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The Tronair 02-7838C0110 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 27" (68.6 cm) closed height and 50" (127.0 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 Hawker Beechcraft T-6A Texan II. Also approved for Pilatus PC-9.
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)
- Pressure Relief Setting: 2,500 + 250/−0 PSIG (172.4 + 17.2/−0 bar)
- Minimum Closed Height: 27" (68.6 cm)
- Maximum Height Obtainable: 50" (127.0 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.
- 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 02-7838C0110 is OEM-approved for the following aircraft types:
- Hawker Beechcraft: T-6A Texan II
- Pilatus: PC-9
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 02-7838C0110 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 | |
|---|---|
| 02-7838-0110 | Previous Model Number |
| 02A7838C0110 | Air Pump Installed (CE) |
| General Information | |
|---|---|
| Part # | 02-7838C0110 |
| Manufacturer | Tronair |
| Manual 1 | View Tronair 02-7838C0110 Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 155 lbs. |
| Shipping Dimensions | 27 x 25 x 27 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| 50866 | Haskel Seal Lubricant |
| G-1100-105006 | Bolt, HH Grade 5, ¼-20 x ¾ Lg |
| G-1100-105510 | Bolt, Hex Head Grade 5, ¼-28 x 1" long |
| G-1100-106512 | Bolt, Hex Head Grade 5, 5/16-24 x 1¼" long |
| G-1100-107010 | Bolt, Hex Head Grade 5, 3/8-16 x 1" long |
| G-1151-107206 | Screw, Socket Head Cap, 3/8-16 x ¾" long |
| G-1202-1055 | Stopnut, ¼-28 Elastic |
| G-1202-1065 | Stopnut, 5/16-24 Elastic |
| G-1203-1105 | Jamnut, 5/8-18 Elastic |
| G-1250-1050N | Flatwasher, ¼ Narrow |
| G-1250-1060N | Flatwasher, 5/16 Narrow |
| G-1250-1100N | Flatwasher, 5/8 Narrow |
| G-1250-1100W | Flatwasher, 5/8 Wide |
| G-1251-1070R | Lockwasher, 3/8 Regular |
| G-1300-25200 | Pin, ¼ dia x 2" long, Roll |
| G-1318-1033 | Pin, 5/8 dia x 3.3" long, Model D |
| 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-1685 | Haskel Repair Fluid Seal Kit |
| K-1686 | Haskel Repair Air Seal Kit |
| K-3333 | Assembly, Blowgun |
| N-2001-08-S-B | Elbow, Straight Thread SAE #6 x 3/8-37° JIC |
| N-2004-15-S | Elbow, 3/8 JIC x 3/8 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, ¼ Hose x SAE #4 |
| N-2740-04-S-B | Tee, Male Branch, ⅜ NPT |
| N-2788-02-S-B | Elbow, 90° Male ¼ Hose x #6 SAE Port |
| N-2789-03-S-B | Connector, Straight Male, ⅜ NPT, ⅜ Hose |
| TF-1043-03*16.0 | Assembly, Hose |
| TF-1043-06*18.0 | Assembly, Hose, 18" long |
| TF-1047-01*05.5 | Hose, ¼ Gray x 5½" long |
| TF-1047-01*10.0 | Hose, ¼ Push-On x 10" Long |
| TR-1505 | Stop, Jack |
| TR-1756 | Plate, Mounting |
| TR-7835 | Assembly, Pump Handle |
| 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-1779 | Label, Serial Number |
| V-1805 | Label, ISO General Danger |
| V-1819 | Label, Hydraulic Jack Caution |
| V-2105 | Label, Hydraulic Jack Instructions |
| Z-5118-01 | Weldment, Jack |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Hawker Beechcraft |
T-6A Texan II
NOTE
This jack is used on the aircraft's main and nose landing gear. Two main jacks and one nose jack are required per aircraft.
|
| Pilatus |
PC-9
NOTE
This jack is used on the main and nose landing gear. Two main jacks and one nose jack are required per aircraft.
|
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QUESTIONS & ANSWERS
Proper placement of the locking pin is essential to safely secure the mechanical extension during lifting. The operation manual emphasizes that the locking pin must be positioned through the ram protection ring groove, with the washer and ball lock correctly located outside the ring. Incorrect placement can lead to component deformation or premature failure under load. Following proper pin placement procedures ensures safe and reliable aircraft lifting.
The ram protection ring helps maintain the mechanical extension's structural integrity during lifting. It ensures the locking pin is properly supported and prevents damage from improper load distribution. Incorrect positioning can result in deformation and unsafe conditions. This feature plays a critical role in maintaining safe operation under load.
When multiple tripod jacks are used, they must be raised and lowered together to keep the aircraft level. Uneven lifting can create structural stress and increase the risk of instability. The manual specifically instructs operators to always raise and lower jacks simultaneously for safe operation. This practice helps ensure balanced and controlled aircraft maintenance.
The built-in pressure relief system helps prevent the jack from being overloaded during lifting operations. Limiting hydraulic pressure reduces the risk of component failure or sudden load release. The manual lists a preset pressure relief value to maintain safe operating limits. This feature is essential for protecting both the equipment and the aircraft.
Before use, technicians should inspect the jack for proper fluid levels, secure fittings, and any visible damage. The manual recommends verifying that the hydraulic fluid is at the correct level and checking for leaks or loose components. It also advises ensuring that all parts are present and properly installed. Performing these checks helps prevent operational issues and enhances safety.
Maintaining the correct level of MIL-PRF-5606 hydraulic fluid ensures smooth and consistent jack operation. Low or contaminated fluid can cause erratic movement or reduced lifting capability. The manual specifies checking fluid levels with the ram fully retracted to ensure accuracy. Proper fluid maintenance supports reliable performance and extends equipment life.
The jack is intended for use by trained aircraft maintenance technicians familiar with proper jacking procedures. The manual states that operators must understand both the equipment and the aircraft-specific lifting requirements. Proper training helps reduce the risk of misuse and ensures safe, efficient operation. It is a critical component of overall aviation safety.
The jack should be used on a clean, dry, and level surface to ensure stability during lifting. The manual also specifies an operating temperature range of -4°F to 122°F for optimal performance. Operating within these conditions helps maintain consistent hydraulic function. It also reduces the risk of equipment damage or instability.
For proper storage, the jack should be kept with the ram fully retracted and stored in a clean, dry environment. The manual notes that it can be stored outdoors, provided it is covered with a waterproof tarp to protect against moisture and debris. Maintaining appropriate storage conditions helps prevent corrosion and extends service life. Proper storage also ensures the jack is ready for use when needed.




