F22 F35 F20 hammer seal kit excavator rock breaker oil seal

PU Rubber PTFE Breaker Seal Kit Excavator Hydraulic Cylinder Parts

F22 F35 F20 hammer seal kit excavator rock breaker oil seal

SEAL KITS---
BOOM CYL SEAL KIT . ARM CYL SEAL KIT . BUCKET CYL SEAL KIT
MAIN PUMP SEAL KIT . HYDRAULIC PUMP SEAL KIT . PIOLVE VALVE SEAL KIT.
GEAR PUMP SEAL KIT VALVE SEAL KIT .PUMP PLUNGE SEAL KIT .
.CONTROL VALVE SEAL KIT. SWING MOTOR SEAL KIT .. TRAVEL MOTOR SEAL KIT .
ADJ CYL SEAL KIT. CENTER JIONT KIT BREAKER SEAL KIT

Oil Seal -- TC TB TCV TCN DB DC DCY TC4Y ISPID BABSL

Piston seal : SPGW SPGO SPG SPGA NCF ODI OSI OUIS OHM OKH DAS , OK SELA OUY D-8

Rod Seal : IDI IUH ISI IUIS D-2 D-3 D-6
　
U Seal : UPI UPH USH USI V99F V96H UN

Buff Seal : HBTS HBY HBTTS D-14

Wiper Seal : DKB DKBI DKBI3 DKBZ DKI , DWI DKH DWIR DSI LBI LBH VAY DH ME-2 ME-8

Wearing Ring : WR KZT RYT

　
Rotary Seal : ROI D-14 SPN

Back Up Ring : N4W BRT-PTFE BRT-NYLON BRT2 BRT3 BRT-G BRT-P BRN2 BRN3

O Ring : Oring Kit P series G series AS series S series M 1.5 series M 2.0 series M 1.9series M 2.4 series

M 3.0 series M4.0 series

Piston seal : SPGW SPGO SPG SPGA NCF ODI OSI OUIS OHM OKH DAS , OK SELA OUY D-8

Rod Seal : IDI IUH ISI IUIS D-2 D-3 D-6

Valve Pusher Floating oil seal Bushing hydraulic cylinder seals cylinder seal kits

Air Inlet System
An air hose failure or a significant air inlet system leak will cause a large drop in boost pressure and power. The engine can be operated at this power level for a short period of time, however, sustained operation under this condition should be avoided.A slight reduction in power or response, or a small increase in exhaust temperature may indie a small air leak in the charge air cooler core or piping.If air leaking is suspected, inspect the air inlet hoses, elbows and gaskets for cracks or damage. Replace the parts as needed. Check for loose clamps and tighten the clamps as needed.Radiator Restrictions
discourages the use of air flow restriction devices mounted in front of radiators with air-to-air aftercooled engines. Air flow restriction can cause higher exhaust temperatures, power loss, excessive fan usage, and a reduction in fuel economy.If an air flow restriction device must be used, the device should have a permanent opening directly in line with the fan hub. The device must have a minimum opening dimension of at least 770 cm2 (120 in2).A centered opening, directly in line with the fan hub, is specified to provide sensing when viscous fan drives are used and/or to prevent an interrupted air flow on the fan blades. Interrupted air flow on the fan blades could cause a fan failure. recommends that a package include an inlet manifold temperature device, such as a light indior, buzzer, etc., set at 65°C (150°F) and/or installation of an inlet air temperature gauge. For the ATAAC (Air-To-Air Aftercooled) engines, air temperature in the inlet manifold should not exceed 65°C (150°F). Temperatures exceeding this limit can cause power loss