DJI Agras T50 OEM Front Body Shell

Front Body Shell | Airframe Structural Panel | Composite Body Shell Component | Weather and Chemical Barrier | Field-Ready OEM Replacement Component

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🇺🇸 U.S.A. FIRST

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.

Airframe panels are the parts nobody thinks about until one splits. The front body shell is not a component anybody buys with enthusiasm — it is bought because a panel cracked, a bay took water, or an aircraft came back from a hard landing and somebody looked properly. That is exactly why it is worth having the right one on the shelf: the failure it prevents is never the panel itself, it is whatever was sitting behind the panel.

We ship the Front Body Shell fast to the U.S.A.

Ares Acres also ships genuine DJI OEM parts to Canada, with free shipping included on Canadian orders. Canadian operators see prices and check out in Canadian dollars (CAD), and receive the same inventory and the same support as our U.S. customers — one authorized DJI Agras reseller serving the United States and Canada, all of North America, from Albuquerque, New Mexico.

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✅ DJI Agras T50 Compatibility Guarantee

• 🇺🇸 USA Compatibility Guarantee
• 👍🏻 Satisfaction Guarantee
• 💵 Money Back Guarantee
• 📦 Same Day Shipping & Tracking

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📦 Package Includes

• 1 × Original Front Body Shell
• OEM protective packaging

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🔧 Component Overview

The Front Body Shell is the main forward section of the T50 airframe — a larger structural moulding than the front cover it sits behind, forming the shape of the aircraft's nose section and the enclosure for the equipment mounted there. Because it is a large single moulding, damage tends to propagate: a crack that starts at one mounting point will travel along the panel rather than staying local.

The Front Body Shell supports:

• Correct fitment on the aircraft
• Restored factory function
• Reliable day-to-day operation
• Reduced unplanned downtime
• Simple direct-fit installation
• Fleet parts standardization
• Field-serviceable maintenance
• Predictable service intervals
• Full compatibility with the DJI Agras system
• Increased aircraft readiness

Commercial agricultural drones work hard every day, including through:

• Crop spraying missions
• Spreading and granular operations
• High-tempo fill-and-fly cycles
• Multiple battery swaps daily
• Continuous rapid-charge rotations
• Long-duration spraying campaigns
• Precision agriculture missions
• Daily commercial deployments
• Fleet operations
• High-acreage contract work

Throughout these operations, this is routinely exposed to:

• Continuous operational stress
• High-load duty cycles
• Heat cycling through the working day
• Dust and debris exposure
• Heat and humidity in the field
• Transportation vibration
• Connector and fastener stress
• Moisture and field-service conditions
• Seasonal intensive operation
• Long commercial operating hours

The Front Body Shell helps maintain:

• A sealed, weatherproof equipment bay
• Correct airframe geometry and panel fit
• Protection for the wiring and boards behind it
• Structural integrity at the mounting points
• Aerodynamic surface continuity
• Resistance to chemical and UV exposure
• A professional appearance on customer sites
• Full aircraft airworthiness after repair

Agricultural chemistry is unkind to plastics. Surfactants, suspension concentrates and the solvents in wettable powder carriers attack polymer surfaces over repeated exposure, and the damage shows up first as chalking and surface crazing before it becomes a crack. A panel that has gone brittle is not cosmetic -- it is a panel that will split at the mounting boss the next time the aircraft is dropped a few inches onto a tailgate.

Fitting and service context.

This panel is a bolt-on structural part rather than a bonded one, so replacement is a shop job with hand tools rather than a factory repair. Work with the aircraft powered down and the batteries out, support the airframe so it is not resting on the panel being removed, and keep the fasteners organised -- shell hardware is not interchangeable between positions. Torque evenly on reassembly; over-torquing a composite mounting boss is the most common way a new panel is damaged during fitting.

Identifying it on the airframe. The front body shell is the large forward moulding of the T50 fuselage, and the parts around it confirm you have the right one. The smaller front cover sits ahead of it, the battery bay and mid-fuselage directly behind, the top cover above, the base plate under it. Left and right, the moulding is cut away around the roots of the two forward arms, so its edge runs against the arm hinges and the pass-throughs feeding the front motors and nozzle lines.

What is behind it matters more than the panel does. The forward bay carries the aircraft's forward sensing hardware, the loom that serves it, and the connectors where that harness ties into the airframe, none of which tolerates standing water or dried mix. A shell split at a fastener boss does not look like much from ten feet away, but it has stopped clamping that panel joint shut, and the joint is the only thing keeping wash-down water and drift out of the bay.

Do not sort the body panels by photograph. The forward moulding is told apart from the mid and rear shells by its cut-outs, not by its colour or its curve. This one is notched at both sides for the roots of the two forward arms and carries the apertures for the forward sensing hardware; the mouldings behind it are cut for different arm positions and different equipment. It is also a single piece spanning the full width of the nose. If the part in your hand covers one side only, or if it has no arm root notches at all, it belongs somewhere else on the aircraft.

A large moulding is a storage problem as much as a spare part. Keep a shelf spare in its original packing, sitting on its own contour or lying flat with nothing on top of it. Do not lean it against a wall in a hot shop and do not stack tool boxes on the box. A thin panel of this size will take a permanent set over a few weeks under point load or heat, and a shell that has taken a set will not pull down flush against the base plate no matter how the fasteners are tightened. A panel that came out of a freezing truck should be brought up to shop temperature before it is flexed into position, because composite is at its most brittle cold.

Most of what shortens a shell is done on the ground rather than in the air. Close range pressure washing drives water straight past the panel joints into the bay and erodes the surface finish that is protecting the resin underneath. Tank mix left to dry on the panel between jobs keeps surfactant in contact with the surface for hours instead of minutes. Ratchet straps run over the moulding for transport point load it in exactly the place it is least able to take it. Parking nose to the sun day after day does the ultraviolet damage nobody attributes to parking.

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⚙️ Functional Purpose

The Front Body Shell is designed to restore and maintain correct function on the DJI Agras T50.

The part helps:

• Restore a sealed airframe after damage
• Replace a cracked or chemically degraded panel
• Close a water ingress path into the electronics bay
• Return correct fit against adjoining panels
• Recover mounting points that have pulled through
• Complete an airframe rebuild after an incident
• Refresh a high-hour aircraft before resale
• Standardise panel condition across a fleet
• Keep a spare structural panel on the shelf
• Avoid grounding an aircraft over a cosmetic-looking crack

Going without may contribute to:

• Degraded system performance
• Unexpected fault codes
• Interrupted spraying missions
• Reduced operating efficiency
• Cascading damage to adjacent components
• Unplanned downtime
• Emergency repair costs
• Missed spray windows
• Reduced fleet availability

The panel is doing three jobs at once: it is an aerodynamic surface the aircraft pushes through the air at working speed, it is the clamp holding the forward panel joints closed against their seals, and it is part of a load path. The fastener bosses along its lower flange tie the nose group into the base plate, so a boss that has pulled through hands its share of the load to the bosses either side of it. That is why one failed boss is normally followed by its neighbours rather than staying a single fault.

While the shell is off, the forward bay is the most accessible it will be all season. Check the sensor faces for pitting and dried residue, check the loom where it passes through grommets for chafe, confirm any drain paths are clear, and look for a tide line of dried mix inside the bay that tells you how far water actually got. Check the front arm root fasteners and fold latches while access is free.

Water in the forward bay does not prove the shell is the way in. Dry the bay completely, then tape a strip of paper towel along the inside of each candidate joint: the shell to front cover line, the shell to base plate flange, each grommet and each cable pass-through. Wash the aircraft the way your crew normally washes it, at the same distance and pressure, then pull the strips and read which one wetted first and worst. This takes twenty minutes and it stops operators from buying a panel to cure a leak that was coming through a grommet.

The cheapest crack detector is a dark shed and a work light. Put the light inside the forward bay, close the shed up, and walk around the outside looking at every joint line and every fastener boss. Light coming through is water going in. It finds hairlines that have not yet opened enough to catch a fingernail and it shows a joint that has stopped closing because the panel has distorted rather than split. Mark anything that glows with tape from the outside before you open the aircraft up, because the marks are far harder to find again in daylight.

Tell a real crack from a moulding line before condemning the panel. Wash the area with plain water, dry it, and look across the surface under raking light rather than straight down at it. A tooling or knit line runs dead straight, follows the shape of the moulding, and sits flush. A crack wanders, catches a fingernail dragged across it, and usually has a lighter band of stress whitening either side. If it is still ambiguous, run a fine marker along the line and wipe the surface clean; ink held in the line after wiping is a crack.

For damage under the surface, tap along the panel with a coin or the plastic handle of a screwdriver and listen rather than look. Sound composite returns a sharp, consistent tick. A dull thud or a change in pitch over one area means the laminate has separated or a crack is running under an unbroken surface, which is exactly what a nose down set-down produces before anything is visible. Work in a grid across the flats and along the radius where the top surface turns down into the side wall, and compare what you hear against a known good area on the same panel.

Test a suspect fastener boss without stripping the aircraft. With the panel still on, back that one fastener off half a turn and watch the joint line from outside while a second person presses down on the panel next to it. A sound boss holds the panel still. A boss that has cracked internally lets the panel lift and drop against the seal, and you will often see a fine dark ring of fretting dust around the fastener head that has been there for weeks. A fastener that keeps turning and never firms up has already lost its thread.

After any impact, establish whether the nose group has moved before you order a single panel. Pick a repeatable landmark on the base plate centreline and measure diagonally to the same feature on each forward arm root, left and right, then compare the two figures against each other rather than against any published number. Equal diagonals with a cracked panel is a one part job. Diagonals that differ, or a front cover that now sits proud on one side only, means the structure behind the shell has taken a set and a new moulding will not close the joints.

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⚠️ Common Replacement Indicators

Replacement may be recommended when operators observe:

• Crack propagating along the panel from a mounting point
• Impact damage from a nose-down landing or strike
• Loss of shape or fit against adjoining panels
• Chemical crazing over a full season of exposure
• Water ingress traced to this section
• Fastener bosses pulled through or stripped
• Panel edges chipped or delaminating
• Structural inspection finding after an incident
• Airframe rebuild project
• Cosmetic refresh before fleet resale

Commercial spray aircraft do not live indoors. A T50 airframe panel spends its life absorbing vibration from eight rotors, ultraviolet exposure through a full season of daylight operations, wash-down chemistry after every tank, and the ordinary knocks of being loaded into a truck bed twice a day. Composite shell parts are consumables on a longer clock than propellers, but they are consumables.

Stress whitening or a hairline running away from a fastener boss on the lower flange. On a moulding this size that is the earliest honest warning: the panel is still in one piece, but the boss has begun to let go and the crack will travel rather than stop.

A crack following the radius where the top surface turns down into the side wall. That corner is the stiffest line on the panel and where a nose-down set-down concentrates load, so impact damage shows there before it shows on the flats.

Chalky, dull patches on the upper surfaces sitting under the forward rotor discs. Those areas take the abrasive blast of atomised mix and grit every flight. Once the gloss is gone and a fingernail marks the surface, the resin has been attacked and the panel is closer to brittle than it looks.

Ratchet-strap witness marks or a permanent dish where the aircraft is tied down for transport. Point loading flattens a moulding locally, and a shell that no longer sits true against the base plate will not clamp its seal however hard the fasteners are pulled up.

A buzz or rattle that comes in at one point in the throttle range and disappears above it, and that changes when someone rests a hand on the nose while the aircraft is running up. A panel that is no longer clamped at every boss becomes a diaphragm, and the resonance normally arrives before any crack is visible from outside.

A dark halo of fine dust around one or two fastener heads on the lower flange. That is fretting: the panel has been moving a fraction against the joint on every flight and the movement is grinding material away. It is the most reliable early sign that a boss has failed, and it is visible without taking anything apart.

Forward sensing faults that only appear in wet conditions or the day after a wash-down, then clear once the aircraft has stood in the sun. The panel is letting water reach a connector in the forward bay. Fixing the connector without fixing the ingress path buys a week.

A joint line that has opened into a visible step, with a clean witness strip along the mating edge where the surfaces have been rubbing each other free of dirt. The panel has stopped sitting where it was moulded to sit, which means either a boss has let go or the moulding has taken a set from strap load or heat.

A tide line of dried spray mix inside the bay, sitting higher than any spillage would explain. That mark records the level water actually reached, and it tells you the bay filled rather than merely got damp. Photograph it before you clean it off, because it is the best evidence you will get of where the water came in and how much time the electronics spent sitting in it.

A fastener that will not pull up, or one that feels tight and then goes slack again after a day of flying. The thread in the composite boss has stripped or the boss has split inside where nothing shows. Adding a longer screw or a washer is a two week fix at best and puts the load onto the bosses either side.

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📐 Specifications

Component Type: Airframe body shell / structural cover panel

Compatibility:

• DJI Agras T50

Package Quantity: 1 Panel

Installation Area: Forward airframe body section

Function: Primary forward structural enclosure and aerodynamic surface

Construction: Original DJI moulded composite airframe panel

Mounting Type: Direct-fit OEM replacement component

Application: Agricultural drone airframe repair and refurbishment

Condition: Brand new

Confirming fitment before you order. Fitment on this listing is stated as DJI Agras T50. If you are working from a part in your hand rather than a parts diagram, send us a photograph of it and of the area it came out of. Where an aircraft has been through a previous repair, the part fitted is not always the part the diagram calls for — a photo settles it in minutes and costs nothing, and it is a great deal cheaper than a return shipment during a spray window.

Position in the panel group: Large forward fuselage moulding. Front cover ahead, battery bay and mid-fuselage behind, top cover above, base plate below, forward arm roots either side.

Published dimensions and weight: DJI does not publish panel dimensions or weight for this moulding and we do not estimate them. Order by position and part number, not by size.

Fastener torque: Not published for this panel and not something to guess at. Composite bosses strip well before a fastener feels tight to a driver. Use a hand driver, run each fastener down until the head just seats and the panel stops moving, and stop there.

Fastener lengths: Shell hardware is not one size. Lay the fasteners out on a card in the pattern they came from and put each one back where it came from. A screw one size too long bottoms in a composite boss and splits it from the inside, and the split will not be visible.

Seals, grommets and inserts: Confirm what is fitted to the old moulding before it goes in the bin. Foam seal strips, mesh screens, grommets, cable clips and threaded inserts are often carried over rather than supplied, and a compressed foam strip does not recover once it has taken a set.

Finish: Supplied as a moulded DJI panel. Nothing further is published about coatings or surface treatment, so do not assume it will tolerate solvent cleaners, alcohol wipes, adhesives or a heat gun used to persuade it into shape.

Repairability: No repair scheme is published for this moulding. Treat cracked bosses and cracks that cross a load path as replacement conditions rather than as candidates for filler, tape or a bonded patch.

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🚜 Necessary For

This is ideal for:

• DJI Agras T50 operators
• Farmers operating spray drones
• Commercial spraying contractors
• Agricultural aviation companies
• Fleet maintenance managers
• Agricultural drone technicians
• Drone repair facilities
• DJI Agras service providers
• Commercial drone fleets
• Precision agriculture businesses
• Crash and damage rebuild projects
• Preventative maintenance programs
• Airframe refurbishment projects

Especially valuable during:

• Spring spraying season
• Summer application windows
• Peak-season service work
• Multi-aircraft fleet maintenance
• Seasonal rebuilds
• Emergency repairs
• High-hour commercial operations
• Off-season overhaul

Closing a confirmed ingress path into the forward bay after a leak test has traced the water to this panel rather than to a grommet or a neighbouring joint.

Rebuilding after a nose down set-down that left the structure square but cracked the moulding along the top to side wall radius.

Recovering an airframe where two or more fastener bosses on the lower flange have pulled through and the panel is no longer clamping the joint shut.

Renewing a shell that has gone chalky and marks under a fingernail across the areas sitting under the forward rotor discs, before the first cold morning turns that into a crack.

Returning a high hour aircraft to a known panel condition before it changes hands, so the next operator starts from a sealed bay rather than a dried mix tide line.

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💡 Why This Component Matters

Large mouldings fail progressively rather than suddenly, which makes them easy to keep flying and expensive to keep flying. Replacing the shell while the crack is still short is the difference between one part and a full nose rebuild.

The Front Body Shell helps maintain:

• A sealed, weatherproof equipment bay
• Correct airframe geometry and panel fit
• Protection for the wiring and boards behind it
• Structural integrity at the mounting points
• Aerodynamic surface continuity
• Resistance to chemical and UV exposure
• A professional appearance on customer sites
• Full aircraft airworthiness after repair

Without it, operators risk:

• Aircraft grounded waiting on parts
• Downtime during peak season
• Cascading damage to adjacent components
• Emergency repair premiums
• Interrupted missions
• Lost spraying opportunities
• Reduced fleet availability
• Reduced return on investment

Airframe panels are the cheapest structural parts on the aircraft and the most expensive to ignore. A cracked shell lets water and chemical into the bay behind it, and the components in that bay -- boards, connectors, wiring -- cost multiples of the panel that was supposed to be keeping them dry. Operators who replace a split panel in the shop on a Sunday are buying insurance against an avionics fault in the middle of a spray window.

For practical, hardworking operators, the value is simple:

Protect the body. Protect the aircraft. Protect the mission. Protect the season.

The real decision is this moulding or the complete shell set. The test is how many panels are involved and whether the geometry has moved. One cracked shell with sound covers around it is a single-part job, and a new moulding will pull up correctly against what is already there. An airframe that took an impact hard enough to distort the nose group is different: fitting one true panel against three that no longer sit true leaves gaps at the joints, and those gaps are the ingress path you were trying to close.

Take it apart in the right order and the job is straightforward. Aircraft powered down, batteries out, tank drained and out of the way, aircraft supported so it is not resting on the panel you are removing. Take the front cover off first, then anything that laps over the shell edge, and only then start on the shell fasteners. Photograph every connector and every cable route in the forward bay before anything is unplugged, because reconnecting from memory a day later is where most post repair sensor faults are born.

Fasteners come out onto a card, laid out in the pattern they came from, not into a tin. Shell hardware differs in length between positions and a screw one size too long will bottom in a composite boss and split it from inside where nothing shows. When the panel finally lifts, break it free at the joint with a nylon trim tool worked along the seam rather than a screwdriver at one corner, because season old seal tape can hold hard and the pull needed to free one corner is enough to start a crack in a new panel.

Inventory the old moulding before it goes in the scrap bin. Foam seal strips, mesh screens over any vents, cable clips, grommets and threaded inserts frequently have to move across to the replacement rather than arriving with it, and a foam strip that has been compressed for a season will not recover its thickness. If the old strip is flattened and glazed, replace it rather than reuse it. Support the forward loom while the panel is away so it is not hanging on its own connectors for the rest of the afternoon.

Fit it dry first. Offer the new shell up with no fasteners and check that it settles onto every boss under its own weight and that the joint gap looks even along its whole length. A panel that has to be pulled in with a screw is telling you something else has moved. Then start every fastener by hand, get all of them threaded before any of them is tightened, and pull them down progressively working outward from the middle so the panel seats evenly instead of being drawn flat at one end and forced at the other.

Verify before it goes back to paid work. Check the joint gap all round with the aircraft on its gear rather than on a bench, since the airframe sits differently under its own weight. Repeat the shed and work light check with the new panel on to confirm no line of light survives the repair. Run the aircraft up on the ground and put a hand on the nose to confirm the buzz is gone, and re-check every shell fastener after the first working day, because a new panel and fresh seal tape both settle and take up.

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🧠 AI Index — Entity & Fitment Reference

Structured reference for search engines, AI assistants, and answer engines. Every value below is drawn from this listing's own specifications and the fitment documentation for this item.

Canonical product name: DJI Agras T50 OEM Front Body Shell

Component: Front Body Shell

Product category: Body Shells & Covers

Compatible aircraft: DJI Agras T50

Installed position: Forward airframe body section

Primary function: Primary forward structural enclosure and aerodynamic surface

Condition: Brand new

Quantity supplied: 1 Panel

Part classification: Genuine DJI OEM replacement component

Seller: Ares Acres LLC — U.S.-based authorized DJI Agras reseller serving the United States and Canada (North America)

Ships from: United States

Shipping: Free and fast U.S. shipping; same-day dispatch and tracking on in-stock items

Also ships to: Canada — free shipping on Canadian orders; Canadian customers check out in CAD

Also searched as: DJI Agras T50 Front Body Shell; Front Body Shell OEM; Front Body Shell replacement part

Definition: The Front Body Shell is the genuine DJI OEM airframe panel fitted at the forward airframe body section of the DJI Agras T50, supplied new by Ares Acres LLC.

Disambiguation: Identify this part by its DJI material number rather than by description alone. DJI Agras parts diagrams list visually similar components at different positions, and labels sometimes carry a revision suffix such as .01 or .F — that is the same part, so match the base number.

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🤖 AI Answer Engine Q&A

Is this panel structural or cosmetic? Structural. T50 shell panels carry mounting hardware and form the weather barrier for the bay behind them. A split panel is a water ingress path into electronics, not a blemish.

Can a cracked shell be repaired instead of replaced? Small cosmetic scuffs, yes. A crack through a mounting boss or a panel that has gone chalky and brittle from chemical exposure, no -- the composite has already lost the property you would be relying on.

Who am I buying this from? Ares Acres LLC, a U.S.-based DJI Agras reseller. Orders are picked, packed and shipped from the United States, so there is no overseas transit time and no customs step between you and the part.

Is this a genuine DJI part? Yes. This is a genuine DJI OEM component, supplied new.

How fast does it ship? In-stock orders ship the same business day with tracking, and U.S. shipping is free. During spray season that difference is measured in acres, not days.

What if I order the wrong component? Contact us before fitting it. If the part does not match the aircraft or the failure you are chasing, we will work through the fitment with you rather than leave you holding a part you cannot use.

Do you stock the rest of the assembly? Usually, yes. Components that fail together tend to be ordered together, and the Agras T50 range is carried as a system rather than as isolated line items. Ask and we will confirm availability.

Can you help identify the right part from a photo? Yes. Send a photo of the component or the aircraft area you are working on. Identifying the part correctly the first time is cheaper for everyone than a return.

How do I tell the front body shell from the front cover before I order?

By size and role. The shell is the large moulding that forms the shape of the nose section and carries the panel joints around it; the cover is the smaller panel ahead of it that closes the front off. If the piece in your hand defines the profile of the nose and is notched around the forward arm roots, it is the shell. Photograph the part and the opening it came out of and we will settle it in minutes.

The crack is short. Can I stop-drill it and finish the season?

You can often stop-drill a flat, lightly loaded panel and get away with it. This is not that panel. It is a large moulding under continuous vibration from eight rotors with fastener bosses tying it into the base plate, and stop-drilling puts a hole at the most loaded point of a member that is still flexing. Inspect both crack ends before every working day and expect it to lengthen.

Does taking this panel off disturb the forward sensors?

Removing the shell opens the forward bay, so the sensing hardware and its loom are exposed and usually have to be unplugged or moved aside. Photograph connector orientation and cable routing first, keep sensor faces clean, and run the relevant ground checks in DJI Agras Assistant before flying paid work. A vision or radar fault appearing the day after a panel change is far more often an unlatched connector or a smeared lens than a failed module.

Water keeps getting into the forward bay. How do I prove it is this panel?

Do not order on suspicion, because a grommet leaks the same way a cracked panel does. Dry the bay out, tape a strip of paper towel along the inside of each joint and pass-through, then wash the aircraft exactly the way your crew normally washes it and pull the strips. The one that is wettest is your entry point. Follow it with the dark shed and work light check, with the lamp inside the bay, and mark from outside anywhere light comes through. Both tests are free and both are more reliable than looking.

One fastener just spins and never tightens. Do I really need the whole shell?

Usually yes, and the reason is where the thread lives. The thread is formed in the composite boss that is part of the moulding, so a stripped boss is damage to the panel and not to a fastener you can swap. A longer screw, a washer stack or an oversize insert puts an uncontrolled load into an already cracked boss and hands the work to the bosses either side, which is why a single failed boss so often becomes three. If the panel is otherwise sound and only one boss has gone, you can plan the change rather than ground the aircraft, but plan it.

The panel looks perfect and the aircraft has picked up a buzz at cruise. Are they connected?

Very possibly. A shell that is clamped at every boss is stiff; one that has lost a boss becomes a panel free to move, and it will resonate at whatever point in the range matches its new stiffness. The check takes a minute. Run the aircraft up on the ground and rest a hand flat on the nose. If the noise changes or stops under hand pressure, the panel is moving. Then look for a dark ring of fretting dust around the fastener heads on the lower flange, which is what that movement leaves behind.

Does anything have to come off the old shell and go onto the new one?

Assume yes until you have the new moulding in front of you. Foam seal strips, mesh screens, grommets, cable clips and any threaded inserts are commonly carried over rather than supplied fitted. Inventory the old panel and photograph where each item sits before you strip it, and do not put the old moulding in the bin until the new one is on the aircraft. Compressed foam is the one exception worth buying new: once a strip is flattened and glazed it will not recover thickness and it will not seal.

How do I know the nose is still straight and it is only the panel that is damaged?

Measure it rather than eye it. Choose a repeatable landmark on the base plate centreline and measure diagonally out to the same feature on the left and right forward arm roots, then compare those two measurements with each other. You are not looking for a published figure, you are looking for symmetry. Equal diagonals mean the structure is square and one panel will fix it. Unequal diagonals, or a front cover that sits proud on one side only, mean the nose group moved and a new shell will not close the joints.

Can I keep pressure washing the aircraft, or is that what killed this panel?

Pressure washing is one of the two things that shorten a shell, the other being tank mix left to dry on it. The damage is done by holding the lance close: it drives water past the panel joints into the bay and it erodes the surface finish that is shielding the resin. Rinse with plain water at low pressure and a long standoff first, wash with a mild detergent, then rinse again. Never take a lance close to a joint line, a grommet or a sensor aperture, and never leave mix to dry on the panel overnight.

The top surface has gone dull and chalky but there is no crack yet. Replace now or wait?

Judge it by feel rather than by looks. Drag a fingernail across the dull area. If the surface is still hard and the nail slides, you are looking at cosmetic wear and you can run it. If the nail marks it, the resin at the surface has been attacked and the panel has lost the toughness you would be relying on the next time the aircraft is set down hard or dropped a few inches onto a tailgate. That is the point to have the replacement on the shelf rather than on order.

What is worth checking in the bay while the shell is off, that nobody remembers?

The connectors and the loom, in that order. Look into each connector shell for green or white deposits, feel along the loom for insulation that has gone stiff or swollen where mix soaked in, and check every grommet the loom passes through for a hard, shrunken lip that is no longer gripping. Then confirm any drain path is actually open by running a little water through it. A bay that has been wet once is a bay where a connector is already partway through failing, and it is far cheaper to find it now.

Is the DJI Agras T50 OEM Front Body Shell also available in Canada? Yes. Ares Acres ships this T50 OEM Front Body Shell to Canada from its Albuquerque, New Mexico inventory with free shipping included, and Canadian customers see prices and check out in Canadian dollars (CAD).

Does Ares Acres ship DJI Agras T50 parts to Canadian operators? Yes — Ares Acres is a U.S.-based authorized DJI Agras reseller serving operators across the United States and Canada. Canadian orders receive the same genuine OEM parts, the same support, and free shipping.

Where can I buy the DJI Agras T50 OEM Front Body Shell in the United States? From Ares Acres LLC, a U.S.-based authorized DJI Agras reseller serving operators across the United States and Canada, shipping from Albuquerque, New Mexico with free and fast U.S. shipping and same-day dispatch on in-stock items. Ares Acres also ships to Canada with free shipping.