R 1EFF : 051-099, 1 32-41-00Page 639 1 1 May 01/05 1 1 1CES 1R **ON A/C 151-199, 401-499,
Subtask 32-41-00-210-059-B
B. Pressure Table
NOTE : The tables below show all the tire pressure values versus aircraft
____
weight (MRW) and tires sizes.
NOTE : (1): (Ref. TASK 32-41-11-000-006) (Ref. TASK 32-41-11-400-006)
____ (Ref. TASK 32-41-12-000-001) (Ref. TASK 32-41-12-400-001).
NOTE : (2):
____
-
If rolling was done with a flat tire or, if pressure loss is due to a fuse plug melting, replace the wheel and the adjacent wheel.
-
If you are sure that the pressure loss occurred while the aircraft was in the parked configuration (after the aircraft stopped), replace only the tire with the low pressure.
-
If you cannot be sure that the wheels did not turn with the tire deflated, you must also replace the adjacent wheel.
R 1EFF : 151-199, 401-499, 1 32-41-00Page 640 1 1 Aug 01/05 1 1 1CES 1
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| MRW 70.4T | |----------------------------------------------------------------| | TIRE PRESSURE | | |-------------------------| | | NLG | MLG | TIRE CONDITION/ACTION NECESSARY | | 30X8.8-15 | 46X16-20 | | | 30X8.8R15 | 46X17R20 | | |------------|------------|--------------------------------------| | More than | More than | Over-inflation. Make sure that the | | 13.1 bar | 13.5 bar | measurement is correct with another | | (190 psi) | (196 psi) | pressure gage. If it is correct, | | | | deflate the tire to the maximum | | | | normal pressure. | |----------------------------------------------------------------| | 12.5 to | 12.9 to | Normal pressure range. Do not adjust | | 13.1 bar | 13.5 bar | the tire pressure. | |(181-190psi)|(187-196psi)| | |------------|------------|--------------------------------------| | 11.9 to | 12.3 to | Inflate the tire to the maximum | | 12.5 bar | 12.9 bar | normal pressure. | |(173-181psi)|(178-187psi)| | |------------|------------|--------------------------------------| | 11.2 to | 11.6 to | Inflate the tire to the maximum | | 11.9 bar | 12.3 bar | normal pressure. You must measure the| |(162-173psi)|(168-178psi)| tire pressure again the next day. If | | | | the tire is under-inflated again, you| | | | must replace the wheel. See NOTE (1) | |------------|------------|--------------------------------------| | 10 to | 10.3 to | You must replace the wheel. | | 11.2 bar | 11.6 bar | See NOTE (1) | |(145-162psi)|(149-168psi)| | |------------|------------|--------------------------------------| | 0 to | 0 to | You must replace the wheel and the | | 10 bar | 10.3 bar | adjacent wheel. See NOTE (1) and (2) | |( 0-145psi) |( 0-149psi) | | ------------------------------------------------------------------
R 1EFF : 151-199, 401-499, 1 32-41-00Page 641 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 301-399,
Subtask 32-41-00-210-059-C
B. Pressure table
NOTE : The tables below show all the tire pressure values versus aircraft
____
weight (MRW) and tires sizes.
NOTE : (1): (Ref. TASK 32-41-11-000-006) (Ref. TASK 32-41-11-400-006)
____ (Ref. TASK 32-41-12-000-001) (Ref. TASK 32-41-12-400-001).
NOTE : (2):
____
-
If rolling has been performed with a flat tire or, if pressure loss is due to a fuse plug melting, replace wheel and adjacent wheel.
-
If you are sure that the pressure loss occurred while the aircraft was in the parked configuration (after the aircraft stopped), replace only the tire with the low pressure.
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