WHEN YOU TOW OR WINCH THE AIRPLANE FROM THE MAIN GEAR Page 4-35 Jul 01/2005
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757
AIRPLANE RECOVERY DOCUMENT
Figure 4-23 LOAD INDICATING DEVICE, TOWING/WINCHING
LOAD CELL CAPACITY IN KIPS LOAD CELL CAPACITY WITH FIT-TINGS *[1] APPROXIMATE DIMENSION RECOMMENDED ALLOY SHACKLE SHACKLE PIN DIA APPROX UNIT WEIGHT LB
A B C DIA
150 A = 150 KIP 17.75 9.0 3.38 80 TON 2.75 60
150 B = 75 KIP 16.25 9.0 3.38 40 TON 2.25 57
150 C = 50 KIP 15.50 9.0 3.38 30 TON 2.00 57
150 D = 100 KIP 17.00 9.0 3.38 61 TON 2.50 60
*[1] 1. COMMON LOAD CELL USES A VARIETY OF FITTINGS
2. SHEAR LINK REPLACEMENT
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Figure 4-23 LOAD INDICATING DEVICE, TOWING/WINCHING (Continued)
3. MANUFACTURED BY STRESS-TEK INC, RENTON, WA USA NOTE: 1. REFER TO SECTION 4-20 FOR TOWING LOAD LIMITS ON MAIN AND NOSE GEAR
2.
ORDER BY PART NUMBER 63-010532-XX. THE DASH NUMBER IS KNOWN WHEN YOU FIND THE REQUIRED LOAD CAPABILITY
3.
1.00 INCH = 2.54 CM; 1 LB = 0.4536 KG; 1 TON = 907.2 KG; 1 KIP = 70 KG/SQ CM
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4-30 WHEN YOU MOVE A DAMAGED AIRPLANE 4-30-1 General
1. It is important for you to examine the folded landing gear for all possible damage. Do this during the initial airplane inspection. If this is not possible, you must do it after you lift the airplane to a sufficient height.
WARNING: YOU MUST BE VERY CAREFUL WHEN YOU MOVE THE AIRPLANE OR CHANGE ITS ATTITUDE. FUEL LEAKAGE MAY OCCUR AND CAUSE A DANGEROUS CONDITION. YOU MUST MONITOR THE AIRPLANE FOR FUEL LEAKAGE.
2. If it is possible, move the damaged airplane on its landing gears. If you use the landing gears, it can be necessary to do one of these procedures:
A. Repair the damaged gear.
B. Install a replacement gear.
C. Install some temporary gear supports to hold the weight of the airplane.
3. If you cannot use the landing gear, you must use a different system to move the airplane. It can be necessary to use one or more of these items:
A. Trucks (low-bed trailers)
B. Movable cranes
C. Transportation dollies
D. House movement equipment
E. Commercial transportation equipment
4. It is possible that you must prepare the ground surface to tow the airplane (see SECTION 2-10 and SECTION 4-10).
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