
This is the field reference guide to solar panel defect types found by drone inspection, covering every fault detectable with thermal and RGB imaging. Use it to understand thermal signatures, assess revenue impact, and prioritise your repair backlog.
Whether you’re reviewing a drone solar inspection report, training a solar panel maintenance team, or evaluating what your current inspection programme is finding (and missing), this guide covers the complete fault taxonomy used by professional solar inspection programmes.
Key takeaway: 12 fault conditions covered with thermal signatures, ΔT ranges, revenue impact, and repair urgency. Hotspots >80°C = CRITICAL. String open-circuit = CRITICAL. Bypass diode failures = HIGH.
How Solar Panel Faults Are Classified
Solar panel faults are classified along three independent axes:

By Detection Method
| Method | Detects | Requirements |
|---|---|---|
| Thermal imaging | Most electrical faults | Daytime, irradiance >400 W/m² |
| RGB/visual imaging | Structural, soiling, physical damage | Daytime, high-resolution camera |
| Electroluminescence (EL) | Micro-cracks, cell defects | Night inspection, darkened conditions |
| Electrical testing | IV curve, insulation resistance | Physical access, test equipment |
By ΔT Severity Band (Common Industry Practice)
| Severity Band | Temperature Delta | Action Required |
|---|---|---|
| Band 1 | ΔT 10–20K above background | Monitor; next maintenance |
| Band 2 | ΔT 20–40K above background | Repair within 30 days |
| Band 3 | ΔT >40K above background | Immediate action required |
These ΔT bands are common industry practice for grading thermal anomalies, not limits taken from the standard. IEC TS 62446-3, published by the IEC (International Electrotechnical Commission), defines the conditions and method for infrared inspection of PV plants and grades findings by Class of Abnormality (CoA); it does not set these ΔT bands.
By Repair Urgency
| Urgency | Timeline | Examples |
|---|---|---|
| CRITICAL | Immediate | Hotspot >80°C, string open-circuit |
| HIGH | 7–30 days | Hot MC4 connector, bypass diode failure |
| MEDIUM | Next maintenance cycle | Delamination, bird dropping soiling |
| LOW | Monitor | Inactive micro-cracks, dust soiling |
Bypass Diode Failures
What They Are
Each solar panel contains 3 bypass diodes, each protecting a group of approximately 20–24 solar cells. The bypass diode’s function is protective: when one cell in its group is shaded or underperforming, the diode activates to route current around that cell group rather than allowing it to become a load resistor.
When the bypass diode itself fails, it fails in one of two modes:
| Failure Mode | What Happens | Thermal Signature |
|---|---|---|
| Short-circuit failure | Diode permanently activates, forcing cell group into reverse bias | Rectangular hot zone covering 1/3 of module; ΔT 20–40K |
| Open-circuit failure | Diode fails to activate when needed | No thermal signature until shaded; then extreme temperatures |
Revenue Impact
- $200–400/panel/year in lost generation (affected cell group permanently non-productive in short-circuit mode)
Repair Urgency
- HIGH — Unresolved bypass diode failures typically progress to hotspot development, accelerating degradation
Repair Action
- Panel replacement (bypass diode replacement in-field is technically possible but rarely economical)
- Warranty claim if within manufacturer warranty period — IEC 62446-3 documentation supports the claim
Hotspots
What They Are
A solar panel hot spot is localised overheating of a single solar cell or small group of cells to a temperature significantly above the surrounding module. Hotspots are caused by:

- Partial shading of a single cell (activating bypass diode is normal response, but if diode is faulty, cell absorbs reverse current)
- Physical damage or cracks reducing current-generating capacity while still absorbing reverse current
- Foreign matter (bird droppings, leaf corner) causing localised shading
- Manufacturing defects causing cell mismatch within a string
Thermal Signature
- Single cell or small cluster (1–4 cells) at extreme temperature differential
- ΔT typically >30K above background, sometimes exceeding 50–80K
- Pattern: small, very bright spot on thermal image against uniform background
Temperature Thresholds
| Temperature | Risk Level | Action |
|---|---|---|
| 50°C above ambient | Significant degradation acceleration begins | Monitor closely |
| 80°C absolute | Fire risk threshold | Immediate action required |
| 100°C | Active hazard — documented panel fires | Shutdown immediately |
Revenue Impact
- Relatively low from single affected cell, but fire risk and physical damage potential make hotspots the highest-urgency fault type
Repair Urgency
- CRITICAL at ΔT >40K (severity band 3) or above 80°C absolute — primary concern is safety, not revenue
Soiling and Shading
What It Is
Soiling refers to deposits on the panel surface that reduce incident irradiance on affected cells:
| Type | Impact | Pattern |
|---|---|---|
| Bird droppings | High-opacity; block light entirely | Localised; can force entire cell group into bypass |
| Dust accumulation | Gradual performance loss across panel | Uniform; site-wide PR reduction |
| Vegetation debris | Leaves, seeds, pollen | Seasonal; clumped rather than uniform |
Thermal Signature
- Bird droppings: Cool patches (lower irradiance = lower temperature) OR warm patches if bypass diode activated
- Dust soiling: Subtle temperature reduction across affected panels, not localised anomalies
- Shape matches physical soiling pattern
Revenue Impact
- Bird droppings: 1–7% PR loss per affected panel (highly variable based on location)
- Uniform dust soiling: 2–5% site-wide PR loss per cleaning interval missed
Repair Urgency
- LOW-MEDIUM — Fully reversible by cleaning, no panel replacement required
- Urgency depends on soiling rate and economic cost of delayed cleaning vs cleaning crew deployment
Potential-Induced Degradation (PID)
What It Is
Potential-Induced Degradation is caused by leakage current flowing through the module from the high-voltage DC circuit to the module frame or mounting structure (grounded). The voltage differential drives ionic migration through the glass — primarily sodium ions — which deposit on the cell surface and interfere with the photovoltaic effect.
PID predominantly affects: p-type crystalline silicon cells (both mono and multicrystalline)
Lower susceptibility: n-type cells (TOPCon, HJT)
Risk Factors
- Negative grounding of DC system (module at negative end at highest potential differential)
- High system voltages (>600V DC — increasingly common as 1000V and 1500V systems become standard)
- High humidity and temperature (accelerates ionic migration)
- Poorly insulated module frames
Thermal Signature
- Subtlest thermal signature of all fault types
- Uniform, diffuse reduction in temperature across entire module — PID-affected panel slightly cooler than neighbours
- Easy to miss without careful cross-panel comparison
- More readily identified through production data analysis (sustained below-expected output from specific string positions)
Revenue Impact
- Early-stage PID: 5–15% module power loss
- Advanced PID: 30%+ loss
- Degradation can progress rapidly in high-humidity climates if not addressed
Reversibility
- Early-stage PID is partially reversible — PID recovery boxes (apply counter-voltage overnight) can restore 60–80% of lost capacity before damage advances
Micro-Cracks and Cell Cracks
What They Are
Physical fractures in the silicon wafer of solar cells, caused by:
- Mechanical stress during transport or installation
- Hail impact
- Thermal cycling (repeated expansion and contraction)
- Wind load on large-format panels
- Snow load on inadequately supported systems
Detection Methods
| Method | Detects | Limitations |
|---|---|---|
| Thermal imaging | Only electrically active cracks | Many micro-cracks are electrically inactive (no thermal signature) |
| Electroluminescence (EL) | All cracks (active + inactive) | Requires darkened conditions + direct electrical connection |
Thermal Signature
- Active cracks: Subtle linear/irregular thermal anomalies — ΔT 10–15K following crack geometry
- Inactive cracks: No thermal signature
Revenue Impact
- Inactive cracks: Minimal near-term impact
- Active cracks: Proportional to fraction of cell area isolated by crack
- Cracks tend to propagate over time — inactive cracks today may become active within 2–5 years
Delamination
What It Is
Delamination is the separation of the encapsulant layer (typically ethylene-vinyl acetate, EVA) from the glass front sheet or backsheet. This creates air pockets within the module laminate structure.
Causes
- Manufacturing defects (poor lamination)
- UV degradation of EVA over time
- Moisture ingress at panel edges
- Thermal cycling stress
Thermal Signature
- Air pockets conduct heat differently from intact laminate
- Diffuse thermal anomalies — warm blotches appearing as irregular patterns
- Most commonly starts at panel edges and corners
- Distinguishable from hotspots by diffuse, non-geometric character and moderate ΔT (10–20K)
Risk Progression
- Delamination itself is not an immediate performance crisis
- Creates pathways for moisture ingress
- Once moisture reaches cell contacts, corrosion begins
- Transition from minor delamination to significant performance loss can be rapid in humid climates
Repair Urgency
- MEDIUM — Not emergency, but monitor closely
- Panels with active delamination showing moisture-related discolouration (yellowing/browning in RGB images) should be prioritised for replacement
String and Connection Faults
What They Are
Failures at electrical connection points in the solar string:
| Fault Type | Failure Mode | Consequence |
|---|---|---|
| MC4 connector failures | Oxidation, contamination, improper mating, physical damage | Resistance increase → localised heating |
| Junction box failures | Loose connection to severe (arcing, fire) | Range from minor to critical |
| String open-circuit | Complete break in string electrical path | Complete loss of string generation |
Thermal Signature
| Fault | Thermal Pattern | ΔT Range |
|---|---|---|
| MC4 connector failure | Small, intensely hot point at connection | 30–80K |
| String open-circuit | Entire string uniformly cold/dark — no current flow | N/A (most dramatic pattern) |
Revenue Impact
| Fault Type | Annual Loss |
|---|---|
| Faulty MC4 connector | $500–2,000/year per connector |
| String open-circuit | $2,000–5,000/year per string (complete loss) |
Repair Urgency
- CRITICAL for string open-circuit (complete string loss)
- HIGH for hot connector faults (fire risk, progressive damage)
Tracker and Mounting Structure Faults
What They Are
Physical issues with solar tracker system (for tracking arrays) or fixed mounting structure:
- Misaligned tracker rows (not following sun correctly)
- Seized tracker drive mechanisms
- Broken or corroded mounting hardware
- Panel mounting angle inconsistencies
- Ground movement causing row misalignment
Detection Method
- RGB aerial imaging (not thermal)
- Tracker misalignment visible from above as rows oriented differently from neighbours
- Structural issues appear as physical deformations, corrosion, or tilting in high-resolution RGB imagery
Thermal Relevance
- Misaligned trackers show up in thermal as panels at different temperature profiles from correctly-aligned neighbours
- Receive different irradiance levels → generate different heat
- Creates thermal patterns that differ from electrical fault patterns
Revenue Impact
- Tracker misalignment: 2–8% yield loss for affected rows (depends on degree of misalignment and season)
Complete Fault Reference Table
| Fault Type | Primary Detection | Thermal Signature | ΔT Range | Revenue Impact/Year | Urgency | Recommended Action |
|---|---|---|---|---|---|---|
| Hotspot (critical) | Thermal | Single cell, intense heat | >40K | $100–500/panel | CRITICAL | Immediate investigation, replace if >80°C |
| String open-circuit | Thermal | Entire string cold | N/A | $2,000–5,000/string | CRITICAL | Same-day investigation |
| Hot MC4 connector | Thermal | Small intense hot point | 30–80K | $500–2,000 | HIGH | Repair within 7 days |
| Bypass diode failure | Thermal | 1/3 module hot zone | 20–40K | $200–400/panel | HIGH | Repair within 30 days |
| Bypass diode failure (minor) | Thermal | 1/3 module hot zone | 10–20K | $100–200/panel | MEDIUM | Next maintenance cycle |
| Bird dropping soiling | Thermal/RGB | Cool/hot irregular patch | 10–25K | $100–400/panel | MEDIUM | Schedule cleaning |
| Delamination | Thermal | Diffuse warm blotches | 10–20K | $50–150/panel | MEDIUM | Monitor; replace within 12–24 months |
| PID | Thermal | Uniform module cooling | Subtle | $200–800/panel | MEDIUM | PID recovery or replacement |
| Dust soiling | Thermal | Subtle site-wide cooling | 5–10K | 2–5% site PR | LOW-MEDIUM | Optimise cleaning schedule |
| Micro-cracks (active) | Thermal/EL | Subtle linear anomaly | 10–15K | $50–150/panel | LOW-MEDIUM | Monitor; EL test to quantify |
| Tracker misalignment | RGB/Thermal | Row at different angle/temp | Variable | 2–8% row yield | MEDIUM | Tracker service call |
| Micro-cracks (inactive) | EL only | No thermal signature | None | Minimal currently | LOW | Annual EL re-test |
Fault Severity Scoring: How to Prioritise a Repair Backlog
When a drone inspection of a 50MW site identifies 200 anomalies, the repair backlog needs a triage framework. Use this three-factor scoring approach:
Factor 1: Safety Risk (Overrides All Other Factors)
| Condition | Action |
|---|---|
| Hotspot >80°C | Immediate shutdown of affected string; repair before re-energisation |
| Hot connector >60°C | Repair within 7 days regardless of revenue impact |
Factor 2: Revenue Impact (For Non-Safety Faults)
Sort remaining fault list by estimated annual revenue loss:
Revenue loss = affected panels × loss per panel × electricity price
Fix the most expensive faults first.
Factor 3: Progression Risk
Some faults progress rapidly if unresolved:
- Bypass diode failures → hotspot cascade
- Delamination with moisture ingress → rapid corrosion
Apply 1.5× multiplier to revenue impact for faults with high progression risk.
The Fault Management Workflow
1. Drone inspection → AI generates fault list with GPS coordinates, panel ID, fault type, ΔT, severity band, photo
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2. Safety triage → Immediately identify band 3 hotspots or string open-circuits requiring rapid response
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3. Revenue prioritisation → Sort remaining faults by estimated annual revenue impact
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4. Work order creation → Generate work orders (ideally automatically via CMMS integration)
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5. Repair scheduling → Assign repair crews by priority and geography
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6. Verification → Post-repair thermal or electrical verification of resolved faults
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7. Documentation → Close work orders with resolution date, method, and cost
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8. IEC 62446 update → Fault register updated; compliance documentation current
Conclusion
Understanding the thermal signatures, revenue impact, and repair urgency of every fault type is foundational to running an effective solar inspection programme. The difference between a thin fault list and a complete one is rarely the drone hardware — it is the quality of the AI analysis and the knowledge of what to look for.
See ClearSpot’s AI fault classification and monitoring software in action for your portfolio. Use the button below to book a demo and we’ll walk through the fault detection and prioritisation workflow for a site your size.
Frequently Asked Questions
A solar panel defect is any issue that reduces panel performance, efficiency or safety. Common defects include hotspots, cracks, delamination, potential-induced degradation and electrical connection faults.
Drones carry radiometric thermal cameras and high-resolution RGB cameras. Thermal imaging reveals temperature anomalies such as hotspots, bypass diode failures and open strings, while RGB imaging shows physical damage, soiling and tracker misalignment.
The most common are hotspots, bypass diode failures, cracked cells, delamination, potential-induced degradation (PID), soiling, string open-circuits and hot MC4 connectors.
A hotspot is localised overheating of a single cell or small group of cells, caused by shading, cell damage or electrical mismatch. Hotspots above 80°C are treated as critical because of fire risk.
Drones detect broken glass and electrically active cell cracks, which show a thermal signature. Inactive micro-cracks have no thermal signature and need electroluminescence (EL) testing to confirm.
PID is power loss caused by leakage current between the high-voltage DC circuit and the grounded frame. It shows up as a subtle, uniform cooling of affected modules and is often confirmed with production data analysis.
Most utility-scale plants fly quarterly or twice a year, plus after extreme weather events, so new faults are caught before they compound.