NOSE GEAR MAXIMUM TOWING LOADS  DESIGN LOAD LIMITS 
LB  KG 
757-200 NLG OLEO *[1]  36,200  16420 
757-300 NLG OLEO *[1]  40,600  18416 
757-200 TOW FITTING *[2]  36,200  16420 
757-300 TOW FITTING *[2]  40,600  18416 
757-200 TOW FITTING *[3]  33,000  14970 
757-300 TOW FITTING *[3]  33,000  14970 
CAUTION: IF THE TOW LOAD IS MORE THAN THE DESIGN LIMITS, YOU MUST MAKE A COMPLETE INSPECTION OF THE NOSE GEAR AND ALL RELATED OR ADJACENT STRUCTURE 

*[1] THE LOAD IS APPLIED EITHER FORWARD OR AFT +/-5 DEGREES FROM THE CENTERLINE. INSTALL THE STRAP IN THE CROSS-HATCHED AREA. THE TOW STRAP MUST BE A MINIMUM OF 4 INCHES(10.2CM) WIDE WHERE IT CONTACTS THE INNER CYLINDER
*[2] 0-45 DEGREES ANGLE OF TURN *[3] 45-90 DEGREES ANGLE OF TURN
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757
AIRPLANE RECOVERY DOCUMENT
Figure 4-17 MAXIMUM TOWING LOADS, MAIN GEAR

MAIN LANDING GEAR MAXIMUM TOWING LOADS  DESIGN LOAD LIMITS 
LB  KG 
757-200 TOW FITTING *[2]  27,110  12323 
757-300 TOW FITTING *[2]  30,500  13835 
757-200 MLG OLEO *[1]  24,560  11140 
757-300 MLG OLEO *[1]  41,000  18598 
CAUTION: IF THE TOW LOAD IS MORE THAN THE DESIGN LIMITS, YOU MUST MAKE A COMPLETE INSPECTION OF THE NOSE GEAR AND ALL RELATED OR ADJACENT STRUCTURE 

*[1] THE LOAD IS APPLIED EITHER FORWARD OR AFT +/-30 DEGREES FROM THE CENTERLINE. INSTALL THE STRAP IN THE CROSS-HATCHED AREA. THE TOW STRAP MUST BE A MINIMUM OF 4 INCHES(10.2CM) WIDE WHERE IT CONTACTS THE LANDING GEAR
*[2] THE LOAD IS APPLIED EITHER FORWARD OR AFT +/-30 DEGREES FROM THE CENTERLINE
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AIRPLANE RECOVERY DOCUMENT
Figure 4-18 757-200 AIRPLANE GROUND STABILITY

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4-20-3 When You Tow or Winch the Airplane from the Main Gear
CAUTION:  DO NOT TOW THE AIRPLANE FROM A GEAR THAT HAS DAMAGE. IF YOU MUST USE THE GEAR, YOU MUST FIRST REPAIR IT.
1.  
There are tow lugs on each of the main gears. For more data see Figure 4-13 and Figure 4-14. Attach the nose gear to a vehicle with a towbar. This vehicle will move and stop (steer and brake) the airplane. For details on the nose gear fitting see Figure 4-13. See Figure 4-19 thru Figure 4-22 for different towing and winching arrangements.

2.  
Use a wire rope cable between the airplane and the tow vehicle or the winch. The cable must have applicable fittings and cable diameters for the required load with sufficient safety factors. Use load indicating devices (see Figure 4-23) between the gear and the cable to prevent damage to the gear from a dangerous load. See SUBJECT 3-20-4 for data about shackles.
　
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