Tronair 02A0517C0140 – 5-Ton Tripod Jack, Air Pump
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The Tronair 02A0517C0140 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. A factory-installed air pump allows rapid initial extension without additional equipment. CE-marked for compliance with European aviation safety standards. OEM-specified for Cessna Mustang 510, 408 SkyCourier. Also approved for Eclipse 500.
Standard Features
- Factory-installed air pump for rapid initial extension and on-aircraft inflation
- 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)
- Air Supply Requirements:
- Minimum: 25 PSI (1.72 bar)
- Recommended: 40 PSI (2.75 bar)
- Maximum: 125 PSI (8.6 bar)
- Pressure Relief Setting: 2,500 + 250/−0 PSIG (172.4 + 17.2/−0 bar)
- Noise Level: 64 dB(A) at a distance of 120" (304.8 cm) at an inlet pressure of 100 PSI (6.9 bar)
- 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.
- Hold-to-Run Air Valve: Requires the operator to hold the air valve lever to raise the ram using the air pump. Releasing the air valve lever stops the upward movement of the ram.
- 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 02A0517C0140 is OEM-approved for the following aircraft types:
- Cessna: Mustang 510, 408 SkyCourier
- Eclipse: 500
- Airbus Military (CASA): CN-235/HC-144A, 212-100, 212-200
- Bell: 206B3, 206L4, 206LT, 214, 214ST and 11 more
- Eurocopter: AS330 Puma, AS365N Dauphin
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 02A0517C0140 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.
Also Available
- Without air pump (hand pump only): Tronair 02-0517C0140
| General Information | |
|---|---|
| Part # | 02A0517C0140 |
| Manufacturer | Tronair |
| Shipping Information | |
|---|---|
| Shipping Weight | 170 lbs. |
| Shipping Dimensions | 35 x 31 x 25 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Specifications | |
|---|---|
| Capacity | 5 tons |
| Closed Height | 17 (43) in (cm) |
| Fully Extended | 46 (117) in (cm) |
| Hydraulic Extension | 22 (56) in (cm) |
| Mechanical Extension | 7 (18) in (cm) |
| Single (S) or Multi (M) Stage | M |
| Weight | 105 (48) lb (kg) |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Agusta | AW169 , AW189 |
| Airbus Military (CASA) | 212-100 , 212-200 , CN-235/HC-144A |
| Bell | 206B3 , 206L4 , 206LT , 214 , 214ST , 222 , 230 , 407 , 407GX , 427 , 429 , 430 , 505 , CH-139 , OH-58 , TH-67 |
| Cessna |
408 SkyCourier
,
Mustang 510
NOTE
Nose/main landing gear jacks – 3 jacks, 2 main jack pads (R-1798), and 1 nose jack pad (R-2008) per aircraft required.
|
| Eclipse | |
| Eurocopter | AS330 Puma , AS365N Dauphin |
| HondaJet |
HA-420 HondaJet
NOTE
Main landing gear jack. Two main jacks are required per aircraft. Control all 3 jacks with air pumps using the optional Manifold Kit (K-1106).
|
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QUESTIONS & ANSWERS
The factory-installed air pump allows technicians to raise the jack more quickly during initial positioning, helping reduce manual pumping effort during aircraft maintenance procedures. This can improve workflow efficiency in busy hangars or flight line environments where fast aircraft turnaround is important. The integrated pneumatic system also eliminates the need for separate external lifting accessories. According to the Tronair operation and service manual, the air system operates with a recommended supply pressure of 40 PSI and a maximum of 125 PSI.
The two-stage hydraulic configuration provides extended lifting capability while maintaining stable and controlled aircraft support throughout the lift cycle. This design allows the jack to accommodate a wider range of aircraft jacking point heights compared to some single-stage models. The staged extension system also helps maintain smoother load distribution during lifting and lowering operations. Tronair’s service manual notes that the hydraulic rams extend in sequence from the largest to the smallest diameter stage for proper operation.
The hold-to-run air valve requires continuous operator engagement for pneumatic lifting, thereby maintaining direct control during aircraft jacking operations. If the operator releases the valve lever, upward ram movement immediately stops. This safety-focused design helps reduce the risk of unintended movement while positioning the aircraft jack under load. Tronair specifically identifies this feature as an operator-controlled safety mechanism within the manual.
The ram protection ring helps ensure proper placement of the locking pin used with the mechanical extension system. Correct pin positioning is critical for maintaining structural integrity and preventing premature component failure during lifting operations. The Tronair manual includes detailed illustrations showing both correct and incorrect pin placements to help technicians avoid unsafe configurations.
The quick-rising center extension allows technicians to bring the jack pad closer to the aircraft jacking point before engaging full hydraulic lifting pressure. This reduces the number of hand pump strokes required during initial setup and can improve maintenance efficiency. Faster positioning is especially useful during inspections, tire changes, and routine aircraft servicing, where multiple jacks may be used simultaneously.
The 5-ton load rating and versatile lifting design make this aircraft tripod jack suitable for a wide range of business jets, utility aircraft, helicopters, and military aircraft. OEM approvals for aircraft, including the Cessna Mustang 510, Eclipse 500, Bell helicopter models, and Airbus Military CASA aircraft, demonstrate its adaptability across multiple aviation sectors. This flexibility can help maintenance facilities standardize ground support equipment across mixed fleets.
The threaded handwheel-style safety nut provides positive mechanical support after the aircraft has been raised. Technicians can lower the safety nut against the ram during lifting operations to help secure the load independently of hydraulic pressure alone. This mechanical locking method is widely recognized throughout the aviation industry as an important aircraft jacking safety practice.
Routine fluid inspections, annual cleaning, caster lubrication, and scheduled load testing help maintain the long-term performance of aircraft jacks. Tronair recommends exercising the jack every 90 days during low-use periods to help protect seals and minimize internal corrosion buildup. The manual also advises using water-repellent protectants on exposed ram surfaces and threads when the jack is stored.
MIL-PRF-5606 hydraulic fluid is widely used throughout the aviation industry because it performs reliably across broad operating temperature ranges and is compatible with many aircraft hydraulic systems. Using aviation-approved hydraulic fluid helps support dependable lifting performance in both hangar and outdoor maintenance environments. Standardized fluid specifications can also simplify maintenance procedures and inventory management for aviation service facilities.
CE certification indicates that the jack complies with applicable European machinery safety requirements and engineering standards. This can simplify equipment approval and operational consistency for maintenance providers supporting international fleets or overseas operations. The included EU Declaration of Conformity confirms compliance with the European Machinery Directive and recognized machinery safety standards.



