Peters2202 Word Scramble
|
Embed Code - If you would like this activity on your web page, copy the script below and paste it into your web page.
Normal Size Small Size show me how
Normal Size Small Size show me how
| Question | Answer |
| What is the main stress aircraft rivets are designed to take? Keep in mind that rivets join metal together in an environment subject to continual flexing, and expansion and contraction. | Shear |
| A type of fuselage construction designed to have the loads carried and transmitted by the substructure (for example: stringers and longerons) is known as: | Semi-Monocoque |
| A width measurement left or right of the vertical center line of the aircraft is the: | Butt Line |
| The property which enables a metal to return to its original shape, when the force which causes the change of shape is removed is known as: | Elasticity |
| The neutral axis of a bend is: | a line created by the points where the compressive load of the bend equals the tension load |
| Bend allowance refers to the | amount of material in a flat-pattern layout that must be allocated to make a bend |
| Setback is the | distance between the bend tangent line and the mold point |
| The radius of a universal rivet set used to drive rivets is | slightly greater than that of the appropriate rivet head |
| The proper drill bit for an MS20470AD3-4 rivet is a number: | 40 |
| The minimum acceptable dimensions, where D equals the diameter of the shank, for a properly driven rivet buck tail is | height 0.50 D, width 1.5 D |
| Which of the following is not a type of aircraft flap? | Rutan |
| Which rivet should be used for joining two pieces of 0.020 inch aluminum alloy? Keep in mind the standard for determining the length and width of rivets. | MS20470AD3-3 |
| A universal head rivet is identified by the number | MS20470 |
| What is the bend allowance for a 90-degree bend in a piece of 0.064 inch material bent over a 3/16 inch radius? | 0.340 |
| Why can aviation snips cut ticker metal than common hand snips? | They have a compound leverage type handle design |
| As a general rule the diameter of a rivet should be | Equal to three times the thickness of the thickness sheet of the joint material |
| K-factor charts calculate | The setback |
| What color cleco fastener is used for a #11 hole? | Brass |
| True or False, the spring brake is not a straight line sheet metal forming machine | True |
| The use of pencils for marking on sheet metal parts should be avoided because | They harden the sheet in area of the mark |
| Clad aluminum alloys are used on aircraft because they | Are less subject to corrosion than uncoated aluminum alloys |
| True or false, cantilever wings have no external bracing. | True |
| When fabricating part from alclad 2024-T3 aluminum sheet stock, | When possible all bends should be made across the grain of the metal (not parallel to the grain direction) |
| The purpose of a relief hole is to | lighten the metal |
| Monocoque fuselages derive their principle strength from | Bulkheads, formers and skin |
| Minimum edge distance for universal head rivets is | 2 Diameters |
| True or false? Rivet edge distance is measured form the center of the rivet to the nearest edge. | True |
| When aluminum alloys are heat treated to their critical temperature and quenched, it is_____________ heat treated. | Solution |
| A rivet with a raised dot on the head would be a | 2017 |
| A rivet designated as a DD rivet would be which type of alloy? | 2024 |
| When brazing, the filler rod should be melted by | Touching the rod to the hot metal |
| __________ is the force per unit area tending to stretch a structural member. | Tension |
| ______________ is actually a combination of two forces acting upon a structural member at one or more points. | Bending |
| Damages that can be repaired by patching, splicing, and insertion without imparment of the original strength is considered: | Repairable damage |
| Whenever possible, use of an elongated octagonal patch for a repair of a smooth skin because this type of patch | Eliminates dangerous stress concentrations |
| The design of major structural repairs not included in the aircraft’s maintenance or structural repair manual must be | Submitted on a form 337 and approved by the FAA |
| The primary function of a fastener in a lap joint is to | Transmit the loads from one layer of the patch to another |
| What should be the included angle of a twist drill for standard sheet metal work? | 118 |
| The load-carrying capabilities of a rivet of any given material are a function of the | the diameter of the rivet |
| What is the usual result of making a bend with too small a radius? | the material is likely to crack |
| What is not a factors that enters into the amount of material required for bend allowance? | coarseness of the material |
| The proper drill bit for an AN470AD5-6 rivet is a number | 21 |
| What must be done to the face of a bucking bar to prevent its marring the rivet? | keep it clean and polished (smooth) |
| What is the best way of accurately locating a rivet hole for drilling in a sheet metal skin? | use a center punch |
| The following metal and rivet combination would be properly matched. | AN470AD4 rivets in .040 2024 sheet |
| When comparing the machining techniques for stainless steel sheet material to those for aluminum alloy sheet, it is normally considered good practice to drill the stainless steel at a | lower speed with more pressure applied to the drill |
| In making wing skin repairs, | rivets selected should be the same alloy as the material being riveted. |
| The identifying marks on the heads of aluminum alloy rivets indicate the | specific alloy used in the manufacture of the rivet. |
| What is the purpose of refrigerating 2017 and 2024 aluminum alloy rivets after heat treatment? | retard age hardening |
| What is the purpose of a lightening hole in a wing rib? | to reduce weight without reducing strength |
| Why should the edges of a circular patch be chamfered and turned down slightly? | to provide a tighter fit on the skin surface |
| A file with two rows of teeth, one row set at 75 degrees and the other row set at 45 degrees, is known as a _____________ file | Double cut |
| How large should the center punch mark be for starting a drill in aluminum alloy skin? | just large enough for the drill to begin cutting, but not made heavy enough to distort the skin. |
| Where a rectangular cutout is used, the radius at each corner should be no less than __________ inch. | 1/2 |
| The starting and ending points of the bend are known as | Bend Tangent Lines |
| Why should a carburizing flame be avoided when welding steel? | it hardens the surface |
| Which item listed below is the most important consideration when selecting a welding rod? | type of metal to be welded |
| In gas welding, the amount of heat applied to material being welded is controlled by | the size of the tip opening |
| In electric-arc welding, the arc is struck between the metal to be welded and the | electrode |
| A flashback is | the burning back of the flame into (or behind) the mixing chamber of the torch |
| An oxyacetylene flame whose inner cone has a sharp point and burns with a hissing sound is a/an: | oxidizing flame |
| Acetylene hoses are | red with left-hand thread fittings |
| Which is correct concerning the use of a file? | Apply pressure on the forward stroke, only, except when filing very soft metals such as lead or annealed aluminum |
| The primary alloying agent of 2024-T36 is indicated by the number | 2 |
| Which rivet may be used as received without further treatment? | 2117-T3 |
| A piece of flat stock that is to be bent to a closed angle of 15 degrees must be bent through an angle of | 165 degrees |
| The purpose of a joggle is to | Allow clearance for a sheet or an extrusion |
| Welding over a brazed or soldered joint is | Not permitted |
| In selecting a torch tip size to use in welding, the size of the tip opening determines the | Amount of heat applied to the work |
| Filing or grinding a weld bead | Reduces the strength of the joint |
| What is the bend allowance for .040 material thickness, 3/16th bend radius, with a 85° bend? | .305 |
| What is the bend allowance for .064 material thickness, 1/8th bend radius, with a 45° bend? | .120 |
| What is the set back for .040 material thickness, 3/16th bend radius, with a 85° bend? | 208 |
| What is the set back for .064 material thickness, 1/8th bend radius, with a 45° bend? | .078 |
| What is the set back for .040 material thickness, 1/8th bend radius, with a 60° bend? | .095 |
Created by:
PetersAviation