TML TEÓRICO 2026

The main structural units on the aircraft are?. Fuselage, wings, stabilizers, flight control surface, main landing gear. Frames, stringers, keal beams.

What type of fuselage introduced new primate load carrying elements in on help to the skin?. Semimonocoque. Monocoque.

Structural wing elements are?. Front spart, rear spar, ribs, stringers, skin. Flaps, slats, spoilers, ailerons. Upper skin and lower skin.

The primary flight control surface are?. Ailerons, elevators, rudder. Wings, stabilizers, fuselage. Engines, APU, RAT.

Materials used in aircraft should meet the following requirements?. High resistance, light weight, high reliability. Low cost, light weight, los reliability.

Materials used in aircrafts receive 5 basics stresses?. Tensión, compresión, flexión, torsión, shear. Torsión, tensión, compresión, peel, cleavage.

Materials: aluminum, titanium, cooper, monel, belongs to the group called. Ferrous materials. Non ferrous materials.

The best method of joining pieces of aluminum is?. Welding. Riveting. Bonded.

Sheet that are made of high-strength aluminum alloy sandwiched between the layers of purealuminum are?. Alloy sheet. Alclad sheet. Bare sheet.

During a flight aircrafts receives 4 main loads, which are?. Lift, stress, drag, thrust. Weight, lift, drag, thrust. Thrust, weight, handling, drag.

A regulatory notice sent out by the authority aviation to the registered owner of an aircraft informinghim or her the discovery of a condition that prevents the aircraft from continuing to meet its conditions for airworthiness, they must be complied whith whithin the specified time limit. We are talking about?. Airworthiness directive. Service bulletin. Supplemental type certifícate.

A 12’’ ruler is an instrument used to make outside measurements with a mínimum accuracy of. 1/32. 1/128. 1/64.

Rivera length come expressed on?. 1/16’’s. 1/32’’ s.

Rivets diameter come expressed on?. 1/16’’ s. 1/32’’ s.

What is the information contained in the SRM?. Front Pages , introduction, SRI. Chapter 51 to 57. Front Pages and chapter 51 to 57. Chapters 51 and chapters 52 to 57.

What Kind of information give is the alphanumerical index?. Chapter subject section , figure number , Ítem number. List of chapters and their titles. Changes made to the manual and the date changes were made.

According to the numbering system used in the Airbus SRM, which sentence is correct?. The first elemet identifies the chapter and is assigned by the ATA 100. The third element identifies the subject and is assigned by the ATA 100. The seccond element identifies the subject and is assigned by Airbus.

Where you can find weight variant (WV) of an airplane an MSN ( Manufacturer Serial Number). Introduction specifically in the section called ‘’Airplane Allocation List’’. In chapter 51. At SRI (Structural Repair Inspection).

To which side of the airplane belongs to the following part number D52371105002. Left Side of Airplane. Right Side of Airplane.

What is the drawing number if we have the following part number: D53341106005. D533411060. D53341106. D54441106.

About the page block 001-009 what information they contain. Information to assess damage (Allowable Damage). Information to indentify the structure. Information to repair the structure.

About the page block 101-199, what information they contain?. Information to identify the structure. Information to assess damage (Allowable Damage). Information to repair the estructure.

About the page block 201-999 Pages , what information contain?. Information to identify the esctructure. Information to repair the estructure. Information to assess damage (Allowable Damage).

What is the title of the ATA 55. Nacelle & pylons. Stabilizers. Windows.

In which of these documents you can find additional information on materials like fastener or stgr specifications used in estructural repairs?. CML (list of consumables). AMM (Aircraft Maintenance Manual). SM ( Standards Manual).

On aircraft Airbus , fuselage stations are expressed in?. Centimeters. Meters. Inches.

If we have the part number D53110189128 in what side of the aircraft the will be installed?. L/H. R/H. Center line.

Talking about part usage, what element is the correct one?. Is customized. Is not customized.

If we have the part number D57110189200, what drawing number is the correct one ?. 571101892. D571101892. D57110189.

The drawing set is not subject to a regular revisión service, The about Statement is?. False. True.

What is the meaning of the first two numérical digits in the next drawing number: D53795432?. The ATA chapter number. Sequence number. Section number.

What is te meaning of: 05C05. Picture sheet 05 and zone C05. Schedule sheet 05 and zone C05. Part usage 05 and zone C05.

What elements make up the set of drawing?. Picture sheet, eschedule sheet, part usage. Picture sheet, schedule sheet, part usage , GAD. Picture sheet, schedule sheet, part usage, PMS, SM.

About the picture and schedule sheet related , which statement is the correct one?. Both document have the same drawing number. Both document have diferent drawing number.

Which document permit goes Down from an assembly or installation drawing to a detail drawing?. Part usage. Part list. DNI. Schedule sheet.

What kind of information is showed by the schedule sheet?. Contains the list of parts called-up (ÍTEMS) on the corresponding picture sheer(s). Dimensions and tolerances. Surface finish data.

Which document permit goes up from a detail drawing to an assembly or installation Drawing?. Schedule sheet. Part list. Part usage.

The amount of upward deflection of an almen strip ‘’A’’ is 0.019’, what is the valué of intesity?. 190. 19A. A19.

About shot used on flap peening, of what material are made of?. Tungsten carbide. Stailenss steel. Aluminum.

When do l remplace my flap?. When 20% of the shot is missing ( or after 30 minutes use). When 50% of the shot is missing. When 100% of the shot is missing.

What type of almen test strip must to be used if we need a intesity of 0.021’’. Type ‘’A’’. Type ‘’C’’. Type ‘’N’’.

About the tool to turn the flap, wicht characteristic must have?. Have to keep the speed witthin+/- 5% during the peening operation. Have to be pneumatic. Máximum weight of 5 pound.

How many points have to be used in order to genérate the saturation curve. 4 points. 6 points. Until the saturation time can be seen on the graph.

If magnetic partirle test is required , ir must be done. After flap peening process. Before flap peening process. Before or after flap peening process.

(Cold working) holes must be at right angles to the surface within a tolerance of…. + or - 2 degrees. 20 degrees. 0.2 degrees.

How is identify the tool in each cold expansión process?. Using STDN (Standard Tool Diameter Number). Using STDC ( Standar Tool diameter Code). Using model number key.

What is the categoría for mandrels?. Capital tooling. Durable tooling. Expandable tooling.

A stepped go/no go configuración pin allows one end to ensure starting hole is within thespecification tolerance prior to cold expansión’’ this is a description of…. Mandrel gafe. Mañero. Combination gafe.

It is used in conjuction with a mandrel to aloe a one-side operation, provide, lubrication, ensure, and protector the hole from damage. The name of this tool is…. Mandrel gafe. Blocks de respaldo. Sleeve.

Damage which can be respired by cutting away the damage section and replacing it whith a like section , then securing the insertion whit splices at each end is classified as. Negligible damage. Damage repairable by insertion. Damage repairable by patching. Damage necessitating replacement of part.

Corrosión is the deterioration of the metales by chemical or electrochemical attack. True. False.

Type of electro-chemical corrosión in nature, it occurs when dissimilar metals are in contact orotherwise connected electrically in the presence of an electrolyte. Exfoliation corrosión. Galvanic corrosión.

Also known as wear corrosión or friction oxidation. Fretting corrosión. Microbial corrosión. Pitting corrosión.

Something made up of different materials combined in such a way that the characteristics of theresulting material are different from those of any of the componets, is the concept of. Alloy. Composite. Honeycomb.

Which are the two general categories of plastic used in resin matrix system. Thermoplastic and thermoset. Thermosetting and época resin.

The greattest advantage for which composite materials are used is. Lower prices. Availability of materials. High strength to weight ratio.

What kind of information contains the SRI (Structural Repair Inspection). Information to inspect damages permissible within the limits and repairs. Information to inspect damages within the limits permissible only. Information to inspect repais only.

About the SRM , how is classified?. No custumized manual. Customized manual. Genéric manual.

What is the interpretatation of the Word ‘REPLACE’ in the part list section identifying the structure in the SRM?. The remplacement part is a recomendation. The replacement part is an obligation. A specific repair is available.

Which of the following is the definition of Allowable Damage?. Damage not affects the structural integrity of a part and the aircraft can continue to opérate. Applies only to composite structures. The aircraft has to be repaired before the next flight.

Whats is FRAME PITCH?. The distance between two adjacent frames. Is the distance between the first frame and the last frame of the aircraft. Is the distance from the datum the first frame of the aircraft.

What manual should be used if you have a damage at the engine nacelles?. The SRM engines (IAE V25000 or CFM56-X). The aircraft SRM. The AMM (Aircraft Maintenance Manual).

What chapters use this way of expressing effectivity CONFIG-1, CONFIG-2’ CONFIG-3, etc.?. Chapters 52 to 57. Chapter 52 and 57. Chapters 51 and 52.

At the present time, the most used reinforcing fibers are?. Fiberglass, boron, ceramic. Aramid, fiberglass, boron. Fiber glass, aramid , carbón/ graphithe.

Process that consist of applying severas layers of fabric material impregnated whith resin onto repairsurface, in order to restore the damage skin is. Prepreg. Wet-lay up. Fabric impregnation.

What kind of information is showed by the part usage. Dimensión and tolerances. Protective treatment data. NHA and effectivity.

How the Airbus drawings are divides?. Are divided into aircraft families. In AID & DD. Tool drawing Electrical Drawing.

In the PU, how how the effectivity is expressed?. Using the MSN. Using the weight variant number. Using the customer versión number.

Where are located the Airbus infernal specificationes ABD0001, ABD002 and ABD003?. SM. SRM. PMS.

Some schedule sheet may not have a picture sheet. True. False.

Complementary drawings are delivered. Six montes after first delivery. Are delivered at first aircraft delivery.

The picture sheet is customized, what does customized mean?. Can be used at any Airbus aircraft. Apply for All A320 Aircraft. Reflect the complete fleet configuration of an airplane.

What type of drawing is showed in the following part number D53795432200. Detail drawing. Assembly drawing. Installation drawing.

What is the meaning of the last four digits in the next drawing number D53795432. The ATA chapter number and section number. Sequence number. Desig office indentification.