EXAMEN ATA 51 STRUCTURES

What are the names and numbers of the Fuselage sections of the A319 aircraft?. Nose Fwd Fuselage(11/12), Fwd Fuselage(13/14 A), Center Fuselage(15), Rear Fuselage(16/17/18), Cone-Rear Fuselage(19/20). Fwd Fuselage(11/12), Center Fuselage(13/14), Rear Fuselage(15), cargo fuselage(16/17/18), cone-Rear Fuselage(19/20). Nose Fwd Fuselage(11/12), Fwd Fuselage(13/14), Center Fuselage(15), Rear Fuselage(16/17/18), Cone-Rear Fuselage(19/19.1).

Where are located (Frames numbers) the FWD and AFT Pressure BULKHEADS?. 1 / 87. 12 / 70. 1 / 70.

Which are the frames numbers of location of the rear fuselage for the aircraft A321?. 47 / 70. 47.5 / 70. 47 / 64.

What are the frames that support the center Wing Box in the center Fuselage Section (Section 15)?. 35, 47. 36, 42. 36, 45.

Where is located (Frames) the Nose Landing Gear Bay compartment?. Frames 9 / 20. Frames 12 / 20. Frames 3 / 9.

Which are the Frames of the Airbus A320 Family where changes occur to make from A320 the A319 or A321?. Fr 35 / Fr 47. Fr 35 / Fr 45. Fr 37 / Fr 47.

What are the frames numbers where the VERTICAL STABILIZER connects to the Fuselage?. Fr 70, 71, 72. Fr 70, 72, 74. Fr 74, 76, 78.

What is the material used in the manufacturing of the Fwd Upper Fuselage - Cockpit (Section 11)?. Alluminum Alloys. CFRP. Titanium Alloys.

What is the section number of the Nose Forward Fuselage Section (Manufacturing Procedures)?. 11/12. 13/14. 12/13.

What does a structural Cut-out means?. A support. A hole. A kind of Rivets.

What is the material of construction for the APU Doors?. Alluminum alloy & Titanium. CFRP. AFRP.

What is the meaning of Longitudinal Skin joints?. It is the connection between the main fuselage sections. It is the connection between skins in a fuselage sections.

What is the meaning of Circumferential Skin joints?. It is the connection between the main fuselage sections. It is the connection between skins in a fuselage sections. It is the connection between the horizontal and vertical stabilizer.

What are the names and numbers of the Fuselage sections of the A321 aircraft?. Nose Fwd Fuselage(11/12), Fwd Fuselage(13/14 A), Center Fuselage(15), Rear Fuselage(16A/16/17/18), Cone-Rear Fuselage(19/19.1). Fwd Fuselage(11/12), Center Fuselage(13/14), Rear Fuselage(15), cargo fuselage(16/17/18), cone-Rear Fuselage(19/20). Nose Fwd Fuselage(11/12), Fwd Fuselage(13/14), Center Fuselage(15), Rear Fuselage(16/17/18), Cone-Rear Fuselage(19/19.1).

Which section of the fuselage is connected by lugs instead of Circumferential skin Joint. Section 18. Section 19. Section 19.1.

What is the material of construction for the MLG Doors?. Alluminum alloy. CFRP. AFRP.

What is the section number of the REAR and CONE Fuselage Section (Manufacturing Procedures)?. 18 / 18.1. 17/ 17.1. 19 / 19.1.

What is the material of construction for the Passeger and crew door (Main a/c Doors)?. Aluminum alloy. CFRP. AFRP.

What is the material of construction for the Emergency exit doors in the A318?. Alluminum alloy. CFRP. QFRP.

What is the section number of Center Fuselage section (Manufacturing Procedures)?. 16. 14. 15.

What are the names of the windows in the cockpit of the A320 Family?. windshield, side and fixed windows. windshield, sliding and fixed side windows. windshield, side and lateral windows.

What is the material used in the manufacturing of the Center Joint in the Horizontal stabilizer of the A319?. CFRP. AFRP. Titanium alloys.

What is the section number of the Forward Fuselage Section (Manufacturing Procedures)?. 11/12. 13/14. 15.

Where are located the Bolted Panel (Load Carrying Panels)?. Wing Box Inner area. Wing Box Outer area. Center Wing Box.

What does a structural Cut-out means?. A support. A hole. A kind of Rivets.

Which section of the fuselage is connected by lugs instead of Circumferential skin Joint. Section 18. Section 19. Section 19.1. 9.

How many panes used the windshield window?. Doble pane. Multi panes. 3 panes.