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FMEA โ€” Failure Mode and Effects Analysis

A complete interactive FMEA guide: RPN calculator, Severity/Occurrence/Detection ratings, a sample FMEA table, DFMEA vs PFMEA, the modern AIAG-VDA Action Priority (AP) method, Fault Tree Analysis (FTA), complementary tools (Fishbone, 5-Why, Pareto, 8D), and the key FMEA standards.

๐Ÿงฎ RPN Calculator
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RPN = S ร— O ร— D ยท Maximum = 1000 ยท Action threshold: RPN>100 (general) / >50 (safety)
โš ๏ธ RPN Limitations โ€” why AIAG-VDA 2019 dropped it
Problem 1: S=9ร—O=1ร—D=1 = RPN of just 9 โ€” but S=9 (life-threatening!) must always be addressed; a low RPN "hides" this.
Problem 2: S=2ร—O=5ร—D=5 = RPN 50 โ€” the same number can arise from many completely different combinations.
Problem 3: No clear breakpoints โ€” RPN 99 vs RPN 101 aren't really different, yet a "threshold of 100" treats them differently.
The modern solution: AIAG/VDA Action Priority (AP) โ€” see dedicated tab. High S = mandatory action, regardless of O/D!
๐Ÿ“Š Severity (S) โ€” impact severity
SDescriptionExample
1No effectCosmetic change only
2-3Slight โ€” customer notices occasionallySlight noise, peeling label
4-6Moderate โ€” performance degradationPartial function loss, delay
7-8High โ€” loss of functionProduct failure, return
9Critical โ€” safety without warningPossible hazardous failure
10CatastrophicCertain hazardous failure
โš ๏ธ S cannot be reduced by controls โ€” only a design change lowers S! S=9-10 = a design red flag that always demands attention.
๐Ÿ“Š Occurrence (O) โ€” failure occurrence frequency
ODescriptionApprox. Cpk
1Almost impossibleCpk>1.67
2-3Rare โ€” well-controlled processCpk 1.33-1.67
4-6Occasional โ€” reasonable processCpk 1.0-1.33
7-8High โ€” unstable processCpk 0.67-1.0
9-10Almost certainCpk<0.67
Lowering O: process improvement, Poka-Yoke, design change. Based on real historical data/Cpk โ€” not subjective estimation!
๐Ÿ“Š Detection (D) โ€” ability to detect before reaching the customer
DDescriptionDetection Method
1Certain detectionPhysical Poka-Yoke โ€” cannot assemble incorrectly
2-3High detection100% automated inspection
4-6Moderate detectionStatistical inspection (SPC), sampling
7-8Low detectionVisual inspection, operator-dependent
9-10Almost undetectableNo control, only found in the field
โš ๏ธ Note the reversed direction! D=1 = excellent detection (good). D=10 = not detected (bad). Improving D is cheaper than improving O โ€” but preventing is better than detecting.
๐Ÿ“‹ Sample FMEA Table โ€” Shaft Bearing
IDFunctionFailure ModeEffectSCauseOControlsDRPNAction
1.1Shaft supportBearing wearNoise, vibration, shaft failure7High load/speed3Vibration check5105โ†‘lubrication frequency
1.2Shaft supportCage failureShaft seizure9Sudden overload2Visual inspection7126โ†‘C/P, โ†“load
1.3Shaft supportCorrosionDimensional growth5Moisture, lack of lubrication4Annual inspection480Grease upgrade
1.4SealingOil leakEnvironmental hazard4Seal wear5Visual inspection360Routine monitoring
๐Ÿ“ Full FMEA Form Structure โ€” all required fields
Identification: Item number ยท Function ยท Requirement
Failure: Potential failure mode ยท Effect on customer ยท Severity (S)
Cause: Root cause ยท Failure mechanism ยท Occurrence (O)
Current control: Prevention control ยท Detection control ยท Detection rating (D)
Calculation: RPN (or AP) ยท Priority ranking
Recommended action: Responsible person ยท Target date ยท Action taken ยท New S/O/D after action
DFMEA โ€” Design FMEA
Examines the design โ€” before the part physically exists.

Asks: How can the design itself fail? Wrong material, incorrect tolerance, unexpected load, stress concentration.

Performed by: Design engineer, during development โ€” before production!
Output: Affects material selection, GD&T, geometry.
PFMEA โ€” Process FMEA
Examines the manufacturing process โ€” how the part is actually produced.

Asks: Where in the process (machining/assembly/inspection) could a failure occur? Worn tool, wrong machine setting, operator error.

Performed by: Process/manufacturing engineer, before series production starts.
Output: Affects the Control Plan, inspections, in-line Poka-Yoke.
๐Ÿ”— The link between DFMEA and PFMEA
DFMEA precedes PFMEA chronologically. Critical characteristics identified in DFMEA (Key Characteristics) become mandatory control points in PFMEA. Both documents are living โ€” updated with every design/process change and field failure.
๐Ÿ†• AIAG/VDA 2019 โ€” Action Priority (AP)
The new standard (2019) replaces the raw RPN calculation with a decision table: High / Medium / Low โ€” based primarily on S, then O, then D.
SODAction Priority
9-104+anyHigh
9-102-35+High
9-102-31-4Medium
7-84+anyHigh
7-81-3anyMedium
1-61-31-3Low
โš ๏ธ The key difference: S=9 with low O still comes out High โ€” it doesn't "hide" behind a low RPN number like in the old method! This is the main reason for the switch.
High โ€” action mandatory
A documented corrective action is required. If no action is taken, a written, reasoned justification is required.
Medium โ€” action recommended
Action recommended at the team's discretion. Documenting the decision (act/don't act) is still required.
Low โ€” no obligation
Can be left as-is, but continue monitoring. Doesn't mean "safe" โ€” only that relative priority is low.
๐ŸŒณ FTA โ€” Fault Tree Analysis
โ–ธ FTA method: from the top failure โ†“ down to basic causes (Top-Down)
โ–ธ FMEA method: from a component โ†‘ up to system effect (Bottom-Up)
โ–ธ Gates: AND = both ยท OR = either
โ–ธ P(AND) = Pโ‚ ร— Pโ‚‚ (independent)
โ–ธ P(OR) = 1-(1-Pโ‚)(1-Pโ‚‚)
โ–ธ MIL-STD-1629A: military/defense FMEA standard
โ–ธ IEC 60812: civilian FMEA standard
โ–ธ AIAG/VDA FMEA: automotive, 2019+
โœ… Criticality Levels (MIL-STD-1629)
CategoryDescriptionMin SF
I โ€” CatastrophicDeath/severe injury/system loss4-10
II โ€” CriticalInjury, major mission damage3-6
III โ€” MarginalMinor injury, delay2-3
IV โ€” MinorInconvenience only1.5-2
๐ŸŒณ Sample Fault Tree โ€” oil supply failure
Top Event: Oil supply failed
  โ”œโ”€ OR โ”€โ”ฌโ”€ Pump failed
        โ”œโ”€ AND โ”€โ”ฌโ”€ Motor failed
                โ””โ”€ Backup not activated
        โ””โ”€ Filter clogged
        โ””โ”€ Pipeline cracked
OR gate = any single branch is enough to cause the overall failure. AND gate = both branches must occur together โ€” true redundancy!
๐ŸŸ Fishbone / Ishikawa
Maps root causes across the 6M's: Man, Machine, Method, Material, Measurement, Environment. Systematic โ€” doesn't get stuck on the first suspect.
โ“ 5-Why
Ask "why" until you reach the true root cause โ€” usually 5 times. Trap: "operator error" is almost never the root โ€” why did the system allow it?
๐Ÿ“Š Pareto Analysis
80% of problems come from 20% of causes. Focuses where to invest โ€” by cost, not just count!
8๏ธโƒฃ 8D Problem Solving
D1 Teamโ†’D2 Descriptionโ†’D3 Containment (24h!)โ†’D4 Verified root causeโ†’D5 Corrective actionโ†’D6 Implementationโ†’D7 Systemic preventionโ†’D8 Recognition.
๐Ÿ”— When to use which tool?
SituationRecommended Tool
New product/process design (preventive)DFMEA / PFMEA
Recurring fault, cause unclear5-Why โ†’ Fishbone
Many defect types, unsure what to tackle firstPareto Analysis
Formal customer complaint (automotive/aerospace)Full 8D
Severe safety failure, multiple failure pathsFTA
StandardDomainNotes
MIL-STD-1629AMilitary/aerospaceThe historical standard โ€” Criticality Analysis (I-IV)
IEC 60812General civilianThe official international FMEA standard
AIAG/VDA FMEA (2019)AutomotiveReplaces RPN with Action Priority. Mandatory under IATF 16949
ARP5580Aerospace (SAE)Based on MIL-STD-1629A, updated
AS9100Aerospace โ€” QMSRequires FMEA as part of risk management
Choose the standard per customer/industry requirement โ€” most automotive today has moved to AIAG/VDA 2019, while aerospace still moves between MIL-STD-1629A and ARP5580.