Tronair 02A7844C0111 – 30-Ton Tripod Jack, Air Pump
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The Tronair 02A7844C0111 is a 30-Ton (60,000 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 Global Express, Global 5000, Global 6000 and others. Also approved for Gulfstream G350, G450 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: 60,000 lbs (27216 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 02A7844C0111 is OEM-approved for the following aircraft types:
- Bombardier: Global Express, Global 5000, Global 6000, Global Express XRS, Global 5500 and 1 more
- Gulfstream: G350, G450, G500, G550, II and 6 more
- Boeing: 707, 717, 727-100, 727-200, DC-9 Series 33 and 3 more
- McDonnell Douglas: DC-9 Series 40, DC-9 Series 50, MD-80
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 02A7844C0111 30-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 02-7844C0111
| Alternate Models | |
|---|---|
| 02-7844-0111 | Previous Model Number - Without Air Pump |
| 02-7844C0100 | Without Air Pump Installed (CE) |
| 02A7844-0110 | Previous Model without CE Rating for European Countries |
| 02A7844-0111 | Previous Model Number |
| General Information | |
|---|---|
| Part # | 02A7844C0111 |
| Manufacturer | Tronair |
| NSN | 1730017084925 |
| Manual 1 | View Tronair 02A7844C0111 Parts, Service, and Operating Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 655 lbs. |
| Shipping Dimensions | 58 x 64 x 55 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| H-2326 | 30-Ton Stop Nut |
| H-2395 | Protective Jack Cover |
| HJ-557 | Jack Pad |
| K-1001 | Hand Pump Seal Kit |
| K-1043-28-02 | Air Pump Kit (P) |
| K-1051 | Ram Seal Kit |
| K-1106 | Manifold Assembly Kit |
| K-1685 | Repair Fluid Seal Kit |
| K-1686 | Repair Air Seal Kit |
| K-2920 | Replacement Caster Kit |
| K-3329 | Replacement Jack Weldment Kit (P) |
| R-1150 | Screw Extension |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Boeing | 707 , 717 , 727-100 , 727-200 , DC-9 Series 33 , DC-9 Series 40 , DC-9 Series 50 , MD-80 |
| Bombardier |
Global 5000
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).
,
Global 5500
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).
,
Global 6000
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).
,
Global 6500
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).
,
Global Express
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).
,
Global Express XRS
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).
|
| Gulfstream |
G350
NOTE
Main landing gear jack: Two jacks per aircraft required. Control all 3 tripod jacks with air pumps with the Manifold Kit (K-1106).
,
G450
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
G500
NOTE
Main landing gear jack: Two jacks required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
G550
NOTE
Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
G600
NOTE
Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
II
NOTE
Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
III
NOTE
Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
IV
NOTE
Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
IVSP
NOTE
Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
,
|
| McDonnell Douglas | DC-9 Series 40 , DC-9 Series 50 , MD-80 |
PRODUCT REVIEWS
QUESTIONS & ANSWERS
The Tronair 02A7844C0111 jack includes multiple safety mechanisms designed to protect both operators and aircraft. Key features include ram locknuts, which must be engaged as the aircraft is lifted, and a velocity fuse, which prevents the ram from lowering in the event of a hydraulic line failure. Additionally, the jack is equipped with a pressure relief valve to avoid overloading during operation. These built-in safeguards ensure that lifting operations are stable and controlled at all times.
This aircraft hydraulic tripod jack is designed to function reliably in a range of environments. According to the manual, it can safely operate between -20°C and 50°C (-4°F to 122°F). However, the unit should always be placed on a dry, level surface to maintain stability. Proper storage with the ram fully lowered also ensures long-term performance even in outdoor conditions.
Tronair recommends a 90-day routine inspection and an annual load test as part of preventative maintenance. Each inspection should include checking hydraulic fluid levels, inspecting hoses, fittings, and ram seals, and lubricating casters. An annual capacity test at 105–110% of rated load ensures the jack maintains performance standards. This schedule helps keep the jack compliant with aviation maintenance practices and extends its service life.
The Tronair 02A7844C0111 jack is designed to use MIL-PRF-5606 hydraulic fluid. This aviation-grade hydraulic oil provides excellent lubricating properties while preventing corrosion and seal degradation. Operators should always follow the manufacturer’s Safety Data Sheet (SDS) for handling, storage, and disposal of hydraulic fluid to ensure environmental and personnel safety.
Yes, the tripod jack is fitted with casters that allow it to be rolled by hand or towed. However, towing should never exceed 5 mph (8 km/h), as going faster may cause damage to the jack or create safety risks for personnel. The casters are designed to carry only the jack’s weight and will compress under load when an aircraft is raised.
Only trained and skilled aircraft technicians should operate this jack. Operators should be familiar with both the jack’s manual and the aircraft manufacturer’s jacking procedures. Additional training is required for installation, servicing, or dismantling, particularly since these processes involve hydraulic system knowledge. Proper operator qualifications are crucial for safety during heavy-lift operations.
For longer moves or shipping, the Tronair 30-ton tripod jack can be lifted by crane using straps through the top of the tripod, or by forklift under the lower tripod support. The manual states the approximate transport weight is around 500 lbs (227 kg), depending on the specific model. Proper strapping and labeling are required to prevent damage during shipment.
If a hydraulic line failure occurs, the velocity fuse in the jack automatically prevents the ram from lowering. Once the line is repaired, the operator can reset the fuse by pumping the hand pump until the ram rises slightly. This built-in redundancy ensures that the aircraft remains stable during an unexpected hydraulic issue.
Before each operation, operators should check the hydraulic fluid level (within 1.5" of the reservoir vent), inspect for leaks, and verify that all bolts and fittings are tight. The velocity fuse must also be checked for proper attachment and function. These pre-use checks help identify issues early and prevent unsafe lifting operations.
When not in use, the jack should be stored with the ram fully lowered and, if outdoors, protected with a waterproof tarp or cover. Storage temperatures should remain within -4°F to 122°F (-20°C to 50°C). If the jack is unused for more than 90 days, the ram should be extended fully and sprayed with a water-repellent lubricant to prevent corrosion.


