Fingerprint

Why the numbers move

A leak is an orifice between the atmosphere and the manifold. With manifold pressure below about half an atmosphere the flow through it is choked, so it passes the same mass of air at idle, at 2,500 rpm and at a light cruise. That fixed mass is a big share of idle air and a small share of cruise air, which is why the correction shrinks with load. At WOT the manifold is close to atmospheric pressure and the leak hardly flows at all.

Because the leaked air never passes the MAF, the MAF reading falls short of the speed density estimate by the leak's share of the airflow. That is the second half of the fingerprint and the one that separates a vacuum leak from an exhaust leak, which moves the trims the same way but leaves the MAF honest.

The reference numbers

Computed by the model at build time: the fault at its clean reference size on a 2.0 l inline four, narrowband upstream sensor, with no noise.

Vacuum leak at reference size on a 2.0 L inline four, narrowband upstream sensor
ReadingIdle2,500 rpm, no loadCruiseWOT snapshot
Total trim bank 1 (%)+14.9+5.4+2.8open loop
Airflow check (%)879496100
MAF (g/s)2.637.2213.6983.76
MAP (kPa)30.022.042.097.0
Upstream B1S1switching, avg 0.45 Vswitching, avg 0.45 Vswitching, avg 0.45 V0.90 V steady
Downstream B1S2 (V)0.660.660.660.90
ECT (C)90909090
Misfire per 1,000 revs0000

Easy to confuse with

On a real car

TrimCase is a training aid built on a simulated engine model. It is not a diagnostic instruction for any real vehicle. Follow the service information for the vehicle in front of you.

Where the model is simpler than an engine

The model puts the leak on the common plenum, so both banks see it equally. A leak at one bank's intake runners would show on that bank more than the other.

The full model is on how the model works.

An example case

Case C-UA-0, clean tier. Open it in projection mode.

Case C-UA-0

Engine
2.0 L inline four, narrowband upstream sensor
Customer says
Rough or uneven idle when warm
Check engine light
Off
Tier
Single fault, clean

Warm engine, sea level, 100 kPa barometric pressure. Simulated data for training, not from a real vehicle.

Freeze frame

No code stored. Snapshot saved by the technician at warm idle.

Codes
None stored
Captured at
Idle
Engine speed
741 rpm
Vehicle speed
0 mph
Calculated load
17.4 %
MAP
29.6 kPa
MAF
2.51 g/s
ECT
89 C / 192 F
IAT
37 C / 99 F
Fuel system
Closed loop
STFT / LTFT bank 1
+1.7 % / +14.5 %

Live data by load cell

Scan data for case C-UA-0, one column per load cell
PIDIdle2,500 rpm, no loadCruiseWOT snapshot
Engine speed (rpm)741250120925000
Vehicle speed (mph)006045
MAP (kPa)29.621.742.197.0
MAF (g/s)2.517.0513.6383.59
Airflow check, MAF as % of speed density estimate (%) worked out859396100
Calculated load (%)17.414.533.585.8
IAT37 C / 99 F35 C / 95 F29 C / 84 F29 C / 84 F
ECT89 C / 192 F90 C / 194 F91 C / 196 F90 C / 194 F
Fuel systemClosed loopClosed loopClosed loopOpen loop
STFT bank 1 (%)+1.7-0.2+0.10.0
LTFT bank 1 (%)+14.5+5.1+2.6+2.6
Total trim bank 1 (%) worked out+16.2+4.9+2.7+2.6
O2 sensor B1S1switching, avg 0.44 Vswitching, avg 0.44 Vswitching, avg 0.44 V0.89 V steady
O2 sensor B1S2 (V)0.660.650.670.90
Injector pulse bank 1 (ms)4.453.497.0920.13
EVAP purge command (%)020350
Misfire count per 1,000 revs0000

Rows marked worked out are arithmetic on the rows above them, done for you: total trim is STFT plus LTFT, and the airflow check divides the MAF by the speed density estimate on the model page.

Trim against airflow

Total fuel trim by load cellBank 1: Idle +16.2 percent, 2500 +4.9 percent, Cruise +2.7 percent. The shaded band is plus or minus 5 percent, the usual healthy range.-20-100+10+20Idle2500CruiseTotal trim, percent. Airflow rises left to right.
Bank 1Shaded: plus or minus 5 percent