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Tronair 02A1036C0111 – 10-Ton Tripod Jack, Air Pump

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Ships around August 17
Do you want an air pump installed on the jack?:
CofC and 8130 available at no cost
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The Tronair 02A1036C0111 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. 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 Challenger 300, Challenger 600, Challenger 601 and others. Also approved for Dassault Falcon 20-200, Falcon 50 and others.

Standard Features

Technical Specifications

Safety Features

Aircraft Applications

The 02A1036C0111 is OEM-approved for the following aircraft types:

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 02A1036C0111 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

General Information
Part #02A1036C0111
ManufacturerTronair
NSN1730015521011
Manual 1View Tronair 02A1036C0111 Manual
Shipping Information
Shipping Weight270 lbs.
Shipping Dimensions38 x 38 x 43 in.
Freight NMFC186600
Schedule B8425420000
ECCNEAR99
Spare Parts
28442Lubricant, Haskel Seal
G-1100-105006Bolt, Hex Head, Grade 5, ¼ - 20 x ¾ LG
G-1100-105510Bolt, Hex Head, Grade 5, 1/4-28 x 1 long
G-1100-106512Bolt, Hex Head, Grade 5, 5/16-24 x 1-1/4 " long
G-1100-107010Bolt, Hex Head, Grade 5, 3/8-16 x 1" long
G-1100-109526Bolt, Hex Head, Grade 5, 1/2-20 x 2-3/4" long
G-1151-107206Screw, Socket Head Cap, 3/8-16 x 3/4" long
G-1202-1050Stopnut, 1/4-20 Elastic
G-1202-1055Stopnut, 1/4-28 Elastic
G-1202-1065Stopnut, 5/16-24 Elastic
G-1203-1095Jamnut, 1/2-20 Elastic
G-1250-1050NFlatwasher, ¼ Narrow
G-1250-1060NFlatwasher, 5/16 Narrow
G-1251-1070RLockwasher, 3/8 Regular
G-1300-25200Pin, Roll, 1/4" diameter x 2" long
G-1318-1033Pin, Model "D" 5/8" diameter x 3.3" long
H-1009-01Assembly, Handle
H-1045Breather
H-1173Valve, Plug
H-1174Pump, Air
H-1516-08Clamp, 2 Ear
H-1536-19Caplug, Tapered
H-2331Stopnut
H-2461Blowgun
HC-2000-336O-ring
HC-2020-336Ring, Backup
HC-2329Reservoir, Translucent
HC-2764Pump, Hand
HJ-225-03Shaft, Extension
HJ-553Ring, Ram Protection
HJ-554Ring, Guide
HJ-557Pad, Jack
HJ-586-02Assembly, Ram
J-3415-01Bracket, Air Pump
K-1050Kit, Ram Seal Replacement
K-1061-02Kit, Reservoir Replacement
K-1685Kit, Repair Fluid Seal
K-1686Kit, Repair Air Seal
K-4585Kit, Jack Weldment
N-2001-08-S-BElbow, Straight Thread, SAE #6 x 3/8-37° JIC
N-2004-15-SElbow, Extra Long
N-2250-03Adapter, Expanding Pipe
N-2410-05Elbow, 90° Male
N-2653-01-S-BElbow, 90° Male ¼ Hose x SAE #4
N-2740-04-S-BTee, Male Branch, SAE #4
N-2788-02-S-BElbow, 90° Male, SAE #6 x ¼ Hose
TF-1043-06*18.0Assembly, Hose, 18" long
TF-1047-01*09.0Hose, ¼ Gray x 9” long
TF-1047-01*10.0Hose, ¼ " Push-on x 10" long
TR-1505Stop, Jack
TR-1756Plate, Mounting
U-1002Wheel
V-1019Label, Capacity 10,000 lbs
V-1102-01Label, Use MIL-PRF-5606
V-1819Label, Hydraulic Jack Caution
V-1820Label, Hydraulic Jack Instruction

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for Select Bombardier & Dassault Aircraft

AIRCRAFT COMPATIBILITY

Compatible Aircraft*
Airbus Military (CASA) C-295 , CN-235/HC-144A
BAe Jetstream 41
Bombardier
Challenger 300 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).
,
Challenger 350 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).
,
Challenger 600 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).
,
Challenger 601 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).
,
Challenger 604 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).
,
Challenger 605 (CL605) 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).
,
Challenger 650 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).
,
Challenger 850 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).
,
CRJ100 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).
,
CRJ200 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).
Dassault
Falcon 20-200 NOTE Main/nose landing gear jack: 1 nose jack and 2 main jacks required per aircraft. Control all 3 jacks with air pumps with the Manifold Kit (K-1106).
,
Falcon 50 NOTE This jack is used on the nose landing gear. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
,
Falcon 50EX NOTE Main landing gear jack: Two jacks are required per aircraft. Control all 3 jacks with air pumps using the Manifold Kit (K-1106).
Lockheed Jetstar C-140
*This list is for general reference only and may not be entirely accurate for all aircraft. Please confirm all equipment meets the requirements of your aircraft with the owners/maintenance manuals prior to purchasing or using with your aircraft.

PRODUCT REVIEWS

5/5
by Francisco Vigil, a Maintenance Facility in Birmingham, Alabama
02/16/2026 02:23:29 PM
We have used Tronair Jacks for years and these are no different. They were delivered expeditiously and well packaged. We will use Tronair in the future.
5/5
by Scott, a Maintenance Facility in Santa Ana, CA 92707
05/12/2016 10:12:19 AM
Thanks again for helping us get these jacks and tail stands in a timely manner. They all came in good shape and work great. Look forward to buying more in the future.

QUESTIONS & ANSWERS

Question:
What advantages does the 20,000-lb lifting capacity provide for business jet and military aircraft maintenance?
Answer:

The 20,000-lb lifting capacity allows the Tronair 02A1036C0111 tripod jack to safely support larger aircraft commonly used in corporate, regional, and military operations. This higher capacity makes it suitable for aircraft such as the Bombardier Challenger series, Dassault Falcon models, and Airbus Military C-295 platforms. Maintenance teams can perform inspections, tire changes, brake servicing, and structural work with confidence when using properly rated aircraft jacks. The manual also specifies a maximum lifting height of 70.25”, providing additional versatility for larger airframes.

Asked May 15, 2026
Question:
How does the velocity fuse improve aircraft jack safety?
Answer:

The built-in velocity fuse helps prevent sudden ram descent in the event of a hydraulic line failure. According to the Tronair manual, the fuse automatically locks the ram in its current position until the hydraulic issue is repaired and the system is reset. This safety feature helps protect technicians, aircraft structures, and nearby equipment during maintenance operations. Additional safeguards like this are especially important when working with heavier business jets and military aircraft.

Asked May 15, 2026
Question:
Why is simultaneous lifting important during aircraft jacking procedures?
Answer:

Tronair specifically instructs operators to raise and lower all aircraft jacks simultaneously to keep the aircraft level throughout maintenance procedures. Proper synchronized lifting helps reduce uneven structural loading and minimizes unnecessary stress on the airframe. This is particularly important for multi-point lifting procedures on larger aircraft such as the Challenger 604 or Falcon 50EX. Maintaining aircraft balance also improves overall ground safety during inspections and repairs.

Asked May 15, 2026
Question:
What benefits does the mechanical extension provide during setup?
Answer:

The 14” mechanical extension allows technicians to position the jack close to the aircraft jacking point before hydraulic lifting begins. This helps reduce the amount of hydraulic travel required and can speed up setup time in busy maintenance environments. The manual also emphasizes proper placement of the locking pin within the ram protection ring to ensure safe operation. Proper extension positioning contributes to smoother lifting and better overall jack stability.

Asked May 15, 2026
Question:
How does the translucent hydraulic reservoir simplify maintenance?
Answer:

The translucent hydraulic reservoir makes it easier for technicians to visually monitor fluid levels during inspections and servicing. Quick fluid verification can help reduce downtime and support consistent hydraulic performance. Tronair recommends maintaining the hydraulic fluid approximately 1.5” below the vent opening using MIL-PRF-5606 fluid. Easier monitoring helps maintenance crews identify low-fluid conditions before they affect jack performance.

Asked May 15, 2026
Question:
What operational advantages does the integrated pneumatic pump provide?
Answer:

The factory-installed pneumatic pump enables rapid initial lifting with compressed shop air, reducing manual pumping effort during aircraft maintenance. This can improve technician efficiency when repeatedly lifting large aircraft throughout the workday. The hydraulic schematic included in the manual shows how the air-driven hydraulic pump works together with the manual hand pump for added flexibility. Manual pumping capability remains available when compressed air is not accessible.

Asked May 15, 2026
Question:
Why is annual load testing important for aircraft tripod jacks?
Answer:

Annual load testing helps verify that the jack can safely support its rated lifting capacity after extended operational use. Tronair recommends testing the jack at 105% to 110% of its rated capacity as part of its preventive maintenance schedule. Regular testing can help identify worn seals, hydraulic leaks, or structural issues before they become safety concerns. This proactive approach supports safer aircraft maintenance operations and long-term equipment reliability.

Asked May 15, 2026
Question:
How does the tripod base design improve jack stability?
Answer:

The tripod design distributes weight evenly across the base to help maintain stability during aircraft lifting procedures. A wide support stance can reduce unwanted movement while supporting heavy aircraft loads on approved level surfaces. Tronair also recommends using a tail stand or a nose stand when applicable to improve aircraft stability. Combined with heavy-duty wheels, the design balances maneuverability with dependable lifting support.

Asked May 15, 2026
Question:
What role does the ram protection ring play in safe jack operation?
Answer:

The ram protection ring helps properly secure the locking pin during mechanical extension setup. The Tronair manual includes multiple diagrams showing correct and incorrect locking pin placement to prevent deformation or unsafe loading conditions. Improper installation could damage the ring or compromise the jack’s structural integrity during lifting operations. This feature adds another layer of protection for technicians working around elevated aircraft.

Asked May 15, 2026
Question:
What benefits does CE compliance provide for international maintenance operations?
Answer:

CE marking confirms that the jack complies with applicable European machinery safety requirements and operational standards. The Declaration of Conformity references compliance with the Machinery Directive 2006/42/EC and EN ISO 12100-1 standards. For international MRO facilities and aviation operators, CE compliance can help support regulatory acceptance and workplace safety initiatives. This makes the Tronair 02A1036C0111 well-suited for global aviation maintenance environments.

Asked May 15, 2026