Aircraft Accident Investigation Report No. ACCID01/06

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CityU Professional Services Ltd Failure Analysis of a Towbar Department of Physics & Materials Science City University of Hong Kong Figure 4-15 : Lower part of the broken bolt (about 16 mm dia.) illustrating fracture between top plate and head-to-tube connector Figure 4-16 shows new large and small shear bolts, as well as the remains of the shear bolts from the incident. Figure 4-16 : Large and small shear bolts - 14 -
CityU Professional Services Ltd Failure Analysis of a Towbar Department of Physics & Materials Science City University of Hong Kong Figure 4-17 shows the fracture surface of the large shear bolt. It can be seen that he fracture surface is very flat. Figure 4-17 : Fracture surface of large shear bolt - 15 -
Page 1 and 2: ACCIDENT INVESTIGATION REPORT AIRCR
Page 3 and 4: 4. Safety Recommendations .........
Page 5 and 6: jerk is not able to be determined a
Page 7 and 8: in this fitting had broken and the
Page 9 and 10: during operation, the shear load is
Page 11 and 12: 1.5. Personnel Information 1.5.1. F
Page 13 and 14: Type A321-231 Aircraft Serial No. M
Page 15 and 16: 1.9. ATC and Communications The acc
Page 17 and 18: 1.11. Flight Recorders During the t
Page 19 and 20: 1.17. Organizational and management
Page 21 and 22: sudden halt. Such foreign object co
Page 23 and 24: 4. Safety Recommendations Safety Re
Page 25 and 26: CityU Professional Services Ltd Fai
Page 37: CityU Professional Services Ltd Fai

Aircraft Accident Investigation Report No. ACCID01/06

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