Tronair 02A0520C0110 – 5-Ton Tripod Jack, Air Pump
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The Tronair 02A0520C0110 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 20" (50.8 cm) closed height and 38" (96.5 cm) maximum extended height, it accommodates a range of aircraft fuselage and wing jacking point heights. 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 Bravo, Citation CJ1, Citation CJ2 and others. Also approved for Bombardier Learjet 60.
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)
- Minimum Closed Height: 20" (50.8 cm)
- Maximum Height Obtainable: 38" (96.5 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.
- 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 02A0520C0110 is OEM-approved for the following aircraft types:
- Cessna: Bravo, Citation CJ1, Citation CJ2, Citation CJ3, Citation Encore 560 and 8 more
- Bombardier: Learjet 60
- Bell: 214, 214ST, 222, 230, 430
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 02A0520C0110 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.
| General Information | |
|---|---|
| Part # | 02A0520C0110 |
| Manufacturer | Tronair |
| Shipping Information | |
|---|---|
| Shipping Weight | 150 lbs. |
| Shipping Dimensions | 31 x 37 x 31 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Specifications | |
|---|---|
| Capacity | 5 tons |
| Closed Height | 20 (51) in (cm) |
| Fully Extended | 38 (97) in (cm) |
| Hydraulic Extension | 12 (30) in (cm) |
| Mechanical Extension | 6 (15) in (cm) |
| Single (S) or Multi (M) Stage | M |
| Weight | 90 (41) lb (kg) |
| Spare Parts | |
|---|---|
| G-1100-105006 | Bolt, Hex Head, Grade 5, ¼ - 20 x ¾ long |
| G-1100-107010 | Bolt, Hex Head, Grade 5, 3/8-16 x 1" long |
| G-1100-109526 | Bolt, Hex Head, ½-20 x 2 ¾" long |
| G-1151-106205 | Screw, Socket Head Cap, 5/16 -18 x 5/8" long |
| G-1203-1095 | Jamnut, ½-20, Elastic |
| G-1250-1050N | Flatwasher, ¼ Narrow |
| G-1251-1070R | Lockwasher, 3/8 Regular |
| G-1307-0418 | Pin, ¼" diameter x 1.8" long |
| G-1318-0825 | Pin, 1/2" diameter x 2.5" long “D” |
| H-1009-01 | Assembly, Pump Handle |
| H-1045 | Breather |
| H-1516-08 | Clamp, 2 Ear Hose |
| H-2334 | Locknut |
| HC-2000-331 | O-ring |
| HC-2021-01 | Ring, Backup |
| HC-2322 | Pump, Hydraulic Hand |
| HC-2328 | Reservoir, Translucent |
| HJ-512 | Ring, Guide |
| HJ-513 | Plate, Mounting |
| HJ-522-01 | Assembly, Ram (includes Seals) |
| HJ-526-01 | Extension |
| HJ-532-01 | Pad, Jack |
| HJ-532-02 | Pad, Jack |
| HJ-536 | Ring, Protection |
| K-1049 | Kit, Ram Seal Replacement |
| K-1061-04 | Kit, Reservoir Replacement |
| K-1334 | Kit, Jack Weldment Replacement |
| N-2001-08-S-B | Elbow, Straight Thread |
| N-2003-06-S | Elbow, 3/8 JIC x ¼ NPT |
| N-2653-01-S-B | Elbow, 90° Male, ¼ Hose x SAE #4 |
| N-2788-02-S-B | Elbow, 90º |
| TF-1043-03*15.0 | Assembly, Hose, 15" long |
| TF-1047-01*09.0 | Hose, 1/4 Gray x 9" long |
| U-1002 | Wheel |
| V-1001 | Label, Made in USA |
| V-1003 | Label, Serial Number |
| V-1016 | Label, Capacity 10,000 lbs |
| V-1102 | Label, Use MIL-PRF-5606 |
| V-1198 | Label, Tronair |
| V-1775 | Label, Pump Force |
| V-1776 | Label, Down |
| V-1805 | Label, ISO General Danger |
| V-1819 | Label, Hydraulic Jack Caution |
| V-1820 | Label, Hydraulic Jack Instruction |
| Z-5031-01 | Weldment, Jack |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Bell | 214 , 214ST , 222 , 230 , 430 |
| Bombardier |
Learjet 60
NOTE
This jack is used on the aircraft's nose landing gear. Control all 3 jacks with air pumps using the optional Manifold Kit (K-1106).
|
| Cessna |
Bravo
NOTE
This jack is required for use on the nose landing gear. Use the Air Pump Manifold Kit (K-1106) to control all 3 jacks at once.
,
Citation CJ1
NOTE
A jack pad kit (K-3314) is required for use with this nose landing gear jack.
,
Citation CJ2
NOTE
A jack pad kit (K-3314) is required for use with this nose landing gear.
,
Citation CJ3
NOTE
A jack pad kit (K-3314) is required for use with this nose landing gear jack.
,
Citation CJ4
NOTE
This jack is used on the nose landing gear.
,
Citation Encore 560
NOTE
Adapter kit (K-3314) required for this nose jack. Control all 3 tripod jacks with air pumps using the Manifold Kit (K-1106).
,
Citation I 500
NOTE
This jack is used on the nose landing gear.
,
Citation I/SP 501
NOTE
This jack is required for use on the nose landing gear.
,
Use the Air Pump Manifold Kit (K-1106) to control all 3 jacks at once.
Citation II 550
NOTE
This jack is used on the nose landing gear.
,
Citation M2
NOTE
A jack pad adapter (K-3314) is required for use on this nose landing gear jack.
,
Citation SII
NOTE
This jack is used on the nose landing gear.
,
Citation Ultra 560
NOTE
A jack pad (R-2008) is required for use with this nose landing gear jack.
,
Citation V
NOTE
This jack is used on the nose landing gear.
|
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QUESTIONS & ANSWERS
The single-stage hydraulic design simplifies operation and maintenance while delivering reliable lifting performance for aircraft maintenance tasks. Fewer moving hydraulic stages can help reduce maintenance complexity and improve long-term serviceability. This configuration also provides a stable lifting platform for aircraft inspections, tire changes, and routine servicing.
The 20” closed height allows the aircraft tripod jack to fit beneath the lower fuselage and wing jacking points commonly found on business jets and utility aircraft. This can reduce setup difficulties when working in confined hangar environments or on aircraft with limited ground clearance. Combined with the 38” maximum height, the jack provides technicians with greater flexibility across multiple aircraft platforms.
The mechanical extension allows technicians to position the jack closer to the aircraft jacking point before hydraulic lifting begins. This helps reduce the amount of hydraulic travel required and can speed up aircraft lifting operations. According to the Tronair manual, the jack includes a 6” mechanical extension combined with 12” of hydraulic extension for added lifting versatility.
The ram protection ring helps ensure the locking pin is installed correctly during mechanical extension setup. Proper placement of locking pins is critical for maintaining structural support and preventing premature component deformation during aircraft jacking procedures. The manual includes detailed examples of both correct and incorrect locking pin positioning to reinforce safe operating practices.
The integrated heavy-duty wheels allow technicians to maneuver the aircraft jack more easily across hangar floors and maintenance areas. Easier transport can reduce setup time when repositioning multiple jacks around larger aircraft. The jack’s approximate 90-lb operating weight also helps balance portability with structural durability during daily maintenance operations.
Raising and lowering all aircraft jacks simultaneously helps maintain proper aircraft balance and structural stability during maintenance procedures. Uneven lifting can place unnecessary stress on the airframe and create unsafe working conditions. Tronair specifically instructs operators to raise and lower jacks together so the aircraft remains level throughout the process.
The translucent reservoir allows technicians to visually monitor hydraulic fluid levels more easily during inspections and routine maintenance. Faster fluid checks can help reduce downtime and support proper hydraulic system performance. The manual specifies maintaining the hydraulic fluid level approximately 1.5 inches below the reservoir vent when the ram is fully retracted.
Annual load testing helps verify that the aircraft jack continues to meet its rated lifting capacity and operational performance requirements. Regular testing can identify wear, hydraulic issues, or structural concerns before they affect maintenance operations. Tronair recommends capacity testing at 105% to 110% of the jack’s rated capacity as part of its preventive maintenance schedule.
OEM-approved aircraft jacks are designed and evaluated for compatibility with specific aircraft lifting points, weight requirements, and maintenance procedures. Using approved ground support equipment helps maintenance facilities align with manufacturer recommendations and aviation safety standards. The 02A0520C0110 is approved for several aircraft models, including the Citation CJ series, Learjet 60, and multiple Bell helicopter platforms.
Proper storage practices help protect hydraulic seals, ram surfaces, and structural components from corrosion and contamination. Tronair recommends storing the jack with the ram fully lowered and protecting it with a waterproof cover when stored outdoors. The manual also advises cycling the ram during long periods of inactivity and applying water-repellent lubricant to exposed surfaces to help preserve performance.


