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The Tronair 02-7815C0110 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. With a 28" (71.1 cm) closed height and 72" (182.9 cm) maximum extended height, it accommodates a range of aircraft fuselage and wing jacking point heights. The two-stage hydraulic design provides controlled lift and positive lock at any extension height. CE-marked for compliance with European aviation safety standards. OEM-specified for Cessna Citation 560 XL, Citation 560 XLS, Citation Sovereign 680 and others.
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: 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)
- Minimum Closed Height: 28" (71.1 cm)
- Maximum Height Obtainable: 72" (182.9 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.
- 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 02-7815C0110 is OEM-approved for the following aircraft types:
- Cessna: Citation 560 XL, Citation 560 XLS, Citation Sovereign 680, Latitude 680A, Citation Longitude 700 and 1 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 02-7815C0110 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
- With factory-installed air pump: Tronair 02A7815C0110
| Alternate Models | |
|---|---|
| 02-7815-0100 | Previous Jack Model Number (Non-CE Compliant) |
| 02-7815-0110 | Previous Model Number |
| 02A7815-0110 | Previous Model Number - With Air Pump |
| 02A7815C0110 | With Air Pump (CE) |
| General Information | |
|---|---|
| Part # | 02-7815C0110 |
| Manufacturer | Tronair |
| Manual 1 | View Tronair 02-7815C0110 Parts, Service, and Operation Manual |
| Shipping Information | |
|---|---|
| Shipping Weight | 405 lbs. |
| Shipping Dimensions | 40 x 48 x 36 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| G-1100-107010 | BOLT, HEX HEAD, GRADE 5, 3/8-16 X 1" LONG |
| G-1100-107510 | BOLT, 3/8-24 X 1 LONG HEX HD GR 5 |
| G-1100-107532 | BOLT, HEX HEAD, GRADE 5, 3/8 - 24 X 3¼" LONG |
| G-1100-107540 | BOLT, 3/8-24 X 4.0" HEX HD GR 5 |
| G-1100-109532 | BOLT, 1/2-20 X 3-1/4" HEX HD GR 5 |
| G-1100-109560 | BOLT, HEX HEAD, GRADE 5, ½ - 20 X 6" LONG |
| G-1154-107214 | SCREW, 3/8-16 X 1-1/2" LG. SOCKET BUTT HD CAP |
| G-1202-1075 | STOPNUT, 3/8-24 ELASTIC |
| G-1203-1075 | JAMNUT, 3/8-24 ELASTIC |
| G-1203-1095 | JAMNUT, 1/2-20 ELASTIC |
| G-1250-1070N | FLATWASHER, 3/8 NARROW |
| G-1251-1070R | LOCKWASHER, 3/8 REGULAR |
| G-1300-25200 | PIN, ROLL, ¼" DIAMETER X 2" LONG |
| G-1318-1033 | PIN, 5/8 X 3.3 LG MODEL D |
| H-1009-01 | ASSEMBLY, PUMP HANDLE |
| H-1045 | BREATHER |
| H-1516-11 | CLAMP, 2-EAR HOSE |
| H-2210-08 | SPRING, COMPRESSION |
| H-3398-07 | SPRING, COMPRESSION |
| H-557 | PAD, JACK |
| HC-2764 | HAND PUMP, HYDRAULIC |
| N-2001-08-S-B | ELBOW, 90° MALE, SAE #6 X 3/8" O.D. - JIC 37° |
| N-2066-06-S-B | PLUG, HOLLOW HEX W/ O-RING |
| N-2412-10 | CONNECTOR, STRAIGHT MALE |
| N-2453-04 | TEE, NYLON UNION |
| N-2789-04-S-B | CONNECTOR, MALE, BEADED HOSE |
| R-1341-02 | SHAFT, EXTENSION |
| TF-1043-06-18.0 | HOSE, 3/8 GREY |
| TF-1043-06*18.0 | ASSEMBLY, HOSE, 18" LONG |
| TF-1047-04-08.0 | HOSE, 3/8 GREY |
| TR-1978 | TUBE, STOP |
| TR-1994 | RING, RAM PROTECTION |
| TR378-03*001.00 | TUBE, SS ½ ID |
| V-1001 | LABEL, MADE IN USA |
| V-1015 | LABEL, JACKING INSTRUCTION |
| V-1019 | LABEL, MAX CAPACITY - 20K |
| V-1102 | LABEL, MIL-PRF-5606 |
| V-1198 | LABEL, TRONAIR |
| V-1354 | TAG, RESERVOIR FILL |
| V-1500 | TAG, CLOSED HEIGHT |
| V-1775 | LABEL, PUMP FORCE |
| V-1776 | LABEL, DOWN |
| V-1805 | LABEL, ISO GENERAL DANGER |
| V-2839 | LABEL, JACK TYPE/SERIAL |
| V-2840 | LABEL, JACK MODEL |
| Z-1060-02 | ASSEMBLY, RAM |
| Z-10952-Z1 | ASSEMBLY, 10 TON TRIPOD JACK |
| Z-2301-02 | WELDMENT, HANDLE |
| Z-2302 | WELDMENT, PIVOT |
| Z-2322 | ASSEMBLY, REAR WHEEL |
| Z-4249-01 | WELDMENT, RESERVOIR |
| Z-4973 | ASSEMBLY, BLOWGUN |
| Z-5153 | ASSEMBLY, AIR PUMP |
| Z-6587 | ASSEMBLY, FRONT WHEEL |
| Z-6588 | WELDMENT, PIVOT |
| Z-7059-02-01 | WELDMENT, TUBE/BASE (P) |
| Z-7062-00 | WELDMENT, JACK |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Cessna |
Ascend
NOTE
Two main landing gear jacks and two jack pad adapter kits (R-1798) per aircraft are required.
,
Citation 560 XL
NOTE
Two main landing gear jacks and two jack pad adapter kits (R-1798) per aircraft required.
,
Citation 560 XLS
NOTE
Two main landing gear jacks and two jack pad adapter kits (R-1798) per aircraft are required.
,
Citation Longitude 700
NOTE
This jack is used on the main landing gear. Two jacks and two adapter pads (R-3053) per aircraft are required.
,
Citation Sovereign 680
NOTE
Main landing gear jack – two jacks and two jack pads (R-1807) per aircraft are required.
,
Latitude 680A
NOTE
This jack is used on the main landing gear. Two jacks and two adapter pads (R-1807) per aircraft are required.
|
PRODUCT REVIEWS
QUESTIONS & ANSWERS
This 10-ton aircraft hydraulic tripod jack is commonly used for scheduled inspections, landing gear servicing, component replacements, and structural checks that require support for the fuselage or wings. It is designed for controlled lifting during line and hangar maintenance. The jack is intended to be used in conjunction with additional jacks to maintain proper aircraft balance. This makes it well-suited for coordinated multi-point jacking procedures.
A two-stage aircraft hydraulic jack utilizes multiple ram diameters to achieve a greater lifting height while maintaining stability. This design enables the jack to accommodate a wide range of aircraft geometries without compromising load control. The staged extension ensures smooth, predictable lifting during aircraft maintenance. It also helps reduce the overall footprint compared to taller single-stage designs.
Technicians should always use the jack on a level, hard surface and ensure proper alignment with the aircraft jack point. Ram locknuts must be engaged once the load is raised to prevent unintended movement. All jacks supporting an aircraft should be raised and lowered simultaneously to maintain balance. Proper personal protective equipment is also recommended during operation.
Ram locknuts serve as a mechanical safety device, supporting the load independently of hydraulic pressure. Once engaged, they reduce the risk of jack collapse due to pressure loss. Using the locknuts is a required safety step during aircraft lifting. Failure to engage them can result in serious injury or damage to the aircraft.
The locking pin must pass fully through the mechanical extension and seat in the groove of the ram protection ring, with the washer and ball lock positioned outside the ring. Incorrect placement – such as inserting the washer inside the groove – can deform or shear the pin, leading to structural failure.
Routine visual inspections should be performed before each use to check for leaks, damage, or worn components. Tronair recommends periodic maintenance inspections – typically on a 90-day cycle – to inspect seals, condition the hydraulic system, and exercise the ram to prevent corrosion or seal degradation.
An annual functional load test is also recommended, typically conducted at 105% to 110% of the jack’s rated capacity, to verify safe load-holding performance. Even jacks used infrequently should be exercised and inspected regularly to maintain reliability, extend service life, and support compliance with maintenance best practices.
The jack is designed to use aviation-approved hydraulic fluid that meets MIL-PRF-5606 specifications. Maintaining proper fluid type and level is essential for reliable operation. Contaminated or incorrect fluid can damage seals and reduce lifting performance. Fluid levels should be checked with the ram fully retracted.
The jack should be operated in a clean, dry environment on a stable surface. Extreme temperatures, moisture, or debris can affect performance and component longevity. Protecting the jack during washing or cleaning operations is recommended. Controlled conditions help preserve seals and hydraulic components.
This aircraft hydraulic tripod jack is designed for use as part of a coordinated jacking system. A proper balance is achieved by positioning multiple jacks according to the Aircraft Maintenance Manual (AMM). The jack’s wide stance and controlled extension help maintain stability. Balanced lifting is essential for safe aircraft maintenance.
No. Modifications without written approval from Tronair are not permitted and will void the warranty. Only Tronair OEM replacement parts should be used during repairs. Using non-approved components can compromise safety and load capacity. OEM parts ensure the jack continues to meet its original design standards.
By providing controlled and stable lifting, the jack enables technicians to perform maintenance tasks safely on the ground. Integrated mechanical and hydraulic safeguards reduce reliance on pressure alone. Properly used aircraft jacks help prevent structural stress and accidental movement. This makes them a critical component of safe aircraft ground support operations.
For optimal longevity, the jack should be stored indoors or covered to protect it from exposure to moisture, Skydrol, or cleaning chemicals. Contaminants or liquids on the ram and cylinder can damage seals and O-rings over time. Always ensure the ram is fully retracted and the locknuts are lowered before storage.
Yes! PJi offers a wide range of replacement parts for Tronair GSE, including the 02-7815C0100 tripod jack. Using OEM parts helps maintain safety certifications and proper jack performance.
Tronair offers a one-year limited warranty on all new ground support equipment (GSE) – including the 02-7815C0110 jack – covering defects in materials and workmanship. Replacement parts carry a standard 90-day warranty.
When the cost to repair a jack approaches or equals the cost of a new unit, replacement is the more economical choice. A heavily worn tripod jack requiring structural repairs, new seals, new fittings, paint, and load testing can approach the price of a new jack. Get a detailed repair quote before committing from our Pilot John International GSE service team.

