KPIs and Benchmarks
Space Avionics Manufacturing KPIs: Benchmark Ranges and How to Measure Them
First pass yield, escapes, derating compliance, test asset utilization, traceability and rework in flight avionics: how to measure each KPI, what moves it, and which figures have a cited source.
In flight avionics manufacturing, the KPIs that predict program health are yield, escapes, derating compliance, environmental test asset utilization and traceability completeness. Track them monthly against realistic bands, and use the bands as reference points for spotting a gap, not as targets.
Every figure here shows its basis. A superscript number links to a public source in the Sources list at the end; in this guide that is NASA's parts derating standard. A figure marked no cited source is kept exactly as originally published because it has not been verified against a public source, so treat it as illustrative.
At a glance
| KPI | Typical | Strong | Basis |
|---|---|---|---|
| First pass yield, Class 3 board assembly | 88 to 93% | 98% or better (world-class) | no cited source |
| Conformal coating first pass yield | 90 to 94% | > 98% (world-class) | no cited source |
| Internal nonconformance, share of units | 3 to 8% (new designs) | < 1 to 2% (world-class) | no cited source |
| Nonconformance disposition cycle time | Not stated | < 30 days (aim) | no cited source |
| Derating compliance, share of parts | 92 to 97% (first pass designs) | 100% (hard target) | 100%: NASA EEE-INST-0021; 92 to 97% no cited source |
| Environmental test asset utilization | 40 to 55% | 75 to 85% (world-class) | no cited source |
| Traceability completeness | 2 to 5% gaps found at as-built review | 100% (realistic target) | no cited source |
| Documentation labor, share of touch labor | 8 to 12% (usual) | Not stated | no cited source |
| On-time delivery, space builds | 60 to 75% | > 90% (world-class) | no cited source |
| Board rework rate | 10 to 20% (new designs) | < 5% (world-class) | no cited source |
Method: How the figures in this guide are sourced
A figure with a superscript number is stated by the cited source, listed under Sources with its publisher and access date, and the sentence gives the part types it applies to. A figure marked no cited source is kept exactly as originally published because no public source stating it has been verified. It is illustrative, not measured industry data.
First pass yield
First pass yield is the headline KPI. For Class 3 board assembly, typical shops run 88 to 93 percent, and world-class sits at 98 percent or better no cited source.
Conformal coating is usually the weakest step. Typical coating first pass yield is 90 to 94 percent, and world-class is above 98 no cited source.
For example, a shop hitting 98 percent first pass yield with under 1 percent escapes behaves nothing like one stuck at 90 percent and 5 percent.
How to measure
- Count good boards over boards started, before any rework.
- Track it per process step, not just at final test, so you see whether solder, coating or harness is bleeding.
- Trend it monthly on a chart rather than estimating from memory.
What moves it
- Fixtured masking.
- Controlled coating viscosity.
- Automated optical inspection of every board ahead of the coating booth.
Predict the coating number from board complexity with the Conformal Coating Yield calculator.
Escapes and nonconformance
Escape rate and nonconformance rate separate mature shops from the rest. A defect escaping to the customer or to flight is the costliest miss.
World-class programs hold field escapes near zero and internal nonconformance under 1 to 2 percent of units, while new designs typically run 3 to 8 percent no cited source.
How to measure
- Escapes: defects found after your final acceptance divided by units shipped.
- Convert escapes to defects per million opportunities (DPMO) where volume allows.
- Nonconformance: nonconforming units over units built, with the recovery cost trended beside the count.
What moves it
- Design for manufacturability reviews.
- First article rigor.
- Closing corrective actions fast, aiming for a disposition cycle time under 30 days rather than open for a quarter no cited source.
Derating compliance
Derating compliance is a reliability KPI with a hard target of 100 percent of parts inside NASA EEE-INST-002 limits, because the standard makes derating a requirement for every part category1. Typical first pass designs come in at 92 to 97 percent compliant before rework no cited source.
The lever is catching breaches at schematic review, not at test. Under EEE-INST-002, a monolithic microcircuit junction should not exceed 110 °C or 40 °C below the manufacturer's maximum rating, whichever is lower1. Discrete transistors and diodes have a separate limit of 125 °C or 40 °C below the rating, whichever is lower1.
Capacitor voltage limits depend on the dielectric. The standard allows 50 percent of rated voltage for solid tantalum and glass capacitors and 60 percent for ceramic and plastic film, applied to the sum of peak AC ripple and DC voltage1. A part past its limit should never reach a built board.
World-class teams gate design release on a clean derating report and refuse to lay out a board until the violation count is zero.
How to measure
- Divide compliant parts by total parts on the bill of materials.
- Count violations per design at schematic review, before layout freeze.
What moves it
- Checking each part's stress against its derating limit at schematic review.
- Gating design release on a clean derating report.
Environmental test asset utilization
Environmental test assets are expensive and usually under-loaded. Thermal chambers, shakers and burn-in ovens at typical shops run 40 to 55 percent utilization, while world-class scheduling reaches 75 to 85 percent no cited source.
Compare planned slots against actual use for each asset. The gap shows whether an asset is truly full or just idle between loads.
How to measure
- Divide productive test hours by available hours, per asset, per month.
- Compute each asset's theoretical slot count and compare it with actual use.
What moves it
- Batching units into shared cycles.
- Running burn-in over weekends, since 168 hour dwells are unattended no cited source.
- Pre-staging fixtures so a shaker is not idle for hours during a changeover that should take 30 minutes no cited source.
Get the theoretical slot count for each asset with the Thermal Cycle Test Capacity calculator, the Vibration Test Schedule calculator and the Burn-In Capacity calculator.
Traceability completeness
Traceability completeness must be 100 percent for flight hardware: every part carries lot, date code and serial back to the as-built record no cited source. The realistic target is 100 percent, because an audit finding here can ground a program no cited source.
Typical shops discover 2 to 5 percent gaps at as-built review; world-class shops catch them at the point of installation no cited source. Documentation labor usually runs 8 to 12 percent of touch labor, so resource it rather than rushing it at the end no cited source.
How to measure
- Divide records complete and verified by records required.
- Log where each gap was found: at installation or at as-built review.
What moves it
- Scanning at kitting and install instead of reconstructing paperwork weeks later from memory.
- Staffing documentation labor from the start of the build.
Size harness touch labor, the base that documentation labor adds to, with the Harness Routing Labor calculator.
Schedule and rework
Schedule and rework KPIs tie the rest together. On-time delivery for space builds is often 60 to 75 percent typical and above 90 percent world-class, dragged down by parts lead time and test queue depth no cited source.
Rework rate, measured as reworked boards over boards built, should trend under 5 percent world-class versus 10 to 20 percent typical on new designs no cited source. Measure cycle time from kit release to acceptance, and watch the environmental test queue.
How to measure
- On-time delivery: builds delivered by the committed date over builds due.
- Rework rate: reworked boards over boards built.
- Cycle time: kit release to acceptance.
What moves it
- Lifting upstream yield, which cuts rework.
- Raising test asset utilization, which cuts cycle time.
See whether the test queue is your bottleneck with the Thermal Cycle Test Capacity calculator.
How to build your own baseline
- First, stabilize first pass yield at each step toward 98 percent, because yield feeds escapes, rework and cycle time simultaneously no cited source.
- Second, gate designs on a clean derating report to protect reliability before a board exists.
- Third, lift test asset utilization from the typical 45 percent toward 80 percent through batching and weekend burn-in no cited source.
- Fourth, resource traceability at 8 to 12 percent of labor so completeness holds at 100 percent no cited source.
- Review all five KPIs monthly on a single trend chart.
- Set one improvement target per quarter and hold the line.
Sources
- EEE-INST-002: Instructions for EEE Parts Selection, Screening, Qualification, and Derating (NASA/TP-2003-212242). NASA Goddard Space Flight Center. published April 2008. Section 5 Derating (p. 15 of PDF); Section C1 Table 4 Capacitor Derating Requirements; Section M3 Table 4 Microcircuit Derating Requirements note 2; Section M3 Table 2 note 8 (burn-in hours). Accessed September 30, 2026.
Published 2026-07-02.