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AIRCRAFT GENERAL B747-200 General Aircraft Descriptions and Limitations 1.

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Presentation on theme: "AIRCRAFT GENERAL B747-200 General Aircraft Descriptions and Limitations 1."— Presentation transcript:

1 AIRCRAFT GENERAL B General Aircraft Descriptions and Limitations 1

2 2

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.

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

5

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

7 7

8 8 Turning Radius With Body Gear Steering 153’ 90’ 14’ 59’ 61’ 96’ 92’ 21’ 39’

9 9 Turning Radius Without Body Gear Steering

10 DOORS & STRUCTURE Aircraft General 10

11 11 Main entry doors

12 Flight Deck Door 12

13 Crew Service Door CREW SERVICE DOOR

14 14 Upper Deck Crew Service Door (RH Side only) Cockpit Escape Hatch Location Doors & Structure Doors & Structure

15 15 Cockpit Escape Hatch NOTE: There is No cockpit indication for this escape hatch

16 FORWARD CARGO DOOR Cargo Compartment Doors AFT CARGO DOOR BULK CARGO DOOR

17 Forward Cargo Door HINGE LATCH LOCK HANDLE EXTERNAL DOOR CONTROLS NEGATIVE PRESSURE RELIEF DOOR (2) VIEW PORTS (8)

18 Aft Cargo Door VIEW PORTS (8)

19 Bulk Cargo Door

20 Electric Service Doors 20

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

22 Antenna Location

23 Cockpit Layout

24 24 Eye Position Locators Black Crosses on L & R Windshield Brace

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.

26 Flight Engineer Station

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

28 Servicing Ports

29 Seating Configuration

30 30 Emergency Equipment

31 31

32 Emergency Equipment Locations (Main Deck) 32

33 Flight Deck & Passenger Exits

34 Emergency Overhead Escape hatch

35 Cabin Emergency Lighting

36 Cabin Floor Level Emergency Escape Path Lighting

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

38 Crew Service Slide Operation

39 Exterior Emergency Lighting

40 Evacuation Slide / Rafts

41 Single Lane Evacuation Slide

42 Dual Lane Slide / Rafts

43 Over-wing Ramp/Slide

44 Raft Survival Equipment

45 Evacuation Emergency Lighting

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

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.

48 Lower Cargo Doors Annunciator

49 49 AIRCRAFT EXTERIOR LIGHTING

50 50

51 51 AIRCRAFT EXTERIOR LIGHTTING

52 LIMITATIONS

53 AIRCRAFT OPERATION (AFM) 14 CFR (a), (b), (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

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

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.

56 Maximum Allowable Runway Contamination 56

57 WIND LIMITS (AFM) Limiting tailwind component is 10 knots. 57

58 CROSSWIND COMPONENT LIMITS (PEAK GUST) 58

59 Maximum Structural Weights (AFM) Max Taxi Weight ,000 lbs Max Takeoff Weight at Brake Release ,000 lbs Max In-flight Weight, Landing= Flaps…...650,000 lbs Max Landing Weight ,000 lbs Max Zero Fuel Weight ,500 lbs Max Fuel Transfer Weight (1 & 4 Res)……638,000 lbs

60 Fuel Tanks 60

61 Fuel Capacity Maximum Fuel Tank Quantities (AFM) 1 & 4 Reserve Tanks.... 3,417 lbs (510 U.S. GAL) 1 & 4 Main Tanks ,935 lbs (4,319 U.S. GAL) 2 & 3 Main Tanks ,051 lbs (12,540 U.S. GAL) 2 & 3 Reserve ,573 lbs (785 U.S. GAL) Center Wing Tank ,993 lbs (17,164 U.S. GAL)

62 Max Speed MAX OPERATING SPEEDS Vmo Mmo S.L. 378 KIAS -- FL KIAS.92M

63 TURBULENCE PENETRATION SPEED KIAS 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

64 ENGINE BASICS 64

65 Baltia’s 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

66 66

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.

68 The high pressure (N2) eleven-stage compressor is driven by a two-stage turbine. 68

69 69


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