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The Tronair 02-7812C0110 is a 5-Ton (10,000 lb) hydraulic aircraft tripod jack engineered to lift aircraft from the forward fuselage or main wing jacking points during maintenance, inspections, and ground operations. With a 54" (137.2 cm) closed height and 94" (238.8 cm) maximum extended height, it accommodates a range of aircraft fuselage and wing jacking point heights. CE-marked for compliance with European aviation safety standards. OEM-specified for Piaggio P-180 Avanti.
Standard Features
- Hand pump with built-in pressure relief valve
- Threaded rams with improved handwheel-style safety nut
- Quick-rising center extension for rapid initial lift
- Easy-access filler/breather cap
- Heavy-duty wheels for easy maneuverability
- Hydraulic fluid: MIL-PRF-5606
- ¾" (2 cm) spherical radius cup jack pad
- CE marked
- Durable powder-coat finish (Tronair Blue)
Technical Specifications
- Rated Capacity: 10,000 lbs (4536 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: 54" (137.2 cm)
- Maximum Height Obtainable: 94" (238.8 cm)
- Hydraulic Fluid: MIL-PRF-5606
- Jack Pad: ¾" (2 cm) spherical radius cup
- Finish: Durable powder coat (Tronair Blue)
Safety Features
- Ram Lock Nut: Prevents the lowering of the ram. The ram lock nut must be lowered as the aircraft is being lifted. Ram lock nuts must be kept within 2" of the stop while raising the aircraft.
- Lock Nut Retention Ring: Prevents the lock nut from being unscrewed from the second stage.
- Pressure Relief Valve: Prevents overload during raising operations.
Aircraft Applications
The 02-7812C0110 is OEM-approved for the following aircraft types:
- Piaggio: P-180 Avanti
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 02-7812C0110 5-ton tripod 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 | |
|---|---|
| 02-7812-0110 | Previous Part Number |
| General Information | |
|---|---|
| Part # | 02-7812C0110 |
| Manufacturer | Tronair |
| Manual 1 | View Tronair 02-7812C0110 Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 350 lbs. |
| Shipping Dimensions | 53 x 58 x 67 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| G-1318-0825 | Pin, 1/2x2.5" Model D |
| G1100-105006 | Bolt, Hex Head, Grade 5, 420 x Long |
| G1100-107010 | Bolt, Hex Head, Grade 5, 3/8-16x1" long |
| G1151-106205 | Screw, Socket Head Cap, 5/16-18x5/8" long |
| G1250-1050N | Flatwasher, 1/4 Narrow |
| G1251-1070R | Lockwasher, 3/8 Regular |
| G1300-25160 | Pin, 1/4" diameter x1-3/4" long, Roll |
| H-1045 | Breather |
| H-2329 | Reservoir, Translucent |
| H-2334 | Locknut |
| HC-1948 | Pump, Hydraulic Hand |
| HJ-513 | Plate, Mounting |
| HJ-522-04 | Assembly, Ram (includes Seals) |
| HJ-526-05 | Extension |
| HJ-532-01 | Pad, Jack |
| HJ-536 | Ring, Protection |
| K-1061-02 | Kit, Reservoir Replacement |
| N-2001-05-S-B | Elbow, Straight Thread |
| N-2004-06-S | Elbow, Extra Long Male |
| N-2653-01-S-B | Elbow, 90° Male, 1¼ Hose x SAE #4 |
| N-2788-02-S-B | Elbow, 900 Male |
| TF-1043-03 15.0 | Assembly, Hose, 15" long |
| TF-1047-01*09.0 | Hose, 1/4 Gray x 9" long |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Piaggio |
P-180 Avanti
NOTE
This jack is used on the main landing gear. Two main jacks are required per aircraft.
|
PRODUCT REVIEWS
QUESTIONS & ANSWERS
The mechanical ram locknut on the Tronair 02-7812C0110 provides an added layer of safety by preventing unintended lowering of the jack under load. Once the aircraft is raised, the locknut is lowered into position to mechanically support the load rather than relying solely on hydraulic pressure. This reduces the risk of pressure loss affecting stability during maintenance. It is a critical safety feature for secure aircraft support.
The tripod configuration distributes the load evenly across three points of contact, enhancing balance and stability during aircraft lifting. Combined with a wide base radius, this design minimizes the risk of tipping during operation. It is particularly beneficial when working on uneven hangar floors or during extended maintenance procedures. This stable footprint supports safer and more controlled lifting.
Operators should always use the jack on a hard, level surface and ensure proper alignment with the aircraft jack point. The manual emphasizes using a tail or nose stand in conjunction with the tripod jack for additional stability. It is also important to raise and lower all jacks simultaneously to keep the aircraft level. Following these precautions helps prevent sudden load shifts and ensures safe operation.
The locking pin must be correctly positioned within the ram protection ring groove to ensure safe operation. Incorrect placement can lead to deformation, reduced load capacity, or potential jack failure under load. The manual highlights several incorrect configurations that can compromise safety, reinforcing the importance of proper installation. Ensuring correct pin placement helps maintain structural integrity and operator safety.
Routine maintenance includes checking hydraulic fluid levels, inspecting seals and O-rings, and ensuring all fasteners are properly tightened. The manual also recommends periodically extending and retracting the jack to keep the seals lubricated and prevent internal corrosion. Cleaning and protecting the ram threads with approved lubricants can further extend service life. Regular maintenance helps ensure consistent performance and reliability.
Preventative maintenance inspections should be performed every 90 days, along with annual load testing to verify performance under rated capacity. The maintenance schedule includes checking for leaks, inspecting structural components, and verifying proper operation of the hydraulic system. Load testing should not exceed the rated capacity plus 10%. These checks help maintain compliance and ensure safe operation over time.
The hydraulic system uses a single-acting cylinder and a hand pump to provide controlled, steady lifting of the aircraft. Internal check valves and pressure relief components help maintain consistent pressure and prevent overload conditions. This allows operators to raise the aircraft gradually and precisely. The result is smoother operation and better control during maintenance procedures.
Yes, the jack is fully serviceable using OEM replacement parts and kits. PJi provides kits for seals, internal components, and hydraulic pump assemblies. Using approved parts ensures proper fit and maintains the jack’s original performance specifications. This serviceability helps extend the equipment's lifespan and reduce long-term operating costs.
Proper storage is essential to protect the jack from contamination and environmental damage. The manual recommends covering the unit during washing or cleaning operations to prevent dirt or chemicals from damaging seals and O-rings. Keeping the jack clean and storing it in a dry environment helps prevent corrosion and seal degradation. Following these practices ensures long-term reliability and consistent performance.


