D) 06 aircraft areas and dimensions
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The document discusses aircraft dimensions and measurements for the Embraer 170 and 175 aircraft. It provides details on total length, height, wing span, wing and tail areas, fuselage diameter, and distances between components. Diagrams illustrate the measurements. The aircraft use a coordinate system to define stations along the longitudinal, lateral, and vertical axes from a point of origin at the front of the aircraft.
D) 06 aircraft areas and dimensions
- 1. ATA 06 Aircraft areas and dimensions
- 2. Table of Content 06-00 Aircraft areas and dimensions Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 The aircraft measurement Embraer 170. . . . . . . . . . . . . . . . . . . . . 3 The aircraft measurement Embraer 175. . . . . . . . . . . . . . . . . . . . . 5 The aircraft measurement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 The aircraft stations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Wing station diagram . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 The vertical stabilizer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 The horizontal stabilizer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 The power plant and the engine pylons . . . . . . . . . . . . . . . . . . . . 15 The aircraft zoning system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 The major aircraft zones . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Sub zones. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 Access panels. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Issue: July04 FOR TRAINING ONLY Revision: 00 GE Capital Aviation Training. Reproduction Prohibited TOC 06 Page 1
- 3. Intentionally left blank Issue: July04 FOR TRAINING ONLY Revision: 00 GE Capital Aviation Training. Reproduction Prohibited TOC 06 Page 2
- 4. 06-00 Aircraft areas and dimensions Introduction This chapter describes the aircraft’s general external dimensions, aircraft zoning and station identification. The fuselage stations show the length measurements along the longitudinal axis. All horizontal measurements are taken from the datum line FS 0 which is lo- cated at the nose tip. The forward pressure bulkhead is located at station 610 and the fuselage is pressurized between the forward pressure bulkhead and the rear pressure bulkhead, which is located at station 23500. Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 1 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 5. Figure 1: Horizontal measurements FS 0 FS 23500 FS 610 Longitudinal axis Forward pressure Rear pressure bulkhead bulkhead Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 2 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 6. The aircraft measurement Embraer 170 The aircraft has a total length from the nose to the tail of 29.90m (98 ft 1 in.), the height from the ground to the top of the vertical tail is 9.67m (31 ft 9 in.) and a vertical tail area of 16.20 m² (174 ft² 54 in²). The distance from the nose gear to the main gear is 10.60 meters (34ft 9 in). The aircraft has a total wing span of 26.00m (85 ft 4 in) with a total wing area of 72.72 m² (782 ft² 180 in²), a horizontal tail span of 9.84 m (32 ft 4 in.), with a horizontal tail area of 23.25 m² (250 ft² 38 in²) and a fuselage external di- ameter of 3.01 m (9 ft 11 in.). The distance from the left to right main gear is 5.20 meters (17ft). Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 3 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 7. Figure 2: Aircraft measurements Embraer 170 Total wingspan: 26.00 (85 ft 4 in) Total wing area: 72.72 m 2 Horizontal tail area: 23.25 m 2 2 (782 ft 180 in2) (250 ft 2 38 in 2) Horizontal tail span: 9.84 m (32 ft 4 in) 9.67 m (31 ft 9 in) Vertical tail area: 16.20 m 2 (174 ft 2 54 in2 ) Distance from nose gear to main gear: 10.6 m (34 ft 9 in) 29.90 m (98 ft 1 in) Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 4 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 8. The aircraft measurement Embraer 175 The aircraft has a total length from the nose to the tail of 31.68m (103 ft 11 in.), the height from the ground to the top of the vertical tail is 9.73m (31ft 9 in.) and a vertical tail area of 16.20m² (174 ft² 54 in²). The distance from the nose gear to the main gear is 11.40 meters (37ft 5 in). The aircraft has a total wing span of 26.00 meters (85 ft 4 in) with a total wing area of 72.72 m² (782 ft² 180 in²), a horizontal tail span of 10.00 meters (32 ft 9 in), with a horizontal tail area of 23.25m² (250 ft² 38 in²) and a fuselage external diameter of 3.01 m (9 ft 11 in). The distance from the left to the right main gear is 5.20 meters (17 ft). Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 5 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 9. Figure 3: The aircraft measurement Embraer 175 11.40 m 37 ft 5 in 31.68 m 10 ft 11in 10.00 m 32 ft 9 in 5.20 m 17 ft 26.00 m 85 ft 4 in Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 6 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 10. The aircraft measurement Located on the left side of the fuselage are two main doors, which qualifies as type 1 emergency exits. Located on the right side of the fuselage are two service doors, which qualify as type 1 exits, and two baggage compartment doors. Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 7 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 11. Figure 4: The aircraft measurement Type 1 emergency exits Main door Main door Type 1 exits Service door 3.01 m (9 ft 11 in) Baggage Service door compartment doors 5.20 m (17 ft) Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 8 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 12. The aircraft stations The aircraft stations are defined by a coordinate system using three main reference axes. The point of origin for the longitudinal axis X, laterall axis Y and vertical axis Z is in front of the aircraft. The ordinates are identified by the letter for the major axes, followed by the dimension in inches from the point of origin. There are additional points of origin selected for locating major assemblies. These points are identified with a suffix letter indicating the assembly. These assemblies are the wings, the vertical stabilizer, the horizontal stabilizer, the power plant and the engine pylons. Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 9 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 13. Figure 5: Fuselage dimension FWD Fuselage Center Fuselage 1 Center Fuselage 2 Center Fuselage 3 Rear Fuselage Tail Cone X=0 X=610 X=6232.5 X=11035 X=16809 X=23295 X=27090 X=29900 Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 10 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 14. Figure 6: Wing station diagram RIB 1 Y= -1380.00 DRY BAY SLAT 1 ENGINE RIB 10 YA= -4617.57 WING REF. SLAT 2 POINT YA = 00.00 SLAT 3 WING SPAR 1 SLAT 4 RIB 26 YA= -12196.00 WING SPAR 3 INBOARD FLAP Y = 00.00 OUTBOARD FLAP WING SPAR 2 YA = 00.00 AILERON WING TRAILING EDGE Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 11 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 15. Figure 7: Vertical stabilizer ZV 7020,10 ZV 4269,00 ZV 1069,00 ZV 622,98 Z= 00,00 ZV= 00,00 A XV= 00,00 Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 12 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 16. Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 13 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 17. Figure 8: Horizontal stabilizer Y = 00.00 YH -2546.40 TRACE YH -5050.00 YH -3883.41 TRACE Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 14 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 18. Figure 9: Power plant and engine pylons X ENG 3877.60 X ENG 5589.90 CANT XP 3256.97 XP XP XP XP 4722.0 6340.0 7201.0 8191.0 Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 15 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 19. The aircraft zoning system The aircraft zoning system provides identification of areas in the aircraft ac- cording to 8 major zones, major sub-zones and zones. The major aircraft zones are: • The lower fuselage, zone 100 • The upper fuselage, zone 200 • The tail cone and horizontal and vertical tail, zone 300 • The power plants and pylons, zone 400 • The left wing, zone 500 • The right wing, zone 600 • The landing gear and landing gear wheel well doors, zone 700 • The aircraft doors, zone 800 Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 16 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 20. Figure 10: The major aircraft zones Right wing Tail cone and horizontal zone 600 and vertical tail Power - plants zone 300 and pylons Upper fuselage zone 400 zone 200 Doors zone 800 Left wing zone 500 Lower fuselage Landing gears zone 100 and gear wheel - well doors 700 Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 17 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 21. Sub zones The major zones are divided into major sub-zones, which are shown by the second digit of the major zone number.The major sub-zones are further di- vided into zones using the third digit of the major zone number. Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 18 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 22. Figure 11: Sub-zones ZONE 116 ZONE 115 ZONE 114 Zone number ZONE 113 ZONE 111 SUBZONE 170 SUBZONE 160 SUBZONE 150 SUBZONE 140 SUBZONE 130 SUBZONE 120 SUBZONE 110 Subzone number Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 19 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 23. Access panels To carry out maintenance on aircraft systems and their components, or to perform inspection of the aircraft structure, adequate access panels and doors are provided in the aircraft surface. Each access panel has an identification number which consists of a three digit zone number followed by two or three letters.The first letter shows the number of the panel within the zone in a logical in a logical sequence and the second letter indicates the location of the panel in relation to the air- craft.An optional third letter is used to identify a floor, wall or ceiling panel. Each panel has a fastener identification code, which identifies the type and the quantity of the fasteners for each panel. Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 20 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited
- 24. Figure 12: Access panels identification letters 191 DL 191 EL 192 CL 192 BL 192 AL 195 HL 195 FL 195 JL 191 AL 195 KL 195 GL 191 BL 191 CL 195 EL Shows the number of the Indicates the location of the panel within the zone panel in relation to the aircraft 195 AL 195 DL 195 BL 195 CL 19 S An optional third letter is used to identify a floor(F), wall(W) or ceiling(C) panel. 19 S Each panel has a fastener identification code: L = Latch S = Screw C = Camloc Issue: July04 FOR TRAINING ONLY Chapter 06-00 Page 21 Revision: 01 GE Capital Aviation Training. Reproduction Prohibited