The 02-0526C0110 jack is intended to lift an aircraft by its fuselage and/or main wing with other hydraulic jacks arranged by position and quantity to provide proper balance, and in conjunction with the correct jack pad, whose maximum load on any one jack does not exceed the rated capacity of the jack.
*This list is for general reference only and may not be entirely acurate for all aircraft. Please confirm all equipment meets the requirements of your aircraft with the owners/maintenance manuals prior to purchasing or using with your aircraft.
by BOBBY LILLIS, a Maintenance Facility in SAN ANTONIO, TEXAS, USA
10/27/2021 08:55:18 AM
by ANDREW in New York
03/03/2021 12:43:53 PM
by Gerybones in SE Forida, USA
01/20/2021 08:03:18 AM
by Anonymous, a Maintenance Facility in Stuart, FL
04/15/2020 07:58:38 AM
08/26/2019 08:55:28 AM
by Dave Neely, a Corporate Flight Department in Lewisburg WV