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The Tronair 02-7862C0100 is a 12-Ton (24,000 lb) hydraulic aircraft axle jack engineered to lift and support one wheel/tire assembly of an aircraft at the axle during maintenance, tire changes, and landing gear servicing. With a 5" (12.7 cm) closed height and 14" (35.6 cm) maximum extended height, it accommodates a range of aircraft axle clearance requirements. CE-marked for compliance with European aviation safety standards. OEM-specified for Cessna Citation Sovereign 680, Latitude 680A, Citation Longitude 700.
Standard Features
- Hand pump with built-in pressure relief valve
- Easy-access filler/breather cap that can be sealed to prevent spills
- Low-profile cylinder designed for minimal axle clearance requirements
- Hydraulic fluid: MIL-PRF-5606
- CE marked
- Durable powder-coat finish (Tronair Blue)
Technical Specifications
- Rated Capacity: 24,000 lbs (10886 kg)
- Operating Temperature: −4°F to 122°F (−20°C to 50°C)
- Pressure Relief Setting: 2,500 + 250/−0 PSIG (172.4 + 17.2/−0 bar)
- Minimum Closed Height: 5" (12.7 cm)
- Mechanical Extension: 2" (5.1 cm)
- Hydraulic Extension: 6" (15.2 cm)
- Maximum Height Obtainable: 14" (35.6 cm)
- Weight: 56 lbs (25 kg)
- Hydraulic Fluid: MIL-PRF-5606
- Jack Pad: ¾" (2 cm) spherical radius cup
- Finish: Durable powder coat (Tronair Blue)
Safety Features
- Safety Lock Valve: Prevents the jack from lowering unintentionally during lifting operations. The jack must be manually released before descending.
- Pressure Relief Valve: Prevents overload during raising operations.
- Filler Cap Seal: Easy-access filler/breather cap can be sealed to prevent hydraulic fluid spills during transport and storage.
Aircraft Applications
The 02-7862C0100 is OEM-approved for the following aircraft types:
- Cessna: Citation Sovereign 680, Latitude 680A, Citation Longitude 700
This list reflects aircraft for which the manufacturer has specifically approved this jack. Additional applications may be possible — always confirm jacking capacity, adapter requirements, and placement procedures with the aircraft maintenance manual before use.
Need your Tronair 02-7862C0100 12-ton axle jack serviced, repaired, or load tested?
Pilot John is an authorized Tronair distributor and factory-authorized Tronair service center. Every jack ships new from our warehouse with Certificates of Conformance (CofC) and FAA Form 8130-3 documentation available at no additional cost. Need jack service, load-testing, or repair? Pilot John handles that too as an OEM-trained GSE service center. For more information or to request service, see our Service Center page, and see our article on why jack load testing matters. Pilot John also operates an ISO-17025 calibration center for all of your tooling and equipment calibration needs — learn more here.
| Alternate Models | |
|---|---|
| 02-7862-0100 | Previous Part Number |
| General Information | |
|---|---|
| Part # | 02-7862C0100 |
| Manufacturer | Tronair |
| Manual 1 | View Tronair 02-7862C010 Parts, Service, and Operation Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 69 lbs. |
| Shipping Dimensions | 26 x 25 x 14 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| B-160-01 | Banner, 'Remove Before Flight' |
| G-1151-109716 | Screw, Socket Head Cap, ½ - 20 x 1 ¾" long |
| G-1300-13040 | Pin, Roll |
| G-1300-19040 | Pin, Roll, 3/16" diameter x ½" long |
| G-1310-0415 | Pin, Ball Lok-T, ¼" x 1.5" Grip |
| G-1310-0645 | Pin, Ball Lok-T, 3/8" x 4.5" Grip |
| G-1351-04 | Rivet |
| G-1398-150 | Third Cylinder Internal Ring |
| G-1398-200 | Second Cylinder Internal Ring |
| G-1398-250 | First Cylinder Internal Ring |
| H-1026*07.0 | Assembly, Lanyard |
| H-1026*12.0 | Assembly, Lanyard |
| H-1595-09 | Hand Pump with Labels |
| HC-1697-20 | Second Cylinder Wiper |
| HC-1697-24 | First Cylinder Wiper |
| HC-1697-28 | Main Cylinder Wiper |
| HC-1969 | Velocity Fuse |
| HC-2000-012 | O-Ring |
| HC-2000-218 | O-Ring |
| HC-2000-224 | Third Cylinder O-ring |
| HC-2000-228 | Second Cylinder O-ring |
| HC-2000-232 | First Cylinder O-ring |
| HC-2008-109 | O-Ring |
| HC-2008-236 | Main Cylinder O-ring |
| HC-2023-224 | Third Cylinder Backup Ring |
| HC-2023-228 | Second Cylinder Backup Ring |
| HC-2023-232 | First Cylinder Backup Ring |
| J-3548-01 | Plate Base |
| J-3549 | Ring, Cylinder Retaining |
| K-1508 | Kit, Hydraulic Hand Pump Seal |
| K-2728 | Nose Adapter Assembly Kit |
| K-3772 | Hand Pump Kit |
| N-2007-08-S-B | Connector, SAE #6 |
| N-2009-08-S | Connector, Male |
| N-2203-06-S | Nipple, Pipe |
| N-2712 | Coupler, Hydraulic (Female) |
| N-2713 | Nipple, Hydraulic (Male) |
| R-1628-03 | Mechanical Extension |
| R-1671 | Pin, Sliding |
| R-2131 | Jack Pad |
| TF-1104-01*31.0 | Assembly, Hose (#4 Mineral Base) |
| Z-3367-01 | Weldment, Nose Adapter Bracket with Labels |
| Z-3369 | Assembly, Nose Adapter Strap |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Cessna | Citation Longitude 700 , Citation Sovereign 680 , Latitude 680A |
PRODUCT REVIEWS
QUESTIONS & ANSWERS
The Tronair 02-7862C0100 hydraulic axle jack is used during aircraft maintenance tasks that require lifting the aircraft at the landing gear, such as tire changes, brake servicing, inspections, and component replacements. Axle jacks are commonly used in line maintenance and hangar environments where precise, controlled lifting is required. This unit supports both nose gear and main gear lifting when used with the appropriate adapters. Proper jacking enables technicians to safely access critical landing gear components without overstressing the aircraft's structures.
Aircraft axle jacks require trained operators because improper use can result in damage to the aircraft, equipment failure, or personal injury. Training ensures technicians understand correct positioning, load limits, and safe operating procedures. The manual emphasizes that employers are responsible for providing adequate operator training. Proper training also helps reduce the risk of unstable loads and uneven lifting.
Before lifting an aircraft, the jack must be placed on a hard, level surface and all aircraft tires not being raised must be properly chocked. The reservoir vent screw must be opened prior to operation, and the jack pad must be correctly aligned with the aircraft’s jacking point. Hands should never be placed between the aircraft and the jack pad. Following these precautions helps prevent sudden movement or load shifts during lifting.
The mechanical extension increases the closed height of the axle jack, allowing it to be positioned closer to the aircraft jacking point before hydraulic lifting begins. This reduces the amount of hydraulic travel required and improves overall stability. Proper use of the extension helps achieve correct lift geometry. It also minimizes the risk of misalignment during initial contact.
Using the specified hydraulic fluid is critical to ensuring safe operation and long-term reliability of the Tronair 02-7862C0100 axle jack. This unit is designed to operate with standard MIL-PRF-5606 hydraulic fluid, which provides the proper viscosity and seal compatibility required for consistent lifting performance. Using incorrect or incompatible fluids can cause seal degradation, reduced lifting efficiency, or internal damage over time. Regularly checking and maintaining proper fluid levels also helps extend service life and supports dependable aircraft jacking operations.
Routine inspections should be performed regularly, with Tronair recommending a daily visual inspection and a more detailed maintenance check at scheduled intervals. Annual load testing is required to confirm the jack can safely lift its rated capacity plus an additional margin. Regular maintenance includes checking for leaks, worn seals, and proper pump operation. Preventative maintenance helps extend equipment life and maintain safe operation.
No modifications may be made without written approval from Tronair. Only Tronair OEM replacement parts should be used. Unauthorized modifications or non-OEM components can void the warranty and compromise safety. Using approved replacement kits ensures proper fit and performance. This policy helps maintain compliance with manufacturer and safety standards.
The nose gear adapter ensures proper load distribution and secure attachment when lifting the aircraft’s nose landing gear. It interfaces directly with the aircraft strut, preventing slippage during lifting. Using the correct adapter is critical for safe and stable jacking operations. Improper or missing adapters can lead to uneven loading or damage to the aircraft.
Yes, the Tronair 02-7862C0100 is designed for use in both controlled hangar settings and ramp environments, provided surface conditions are stable and level. Its compact size and portable hand pump allow flexibility in various maintenance locations. Environmental conditions should always be evaluated prior to use. Proper ground conditions are essential for safe lifting.
Annual load testing verifies that the axle jack can safely lift its rated capacity under controlled conditions. The test involves applying a load equal to the jack’s capacity plus an additional safety margin. This process confirms the integrity of the hydraulic system and structural components. Regular load testing helps ensure compliance with maintenance and safety standards.



