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DJI Agras T100 OEM Load Adaptive Cable / Load Board Connection Cable — a replacement signal and interface harness used to connect compatible load/payload control hardware within the DJI Agras T100 ecosystem. This cable provides the electrical path required for supported payload-board communication and system integration.
Ares Acres LLC is a U.S.-based authorized DJI Agras reseller supporting American agricultural drone operators with genuine DJI Agras OEM replacement parts, accessories, and field-ready inventory.
FREE & FAST Shipping is included for all U.S. customers.
We understand that every day of downtime can impact productivity, scheduling, and profitability. That's why we focus on providing fast fulfillment, responsive customer support, and reliable access to the parts operators need most.
Ares Acres LLC supplies DJI Agras wiring and interface components for commercial operators and repair facilities maintaining advanced payload and control systems.
We use specialized technicians to verify and dispatch the Load Adaptive Cable / Load Board Connection Cable ordered.
Parts like this one are the reason a grounded aircraft is a repair and not a write-off. A single component held in U.S. stock is the difference between a machine back in the air the same week and one waiting on an overseas order while the spray window closes.
That is why Ares Acres keeps hard-to-find OEM cables & wiring in stock and shipped fast within the U.S.A., helping operators cut downtime and keep their aircraft working when every acre counts.
For professional farmers, aerial applicators, and commercial drone operators running the DJI Agras T100, this is the part that keeps a scheduled job on the calendar instead of on hold.
Confirm connector type, cable length, pin arrangement, and destination board before ordering. Similar-looking DJI cables may use different pinouts.
One load adaptive / load-board connection cable in the supplier-listed configuration. Load board, sensors, payload module, aircraft harness, adapters, and mounting hardware are not assumed included.
The load adaptive cable is an electrical interconnect between the aircraft or payload system and a compatible load-control board. It carries the signals required for the connected hardware to communicate and operate as designed. Damage to the cable or connectors can interrupt payload recognition, data transfer, power/signal integrity, or accessory operation.
This is a signal harness rather than a power lead, and where it runs matters more than what it is made of. The load board is the interface between the aircraft and whatever task module is fitted to it, so this cable spans a joint that is designed to be opened: the payload comes off for cleaning, gets swapped between jobs, and gets lifted on and off a trailer. Every one of those events puts a hand on this harness. One end lands on the load board connector, the other on the aircraft-side interface, and in between it is clipped and tied along the frame. That routed middle section, not the copper, usually decides how long the cable lasts.
Because it carries signals instead of load current, its failures are quiet. A damaged power lead gets hot or stops outright. A signal harness with one strained conductor, a pin backed a fraction out of its housing, or moisture wicked under a boot will pass a check with the aircraft sitting still, then drop out under vibration or once the airframe warms in the sun. That is why these get diagnosed last, after two or three other parts have already been changed.
Several harnesses in the same bay look alike at a glance, and the jacket color is not what separates them. Count the ways in the connector shell and compare that count against the cable you removed. Look at how thick the bundle is where it enters the boot, because a power lead into the same board carries fewer and heavier conductors than a signal harness does. Then find the marking on the jacket or the label near the boot and read it, since that is the only identification that survives a rebuild.
A connector that physically mates is not proof of the right cable. The same connector families appear on several harnesses on one airframe, so a wrong part can land, latch, and feel completely correct while the pin assignment behind it belongs to something else entirely. If what you are fitting does not carry the same marking as what came out, do not power the aircraft up to find out. Confirm the callout first. That is a five-minute conversation, and the alternative reaches a board.
The environment this cable lives in is harder on it than the copper deserves. It sits low on the airframe near the payload joint, in the path of drift coming back up off the crop, in the wash-down stream every time the aircraft is cleaned, and in granular dust that behaves like a mild abrasive once it works in between a jacket and a clip. None of that attacks the conductor directly. It attacks the boot, the seal, and the clip, and the conductor fails afterward.
Watch how a payload actually comes off during a working day and you can see where this harness gets hurt. The module is heavy, the joint sits at knee height, and whoever is lifting usually has one hand on the module and one hand somewhere unhelpful. The cable gets used as a handle, gets trapped between the module and the frame as it lands, or gets left hanging while the module is set down on the ground. None of those events leaves a mark on the day it happens.
The conductors in a load interface do not all do the same job, and that shapes how a fault looks to the operator. Some identify the module so the aircraft knows what is attached, some carry bus traffic between the load board and the flight system, and some carry the low-current supply that wakes the board. Lose the identification path and the aircraft may not see the payload at all, which reads as a missing accessory rather than a wiring fault. Lose part of the bus and the module is recognized but reports erratically or drops mid-flight. Lose the supply leg and the board is simply dead while everything around it behaves normally. Matching the symptom to the group of conductors it implicates is the quickest way to decide whether this harness is worth suspecting.
The fastest way to split a fault between the aircraft side and the payload side costs nothing if you have two of anything. Put the suspect module on a second aircraft: if the fault travels with it, stop looking at this harness. Put a second module on the suspect aircraft: if the fault stays behind with the aircraft, then the aircraft side owns it, and this harness plus the load board is the whole of the aircraft side worth suspecting. Two swaps and the problem is halved without touching a meter.
Once the fault is on the aircraft side, localize it before you order anything. Divide the run into three sections with a strip of tape at each boundary, then work one section at a time with the system powered and the fault visible: flex only that section, watch the state, move on. A fault you can provoke inside one taped section and cannot provoke in the others tells you where to look closely, and whether the damage is at a connector or out in the routed middle.
Some of these faults only exist warm. A joint that is marginal at shop temperature can open once the aircraft has sat in the sun on a headland, because every material in that joint expands at a different rate. If an operator reports something that only shows up an hour into the day and never on the bench, believe them, and test the aircraft in the condition the fault lives in rather than the condition that happens to be convenient.
Replace the cable when connectors are cracked, pins are bent or corroded, insulation is cut, the harness has been pinched, communication is intermittent, or continuity testing identifies an open or high-resistance conductor.
Payload faults that come and go with movement: clean on the bench, clean at hover, dropping out in a turn or over rough ground. Intermittency that tracks vibration is a harness signature, not a board signature.
The module is recognized on one power cycle and not the next, particularly after the payload has been off and refitted. Mate cycles are what fatigue a connector, and the mating ends are where these fail first.
Chalky deposits, green corrosion, or a jacket gone stiff near either connector. Spray mix and granular dust both find the joint, and a hardened boot or strain relief holds contaminated moisture against the pins instead of keeping it out.
A jacket that is cut, flattened, or polished shiny where it passes a clip or a frame edge. A pinched harness reads continuous on a meter and still fails, because the damage is in the insulation and the surviving strand count, not the end-to-end path.
The aircraft sees the payload but what it reports back is erratic: a rate that jumps, a level that reads impossibly, a value that freezes and then catches up all at once. That is bus traffic getting through with errors rather than not getting through at all, which is exactly what a partly damaged signal conductor or a contaminated pin produces. A dead module does not generate plausible but wrong numbers. A damaged interface does.
The fault turns up after a wash-down and is gone by the next morning. That is moisture sitting in a connector rather than a broken conductor, and the harness may well still be serviceable. Unmate both ends, dry them with low-pressure air rather than heat, and look hard at the boot and seal that let water in. If it happens after every wash, the joint has stopped sealing and the harness is living on borrowed time even though nothing looks wrong.
The module drops out with a full tank and behaves with an empty one, or drops on the turn at the end of a pass but never down the middle of it. Load and attitude change how the airframe and the payload sit relative to one another, which changes where the harness is pulled. A symptom that keys to weight or to a maneuver is pointing at a run that is short, tight, or caught on something, not at electronics.
A pin backed out of its housing is the most common finding here and the one most often missed, because from the outside the connector looks clean. With the harness unmated, run a light across the face of the shell at a low angle and compare pin depths; the backed-out one sits deeper than its neighbors. Then take each wire behind the housing between finger and thumb and pull gently. The one that moves is the one that has stopped locking.
A connector that mates with noticeably less resistance than it used to, or than its opposite number, has spread contacts inside it. That is what a couple of seasons of daily payload swaps does, and it is progressive rather than sudden. It will still work perfectly on the bench. It stops working somewhere over a field, in a turn, and then works again by the time the aircraft is back on the ground being looked at.
Remove aircraft power before disconnecting or installing payload wiring. Do not pull directly on the cable conductors; release connector locks first. Route the harness along the original path and secure it away from moving joints, sharp edges, high-current wiring, and chemical exposure.
Harness class: Signal and low-current interface cable, not a battery or motor power lead
Runs between: The load board connector and the aircraft-side payload interface, clipped along the frame in between
Most vulnerable points: The two connector mating ends, and any point where the routed section crosses a clip, a frame edge, or a joint that moves
Published pinout: DJI does not publish pin arrangement, conductor count, or length for this harness. Similar-looking DJI cables carry different pinouts, so match by parts-diagram callout or by the marking on the cable you are removing.
Mating cycles: No mate-cycle rating is published for this harness. Treat the connector as the wear item it is. An aircraft whose payload comes off every day puts far more cycles through this joint than one running a single module all season, and it should be inspected on that basis rather than on a calendar.
Repairability: Not a serviceable assembly. There is no field pin-replacement kit, no published crimp specification, and no boot or seal offered separately. Where a pin, a shell, or the jacket is damaged, the harness itself is the replacement item.
Test values: No resistance, insulation, or continuity figures are published for this cable, so testing has to be comparative rather than absolute. Compare each conductor against the others in the same harness, measured the same way with the same leads. An outlier among its own siblings is the finding. A single number on its own means very little.
Cleaning: No cleaning procedure or approved solvent is published for this harness. Nothing aggressive belongs near the contacts, and pressure washing aimed directly at the payload joint is what drives water past a seal that would otherwise have kept it out. Rinse the area; do not point the wand at it.
Hardware along the run: Clips, ties, grommets, boots, and retaining hardware along the routed section are not part of this item. Have replacement ties on the bench before you start, because a run put back with the wrong tie spacing is simply the next failure.
Confirm fitment by part number before ordering. Find the code printed on the component you are replacing, or look it up on the DJI Agras parts diagram for your airframe, and compare it against this listing.
Revision suffixes are still the same part. DJI labels sometimes carry a trailing revision such as .01, .02, or .F. Those denote a production revision, not a different component. Match the base number and disregard the suffix.
Visually similar is not the same. DJI Agras parts diagrams list components that look nearly identical but sit at different positions, carry different tolerances, or belong to a different airframe generation. Ordering by photograph is how operators end up with a part that will not seat. Order by number.
Verified fitment for this listing: DJI Agras T100. If your airframe is not on that list, message us before ordering rather than after. We would rather answer a question than process a return, and so would you.
Not sure? Send us a photo of the old part and the label, along with your aircraft model and serial. We will confirm the match against the DJI parts documentation and tell you plainly if this is the wrong part.
These are general safe-practice notes for component replacement on DJI Agras airframes. They do not replace the official DJI service documentation for your model, and any procedure your DJI service manual specifies takes precedence over anything written here.
Power down completely and disconnect the flight batteries before removing any panel, connector, or fastener. Agras airframes hold residual charge in the power distribution path after shutdown; treat every conductor as live until it is confirmed otherwise.
Photograph the assembly before you disturb it. Cable routing, connector orientation, and fastener lengths on Agras airframes are not interchangeable, and the Load Adaptive Cable / Load Board Connection Cable is easier to fit correctly when you can see how the original sat.
Observe ESD precautions. Ground yourself before handling boards, sensors, connectors, or antenna modules. Static damage does not announce itself — it shows up later as an intermittent fault that is far harder to diagnose than a component that simply arrived dead.
Seat every connector fully and restore the original strain relief. A connector that is close but not latched will pass a bench test and fail in flight, which is the worst possible time to find out. Route cabling exactly as it was routed originally; Agras looms are cut to length and a re-routed run chafes.
Test before you spray. Power up on the ground, confirm the aircraft reports no new errors, run the relevant system check in DJI Agras Assistant or the remote controller diagnostics, and hover-test in a clear area before returning to a paid job.
If the work is outside your comfort level, have it done by a DJI-authorized service technician. The part cost is small next to the airframe.
Chasing an intermittent payload fault that follows vibration rather than a particular module.
Restoring a load interface after the harness was pulled, pinched, or contaminated during a payload swap.
Recommissioning an aircraft after work at the payload joint, where the harness was unmated, moved, or contaminated during the job. Fitting a new one closes the question so the first paid load of the season is not also the test flight for a connector somebody had their hands on last week. On an interface that tells the aircraft what is hanging underneath it, that is a cheap way to buy certainty.
Fleet aircraft whose modules get swapped between airframes through the day. Every swap is a mate cycle on both connectors, so the airframe that does the most swapping wears its interface out first while looking identical to the one parked beside it. Those are the aircraft worth carrying a spare harness for, and worth inspecting the joint on before a heavy week rather than in the middle of one.
Closing out a warranty or insurance job cleanly where the damage report says the payload joint took a knock. A harness that has been crushed, stretched, or had a module dropped onto it can test perfectly well and still be the reason the aircraft comes back in three weeks. Replacing it while the area is already open costs a fraction of returning to it later.
Canonical product name: DJI Agras T100 Load Adaptive Cable
Aircraft: DJI Agras T100
System: Payload/load-board electronics
Primary function: Board-to-system electrical connection
Seller: Ares Acres LLC
Also searched as: T100 load cable, load board cable, payload board harness, T100 adaptive cable
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Ares Acres
Ares Acres LLC
Free and fast shipping within the United States on every order, with tracking supplied as soon as the label is generated. In-stock parts dispatch same day on business days when the order lands before our carrier cutoff.
We ship from the U.S., not from overseas. That is the whole reason Ares Acres exists. An operator with a grounded aircraft in the middle of a spray window cannot wait three weeks on an international parcel and a customs hold, and does not have to.
Genuine OEM only. Every part we list as OEM is a genuine DJI component in new condition. We do not substitute aftermarket parts, and we do not relabel. If a listing says OEM, that is what ships.
Ordered the wrong part? Contact us. Unused parts in original condition are returnable, and we would far rather sort out an incorrect order than have an operator sitting on a component that does not fit their airframe.
Need help identifying a part? Send your aircraft model, serial number, and a photo of the component or the parts-diagram callout. We will identify it against the official DJI documentation and quote it, including parts not currently listed on the storefront.
Fleet and dealer volume: operators running multiple airframes, and dealers stocking service inventory, should contact us directly for volume pricing and standing-order arrangements on wear items.
What does this cable connect?
It connects compatible T100 load/payload control-board hardware to the supporting aircraft or accessory system.
Can similar-looking cables have different pinouts?
Yes. Confirm the exact connector and application before ordering.
Can a damaged cable cause intermittent payload faults?
Yes. Pin, conductor, or connector damage can interrupt communication.
Is this a genuine DJI OEM Load Adaptive Cable / Load Board Connection Cable?
Yes. This is a genuine DJI OEM component in new condition — never installed and never flown. Ares Acres LLC is a U.S.-based authorized DJI Agras reseller. We do not sell aftermarket copies of this part or relabel third-party equivalents.
Will this fit my aircraft?
This part is supplied for the DJI Agras T100. Confirm against your model's DJI Agras parts diagram before ordering. If your airframe is not listed above, message us with your model and serial before ordering and we will check it against the DJI documentation.
How fast does it ship, and where does it ship from?
It ships free and fast from within the United States, with tracking. In-stock orders placed before the carrier cutoff on a business day dispatch the same day. Nothing routes through an overseas warehouse or customs.
Can I install the Load Adaptive Cable / Load Board Connection Cable myself?
Many operators do. Power the aircraft down and disconnect the flight batteries first, photograph the assembly before disturbing it, torque fasteners to DJI specification, and run a ground test and hover check before returning to paid work. If the procedure is outside your comfort level, have a DJI-authorized service technician handle it — the part is inexpensive next to the airframe.
What if I order the wrong part?
Contact us. Unused parts in original condition are returnable. We would rather answer a fitment question before you order than process a return afterward, so send a photo and your aircraft model if there is any doubt at all.
Do you stock other parts for this aircraft?
Yes. Ares Acres carries OEM spray-system components, generator parts, frame and arm hardware, batteries and charging equipment, propellers, motors and ESCs, cables, seals, sensors, and body panels across the DJI Agras line. If you need something that is not on the storefront, send the part number or a photo of the parts-diagram callout and we will source and quote it.
How do I tell whether the fault is the cable, the load board, or the module?
Work by movement and substitution, not by meter alone. With the system powered and the fault showing, flex the harness by hand along its length and at both connectors and watch for the state to change; a fault you can provoke by hand is in the harness. Then swap the module if you have a second one, which clears or condemns it in one step. Then unplug and inspect both connector housings under light before ordering anything, because one backed-out or bent pin looks exactly like a dead board and costs nothing to fix.
A continuity test passed. Can the cable still be bad?
Yes, and this is the usual trap with signal harnesses. A continuity beep confirms a path exists. It does not tell you the resistance of that path, and it does not load the conductor. A cable down to a few surviving strands, a pin touching on one edge only, or moisture bridging two adjacent pins will all pass. Measure resistance rather than listening for a beep, check pin-to-pin for leakage as well as end-to-end, and do all of it while flexing the cable and working both connectors.
Can I splice the damaged section instead of replacing the harness?
It is a poor trade on a payload interface. A splice adds two joints and a stiff spot in the middle of a run that is meant to flex, it changes the electrical character of a line carrying data rather than plain DC, and it almost always goes back without the original strain relief. On a harness that determines what the aircraft believes is hanging underneath it, the replacement is cheap and the in-flight failure is not.
What else should I check while the payload is off?
Look into the load board connector and the aircraft-side connector under good light for a recessed, bent, or corroded pin, and check that neither shell is cracked. Check the clips and ties that carry the run, because a broken clip lets the harness swing and is often the reason the first one failed. Clean spray residue off the mating faces and seals of the payload joint. Then refit the module and confirm the aircraft recognizes it through a full function check before you put chemical in it.
Is contact cleaner or dielectric grease a good idea on these connectors?
Go carefully. A dedicated electrical contact cleaner that flashes off dry, used on a fully unmated and unpowered connector, is reasonable on a dirty joint. General solvents are not, because they attack the plastic and the seals. Grease is where people go wrong: packing a sealed connector with it can hold the shells apart, trap the very moisture it was meant to exclude, and make the next inspection unreadable. If a joint needs grease to work, it needs replacing.
How much slack should the new harness have when I route it?
Match the original, and match where the original put it. This run crosses a joint that opens, so the slack has to sit where the joint moves and in the plane it moves in. A service loop coiled in the wrong place is the same as no slack at all. Fit the fixed end first, work toward the end that moves, then check by hand that nothing is being pulled at either boot with the payload fully seated.
Should I keep one on the truck, or just order when it fails?
Order ahead if your payload comes on and off regularly. The failure this part produces is intermittent, it almost always shows up mid-job, and an aircraft with a payload interface that comes and goes is not one to keep spraying with. It is a small flat item that takes no shelf space, and having it turns an afternoon fault into an afternoon fault rather than the end of the week.
Two different modules behave badly on the same aircraft. Does that clear the modules?
It points hard at the aircraft side, which is this harness and the load board it lands on. Before ordering, unmate both ends and inspect the two connector faces under good light, then flex the run with the system powered and the fault showing. If nothing you do to the harness provokes the fault and both faces are clean and full, the board becomes the likelier candidate rather than the cable.
Can I cut the ties and reroute the new harness the way that looks tidier?
No, and this is the most common way a replacement fails early. The original routing exists because it keeps the harness off edges that would chafe it, out of the path of things that move, and away from wiring it should not sit alongside. Mark every tie point with tape before you cut anything, count the clips as you go, and put the new one back through the same points in the same order.
What does damage look like on a harness that has been used as a handle?
Look at the boots first, because that is where the load lands. A boot that has pulled away from the shell, that sits at an angle it was never molded to sit at, or that shows jacket drawn slightly out of it has taken a pull. Then look for a jacket gone slightly narrower just outside the boot, which is stretch. Neither shows up on a meter, and both mean the conductors inside have already been loaded past what they were built to see.
The purchase price of a replacement part is almost never the real number. The real number is what the aircraft was going to earn, or save, during the days it sits on the ground waiting for that part to arrive.
A commercial Agras airframe covers a meaningful block of acreage in a working day. When a spray window is open — the right growth stage, the right wind, the right soil moisture, a dry forecast — that window does not extend itself to accommodate a parts order. It closes. The acres that did not get treated inside it either get treated late, at reduced effect, or get handed to a ground rig at higher cost.
Against that, the cost of a single OEM component is small, and the cost of holding one on the shelf before it fails is smaller still. Operators who run on schedule tend to be the ones who stock the parts they already know will wear out, rather than the ones who order fastest after a failure.
For the Load Adaptive Cable / Load Board Connection Cable, that logic is straightforward: it is an inexpensive component relative to the DJI Agras T100 it serves, it is a known service item rather than a surprise, and having one in the truck or the shop converts a multi-day grounding into an afternoon of work.
This is also why we ship from U.S. stock rather than drop-shipping from overseas. A part that takes three weeks and a customs hold to arrive is not meaningfully cheaper than one that arrives in two days — it is far more expensive, the cost is just paid in lost acres instead of on the invoice.

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