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The Tronair 02-7866-0100 is a hydraulic aircraft tail stand engineered to support the tail section of an aircraft during maintenance and weight-and-balance operations. CE-marked for compliance with European aviation safety standards. OEM-specified for Hawker Beechcraft Beech Bonanza.
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
- 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)
- 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 02-7866-0100 is OEM-approved for the following aircraft types:
- Hawker Beechcraft: Beech Bonanza
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 02-7866-0100 bonanza tail stand 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.
| General Information | |
|---|---|
| Part # | 02-7866-0100 |
| Manufacturer | Tronair |
| Shipping Information | |
|---|---|
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| H-2395 | COVER, PROTECTIVE JACK |
| K-4170 | KIT, STABILIZER SCREW |
| K-4199 | KIT, RAM O-RING |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Hawker Beechcraft | Beech Bonanza |
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QUESTIONS & ANSWERS
The two-stage tail jack design provides greater vertical reach while maintaining a compact closed height for storage and positioning. This allows technicians to make precise tail-height adjustments during leveling procedures without overextending a single ram. The staged extension also helps distribute the load more effectively, improving stability throughout the lift. As a result, it offers better control when working on aircraft like the Beechcraft Bonanza.
The integrated tail hold-down lug adapter is specifically designed to securely interface with the aircraft’s tail structure. It uses a ball-lock pin system to establish a positive mechanical connection before lifting begins, reducing the risk of slippage. Additionally, the wedge adjustment mechanism removes unwanted vertical play between the jack and the aircraft connection point. This ensures a tighter, more stable setup during maintenance operations.
The wedge adjustment system allows technicians to eliminate looseness between the adapter and the aircraft’s tail lug. By tightening the wedge assembly, vertical movement is minimized, which helps maintain accurate positioning during lifting. This added precision is especially important for leveling procedures and weight distribution tasks. It ultimately improves both safety and efficiency in aircraft maintenance.
The jack features multiple mechanical locking points that secure the rams against both upward and downward movement. The first- and second-stage locknuts work in conjunction with ball lock pins to prevent unintended motion once the load is applied. This layered safety approach ensures that the aircraft remains securely supported even if hydraulic pressure fluctuates. It is a critical feature for maintaining safe working conditions under load.
The tail-leveling jack includes direction control, flow control, and pressure release valves that allow operators to finely control ram movement. These controls enable smooth raising and lowering, and allow the jack to be held in a neutral position without drift. The flow control valve, in particular, regulates the speed of movement for safer adjustments. This level of control is essential for delicate leveling operations.
The jack is designed to operate under both gravity-assisted and powered conditions, depending on load direction. This allows the system to move efficiently, whether the load is assisting or resisting ram movement. For example, gravity-assisted lifting can reduce manual effort during certain stages of operation. This versatility improves workflow efficiency and reduces operator fatigue.
Despite its heavy-duty construction, the jack is equipped with swivel casters that allow it to be repositioned easily around the aircraft. The manual notes that the jack can be rolled into place and aligned parallel to the fuselage for proper operation. Floor locks provide stability once the jack is positioned. This combination of mobility and secure placement supports efficient hangar operations.
When used as part of a multi-jack setup, the tail-leveling jack must be raised and lowered simultaneously with other jacks. This coordinated movement ensures the aircraft remains level and prevents structural stress. The manual emphasizes synchronized operation as a key safety requirement. Following this practice helps protect both the aircraft and maintenance personnel.
Routine maintenance includes checking hydraulic fluid levels before use, inspecting for leaks, and performing periodic load testing. Tronair recommends lubricating casters every three months and conducting annual capacity tests. Keeping the system clean and replacing worn seals also helps prevent hydraulic issues. These practices ensure consistent performance and extend the life of the aircraft tail jack.




