757 Airplane Recovery Document 飞机恢复文件(7)

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2-10 RECOVERABLE EMPTY WEIGHT (REW) WORKSHEET 2-32 2-11 WEIGHT AND CENTER OF GRAVITY WORKSHEET 2-33 2-12 MAJOR COMPONENTS, WEIGHT AND CENTER OF GRAVITY 2-33 2-13 MODEL 757-200 CARGO DOOR SIZES, LOCATIONS AND HEIGHT ABOVE
GROUND 2-40 2-14 MODEL 757-300 CARGO DOOR SIZES, LOCATIONS AND HEIGHT ABOVE GROUND 2-41 2-15 MODEL 757-200 LOWER LOBE CARGO DOOR LOCATIONS, BULK CARGO
CONFIGURATION 2-42 2-16 MODEL 757-200 CONTAINER/PALLET LOADING LOCATIONS 2-43 2-17 MODEL 757-300 LOWER LOBE CARGO DOOR LOCATIONS, BULK CARGO
CONFIGURATION 2-44 2-18 MODEL 757-200 LOWER LOBE CARGO, OPTIONAL TELESCOPING MODULE
SYSTEM 2-45 2-19 NO. 1 AND 2 CARGO DOOR MECHANISMS 2-50 2-20 NO. 1 AND 2 CARGO DOORS AND CONTROL 2-51 2-21 NO. 1 AND NO. 2 CARGO DOOR HINGE DRIVE ROTARY ACTUATOR 2-52 2-22 MODEL 757-200 FORWARD CARGO COMPARTMENT, LOWER LOBE 2-53 2-23 MODEL 757-200 AFT CARGO COMPARTMENT, LOWER LOBE 2-54 2-24 MODEL 757-200 BULKHEAD RESTRAINT NETS, LOWER LOBE 2-55 2-25 NO. 3 CARGO DOOR INSTALLATION 2-58 2-26 MAIN CARGO DOOR MANUAL OPERATION, 757-200PF AND -200 COMBI 2-61 2-27 MAIN CARGO DOOR EXTERNAL OPENING, 757-200PF AND -200 COMBI 2-62

LIST OF FIGURES

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Figure Title Page
2-28 MAIN DECK CARGO DOOR CLEARANCE ENVELOPE, 757-200PF AND -200 COMBI 2-64 2-29 OPTIONAL TELESCOPING MODULE SYSTEM 2-66 2-30 MODEL 757-300 BULK CARGO WITH OPTIONAL SCANDINAVIAN BELLYLOADER (SBL) CARGO SYSTEM 2-68 2-31 MODEL 757-300 OPTIONAL SCANDINAVIAN BELLYLOADER (SBL) CARGO SYSTEM 2-69 2-32 DEFUEL VALVE 2-74 2-33 DEFUELING 2-75 2-34 WING TANK FUEL WEIGHT 2-77 2-35 ENGINE FUEL CROSSFEED INSTALLATION 2-78 2-36 DEFUELING WITH EXTERNAL POWER SOURCE 2-79 2-37 FUEL DRAINS 2-82 2-38 FIN/BODY JOIN 2-88 2-39 INTERNAL ACCESS, VERTICAL FIN, BODY SECTION 48 2-89 2-40 EXTERNAL ACCESS, VERTICAL FIN 2-90 2-41 GUST LOADS ON THE VERTICAL FIN DURING REMOVAL 2-91 2-42 SLING AND TETHER FITTING ATTACH POINTS, VERTICAL FIN 2-92 2-43 CRANE AND SLING ATTACHMENT GEOMETRY, OUTBOARD TILT, VERTICAL FIN 2-93 2-44 DORSAL FIN SCREW LOCATIONS 2-94 2-45 TENSION BOLT INSTALLATION, VERTICAL FIN 2-95 3-1 AIRPLANE MOVEMENT OF FIRST-DESIGN BALLOON TYPE PNEUMATIC BAGS 3-8 3-2 TETHERING (STABILIZING) LINE MATERIALS DATA 3-13 3-3 TETHERING DIAGRAM 3-16 3-4 ENGINE TETHERING 3-17 3-5 ENGINE TETHERING DIRECTIONS AND ALLOWABLE LOADS 3-18 3-6 TETHERING LINES ATTACHED TO THE MAIN LANDING GEAR 3-19 3-7 TETHERING LINES ATTACHED TO THE NOSE LANDING GEAR 3-20 3-8 THROUGH-FUSELAGE TETHERING 3-21 3-9 DOOR TETHER FIXTURE DETAILS 3-22 3-10 EXAMPLES OF ANCHOR INSTALLATIONS 3-23 3-11 THE RATED CAPACITY OF NYLON ROPE SLINGS 3-27 3-12 AVERAGE BREAKING STRENGTH OF SELECTED SLING MATERIALS 3-28 3-13 SLING CONFIGURATIONS 3-30 3-14 WIRE ROPE CLIPS 3-31

LIST OF FIGURES

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Figure Title Page
3-15 TETHERING (STABILIZING) LINE THIMBLE DATA 3-32 3-16 LIFTING ATTACHMENTS 3-33 3-17 TETHERING (STABILIZING) LINE SHACKLE DATA 3-35 3-18 SCREW-PIN ANCHOR SHACKLES, TYPE IV, CLASS 1 3-36 3-19 MODEL 757-200 NOSE GEAR FOLDED 3-43 3-20 MODEL 757-200 MAIN GEAR FOLDED 3-44 3-21 MODEL 757-200 FOLDED MAIN GEAR ONE SIDE 3-45 3-22 MODEL 757-200 FOLDED NOSE GEAR AND MAIN GEAR ONE SIDE 3-46 3-23 MODEL 757-200 ALL GEARS FOLDED, BOTH ENGINES SHEARED FROM
　
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