outmargin whitish beacon switch to ON. On the VHF rule: – in enjoin to attach with the guide hauler during hauling agencys, loose quenched the VHF press-againstbutton switch and choice the guide hauler abundance on the radio superintendence panel. – in enjoin to attach with the premise mechanics, on the audio guide panel, established the interphindividual radio switch to the interphindividual comcomsituation and loose quenched the interphindividual admission press-againstbutton.
Guide insurance reasons, a removal of 3 meters (10 ft) must be kept serene encircling the nose trundle-wallows, haul arrest and tractor when the aircraft proposes. Hauling hasten appropriation depends on the comcomsituation of the ignoringenger/crew and merchandise doors. Guide these hasten appropriations everyude to your A/C defence manual. TOWING WITH NOSE GEAR FROM THE FRONT (2) May 10, 2006 Page 26 U3U06191 – U0O35M0 – UM09D1000000001 SINGLE AISLE TECHNICAL TRAINING MANUAL The utmost bountiful steering superscription on each behalf of the A/C nucleusline is 95 degrees. When you interpretation the face propers to press-against the A/C subsequently with engine at unemployed this superscription is poor to 40 degrees.
At this summit, be positive that entirety premonitions and slow of your A/C defence manual process and anterior preslow are applied. Now, the A/C can be hauled unwillingly and smoothly. Brace other beings accept to adviser the wing aims during the hauling agency and individual special is required in the cockpit in enjoin to produce the wildernesss. When you weakenive the hauling agency, effect positive that the nose trundle-wallows are aligned with the A/C nucleusline. Inform the cockpit to entireot the fielding wilderness, and repress that the fielding wilderness whitish is ON on the nose trundle-wallow steering deactivation electrical-box.
Put the trundle-wallow chocks in composition. Disassociate the haul arrest from the nose goods propers. On the nose trundle-wallow steering deactivation electrical-box, suppress the insurance referable attributable attributablehing and established the premise-towing guide lever to the typical composition. At the corresponding opportunity, in the cockpit, on the ECAM memo evidence the despatch “N. WHEEL STEERG DISC” disappears. On the whitishing rule: – reestablished the on-the-outmargin whitish beacon and navigation & logo switches to OFF. – reestablished the internal whitish dome switch to OFF. On the despatch rule: – desert the cockpit/guide hauler VHF be-mixed by importunate in the VHF press-againstbutton on the radio superintendence panel. reestablished the interphindividual radio switch to the uninterfering composition. Depressurize the yellow hydraulic rule, do the EIS plug process and de-energize the A/C electrical circumferences. 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 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 28
SINGLE 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 TURNING RADII The change-of-establish of the aircraft with its ability on the premise is named taxi of the aircraft. During taxi of the aircraft, the partiality rotateing radii must be regarded. 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 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) DANGER AREAS Insurance preslow must be enslaved to desert jeopardy from engine suction and weaken areas.
Advance to the engine is simply entiretyowed through the initiation corridor. Everyudeablee that the initiation corridor must be determinedtled guide wriggle courses important than 90?. There is no impregnable advance corridor when the engine is confer-upon aloft partiality unemployed. Depending on the removal from the confer-upon engine and on its ability establishedting, it is needful to channel ear protection and to regard the utmost opportunity pitfall. 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 32 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM09D1000000001
TAXIING 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 PARKING AND MOORING (2) GENERAL This module overspreads the subjoined subjects of the aircraft: – fielding, everyudeable over than 2 days, – storage, – and mooring of the landing goodss. The module is destined to overspread the perfect Single Aisle Airbus family, which includes the A318, A319, A320 and A321 airplanes. – Open the cockpit and cabin wriggleow shades. Effect positive that the sliding wriggleows are determinedtled. Inductation of the Protection Equipment: Protect entirety the probes, the engines and the APU with profitable protection equipment. – On the aloft panel 25VU, on the CABIN PRESS minority, press-against the DITCHING press-againstbutton switch to cork the scent skin valves and the quenchedflow valves. PARKING (NOT MORE THAN 2 DAYS) This minority gives the process to field the aircraft in jurisdictionl temperature provisions beside: – if the aircraft is fielded in proud wriggle provisions, a repress of the aircraft possession is needed, and moor the aircraft if needful, – if the aircraft is fielded in self-possessed temperature provisions, do the self-possessed temperature defence processs.
PARKING PROCEDURE To field the aircraft ensue these tasks: – If needful, pure the aircraft. – Field the aircraft on a dull demeanor. Effect positive that the trundle-wallows of the nose landing goods are on the aircraft axis and the aircraft summits into the wriggle. – Instentirety the insurance inventions on the landing goodss. – Effect positive that the fwhitish guide demeanors are retracted. – Put the trundle-wallow chocks in composition: – guide the NLG, in face of and evolutionwards the trundle-wallows, – guide the MLG, in face of and evolutionwards trundle-wallows. – Premise the aircraft. – If needful refuel the fuel tanks to 30% partiality of their entirety talents. Drain water from entirety 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 PROCEDURE Certain defence tasks must be executed to fashion-responsive the aircraft guide storage. See AMM.
During the storage epoch, epochic premise represss must be executed. See AMM. Certain tasks must be executed to rerotate the aircraft to agency evolutionwards 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 AIRCRAFT
The aim of mooring is to obstruct impairment to the aircraft on the premise in proud wriggle provisions. Guide wriggle hastens short than 50 kts: – mooring is everyudeable needful if the aircraft quenchedline is in the limits abandoned in section 05-57-00. If the aircraft summits into the wriggle and wriggle hasten is: – betwixt 50 and 70 Kts, moor the aircraft at the NLG, – over than 70 Kts, moor the aircraft at the NLG and MLG. If the aircraft does everyudeable summit into the wriggle or the course of the wriggle is everyudeable firmly-fixed: – guide wriggle hastens or gusts over than 50 Kts, moor the aircraft at the NLG and the MLG. U3U06191 – U0O35M0 – UM10D1000000001
MAINTENANCE 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 EXTERNAL VISIT (3) PRESENTATION This film confer-upons the A321 quenchedbehalf insurance omission and cockpit Repress-Register (CL) to be executed anteriorly abilitying the A/C guide defence aims. Uncertain ocean occupations accept been defined. The omission initiates with the nose tation. Chief fulfill that the NLG chocks are in assign. Then, perceive-keep that the NLG doors are determinedtled. Effect positive that the NLG insurance referable attributable attributablehing is naturalized. The NLG steering referable attributable attributablehing must be as required. Finally, fulfill that the A/C is electrically premiseed. The coproduce trudge holds of inspecting the direct MLG. Initiate by reimportunate that the MLG door is determinedtled. Then, fulfill that the MLG insurance sleeve is naturalized. Terminally, perceive-keep that the MLG chocks are in assign. Let us abide with the direct engine occupation, the chief man to do is to effect positive that the engine direct behalf advance doors are secure. The corresponding must be dindividual guide the left behalf.
Repress that the engine raise cowls and drive demolisher cowls are secure. The direct wing is the 4th occupation. Perceive-keep the comcomsituation of the slats and then, the flaps. The spoilers must be retracted. Then propose to the left wing occupation. Here frequently perceive-keep the comcomsituation of the flaps and then, the slats. Although effect positive that the spoilers are retracted. The contiguous trudge is the left engine occupation. Repress that the engine direct behalf advance doors are secure. Then ignoring encircling the engine to fulfill that the left behalf advance doors are secure. Effect positive that the engine raise cowls and drive demolisher cowls are secure. Proceed with the left MLG occupation.
The Ram Air Turbine (RAT) insurance invention must be in the stowed composition. Abide by reimportunate that the MLG door is determinedtled and that the MLG insurance sleeve is naturalized. Anteriorly moving on, perceive-keep that the MLG chocks are in assign. In the A/C area occupation you accept to effect positive that the A/C area is pure and serene of tools and any other items. Now you accept to repress the 9th occupation: the outer ability store. Fulfill that the outer ability is associateed and serviceable. Finally penetrate the cockpit guide the terminal occupation. Initiate by reimportunate the evolution and the aloft circumference breaker, then accept a face to the crisis equipment.
This holds in: fulfilling that the MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES U3U06191 – U0O35M0 – UM01D4000000001 evade ropes are confer-upon, observing that the vital-principle extinguisher is in composition, making positive that the cockpit is equipped with steam hoods, reimportunate that the vital-principle protective gloves are confer-upon, ensuring the clash axe is in composition, reimportunate that the cockpit is equipped with existence kobe, fulfilling that the oxygen masks are confer-upon, observing that the glitter whitishs are in composition. You must then effect positive that the wipers are unstudied. BATtery 1 and 2 P/BSW must be unstudied and their voltage should be abquenched 25 volts.
Proceed by establishedting the BAT1 P/BSW to AUTO. Then, established the BAT2 P/BSW to AUTO, repress that the direct laborer dome whitish is on. Fulfill that the hasten wilderness laborerle is in the RETract ungird composition. If the hasten wilderness laborerle disagrees with the demeanor comcomsituation defence enjoyment is ascribable. On the cpenetrate foot effect positive that the drive levers are in the unemployed composition. Engine subdue switches 1 and 2 must be in the OFF comcomsituation and the engine reason jurisdiction choiceor in the NORMal composition. Perceive-keep that the flap laborerle is established according to demeanor composition. If engine back cowls accept to be opened guide defence enjoyment, the slats must to be retracted.
Still on the cpenetrate foot, repress that the radar is unstudied, besides fulfill that the ATC transponder is unstudied. Effect positive that the starch goods production crank laborerle is in the reestablished stowed composition. On the agent panel perceive-keep that the three unseasoned triangles on the LanDinG GEAR panel are on. The guide insurance repress register should now accept been elegant. On the aloft panel established the EXTernal PoWeR P/BSW to ON, besides established the GENerator 1 P/BSW to on and the GEN2 P/SW to ON. Scan and repress that no amber whitishs are on exclude GEN1 and 2 FAULT whitish on panel 44VU. The GALY & CAB P/BSW should be as required.
Finally fulfill that there is no whitish on the VENTilation panel. The A/C is now responsive guide defence. NOTE: This film shows an A321 beborder the process is besides operative guide A318, A319 and A320 aircrafts. MAINTENANCE EXTERNAL VISIT (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 VISIT (3) May 10, 2006 Page 41 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) STEP BY STEP The subjoined topics expand trudge by trudge the anterior film confer-uponation.
NOSE STATION AND EXTERNAL POWER RECEPTACLE To the occupation 1, in chief, fulfill that the NLG chocks are in assign. Then, perceive-keep that the NLG doors are determinedtled. Effect positive that the NLG insurance referable attributable attributablehing is naturalized. The steering referable attributable attributablehing must be as required. Finally, fulfill that the A/C is electrically premiseed. NOTE: Everyudeablee: The A/C can besides be premiseed from the MLG. Guide the occupation 9, fulfill that the outer ability is associateed and serviceable. U3U06191 – U0O35M0 – UM01D4000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 42 SINGLE AISLE TECHNICAL TRAINING MANUAL
U3U06191 – U0O35M0 – UM01D4000000001 STEP BY STEP & NOSE STATION AND EXTERNAL POWER RECEPTACLE MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 43 SINGLE AISLE TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) RIGHT AND LEFT MLG STATION The occupation 2 and 7 hold of inspecting the Direct (R) and Left (L) MLG. Initiate by reimportunate that the MLG door is determinedtled. Then, fulfill that the MLG insurance sleeve is naturalized. Finally, perceive-keep that the MLG chocks are in assign. To the left occupation, the Ram Air Turbine (RAT) stowed comcomsituation insurance invention must be naturalized.
U3U06191 – U0O35M0 – UM01D4000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 44 SINGLE AISLE TECHNICAL TRAINING MANUAL U3U06191 – U0O35M0 – UM01D4000000001 RIGHT 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 occupation 3, the chief man to do is to effect positive that the engine direct and left behalf advance doors are secure.
The corresponding must be dindividual on occupation 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 Repress that the engine raise cowls and drive demolisher cowls are secure. 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 EXTERNAL VISIT (3) May 10, 2006 Page 49 SINGLE AISLE TECHNICAL TRAINING MANUAL
MAINTENANCE EXTERNAL VISIT (3) RIGHT AND LEFT WING STATION The R and L wing are the 4 and 5 occupations. Perpetuate the comcomsituation 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 occupation 8, you accept to effect positive that the A/C area is pure and serene 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 AISLE 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 REAR AND OVERHEAD C/B PANELS
Initiate by reimportunate that the evolution C/Bs and the aloft C/Bs are in determinedtled composition. 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 PANELS 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 EQUIPMENT
Then, accept a face the crisis equipment. This holds in fulfilling that the evade ropes are confer-upon, observing that the vital-principle extinguisher is in composition, making positive that the cockpit is equipped with steam hoods, reimportunate that the vital-principle protective gloves are confer-upon, ensuring that the clash axe is in composition, reimportunate that the cockpit is equipped with existence kobes, fulfilling that the oxygen masks are confer-upon and observing that the glitter whitishs are in composition. 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 cpenetrate foot, fulfill that the hasten wilderness laborerle is in the retract/ungird composition. If the hasten wilderness laborerle disagrees with the demeanor composition, defence enjoyment is ascribable. Effect positive that the drive levers are in the IDLE composition.
ENG MASTER SWs 1 and 2 must be in the OFF comcomsituation and the engine reason jurisdiction choiceor in the NORMal composition. Perceive-keep that the flap laborerle is established according to demeanor composition. If engine demolisher cowls accept to be opened guide defence enjoyment, the slats must be retracted. Repress that the radar is unstudied. Besides, fulfill that the Air Traffic Guide (ATC) transponder is unstudied. Effect positive that the starch goods production laborerle is in the reestablished and stowed composition. U3U06191 – U0O35M0 – UM01D4000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 58
SINGLE 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 TECHNICAL TRAINING MANUAL MAINTENANCE EXTERNAL VISIT (3) COCKPIT STATION (continued) OVERHEAD PANEL CHECK LIST AND A/C POWER SUPPLY You must then effect positive that the wipers are unstudied. BATteries 1 & 2 P/BSWs must be OFF and the voltage should be abquenched 25 volts. Proceed by establishedting the BAT 1 P/BSW to AUTO composition. Then, established the BAT 2 P/BSW to AUTO composition.
NOTE: Everyudeablee: if BAT voltage is adown 25V, a charging cycle of 20 minutes is required. Repress that the direct laborer dome whitish is on. A/C ability contribute process: On the aloft panel, established the EXTernal PoWeR P/BSW to ON. Besides, established the GEN 1 P/BSW to ON and the GEN 2 P/BSW to ON. Scan and repress that no amber whitishs are on exclude GENerator (GEN) 1 and GEN 2 FAULT whitishs on panel 35VU. The GALY & CAB P/BSW should be as required. Finally, fulfill there is no whitish on the scent panel. The A/C is now responsive to defence. U3U06191 – U0O35M0 – UM01D4000000001 MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES
MAINTENANCE 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 SAFETY CHECK LIST COMPLETED On the agent panel, effect positive that the L/G lever is in the down comcomsituation and perpetuate that the three unseasoned arrows on the L/G panel are on.
The guide insurance CL should now accept been elegant. 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 SAFETY CHECK LIST COMPLETED MAINTENANCE COURSE – CAT A (V2500-A5/ME) AIRCRAFT GENERAL PRACTICES MAINTENANCE EXTERNAL VISIT (3) May 10, 2006 Page 63

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