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The Tronair 02-0520C0111 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. CE-marked for compliance with European aviation safety standards. OEM-specified for Cessna Bravo, Citation CJ1, Citation CJ2 and others. Also approved for Grob G120A, G120TP.
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)
- 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 02-0520C0111 is OEM-approved for the following aircraft types:
- Cessna: Bravo, Citation CJ1, Citation CJ2, Citation CJ3, Citation Encore 560 and 8 more
- Grob: G120A, G120TP
- 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 02-0520C0111 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 | |
|---|---|
| 02-0520-0100 | Previous Model Number |
| 02-0520-0110 | Previous Model Number |
| 02-0520C0110 | Previous Model Number (CE) |
| 02C0520C0111 | Spring Loaded Casters (Factory Installed) |
| General Information | |
|---|---|
| Part # | 02-0520C0111 |
| Manufacturer | Tronair |
| Manual 1 | View Tronair 02-0520C0111 Parts and Operation Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 150 lbs. |
| Shipping Dimensions | 25 x 21 x 25 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Specifications | |
|---|---|
| Capacity | 5 tons |
| Closed Height | 20" (51 cm) |
| Fully Extended | 38" (97 cm) |
| Hydraulic Extension | 12" (30 cm) |
| Mechanical Extension | 6" (15 cm) |
| Single (S) or Multi (M) Stage | M |
| Weight | 90 lbs. (41 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 2¾" 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, ½" 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-1948 | Pump, Hydraulic Hand |
| HC-2000-331 | O-Ring |
| HC-2021-01 | Ring, Backup |
| 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-2053-05-S-B | Plug, Hex Head w/o O-ring, SAE #6 |
| N-2653-01-S-B | Elbow, 90º 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*06.0 | Hose, ¼ Gray x 6" Long |
| TF-1047-01*09.0 | Hose, ¼ 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-1198-02 | 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.
|
| Cessna |
Bravo
NOTE
This jack is used on the nose landing gear.
,
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 jack.
,
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
An adapter kit (K-3314) is required for this nose landing gear jack.
,
Citation I 500
NOTE
This jack is used on the nose landing gear.
,
Citation I/SP 501
NOTE
This jack is used on the nose landing gear.
,
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.
|
| Grob | G120A , G120TP |
PRODUCT REVIEWS
QUESTIONS & ANSWERS
Yes, the jack is designed for use between -4°F and 122°F (-20°C to 50°C), and it can be stored outdoors if properly protected. Tronair recommends using a full coverage waterproof tarp or canvas during outdoor storage to shield the hydraulic seals and components from dirt, water, and foreign debris.
The 02-0520C0111 jack is designed to operate with MIL-PRF-5606 hydraulic fluid. This fluid is non-polluting and widely used in aviation hydraulic systems, ensuring compatibility with other aircraft ground support equipment and easy maintenance.
The jack must be placed on a clean, level, and hard surface directly under the aircraft’s approved jack pad. Operators should never attempt to align the jack by striking its legs, as this can damage the structure and lead to unsafe conditions. Always follow the aircraft manufacturer’s jacking procedures.
The jack includes a ram locknut that mechanically secures the load and a pressure relief valve to prevent overload during lifting. Additionally, caution labels are placed directly on the unit to guide operators during use, reducing the chance of misuse.
The jack can be operated manually via a hydraulic hand pump or pneumatically when equipped with the optional air pump. To raise the aircraft, the operator extends the ram while keeping the locknut within one inch of the cylinder base. To lower, the locknut is released and the pump valve opened slowly to ensure a controlled descent.
Tronair recommends a 90-day inspection and a 12-month load test. Routine checks should include monitoring fluid levels, inspecting casters, and cleaning the jack annually or as needed. Seal replacement kits are available to support long-term reliability.
The jack can be rolled by hand on its integrated casters for short distances around the hangar. For longer moves or shipping, it should be lifted with a forklift or crane and secured in a freight-rated crate to prevent damage.
This jack is intended for use by trained and skilled aircraft maintenance personnel. Operators must be familiar with both the operation of the jack and the specific jacking procedures for the aircraft being serviced. Employers are responsible for ensuring adequate operator training.
