Tronair 02A1036C0111 – 10-Ton Tripod Jack, Air Pump
Create yours now for free.
Need a Quote?
The Tronair 02A1036C0111 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. The single-stage hydraulic design provides controlled lift and positive lock at any extension height. A factory-installed air pump allows rapid initial extension without additional equipment. 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
- 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: 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)
- 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 02A1036C0111 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
- Airbus Military (CASA): CN-235/HC-144A, C-295
- BAe: Jetstream 41
- Lockheed: Jetstar C-140
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 02A1036C0111 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
- Without air pump (hand pump only): Tronair 02-1036C0111
| General Information | |
|---|---|
| Part # | 02A1036C0111 |
| Manufacturer | Tronair |
| NSN | 1730015521011 |
| Manual 1 | View Tronair 02A1036C0111 Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 270 lbs. |
| Shipping Dimensions | 38 x 38 x 43 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| 28442 | Lubricant, Haskel Seal |
| G-1100-105006 | Bolt, Hex Head, Grade 5, ¼ - 20 x ¾ LG |
| G-1100-105510 | Bolt, Hex Head, Grade 5, 1/4-28 x 1 long |
| G-1100-106512 | Bolt, Hex Head, Grade 5, 5/16-24 x 1-1/4 " long |
| 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-1151-107206 | Screw, Socket Head Cap, 3/8-16 x 3/4" long |
| G-1202-1050 | Stopnut, 1/4-20 Elastic |
| G-1202-1055 | Stopnut, 1/4-28 Elastic |
| G-1202-1065 | Stopnut, 5/16-24 Elastic |
| G-1203-1095 | Jamnut, 1/2-20 Elastic |
| G-1250-1050N | Flatwasher, ¼ Narrow |
| G-1250-1060N | Flatwasher, 5/16 Narrow |
| G-1251-1070R | Lockwasher, 3/8 Regular |
| G-1300-25200 | Pin, Roll, 1/4" diameter x 2" long |
| G-1318-1033 | Pin, Model "D" 5/8" diameter x 3.3" long |
| H-1009-01 | Assembly, Handle |
| H-1045 | Breather |
| H-1173 | Valve, Plug |
| H-1174 | Pump, Air |
| H-1516-08 | Clamp, 2 Ear |
| H-1536-19 | Caplug, Tapered |
| H-2331 | Stopnut |
| H-2461 | Blowgun |
| HC-2000-336 | O-ring |
| HC-2020-336 | Ring, Backup |
| HC-2329 | Reservoir, Translucent |
| HC-2764 | Pump, Hand |
| HJ-225-03 | Shaft, Extension |
| HJ-553 | Ring, Ram Protection |
| HJ-554 | Ring, Guide |
| HJ-557 | Pad, Jack |
| HJ-586-02 | Assembly, Ram |
| J-3415-01 | Bracket, Air Pump |
| K-1050 | Kit, Ram Seal Replacement |
| K-1061-02 | Kit, Reservoir Replacement |
| K-1685 | Kit, Repair Fluid Seal |
| K-1686 | Kit, Repair Air Seal |
| 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-2250-03 | Adapter, Expanding Pipe |
| N-2410-05 | Elbow, 90° Male |
| 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, 18" long |
| TF-1047-01*09.0 | Hose, ¼ Gray x 9” long |
| TF-1047-01*10.0 | Hose, ¼ " Push-on x 10" long |
| TR-1505 | Stop, Jack |
| TR-1756 | Plate, Mounting |
| 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 |
Customers also viewed
Customers who bought this item also purchased
AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Airbus Military (CASA) | C-295 , CN-235/HC-144A |
| BAe | Jetstream 41 |
| Bombardier |
Challenger 300
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).
,
Challenger 350
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).
,
Challenger 600
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).
,
Challenger 601
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).
,
Challenger 604
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).
,
Challenger 605 (CL605)
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).
,
Challenger 650
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).
,
Challenger 850
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).
,
,
|
| Dassault |
Falcon 20-200
NOTE
Main/nose landing gear jack: 1 nose jack and 2 main jacks required per aircraft. Control all 3 jacks with air pumps with the Manifold Kit (K-1106).
,
Falcon 50
NOTE
This jack is used on the nose landing gear. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
Falcon 50EX
NOTE
Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
|
| Lockheed | Jetstar C-140 |
PRODUCT REVIEWS
QUESTIONS & ANSWERS
The 20,000-lb lifting capacity allows the Tronair 02A1036C0111 tripod jack to safely support larger aircraft commonly used in corporate, regional, and military operations. This higher capacity makes it suitable for aircraft such as the Bombardier Challenger series, Dassault Falcon models, and Airbus Military C-295 platforms. Maintenance teams can perform inspections, tire changes, brake servicing, and structural work with confidence when using properly rated aircraft jacks. The manual also specifies a maximum lifting height of 70.25”, providing additional versatility for larger airframes.
The built-in velocity fuse helps prevent sudden ram descent in the event of a hydraulic line failure. According to the Tronair manual, the fuse automatically locks the ram in its current position until the hydraulic issue is repaired and the system is reset. This safety feature helps protect technicians, aircraft structures, and nearby equipment during maintenance operations. Additional safeguards like this are especially important when working with heavier business jets and military aircraft.
Tronair specifically instructs operators to raise and lower all aircraft jacks simultaneously to keep the aircraft level throughout maintenance procedures. Proper synchronized lifting helps reduce uneven structural loading and minimizes unnecessary stress on the airframe. This is particularly important for multi-point lifting procedures on larger aircraft such as the Challenger 604 or Falcon 50EX. Maintaining aircraft balance also improves overall ground safety during inspections and repairs.
The 14” mechanical extension allows technicians to position the jack close to the aircraft jacking point before hydraulic lifting begins. This helps reduce the amount of hydraulic travel required and can speed up setup time in busy maintenance environments. The manual also emphasizes proper placement of the locking pin within the ram protection ring to ensure safe operation. Proper extension positioning contributes to smoother lifting and better overall jack stability.
The translucent hydraulic reservoir makes it easier for technicians to visually monitor fluid levels during inspections and servicing. Quick fluid verification can help reduce downtime and support consistent hydraulic performance. Tronair recommends maintaining the hydraulic fluid approximately 1.5” below the vent opening using MIL-PRF-5606 fluid. Easier monitoring helps maintenance crews identify low-fluid conditions before they affect jack performance.
The factory-installed pneumatic pump enables rapid initial lifting with compressed shop air, reducing manual pumping effort during aircraft maintenance. This can improve technician efficiency when repeatedly lifting large aircraft throughout the workday. The hydraulic schematic included in the manual shows how the air-driven hydraulic pump works together with the manual hand pump for added flexibility. Manual pumping capability remains available when compressed air is not accessible.
Annual load testing helps verify that the jack can safely support its rated lifting capacity after extended operational use. Tronair recommends testing the jack at 105% to 110% of its rated capacity as part of its preventive maintenance schedule. Regular testing can help identify worn seals, hydraulic leaks, or structural issues before they become safety concerns. This proactive approach supports safer aircraft maintenance operations and long-term equipment reliability.
The tripod design distributes weight evenly across the base to help maintain stability during aircraft lifting procedures. A wide support stance can reduce unwanted movement while supporting heavy aircraft loads on approved level surfaces. Tronair also recommends using a tail stand or a nose stand when applicable to improve aircraft stability. Combined with heavy-duty wheels, the design balances maneuverability with dependable lifting support.
The ram protection ring helps properly secure the locking pin during mechanical extension setup. The Tronair manual includes multiple diagrams showing correct and incorrect locking pin placement to prevent deformation or unsafe loading conditions. Improper installation could damage the ring or compromise the jack’s structural integrity during lifting operations. This feature adds another layer of protection for technicians working around elevated aircraft.
CE marking confirms that the jack complies with applicable European machinery safety requirements and operational standards. The Declaration of Conformity references compliance with the Machinery Directive 2006/42/EC and EN ISO 12100-1 standards. For international MRO facilities and aviation operators, CE compliance can help support regulatory acceptance and workplace safety initiatives. This makes the Tronair 02A1036C0111 well-suited for global aviation maintenance environments.



