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The Tronair 02-1036C0111 is a 10-Ton (20,000 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 36" (91.4 cm) closed height and 70" (177.8 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 Bombardier Challenger 300, Challenger 600, Challenger 601 and others. Also approved for Dassault Falcon 20-200, Falcon 50 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: 20,000 lbs (9072 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: 36" (91.4 cm)
- Mechanical Extension: 14" (35.6 cm)
- Hydraulic Extension: 20" (50.8 cm)
- Maximum Height Obtainable: 70" (177.8 cm)
- Weight: 185 lbs (84 kg)
- 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 02-1036C0111 is OEM-approved for the following aircraft types:
- Bombardier: Challenger 300, Challenger 600, Challenger 601, Challenger 604, Challenger 605 (CL605) and 5 more
- Dassault: Falcon 20-200, Falcon 50, Falcon 50EX
- Gulfstream: I
- Airbus Military (CASA): CN-235/HC-144A, C-295
- BAe: Jetstream 41
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 02-1036C0111 10-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 02A1036C0111
| Alternate Models | |
|---|---|
| 02-1036-0100 | Previous Model Number |
| 02-1036-0111 | Previous Model Number |
| 02-1036C0110 | Previous Part Number |
| 02A1036-0100 | Previous Model Number - With Air Pump |
| 02A1036C0111 | Air Pump Installed (CE) |
| 1036-100 | Previous Model Number |
| K-1043-15 | Air Pump Field Install Kit |
| General Information | |
|---|---|
| Part # | 02-1036C0111 |
| Manufacturer | Tronair |
| NSN | 1730016480242 |
| Manual 1 | View Tronair 02-1036C0111 Parts and Operation Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 245 lbs. |
| Shipping Dimensions | 38 x 38 x 43 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| G-1100-105006 | Bolt, Hex Head, Grade 5, ¼ - 20 x ¾ LG |
| G-1100-107010 | Bolt, Hex Head, Grade 5, 3/8-16 x 1" long |
| G-1100-109526 | Bolt, Hex Head, Grade 5, 1/2-20 x 2-3/4" long |
| G-1202-1050 | Stopnut, 1/4-20 Elastic |
| G-1203-1095 | Jamnut, 1/2-20 Elastic |
| G-1250-1050N | Flatwasher, 1/4 Narrow |
| G-1251-1070R | Lockwasher, 3/8 Regular |
| H-1009-01 | Assembly, Handle |
| H-1045 | Breather |
| H-1516-08 | Clamp, 2 Ear |
| HC-2329 | Reservoir, Translucent |
| HC-2764 | Pump, Hand |
| K-4585 | Kit, Jack Weldment |
| N-2001-08-S-B | Elbow, Straight Thread, SAE #6 x 3/8-37° JIC |
| N-2004-15-S | Elbow, Extra Long |
| N-2653-01-S-B | Elbow, 90° Male ¼ Hose x SAE #4 |
| N-2740-04-S-B | Tee, Male Branch, SAE #4 |
| N-2788-02-S-B | Elbow, 90° Male, SAE #6 x ¼ Hose |
| TF-1043-06*18.0 | Assembly, Hose |
| TF-1047-01*09.0 | Hose, 1/4" I.D. Gray |
| U-1002 | Wheel |
| V-1019 | Label, Capacity 10,000 lbs |
| V-1102-01 | Label, Use MIL-PRF-5606 |
| V-1819 | Label, Hydraulic Jack Caution |
| V-1820 | Label, Hydraulic Jack Instruction |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Airbus Military (CASA) | C-295 , CN-235/HC-144A |
| BAe | Jetstream 41 |
| Bombardier |
Challenger 300
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
Challenger 350
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
Challenger 600
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
Challenger 601
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
Challenger 604
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
Challenger 605 (CL605)
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
Challenger 650
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
Challenger 850
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
CRJ100
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
,
CRJ200
NOTE
This jack is used on the aircraft's main landing gear. Two main jacks are required per aircraft.
|
| Dassault |
Falcon 20-200
NOTE
This jack is used on the main and nose landing gear. One nose jack and two main jacks are required per aircraft.
,
Falcon 50
NOTE
This jack is used on the nose landing gear.
,
Falcon 50EX
NOTE
This jack is used on the nose landing gear.
|
| Gulfstream |
I
NOTE
This jack is used on the nose landing gear.
|
| Lockheed | Jetstar C-140 |
PRODUCT REVIEWS
Tronair is the best brand.
They will be used on a B737.
QUESTIONS & ANSWERS
Operators must always lower the ram locknuts after the aircraft is under load, as these are critical safety devices. Personnel should never work under a raised aircraft unless the load is secured, and care should be taken to avoid pinch points around the ram and locknuts. The jack must also be positioned on a clean, level surface and used only by trained technicians familiar with aircraft jacking procedures.
Before each use, the jack should be visually inspected for leaks, damage, or missing components. Technicians should check the hydraulic fluid level, confirm the ram and locking pins are in good condition, and verify that all nuts and bolts are tightened to specification. A quick function check – raising the ram to full stroke – also helps confirm the system is free of leaks before lifting an aircraft.
Preventative maintenance should be conducted regularly, with fluid level checks before each use. Casters should be lubricated every three months, and a thorough cleaning should be done annually or as needed. Additionally, the jack must undergo a load test at 105% to 110% of its rated capacity once a year to confirm performance and safety compliance.
When stored, the ram should always be fully lowered to protect seals and prevent contamination. If the jack is unused for 90 days, technicians should extend the ram fully, spray it with a BUNA N-compatible water-repellent lubricant, and then retract it for long-term protection. These practices prevent rust, seal degradation, and loss of hydraulic integrity.
To lower an aircraft, all jacks must be lowered simultaneously to keep the aircraft level. If the ram locknut is tight, the jack should first be raised slightly to release it. The pump release valve is then loosened carefully to allow a slow, controlled descent, while the ram locknut is raised as the jack lowers.
The jack must only be operated by skilled and trained aircraft technicians who are familiar with jacking procedures for the specific aircraft type. Employers are responsible for providing a training program covering operational safety, proper placement, and use of the jack. Maintenance and troubleshooting, however, should be performed only by technicians trained in hydraulic systems.
The tripod jack can be moved manually by rolling it on its casters. For longer transport or heavy handling, it can be lifted with a crane using straps through the tripod top or by using a forklift under the lower tripod support. At approximately 185 lbs (83.9 kg), it is designed for manageable ground handling.
K-3441 is the compatible pump seal kit for the 02-1036C0111 aircraft hydraulic tripod jack. This replacement kit is designed to restore proper sealing performance in the hydraulic pump, ensuring smooth operation and preventing leaks during lifting tasks. Using the correct OEM-approved pump seal kit helps extend the jack's service life and maintain safe, reliable aircraft maintenance operations.
The Tronair K-1050 ram seal kit is the approved replacement kit for the ram assembly of the 02-1036C0111 hydraulic tripod jack. Installing this kit helps maintain the jack’s lifting capacity by preventing hydraulic fluid leaks and preserving proper pressure within the ram. Regular inspection and timely replacement of ram seals are critical for keeping the jack dependable, especially during heavy-duty aircraft maintenance procedures.
