Quality Reliability interview prep.
Quality engineers, reliability engineers, supplier quality engineers, MRB chairs at primes + tier-1 suppliers (commercial aviation, military, space, missiles, electronics).
What interviewers look for
- Can the candidate apply AS9100 QMS discipline + AS9102 FAI + Nadcap fluently across product + process?
- Are they fluent in MRB / nonconformance disposition - use-as-is, rework, repair, scrap - with engineering + customer alignment?
- Can they execute FRACAS closed-loop + structured root cause (8D / 5-Why / Fishbone)?
- Do they understand reliability math - MTBF allocation, MIL-HDBK-217 / Telcordia, FMECA, FTA, HALT / HASS?
- Are they fluent in SPC + Cpk / Ppk + MSA + statistical sampling per ANSI / ASQ Z1.4 + Z1.9?
- Can they manage supplier quality + source inspection + SCAR + Nadcap special-process oversight?
- Are they audit-ready - AS9100, DCMA QAR, FAA / EASA conformity, customer surveillance?
Behavioural questions to expect
Walk me through your quality + reliability background.
What it tests: Story arc - engineering / statistics training, AS9100 exposure, FRACAS + supplier work, safety-critical context - because A+D quality interviewers need to see audit-ready discipline from the first answer.
Tell me about a quality or reliability programme you've owned.
What it tests: Programme + closed-loop thinking - scope, audit-trail, outcome - because A+D quality is judged on evidence + sustained improvement, not one-shot fixes.
Why aerospace + defense quality + reliability vs commercial manufacturing or medical device?
What it tests: Authentic alignment - safety-of-flight stakes, audit-trail discipline, decade-scale fleet thinking - because the regulatory + consequence delta is the differentiator.
Why this domain - aviation / space / missiles / electronics?
What it tests: Specificity. Generic answers fail because A+D quality varies a lot across domains (commercial certification vs DoD MIL-STD vs space single-string).
Why this firm?
What it tests: Real homework - programme, quality posture, recent events - not generic name-drop.
What's your read on our programme + quality posture?
What it tests: Industry literacy - programme stage, regulatory engagement, recent quality events.
Tell me what you understand about our quality culture + management system.
What it tests: QMS maturity - AS9100 certification, Nadcap scope, independence of quality function, FRACAS deployment.
Walk me through a nonconformance + MRB disposition you led.
What it tests: MRB fluency - use-as-is / rework / repair / scrap reasoning, engineering + customer alignment, AS9100 audit trail.
Technical concepts to master
AS9100 QMS + Nadcap
- AS9100 structure
- ISO 9001 backbone + aerospace requirements - risk-based thinking, configuration management, FAI, counterfeit parts, product safety.
- Nadcap special processes
- Industry-managed accreditation programme for special processes whose conformity cannot be verified by inspection of the end product alone.
- AS9102 First Article Inspection
- Documented validation that the production process can produce a part meeting all engineering + design requirements - Form 1 (part), Form 2 (materials + processes), Form 3 (characteristics).
- Counterfeit parts mitigation
- AS5553 (electronic) + AS6174 (material) requirements to prevent counterfeit / suspect-unapproved parts entering the supply chain.
MRB + nonconformance + FRACAS
- MRB (Material Review Board)
- Cross-functional board (Quality, Engineering, Customer / Airworthiness as required) that dispositions nonconforming material - use-as-is, rework, repair, scrap.
- NCR / CAR / SCAR
- Nonconformance Report (the issue), Corrective Action Request (internal), Supplier Corrective Action Request (external) - the closed-loop documents.
- FRACAS (Failure Reporting, Analysis + Corrective Action System)
- Closed-loop process capturing field + test + production failures, driving root cause + corrective action + reliability growth.
- 8D + 5-Why + Fishbone (Ishikawa)
- Structured root-cause methodologies - 8D is 8-step team-based, 5-Why drills causality, Fishbone organises causal categories (man, machine, method, material, measurement, environment).
Reliability math + test
- MTBF allocation + apportionment
- Top-down distribution of a system MTBF (or MTBCF / Ao) requirement across subsystems + components - feasibility, complexity, mission-profile weighted.
- Prediction methods (MIL-HDBK-217 / Telcordia / FIDES / PoF)
- Empirical or physics-of-failure prediction of component + assembly failure rate, fed by mission profile + environment.
- FMEA / FMECA / FTA
- FMEA + FMECA = bottom-up failure mode + criticality. FTA = top-down deductive analysis of undesired events.
- HALT / HASS / ALT
- HALT = highly accelerated life test (stress-to-failure design margin); HASS = production screen; ALT = time-compressed life test for prediction.
SPC + sampling + MSA
- SPC + control charts
- Xbar-R / Xbar-S / individuals + moving range / p / np / c / u charts monitor process stability; Western Electric / Nelson rules detect special-cause variation.
- Cpk + Ppk + Cp + Pp
- Cp / Cpk = short-term (within-subgroup) capability; Pp / Ppk = long-term (overall) performance. Cpk + Ppk account for centring.
- Statistical sampling (Z1.4 / Z1.9 / 1916)
- ANSI / ASQ Z1.4 (attributes), Z1.9 (variables), MIL-STD-1916 (DoD preferred) define sampling plans by AQL + inspection level.
- MSA (Measurement System Analysis)
- Gauge R&R (repeatability + reproducibility), bias, linearity, stability studies validate measurement-system fitness.
Practical drills
- A machined titanium fitting on a flight-critical assembly is presented to MRB with a 0.003 inch oversized hole (drawing tolerance +/- 0.002 inch). The customer wants delivery in 5 days for a flight test. Walk through your MRB approach.
- A new airborne electronics LRU has a contractual MTBF requirement of 5,000 hours in fighter aircraft environment. The LRU has 4 CCAs - power supply, processor, signal conditioning, I/O. Walk through your allocation + prediction approach.
- A tier-1 supplier reports 3 in-service failures of a circuit card assembly in the past 60 days - all traced to solder joint cracking on a particular BGA component. The fleet has 200 units in service. PPAP was approved 18 months ago. Walk through your engineering + quality response.
Smart-question anchors
- Programme + production stage - LRIP / FRP / sustainment shaping quality + reliability load
- Quality function authority - independent of programme + reporting line to chief quality officer
- AS9100 + Nadcap + customer surveillance posture - audit history + Nadcap special processes on-site
- DCMA QAR + FAA + EASA engagement - daily oversight model + recent findings
- Reliability programme maturity - FRACAS deployment, MIL-HDBK-217 vs Telcordia vs FIDES practice, HALT / HASS adoption
Related roles
Sourced from
- SAE AS9100D + AS9102B + AS9145 + AS13100 aerospace QMS standards
- Performance Review Institute (PRI) Nadcap programme + audit handbooks
- MIL-HDBK-217F + MIL-HDBK-781A + MIL-STD-1629A DoD reliability standards
- Telcordia SR-332 + FIDES Guide 2022 reliability prediction methodologies
- AIAG MSA + FMEA Reference Manuals + ANSI / ASQ Z1.4 + Z1.9 sampling
- SAE ARP4754A + ARP4761 aerospace recommended practices
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