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AIRCRAFT GENERAL B747-200 General Aircraft Descriptions and Limitations 1 Slide 2 2 Slide 3 3 231 Ft. 10 In. 72 Ft. 9 In. 195 Ft. 8 In. 36 Ft. 2 In. 89 Ft. 5 In. 114 Ft. 10 In. 225 Ft. 2 In. 63 Ft. 5 In. 32 Ft. 1 In. Eye Level 27 Ft. 11 In. Approx. 81 Ft. 9 In. Slide 4 4 Bulk Cargo Lower Aft Cargo Lower Fwd Cargo Crew Service Escape Hatch L1 L5 Primary Structure - Aluminum, Steel, Titanium Secondary Structure - Graphite Composite, Fiberglass, Nomex L2 L3 L4 R1 R2 R3 R4 R5 Doors & Structure Doors & Structure Slide 5 Slide 6 6 Aircraft Deck Structure Aft Cargo Door Bulk Cargo Door Forward Cargo Door Crew Service Door (200) Main Deck Cabin Compartment LWR Aft Cargo Compartment Bulk Cargo Compartment *LWR Forward Cargo Compartment Cockpit Upper Deck *E & E Compt. L1 Door L5 Door * Areas can be accessed in Flight Slide 7 7 Slide 8 8 Turning Radius With Body Gear Steering 153 90 14 59 61 96 92 21 39 Slide 9 9 Turning Radius Without Body Gear Steering Slide 10 DOORS & STRUCTURE Aircraft General 10 Slide 11 11 Main entry doors Slide 12 Flight Deck Door 12 Slide 13 Crew Service Door CREW SERVICE DOOR Slide 14 14 Upper Deck Crew Service Door (RH Side only) Cockpit Escape Hatch Location Doors & Structure Doors & Structure Slide 15 15 Cockpit Escape Hatch NOTE: There is No cockpit indication for this escape hatch Slide 16 FORWARD CARGO DOOR Cargo Compartment Doors AFT CARGO DOOR BULK CARGO DOOR Slide 17 Forward Cargo Door HINGE LATCH LOCK HANDLE EXTERNAL DOOR CONTROLS NEGATIVE PRESSURE RELIEF DOOR (2) VIEW PORTS (8) Slide 18 Aft Cargo Door VIEW PORTS (8) Slide 19 Bulk Cargo Door Slide 20 Electric Service Doors 20 Slide 21 CENTER LAVATORY SERVICE DOOR GROUND AIR CONDITIONING ACCESS DOOR EXTERIOR POWER RECXEPTACLE FWD ELECTRONICS DOOR FWD LAVATORY SERVICE DOOR AIR CONDITIONING ACCESS PANELS AND DOORS APU BATTERY ACCESS DOOR APU ACCESS DOORS AFT POTABLE WATER SERVICE ACCESS DOOR CENTER ELECTRONICS DOOR FWD POTABLE WATER SERVICE ACCESS DOOR Miscellaneous Doors Slide 22 Antenna Location Slide 23 Cockpit Layout Slide 24 24 Eye Position Locators Black Crosses on L & R Windshield Brace Slide 25 25 Cockpit Windows Forward windows Thick laminated acrylic and hardened glass. Thick laminated acrylic and hardened glass. Side windows Acrylic and vinyl laminate. Acrylic and vinyl laminate. Single layer of acrylic will hold full cabin pressure. Window heat is not required for bird strike protection. Window heat is not required for bird strike protection. L1 & R1 window heat provides anti-ice & defogging, rest defogging only. L1 & R1 window heat provides anti-ice & defogging, rest defogging only. Slide 26 Flight Engineer Station Slide 27 CENTER LAVATORY SERVICE DOOR GROUND AIR CONDITIONING ACCESS DOOR EXTERIOR POWER RECXEPTACLE FWD ELECTRONICS DOOR FWD LAVATORY SERVICE DOOR AIR CONDITIONING ACCESS PANELS AND DOORS APU BATTERY ACCESS DOOR APU ACCESS DOORS AFT POTABLE WATER SERVICE ACCESS DOOR CENTER ELECTRONICS DOOR FWD POTABLE WATER SERVICE ACCESS DOOR SERVICING PORTS Slide 28 Servicing Ports Slide 29 Seating Configuration Slide 30 30 Emergency Equipment Slide 31 31 Slide 32 Emergency Equipment Locations (Main Deck) 32 Slide 33 Flight Deck & Passenger Exits Slide 34 Emergency Overhead Escape hatch Slide 35 Cabin Emergency Lighting Slide 36 Cabin Floor Level Emergency Escape Path Lighting Slide 37 Crew Service Door Slide FLOOR TRACK RELEASE FLOOR TRACKS ESCAPE SLIDE PACK CHUTE MANUAL INFLATION HANDLE FLOOR RAMP ASSIST HANDLE PACKBOARD MANUAL RELEASE HANDLE Slide 38 Crew Service Slide Operation Slide 39 Exterior Emergency Lighting Slide 40 Evacuation Slide / Rafts Slide 41 Single Lane Evacuation Slide Slide 42 Dual Lane Slide / Rafts Slide 43 Over-wing Ramp/Slide Slide 44 Raft Survival Equipment Slide 45 Evacuation Emergency Lighting Slide 46 Evacuation After Ditching Each crewmember must have his evacuation assignment committed to memory. The Captain is to ensure that the command to evacuate and any other specific instructions are issued An evacuation must not be initiated while the airplane is moving. The suitability of an exit should be evaluated before it is used. If possible, persons should board directly from the airplane into the life rafts. The first capable person to board the raft should assist in boarding Slide 47 Raft Seaworthiness Persons in the raft should sit with their backs against the rail and their feet toward the center. When all persons are aboard the raft, the lanyard must be cut. Rafts should be tied together only in a very calm sea. Check pressure of raft tubes; additional manual inflation may be necessary. Slide 48 Lower Cargo Doors Annunciator Slide 49 49 AIRCRAFT EXTERIOR LIGHTING Slide 50 50 Slide 51 51 AIRCRAFT EXTERIOR LIGHTTING Slide 52 LIMITATIONS Slide 53 AIRCRAFT OPERATION (AFM) 14 CFR 121.323(a), 121.323(b), 121.323(c) The aircraft is approved for the following kinds of flight and operation; both day and night, when the required equipment is installed and approved in accordance with the applicable Federal Aviation Regulations: Visual (VFR) Instrument (IFR) Icing Conditions Extended Overwater 53 Slide 54 Maximum Operating Altitude OPERATIONAL LIMITS (AFM) Maximum operating altitude is 45,100 feet pressure altitude. Maximum takeoff and landing altitude is 1,000 to 10,000 feet pressure altitude. Maximum Runway Slope 2%. Takeoff, landing, and en route operational temperature and altitude limits are shown on the Operating Envelope chart to the right Slide 55 Max APU Operating Altitude Do not use APU generator power in-flight. Do not operate APU in-flight in icing conditions. Do not operate APU above 20,000 feet pressure altitude. Operation between 15,000 feet and 20,000 feet pressure altitude is limited to "no load" only. In-flight start of the APU is not authorized. Slide 56 Maximum Allowable Runway Contamination 56 Slide 57 WIND LIMITS (AFM) Limiting tailwind component is 10 knots. 57 Slide 58 CROSSWIND COMPONENT LIMITS (PEAK GUST) 58 Slide 59 Maximum Structural Weights (AFM) Max Taxi Weight......................................816,000 lbs Max Takeoff Weight at Brake Release....814,000 lbs Max In-flight Weight, Landing= Flaps...650,000 lbs Max Landing Weight...............................630,000 lbs Max Zero Fuel Weight............................526,500 lbs Max Fuel Transfer Weight (1 & 4 Res)638,000 lbs Slide 60 Fuel Tanks 60 Slide 61 Fuel Capacity Maximum Fuel Tank Quantities (AFM) 1 & 4 Reserve Tanks.... 3,417 lbs (510 U.S. GAL) 1 & 4 Main Tanks....... 28,935 lbs (4,319 U.S. GAL) 2 & 3 Main Tanks....... 84,051 lbs (12,540 U.S. GAL) 2 & 3 Reserve............... 5,573 lbs (785 U.S. GAL) Center Wing Tank......114,993 lbs (17,164 U.S. GAL) Slide 62 Max Speed MAX OPERATING SPEEDS Vmo Mmo S.L. 378 KIAS -- FL240 392 KIAS.92M Slide 63 TURBULENCE PENETRATION SPEED 290-310 KIAS.82-.85 M OPERATIONS IN REDUCED VERTICAL SEPARATION MINIMUM (AFM) For all operations in Reduced Vertical Separation Minimum airspace, 0.90 Mach is not to be exceeded and for operations at gross weights less than 235,868 kilograms (520,000 pounds), 0.87 Mach is not to be exceeded between flight level 290 and 340. 63 Slide 64 ENGINE BASICS 64 Slide 65 Baltias aircraft are powered by Pratt & Whitney JT9D turbofan engines. The engine is a two-spool, axial flow turbofan of high compression ratio and high bypass ratio. 65 Slide 66 66 Slide 67 67 The engine incorporates two multistage turbine-driven compressors utilizing concentric shafting. The low pressure (N1) compressor, consisting of one fan stage and three compressor stages, is driven by a four-stage turbine. Slide 68 The high pressure (N2) eleven-stage compressor is driven by a two-stage turbine. 68 Slide 69 69