Banco Taller de sillas RNG

1. What is the first step in the procedure for removing air bubbles under the decor foil?. Make a hole in the bubbles with a needle. Apply the adhesive with a syringe. Examine the decor foil and use a marker to put circular marks around the bubbles. Wait a few minutes until the decor foil returns to its initial shape.

2. In the replacement of decor foil attached with heat-activated adhesive, what is the recommended temperature for using vacuum equipment to bond the foil?. 100 deg.C (212.00 deg.F). 80 deg.C (176.00 deg.F). 70 deg.C (158.00 deg.F). 90 deg.C (194.00 deg.F).

3. When installing a new decor foil attached with pressure-sensitive adhesive, what is the recommended action after removing the protective layer from the foil?. Apply the adhesive to the decor foil with a brush. Bond the decor foil to the repair area with vacuum equipment. Slowly pull the decor foil from the component while applying hot air. Push the decor foil on the repair area with a rubber roller starting at the center.

4. How long should you let the adhesive dry at room temperature when using Contact Adhesive-Rubber & Plastic Bonding Nitrile base in the heat-activated adhesive replacement procedure?. 2 hours. 45 minutes. 15 minutes. 12 hours.

5. Which material is recommended for cleaning the repair area before installing a new decor foil?. Non Aqueous Cleaner--Isopropyl Alcohol and a lint-free cotton textile. Water and soap solution. Non Aqueous Cleaner--Methyl-Ethyl-Ketone and a lint-free cotton textile. Rubber roller.

6. What should be done if unwanted adhesive remains after removing air bubbles under the decor foil?. Apply more adhesive to the repair area. Use a scraper to immediately remove the unwanted adhesive. Use a needle to make a hole in the bubbles. Wait for the adhesive to cure completely.

7. During the removal of damaged decor foil attached with heat-activated adhesive, what is the maximum temperature for the hot air blower?. 70 deg.C (158.00 deg.F). 90 deg.C (194.00 deg.F). 100 deg.C (212.00 deg.F). 150 deg.C (302.00 deg.F).

8. What type of gloves should be worn during the removal of damaged decor foil to prevent burns from the hot air blower?. Latex gloves. Insulated gloves. Cotton gloves. Nitrile gloves.

9. How should the surface be smoothed after removing air bubbles and curing the adhesive?. Apply pressure with a lint-free cotton textile. Use a hot air blower. Smooth with a rubber roller starting at the center of the repair area. Use a cloth-emery.

10. What is the recommended relative humidity range for replacing decor foil attached with heat-activated adhesive?. 15-45%. 20-60%. 25-50%. 35-75%.

11. Which type of parts have decorative surfaces and are used for interiors?. Type I. Type II. Type III. Type IV.

12. What is required for suppliers before shipping THERMOPLASTIC PARTS Class 3 production parts?. Approval on BAC5321 QPL. No first-part qualification. AS9100 accreditation. Consideration as Class 1.

13. If an engineering drawing shows a Type I classification but no class designation, how should it be treated?. Class 2. Class 3. Class 1. It varies.

14. What additional approval might be required prior to production aside from the QPL listing?. D1-4426 accreditation. BAC5321 QPL. Type I classification. Class 2 qualification.

15. Which class includes microcellular-foamed parts that require first-part qualification?. Class 1. Class 2. Class 3. Class 4.

16. Which document must processors be listed on to mold parts from BMS8-269 polyamide-imide (PAI) resins?. D042T612. BAC5321 QPL. Table I. Section 9.

17. Under what condition can regrind be used for production THERMOPLASTIC PARTS?. When authorized on the Engineering drawing. When approved by the processor. When it meets Table I requirements. When listed in Section 9.

18. Which class of parts for THERMOPLASTIC PARTS may require additional evaluation for using specific resins?. Class 1. Class 2. Class 3. Class 4.

19. Which resin is not mentioned as compatible with for THERMOPLASTIC PARTSClass 3 processing?. BMS8-251 Polycarbonate. BMS8-321 Polyetherimide. BMS8-328 Polyphenylsulfone. BMS8-269 Polyamide-imide.

20. What must gases used for for THERMOPLASTIC PARTS Class 3 parts comply with?. D042T612. BAC5321 QPL. Table I requirements. Section 9 requirements.

21. How should raw materials for THERMOPLASTIC PARTS be stored and handled?. According to Boeing's guidelines. According to resin manufacturer's recommendations. According to processor's guidelines. According to customer specifications.

22. What should be done with damaged, contaminated, or spilled raw materials for THERMOPLASTIC PARTS?. Recycled. Reprocessed. Discarded. Stored separately.

23. What must be maintained if raw materials for THERMOPLASTIC PARTS are moved to a new container?. A. Color consistency. B. Temperature. C. Traceability. D. Moisture levels.

24. When raw materials for THERMOPLASTIC PARTS are moved to a new container, what must be done with the previous labeling?. Covered up. Modified. Kept intact. Removed.

25. How should Boeing Material Specification (BMS) raw-materials for THERMOPLASTIC PARTS be stored and handled?. To ensure quality. To minimize space. To maintain traceability to the resin manufacturer's certificate. To comply with environmental regulations.

26. What does a Boeing Approval Notice include?. A letter from the supplier. Boeing test report number and issue date. A summary of quality control procedures. A list of approved suppliers.

27. How is an Engineering Drawing defined in this specification for THERMOPLASTIC PARTS?. A manually produced drawing. A collection of product definition data. A digital-only dataset. A pictorial presentation.

28. What are Exterior THERMOPLASTIC PARTS intended for?. Use outside the aircraft pressure shell. Use within the aircraft pressure shell. Use in cargo compartments. Use in aircraft interiors.

29. What is "Flash" in the context of injection molding in THERMOPLASTIC PARTS?. A layer of closed cells in part interiors. Excess material forced out between mold surfaces. A type of resin. A specific parting line.

30. What is a Letter of Certification (LOC)for THERMOPLASTIC PARTS ?. A letter containing test data and referencing Boeing Approval Notices. A document outlining production schedules. A certification of raw material quality. A Boeing internal memo.

31. Which type of dryers can be used for drying THERMOPLASTIC PARTS molding pellets?. Microwave ovens. Desiccated bulk resin dryers. Infrared heaters. Steam dryers.

32. When must the THERMOPLASTIC PARTS resin pellets be dried?. After introducing them into the molding machine hopper. During the molding process. Prior to introducing them into the molding machine hopper. After the production run.

33. What should the moisture content of the resin be measured with?. A thermometer. A moisture analyzer. A hygrometer. A barometer.

34. What should be done with THERMOPLASTIC PARTS material dried at a temperature higher than the manufacturer's recommended maximum?. It can be used in production parts. It should be re-dried. It must not be used in production parts. It should be cooled down.

35. How must the dew point level be monitored in the THERMOPLASTIC PARTS when using desiccated bulk resin dryers?. With a thermometer. With a moisture analyzer. With a hygrometer. With a dew point meter.

36. What must be ensured about the molding machines during production THERMOPLASTIC PARTS ?. They must be newly purchased. They must have enough temperature, injection pressure, and platen clamping force capability. They must be approved by Boeing. They must be operated manually.

37. What must be maintained during the initial and all subsequent production runs of the THERMOPLASTIC PARTS ?. Consistent color of the parts. Adherence to the established processing parameters. Continuous operation without breaks. Uniform size of the parts.

38. When must deviations greater than 2 percent of the established parameters for THERMOPLASTIC PARTS be noted and justified?. When they occur once. When they occur in five or more parameters during a given production run. When they do not affect the final product. When they are minor.

39. How must flash and gates be trimmed for Type I and III THERMOPLASTIC PARTS?. To under 0.010 inch protrusion. To under 0.005 inch protrusion. To exactly 0.005 inch protrusion. To exactly 0.010 inch protrusion.

40. How should completed THERMOPLASTIC PARTS be marked when enough area is available?. With a barcode. With a QR code. With molded-in raised lettering. With embossed numbers.

41. What information must be included when marking completed THERMOPLASTIC PARTS?. Part number, processor's identification, and date of manufacture. Part number and date of manufacture only. Part number, unit serial number, and date of manufacture. Part number and unit serial number only.

42. When should the unit serial number be included in the THERMOPLASTIC PARTS marking?. Always. Only when called out by Engineering drawing. Only for Class 1 parts. Only for Class 2 parts.

43. How must the THERMOPLASTIC PARTS be identified?. With a sticker. With stamped letters. With molded-in raised lettering or in accordance with BAC5307. With handwritten information.

44. What method is specified for marking completed THERMOPLASTIC PARTS?. Raised lettering only. Embossed numbers only. Either raised lettering or in accordance with BAC5307. Stamped letters only.

45. What must be included in the Seat Shell Assembly B787? markings when enough area is available?. Part number, unit serial number, processor's identification, and date of manufacture. Part number, unit serial number, processor's identification, and manufacturing location. Part number, unit serial number, and date of manufacture. Part number, manufacturing location, and date of manufacture.

46. How should seat backs be deployed and stowed for the Seat Shell Assembly B787?. By pressing a button. By lifting the armrests. By pulling up on the loop or notch at the aft edge of the food tray. By rotating them 180° in the vertical plane.

48. What happens to the fire blocking capacity of the fabric of the Seat Shell Assembly B787 after twenty washings?. It remains the same. It decreases. It increases. It becomes waterproof.

49. What factors affect the thermal performance of cushions of the Seat Shell Assembly B787 ?. The material and the cushion's size. The cushion's cleanliness and the density of the cushions. The cushion's firmness and the material. The cushion's color and the foam's texture.

50. What component is found in the front section of the Seat Shell Assembly B787 and is used for storing headphones and sunglasses?. Headphone/sunglasses stowage compartment. Cocktail table. Life vest stowage compartment. Monitor.

51. What is a feature of the components visible in the Seat Shell Assembly B787?. Metallic finishes. Decorative finishes, upholstery, or bonded decorative laminate. Wood finishes. Matte finishes.

53. What is the function of the bumpers installed on the Seat Shell Assembly B787 ?. Protect against accidental damage to the panels. Serve as footrests. Hang coats. Enhance air ventilation.

54. What is found in the rear section of the Seat Shell Assembly B787 , specifically in certain part numbers?. Seat cushion support assembly. Coat hook. Monitor. Decompression grilles.

87. What is the main material used for the column of the captain and first officer seats PN TAAI1-03 SERIES?. Composite material. Aluminum. Light alloy. Filament winding composite material.

88. Which part of the captain and first officer seats PN TAAI1-03 SERIES is responsible for the inclination of the armrests and can be adjusted up to 24°?. Lower part. Seat back rest. Armrest. Lumbar rest.

89. What material is used for the structure of the lumbar rest arms of the captain and first officer seats PN TAAI1-03 SERIES?. Composite material. Aluminum. Light alloy. Integral skin foam.

90. How is the assist armrest assembly of the captain and first officer seats PN TAAI1-03 SERIES kept in its storage position?. Gas cylinder. Spring. Hydraulic piston. Rack and pinion mechanism.

91. Where is the control mechanism for adjusting the head rest of the first officer seat PN TAAI1-03 SERIES?. Right of the captain's seat. Left of the first officer's seat. On the captain's armrest. On the first officer's armrest.

92. What is the range of reclining for the seat back of the captain and first officer seats PN TAAI1-03 SERIES ?. -7° to -27°. -10° to -30°. -5° to -25°. -15° to -35°.

93. Which component of the lumbar rest of the captain and first officer seats PN TAAI1-03 SERIES is responsible for vertical adjustment?. Pinions. Racks. Rack pinions on cams. Swivel rest pallet.

94. How is the assist armrest assembly of the captain and first officer seats PN TAAI1-03 SERIES adjusted in relation to a horizontal plane?. Gas cylinder. Spring. Hydraulic piston. Aluminum alloy carrier arm.

95. What material are the armrest shrouds of the captain and first officer seats PN TAAI1-03 SERIES made of?. Composite material. Aluminum. Light alloy. Integral skin foam.

96. What is the purpose of the gas cylinder in the assist armrest assembly of the captain and first officer seats PN TAAI1-03 SERIES ?. To adjust armrest inclination. To keep the armrest in storage position. To lock the armrest in place. To control vertical adjustment.

97. What is the mechanism used to adjust the inclination of the armrests of the captain and first officer seats PN TAAI1-03 SERIES?. Lever. Hydraulic piston. Gas cylinder. Spring.

98. How many parts constitute the lower part of the captain and first officer seats PN TAAI1-03 SERIES ?. One. Two. Three. Four.

99. What is the material of the main structure of the armrests of the captain and first officer seats PN TAAI1-03 SERIES ?. Composite material. Aluminum. Light alloy. Integral skin foam.

100. Which part of the captain and first officer seats PN TAAI1-03 SERIES is responsible for the depth adjustment of the lumbar rest?. Lumbar rest arms. Lumbar rest mechanism. Lumbar rest hinge. Lumbar rest structure.

101. What is the range of vertical displacement for the head rest of the captain and first officer seats PN TAAI1-03 SERIES?. 90 mm. 100 mm. 110 mm. 120 mm.

102. What is the angle of forward incline for the head rest of the captain and first officer seats PN TAAI1-03 SERIES?. 20°. 23°. 25°. 27°.

103. How is the storage position of the assist armrest assembly of the captain and first officer seats PN TAAI1-03 SERIES maintained?. Gas cylinder. Hydraulic piston. Spring. Rack and pinion mechanism.

104. Where is the control mechanism for adjusting the lumbar rest of the captain and first officer seatsPN TAAI1-03 SERIES located?. On the captain's armrest. On the first officer's armrest. On the lumbar rest arms. On the seat back rest.

105. What is the material of the column of the captain and first officer seats PN TAAI1-03 SERIES?. Composite material. Aluminum. Light alloy. Filament winding composite material.

106. What is the purpose of the gas cylinder in the assist armrest assembly of the captain and first officer seats PN TAAI1-03 SERIES ?. To adjust armrest inclination. To keep the armrest in storage position. To lock the armrest in place. To control vertical adjustment.

107. What material connects the seat to the aircraft floor in the lower part for the P/N TAA12-13 SERIES?. Aluminum alloy. Composite material. Light alloy panel. Steel.

108. How are the armrests adjusted for the P/N TAA12-13 SERIES?. Electrically. Manually. Automatically. Mechanically.

109. Which mechanism is responsible for the longitudinal displacement of the seat bottom for the P/N TAA12-13 SERIES?. Needle bearing. Gear actuator. Reduction gear. Electric motor.

110. What is the purpose of the AVIAC and LABINAL actuators for the P/N TAA12-13 SERIES?. To adjust recline. To control power. To move the seat. To operate the brakes.

111. How does the AVIAC actuator differ from the LABINAL actuator internally for the P/N TAA12-13 SERIES?. Different motors. Different gears. Different brakes. Different sensors.

112. How does the AVIAC actuator respond to over torque conditions for the P/N TAA12-13 SERIES?. Cuts off power using switches. Stops immediately. Applies peak current. Releases gear mechanism.

113. What allows for manual override of the electrical displacement of the seat bottom for the P/N TAA12-13 SERIES?. Needle bearing. Gear actuator. Mechanical control. Electric motor.

114. How is the vertical displacement of the seat controlled electrically for the P/N TAA12-13 SERIES?. Joystick control. Button control. Handle control. Lever control.

115. How is the vertical displacement of the seat overridden mechanically for the P/N TAA12-13 SERIES?. Handle V. Handle R. Handle H. Handle L.

116. How is the seat backrest adjusted electrically within its reclining limits for the P/N TAA12-13 SERIES?. Joystick control. Button control. Handle control. Lever control.

117. How is the headrest adjusted for the P/N TAA12-13 SERIES?. Knob control. Button control. Lever control. Handle control.

118. What controls the lumbar rest's vertical and horizontal positions for the P/N TAA12-13 SERIES?. Knob and button. Lever and knob. Button and lever. Joystick and knob.

119. How is the armrest adjusted for the P/N TAA12-13 SERIES?. Button control. Lever control. Knob control. Handle control.

120. How is the storage position of the armrest achieved for the P/N TAA12-13 SERIES?. Button control. Lever control. Knob control. Handle control.

121. What adjusts the assist armrest's tilt and inclination for the P/N TAA12-13 SERIES?. Knob control. Lever control. Button control. Handle control.

122. What materials make up the structure of the armrest for the P/N TAA12-13 SERIES?. Steel. Light alloy. Composite material. Aluminum alloy.

123. What mechanism is responsible for the locking of the seat bottom in the horizontal or vertical direction for the P/N TAA12-13 SERIES?. Gear actuator. Needle bearing. Reduction gear. Electric motor.

124. How does the LABINAL actuator respond to over current conditions for the P/N TAA12-13 SERIES?. Cuts off power using sensors. Stops immediately. Applies peak current. Releases gear mechanism.

125. What action is required to manually override the electrical displacement of the seat back for the P/N TAA12-13 SERIES?. Handle V. Handle R. Handle H. Handle L.

126. Which component enables the passage of the control column for the TAA12-13 SERIES seat?. Assist armrest. Seat bottom. Armrest. Seat back rest.

127. Which material is used in the construction of the base frame of seat 3710C TYPE U92 SERIES?. Steel. Aluminum. Plastic. Carbon fiber.

128. How does the seatpan of the seat 3710C TYPE U92 SERIES ensure passenger stability during strong turbulences?. It has safety straps. It holds the pelvis in the correct sitting position. It has an inflatable cushion. It has a rubber edge.

129. What is a feature of the seatpan in the exit area of seat 3710C TYPE U92 SERIES?. It is made of steel. It has a fixed front edge. It has an elastic front edge. It is reinforced with carbon fiber.

130. How is the seat bottom cushion attached to the seatpan in the seat 3710C TYPE U92 SERIES?. Using screws. Using glue. It is stitched. It is attached to the seatpan.

131. What specific support does the backrest cushion of seat 3710C TYPE U92 SERIES provide?. Shoulder support. Lumbar and side support. Neck support. Full back support.

132. How are the dress covers attached to the cushions in the seat 3710C TYPE U92 SERIES?. They are stapled. They are sewn together. They are attached with Velcro. They are glued.

133. Why do some backrests in the seat 3710C TYPE U92 SERIES not have a literature pocket?. It is an optional feature. They are designed for first-class seats. They are intended for seats with no place behind. They are for emergency exits only.

134. What ensures maximum legroom for the passenger behind in the seat 3710C TYPE U92 SERIES?. The slim backrest construction. The adjustable seat height. The position of the armrest. The lightweight base frame.

135. What is unique about the backrest table assembly in the seat 3710C TYPE U92 SERIES?. It can be detached. It is a one-piece table with cup recess. It has multiple adjustable positions. It is made of plastic.

136. What feature is specific to the IAT armrest in the seat 3710C TYPE U92 SERIES?. It is non-movable. It contains a table for passengers without a backrest food tray. It has built-in storage compartments. It is made of steel.

137. How can the seat 3710C TYPE U92 SERIES be moved or removed from its position?. By loosening the screws. By using the quick-detach feature. By unhooking the seat legs. By unlocking the armrests.

138. What is the correct procedure for deploying the food tray in the seat 3710C TYPE U92 SERIES?. Press a button and pull the tray. Open the fastener, fold out the tray, and move it to the desired position. Unhook the tray and pull it down. Rotate the tray from under the armrest.

139. What must be done to the seat belts in the seat 3710C TYPE U92 SERIES before the start of the aircraft?. They must be removed. They must be locked. They must be adjusted to maximum length. They must be cleaned.

140. How do you access the life vest in the seat 3710C TYPE U92 SERIES?. Pull the pull-strap on the front side. Open the compartment under the seat. Reach under the seat cushion. Press a button on the armrest.

141. What ensures that baggage does not move under the seat 3710C TYPE U92 SERIES?. A baggage net. A baggage bar assembly. Adjustable straps. Non-slip material.

142. How are the front and rear seatlegs of seat 3710C TYPE U92 SERIES attached to the aircraft floor?. Using Velcro. They are welded. With a front stud and a 3-stud rear fitting. Using adhesive.

143. What method is used to attach cushions and dress covers to the seat structure in seat 3710C TYPE U92 SERIES?. Glue. Hook and loop tapes. Bolts. Magnets.

144. What action is needed to deploy the in-armrest table in the seat 3710C TYPE U92 SERIES?. Press a button and pull. Open the armcap, hold the handle, and turn up the table. Lift the armrest and pull the table out. Slide the table out.

145. How do you unlock the handicap armrest in the seat 3710C TYPE U92 SERIES?. Push the lever underneath the armrest. Pull the handle on the side. Press the button on top. Slide the armrest up.

146. What indicates that the handicap armrest in the seat 3710C TYPE U92 SERIES is locked in place?. A green light. A "click" sound. A visual marker. An indicator flag.

147. Which material is used in the construction of the base frame of seat 3710D TYPE - U93 SERIE?. Steel. Aluminum. Plastic. Carbon fiber.

148. What is the purpose of the shape of the seat bottom in seat 3710D TYPE - U93 SERIE?. To provide lumbar support. To hold the pelvis in the correct sitting position. To prevent back pain. To reduce seat weight.

149. What feature does the seat bottom in the exit area of seat 3710D TYPE - U93 SERIE have for better seating comfort?. Elastic front edge. Extra padding. Adjustable height. Reclining capability.

150. How is the seat bottom cushion attached to the seatpan in seat 3710D TYPE - U93 SERIE?. Using screws. Using glue. It is attached to the seatpan. It is stitched.

151. What ergonomic features are provided by the backrest cover in seat 3710D TYPE - U93 SERIE?. Neck support. Lumbar and side support. Shoulder support. Full back support.

152. How are the dress covers attached to the seat structure in seat 3710D TYPE - U93 SERIE?. They are stapled. They are sewn together. They are attached with Velcro. They are glued.

153. What is the literature pocket in seat 3710D TYPE - U93 SERIE made of?. Plastic. Netting. Fabric. Leather.

154. Why do some backrests in seat 3710D TYPE - U93 SERIE not have a literature pocket?. It is an optional feature. They are designed for first-class seats. They are intended for seats with no place behind. They are for emergency exits only.

155. What ensures maximum legroom for the passenger behind in seat 3710D TYPE - U93 SERIE?. The slim backrest construction. The adjustable seat height. The position of the armrest. The lightweight base frame.

156. Which of the following is not an optional feature of the backrests in seat 3710D TYPE - U93 SERIE?. Coat hook. Cup holder. Integrated table retainer. Tablet holder.

157. What material is the standard armrest in seat 3710D TYPE - U93 SERIE made of?. Aluminum. Plastic injection moulding. Steel. Wood.

158. Which armrests in seat 3710D TYPE - U93 SERIE are movable?. Wall side armrests. All armrests. Handicap-solution aisle side and center armrests. None of the armrests.

159. What feature is specific to the IAT armrest in seat 3710D TYPE - U93 SERIE?. It contains a table for each passenger without a backrest food tray. It is non-movable. It has built-in storage compartments. It is made of steel.

160. How is the table backrest assembly in seat 3710D TYPE - U93 SERIE kept in the stowed position?. By a locking mechanism. By a magnetic latch. By a table release mechanism. By a friction fit.

161. Where is the IAT installed in seat 3710D TYPE - U93 SERIE?. In the backrests of all seats. In the armrests of the front-row seats. Under the seat cushions. In the overhead compartments.

162. How is the life vest accessed in seat 3710D TYPE - U93 SERIE?. By unzipping the seat cushion. By pressing a button. By pulling a pull-strap on the front side. By opening a compartment on the armrest.

163. What ensures that baggage does not move below seat 3710D TYPE - U93 SERIE?. A baggage net. A baggage bar assembly. Adjustable straps. Non-slip material.

164. How are the front and rear seatlegs of seat 3710D TYPE - U93 SERIE attached to the aircraft floor?. Using Velcro. They are welded. With a front stud and a 3-stud rear fitting. Using adhesive.