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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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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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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