Tronair 02A7856C0100 – 5-Ton Tripod Jack, Air Pump
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The Tronair 02A7856C0100 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. A factory-installed air pump allows rapid initial extension without additional equipment. CE-marked for compliance with European aviation safety standards. OEM-specified for Cessna Caravan 208, Caravan 208B, Caravan 406 and others. Also approved for Bombardier Challenger 300, Challenger 350.
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: 10,000 lbs (4536 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 02A7856C0100 is OEM-approved for the following aircraft types:
- Cessna: Caravan 208, Caravan 208B, Caravan 406, Citation 560 XL
- Bombardier: Challenger 300, Challenger 350
- Dassault: Falcon 10-100
- Embraer: EMB-110
- Bell: 206B3, 206L4, 206LT, 427, CH-139 and 4 more
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 02A7856C0100 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.
Also Available
- Without air pump (hand pump only): Tronair 02-7856C0100
| General Information | |
|---|---|
| Part # | 02A7856C0100 |
| Manufacturer | Tronair |
| Manual 1 | View Tronair 02A7856C0100 Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 200 lbs. |
| Shipping Dimensions | 35 x 35 x 43 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| 50866 | Haskel Seal Lubricant |
| G1100-105006- | Bolt, HH Grade 5, 1/4-20x3/4 Lg |
| G1100-105510- | Bolt, Hex Head, Grade 5, 1/4-28x1" long |
| G1100-106512- | Bolt, Hex Head, Grade 5, 5/16-24x1 1/4" long |
| G1100-107010- | Bolt, Hex Head, Grade 5, 3/8-16x1" long |
| G1151-107206- | Screw, Socket Head Cap, 3/8-16x3/4" long |
| G1202-1055- | Stopnut, 1/4-28 Elastic |
| G1202-1065- | Stopnut, 5/16-24 Elastic |
| G1203-1105- | Jamnut, 5/8-18 Elastic |
| G1250-1050N- | Flatwasher, 1/4 Narrow |
| G1250-1060N- | Flatwasher, 5/16 Narrow |
| G1250-1100N- | Flatwasher, 5/8 Narrow |
| G1250-1100W- | Flatwasher, 5/8 Wide |
| G1251-1070R- | Lockwasher, 3/8 Regular |
| G1300-25200- | Pin, 1/4" diameter x 2" long, Roll |
| G1318-1033- | Pin, 5/8" diameter x 3.3" long, Model D |
| H-1009-01 | Assembly, Pump Handle |
| 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-1050 | Kit, Seal Replacement |
| K-1061-02 | Kit, Reservoir Replacement |
| K-1685 | Haskel Repair Fluid Seal Kit |
| K-1686 | Haskel Repair Air Seal Kit |
| K-3333 | Assembly, Blowgun |
| K-4021 | Kit, Jack Weldment Replacement |
| N-2001-08-S-B | Elbow, Straight Thread, SAE #6 x 3/8-37° JIC |
| N-2004-15-S | Elbow, 3/8 JICx3/8 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, 1/4 Hose x SAE #4 |
| N-2740-04-S-B | Tee, Male Branch, 3/8 NPT |
| N-2788-02-S-B | Elbow, 90° Male 3/8 Hose x #6 SAE Port |
| N-2789-03-S-B | Connector, Straight Male, 3/8 NPT, 3/8 Hose |
| TF-1043-03*16.0 | Assembly, Hose |
| TF-1043-0618.0* | Assembly, Hose, 18" long |
| TF-1047-01*05.5 | Hose, 1/4 "I.D. Gray |
| TF1047-01-*05.5 | Hose, 1/4 "I.D. Gray x 5 1/2" long |
| TF1047-01-*10.0 | Hose, 1/4 " Push-On x 10" Long |
| TR-1505 | Stop, Jack |
| TR-1756 | Plate, Mounting |
| 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-1805 | Label, ISO General Danger |
| V-1819 | Label, Hydraulic Jack Caution |
| V-2105 | Label, Hydraulic Jack Instructions |
| V1779- | Babel, Serial Number |
| Z-5118-01 | Weldment, Jack |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Bell | 206B3 , 206L4 , 206LT , 407 , 407GX , 427 , CH-139 , OH-58 , TH-67 |
| Bombardier |
Challenger 300
NOTE
This jack is used on the aircraft's nose landing gear. Control all 3 jacks with air pumps using the optional Manifold Kit (K-1106).
,
Challenger 350
NOTE
This jack is used on the aircraft's nose landing gear. Control all 3 jacks with air pumps using the optional Manifold Kit (K-1106).
|
| Cessna |
Caravan 208
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required. Use the Air Pump Manifold Kit (K-1106) to control all 3 jacks at once.
,
Caravan 208B
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required. Use the Air Pump Manifold Kit (K-1106) to control all 3 jacks at once.
,
Caravan 406
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required. Use the Air Pump Manifold Kit (K-1106) to control all 3 jacks at once.
,
Citation 560 XL
NOTE
This jack is used on the nose landing gear. The optional Manifold Kit (K-1106) lets you control all 3 jacks at once.
|
| Dassault |
Falcon 10-100
NOTE
Main/nose landing gear jack: 1 nose and 2 main jacks required per aircraft. Control all 3 jacks with air pumps with the Manifold Kit (K-1106).
|
| Embraer | |
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QUESTIONS & ANSWERS
The Tronair 02A7856C0100 5-ton tripod jack is designed to support a broad range of regional, business, and utility aircraft maintenance operations. Its OEM-approved compatibility with aircraft such as the Cessna Caravan, Bombardier Challenger 300/350, and Citation 560 XL makes it a versatile solution for mixed-fleet operators. Maintenance facilities can use the same aircraft tripod jack across multiple platforms, helping streamline equipment management and reduce downtime. This flexibility is especially valuable for FBOs, MRO providers, and regional operators.
The integrated pneumatic air pump allows technicians to raise the jack more quickly during the initial lifting phase compared to manual pumping alone. This helps reduce operator fatigue and improves efficiency during repetitive maintenance tasks such as wheel changes, brake servicing, and landing gear inspections. The system operates with shop air pressures ranging from 25 PSI minimum to 125 PSI maximum, allowing compatibility with many standard maintenance facilities. Faster jack positioning can help improve aircraft turnaround times.
The hold-to-run air valve requires the technician to actively engage the control lever for upward ram movement, adding an extra layer of operational safety. Once the operator releases the valve, upward movement immediately stops, helping maintain controlled lifting conditions. This feature reduces the likelihood of unintended jack extension during aircraft maintenance procedures. Controlled operation is particularly important when working beneath elevated aircraft structures.
The jack is engineered for operation from -4°F to 122°F (-20°C to 50°C), ensuring reliable performance across a wide range of hangar and ramp conditions. Its durable powder-coated finish helps resist corrosion, exposure to hydraulic fluid, and everyday wear commonly found in aviation maintenance facilities. The heavy-duty tripod structure also helps provide stable lifting performance on approved level surfaces. These features contribute to long-term durability in commercial aviation environments.
The threaded ram locknut provides a mechanical load-holding feature that supplements the hydraulic lifting system. Once the aircraft is raised, technicians lower the locknut into position to help secure the load during maintenance operations. This mechanical support helps reduce reliance on hydraulic pressure alone while the aircraft is elevated. Proper use of the ram locknut is emphasized throughout Tronair’s operation and service manual.
Routine inspection and preventative maintenance are essential to the long-term performance of jacks. Tronair recommends checking hydraulic fluid levels before each use, lubricating casters every three months, and performing annual capacity testing at 105% to 110% of rated load capacity. The manual also recommends replacing worn O-rings, backup rings, and seals as needed to prevent hydraulic leakage and maintain lifting performance. Following the manufacturer’s maintenance schedule can help maximize equipment reliability.
The operation manual emphasizes proper installation of the locking pin within the ram protection ring groove to help maintain structural integrity during lifting operations. Incorrect pin placement can damage the ram protection ring or locking components, potentially compromising safe operation. Tronair also specifies that only one locking pin should be used in the designated location and that damaged pins or protection rings should never be reused. These procedures help ensure safe aircraft lifting practices.
The single-stage hydraulic design offers a straightforward lifting system with fewer moving hydraulic components than multi-stage jacks. This simplified design can facilitate servicing, reduce maintenance complexity, and ensure dependable lifting performance in approved aircraft applications. Combined with the mechanical extension, the jack still provides a substantial lifting range while maintaining stability. Single-stage systems are commonly used in aviation ground support equipment because of their durability and reliability.
The jack provides a maximum lifting height of 64", allowing technicians to reach elevated fuselage and wing jacking points on various aircraft types. This extended lifting range supports maintenance procedures involving landing gear servicing, tire replacement, and structural inspections. The combination of mechanical and hydraulic extension helps technicians position the jack accurately before full lifting begins. Proper lifting height capability is critical for safely supporting larger regional and business aircraft.
Even when a tripod jack is OEM-approved for certain aircraft models, technicians must still follow the aircraft manufacturer’s maintenance manual for proper jacking procedures, adapter selection, and load distribution requirements. Aircraft weight distribution, jacking point locations, and stabilization requirements can vary significantly between platforms. Tronair specifically advises operators to use the jack only in approved applications and to follow proper balancing procedures. Following approved aircraft maintenance practices helps protect both technicians and aircraft structures during lifting operations.



