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The Tronair 02-1240C0111 is a 12-Ton (24,000 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 40" (101.6 cm) closed height and 78" (198.1 cm) maximum extended height, it accommodates a range of aircraft fuselage and wing jacking point heights. The single-stage hydraulic design provides controlled lift and positive lock at any extension height. CE-marked for compliance with European aviation safety standards. OEM-specified for Dassault Falcon 2000, Falcon 2000EX, Falcon 900 and others.
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: 24,000 lbs (10886 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: 40" (101.6 cm)
- Maximum Height Obtainable: 78" (198.1 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 02-1240C0111 is OEM-approved for the following aircraft types:
- Dassault: Falcon 2000, Falcon 2000EX, Falcon 900, Falcon 900EX
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 02-1240C0111 12-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
- With factory-installed air pump: Tronair 02A1240C0111
| Alternate Models | |
|---|---|
| 02-1240-0111 | Previous Model Number |
| 02A1240C0111 | With Air Pump Installed on Jack |
| General Information | |
|---|---|
| Part # | 02-1240C0111 |
| Manufacturer | Tronair |
| NSN | 4910016784758 |
| Manual 1 | View Tronair 02-1240C0111 Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 350 lbs. |
| Shipping Dimensions | 38 x 38 x 42 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| 50866 | Haskel Seal Lubricant |
| G1100-105006- | Bolt, HH Grade 5, 1/4-20x3/4 Lg |
| G1100-105510- | Bolt, Hex Head, Grade 5, 1/4-28x1" long |
| G1100-106512- | Bolt, Hex Head, Grade 5, 5/16-24x1 1/4" long |
| G1100-107010- | Bolt, Hex Head, Grade 5, 3/8-16x1" long |
| G1151-107206- | Screw, Socket Head Cap, 3/8-16x3/4" long |
| G1202-1055- | Stopnut, 1/4-28 Elastic |
| G1202-1065- | Stopnut, 5/16-24 Elastic |
| G1203-1105- | Jamnut, 5/8-18 Elastic |
| G1250-1050N- | Flatwasher, 1/4 Narrow |
| G1250-1060N- | Flatwasher, 5/16 Narrow |
| G1250-1100N- | Flatwasher, 5/8 Narrow |
| G1250-1100W- | Flatwasher, 5/8 Wide |
| G1251-1070R- | Lockwasher, 3/8 Regular |
| G1300-25200- | Pin, 1/4" diameter x 2" long, Roll |
| G1318-1033- | Pin, 5/8" diameter x 3.3" long, Model D |
| H-1009-01 | Assembly, Pump Handle |
| H-1045 | Breather |
| H-1174 | Pump, Air |
| H-1252 | Spring |
| H-1516-11 | Clamp, 2 Ear Hose |
| H-2331 | Locknut |
| HC-2000-336 | O-ring |
| HC-2020-336 | Ring, Back-up |
| HC-2322 | Pump, Hydraulic Hand |
| HC-2329 | Reservoir, Translucent |
| HJ-225-04 | Extension |
| HJ-553 | Ring, Protection |
| HJ-554 | Ring, Guide |
| HJ-557 | Pad, Jack |
| HJ-586-03 | Assembly, Ram (includes seals) |
| J-3415-01 | Bracket, Air Pump |
| K-1050 | Kit, Seal Replacement |
| K-1061-02 | Kit, Reservoir Replacement |
| K-1685 | Haskel Repair Fluid Seal Kit |
| K-1686 | Haskel Repair Air Seal Kit |
| K-3333 | Assembly, Blowgun |
| K-4021 | Kit, Jack Weldment Replacement |
| N-2001-08-S-B | Elbow, Straight Thread, SAE #6 x 3/8-37° JIC |
| N-2004-15-S | Elbow, 3/8 JICx3/8 NPT |
| N-2005-08-S | Connector, Male |
| N-2066-06-S-B | Plug, O-Ring Hex Head #6 SAE Port |
| N-2410-11 | Elbow, 90° Male |
| N-2653-01-S-B | Elbow, 90° Male, 1/4 Hose x SAE #4 |
| N-2740-04-S-B | Tee, Male Branch, 3/8 NPT |
| N-2788-02-S-B | Elbow, 90° Male 3/8 Hose x #6 SAE Port |
| N-2789-03-S-B | Connector, Straight Male, 3/8 NPT, 3/8 Hose |
| TF-1043-03*16.0 | Assembly, Hose |
| TF-1043-0618.0* | Assembly, Hose, 18" long |
| TF-1047-01*05.5 | Hose, 1/4 "I.D. Gray |
| TF1047-01-*05.5 | Hose, 1/4 "I.D. Gray x 5 1/2" long |
| TF1047-01-*10.0 | Hose, 1/4 " Push-On x 10" Long |
| TR-1505 | Stop, Jack |
| TR-1756 | Plate, Mounting |
| U-1053 | Caster, Stem |
| V-1001 | Label, Made in USA |
| V-1017 | Label, Maximum Capacity 24,000 lbs |
| V-1102-01 | Label, 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-2105 | Label, Hydraulic Jack Instructions |
| V1779- | Babel, Serial Number |
| Z-5118-01 | Weldment, Jack |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Dassault |
Falcon 2000
NOTE
This jack is used on the main and nose landing gear. Two main jacks and one nose jack are required per aircraft.
,
Falcon 2000EX
NOTE
This jack is used on the main and nose landing gear. Two main jacks and one nose jack are required per aircraft.
,
Falcon 900
NOTE
This jack is used on the main and nose landing gear. Two main jacks and one nose jack are required.
,
Falcon 900EX
NOTE
This jack is used on the main and nose landing gear. Two main jacks and one nose jack are required per aircraft.
|
PRODUCT REVIEWS
QUESTIONS & ANSWERS
The Tronair 02-1240C0111 is engineered to lift aircraft by the fuselage or main wing when used in coordinated jacking configurations, ensuring proper balance and stability. It is specifically configured for certain Dassault Falcon aircraft, but must always be used in accordance with the aircraft manufacturer’s jacking procedures. The jack is not intended for metal forming or non-aviation lifting tasks. Proper aircraft-specific jack pads and positioning are critical to safe operation.
This hydraulic tripod jack includes a user-operated ram locknut that mechanically secures the load once the aircraft is raised. It also features a pressure relief valve to prevent overload during lifting operations. Warning labels and clear operating instructions are integrated into the unit to support technician awareness. These layered safeguards are designed to reduce the risk of accidental lowering or hydraulic overload.
The ram locknut is a primary mechanical safety device and must be lowered as the aircraft is being raised. Failure to properly engage the locknut can result in serious injury or equipment damage. The manual emphasizes that personnel must never work under a raised load unless it is secured by suitable means, such as the engaged locknut. This redundancy ensures the aircraft remains supported even if hydraulic pressure is lost.
The jack is intended for use on a clean, level surface within an operating temperature range of -20°C to 50°C (-4°F to 122°F). Maintaining proper environmental conditions helps preserve hydraulic integrity and structural stability. The unit is considered non-polluting when operated with the recommended hydraulic fluid. Storage guidelines also recommend keeping the ram fully retracted when not in use.
The jack requires MIL-PRF-5606 hydraulic fluid for proper operation and maintenance. Fluid levels should be checked before each use and maintained approximately 1.5" below the reservoir vent cap. Using the specified fluid ensures compatibility with internal seals and components. Substituting other fluids could lead to premature seal degradation or hydraulic failure.
Routine maintenance includes checking fluid levels before each use, lubricating casters every 3 months, and performing an annual capacity test at 105% to 110% of rated capacity. Annual cleaning and inspection are also recommended. If the jack is unused for 90 days, corrosion-prevention measures should be applied to the ram. These preventive steps help extend service life and maintain lifting accuracy.
Yes. The manual recommends annual load testing at up to 110% of rated capacity to verify performance and safety . Testing must always be conducted against a controlled load, not against the jack itself. Observing proper test protocols confirms that hydraulic components and structural elements remain within certified operating limits. Regular testing supports compliance with aviation maintenance standards.
The jack is intended for use by skilled, trained aircraft technicians familiar with both hydraulic systems and aircraft jacking procedures. Installation, maintenance, and dismantling must also be performed by qualified personnel. Employers are responsible for providing appropriate training programs. Proper operator qualification reduces risk during critical lifting operations.
No. The manual clearly states that modifications without written approval from Tronair void all warranties and release the manufacturer from liability. Only Tronair OEM replacement parts are authorized for use. Using non-approved components can compromise structural integrity and safety. Adhering to OEM guidelines ensures continued compliance and warranty protection.
Tronair warrants that the jack is free of manufacturing or material defects for one year from the date of shipment to the original customer. Warranty coverage is limited to repair or replacement of defective components and does not include normal maintenance items. Replacement parts carry a 90-day warranty from the date of shipment. Unauthorized modification or misuse immediately voids warranty coverage.



