AVIATION Reports - 1998 - A98H0003

List of Figures

• Figure 1: - HB-IWF overall dimensions and seat configuration
• Figure 2: - MD-11 design and configuration
• Figure 3: - Cockpit attic and forward cabin drop-ceiling areas
• Figure 4: - Area behind cockpit rear wall (Galley 2 and riser duct assembly removed)
• Figure 5: - Cockpit attic area and cut-out above cockpit rear wall
• Figure 6: - Muff assembly with MPET-covered insulation blanket
• Figure 7: - Forward cabin drop-ceiling area above Galley 2
• Figure 8: - MD-11 environmental system – Swissair configuration
• Figure 9: - Overhead diffuser assembly
• Figure 10: - Cockpit area airflow – typical
• Figure 11: - MD-11 cockpit
• Figure 12: - Cockpit CB panels
• Figure 13: - Wire construction
• Figure 14: - IFEN installation – general
• Figure 15: - IFEN (CB and Wiring) installation – cockpit and forward cabin drop-ceiling areas
• Figure 16: - Map light
• Figure 17: - Emergency equipment location – cockpit and forward cabin
• Figure 18: - Heavy lift operation
• Figure 19: - Reconstruction mock-up
• Figure 20: - Wire segments with melted copper
• Figure 21: - Exhibit 1-4372
• Figure 22: - IFEN PSU cable segments
• Figure 23: - Location of identified aircraft wires with regions of copper melt
• Figure 24: - Airframe structure and air distribution system
• Figure 25: - Heat damage – airframe structure
• Figure 26: - Heat damage – air distribution system
• Figure 27: - Cockpit attic and forward cabin drop-ceiling areas mock-up
• Figure 28: - Heat damage – upper and lower avionics CB panels
• Figure 29: - Heat damage – overhead CB panel
• Figure 30: - Position of recovered IFEN wires – outboard conduit
• Figure 31: - Position of recovered IFEN wires – middle conduit