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Buzz on channels 2 and 20: diagnosis

Rendered from the working notes 03-diagnosis.md on 2026-10-11.

Diagnosis: buzz on channels 2 and 20, TRC, 2026-09-25

Written by the pane after reading 01-session-reconstruction.md in full, the GX4816 photos, the Radial Catapult manual (~/trc-studio-manuals/radial-engineering-catapult-rx4__24.pdf) and the electrical project findings. Confidence labels: high / moderate / low.

A. What the evidence pins down (fact, from the transcript)

  1. The buzz was heard on the Trident monitor path (amps next to the Trident, "all monitors, solo master"). So "channel 2" in tonight's tests is Trident channel 2, fed by the mix-room Catapult split. The same source line also feeds GX4816 input 2 through the mic-closet Catapult.
  2. The buzz needs THREE things present at once: (a) the Cat6 link between the mix-room Catapult and the mic-closet Catapult, (b) the XLR from the mic-closet Catapult output 2 into GX4816 input 2, (c) nothing else. It does NOT need GX power, the SLink to the SQ-7, or the SQ-7 on. (T2, T5, T6, T13, T25)
  3. Replacing the XLR patch (T8) and replacing the whole Cat6 run (T30 to T32) did not remove it. The original Cat6 passed a wiremap (T18).
  4. A source plugged straight into GX input 2 with the Catapult bypassed is clean (P7, T28). Trident channel 2 with the mic-closet side disconnected is clean (P1, P3 to P5).
  5. Channels 1 and 16 are clean on the very same path. Channel 20 behaves like channel 2, except pulling its XLR leaves a faint residue (T24).
  6. Unplugging GX aux outputs (to PAs, in-ears, monitors) changes the buzz inconsistently but never removes it (T9). Greg's body position near the rack makes it louder (T21). Catapult ground lift: no change (P10).
  7. Mic-closet Catapult output straight into a QSC powered monitor, no A&H in the path, also buzzed and stopped when the Cat6 was pulled (P15). Channel used in that test not recorded.

B. The mechanism that fits every observation (moderate-high confidence)

Common-mode noise converted to differential noise on two specific channels.

Why each observation fits:

Observation Fit
GX off, SLink out, SQ off, buzz stays passive phantom network still connects pins 2/3 to chassis
XLR into GX input 2 pulled, buzz gone removes the only chassis connection on that pair
Cat6 pulled, buzz gone removes the pair from the mic closet entirely
new Cat6 and new XLR, buzz stays the imbalance is not in a cable
direct into GX input 2, clean a mic is floating; no second ground, no common-mode drive
Catapult ground lift, no change lift breaks pin 1 only; the path is pins 2 and 3
GX aux outputs change it every aux load is another grounded device shifting the GX chassis potential
body near the rack makes it worse an unbalanced node is an antenna for electrostatic mains fields
ch 20 XLR pulled leaves a residue ch 20 shares its Cat6 with three other channels still tied to the GX; residual coupling inside the bundle
Catapult direct to QSC buzzes (P15) a powered monitor is a second grounded device exactly like the GX

Greg's "that nullifies my hypothesis" at 04:34Z was premature. The direct-into-GX test only shows the GX is quiet with one ground reference; it says nothing about how GX input 2 behaves with two.

B2. What the studio records add (from 02-system-model.md, all cited there)

C. Alternative causes, ranked

  1. Imbalance inside GX4816 inputs 2 and 20 (moderate). A&H inputs use matched phantom resistors; a hot-patch with phantom on or a static event takes one out. The phantom LEDs in tonight's photo look lit on some inputs in rows 1 and 2; if phantom is on at 2 and 20 and off at 1 and 16, that alone is a difference to test.
  2. Imbalance in the mic-closet Catapult channel 2 / 20 (moderate). Same symptom, different box. Cheap to discriminate (test 1 below).
  3. Ground potential difference is the driver in every case (high that it exists, given the IG finding). Even a perfect channel gets some buzz if the difference is large; channels 2 and 20 are just the worst. Fixing the bond (IG bus to service ground) lowers the whole floor.
  4. Phantom power from two consoles on one line (low-moderate). If the Trident or the SQ-7 has phantom engaged on 2 and 20 only, 48 V is being pushed through the passive split into the other console's input network, which is a DC ground-loop path on exactly those channels. Untested (T26 result missing).
  5. Split pair in the Cat6 termination (low). Would explain a single channel but not survival of a full cable swap; ruled out unless the silver cable was also hand-crimped.
  6. Noise source is a specific load (unknown). LED drivers, dimmers, Lorex camera PoE switch, the PA amps on the GX auxes, HVAC. The planned all-off test (T33) never ran.

Ruled out by the tests: the XLR patch cable, the Cat6 cable as a cable, the SLink, the SQ-7, GX power, the DPA snake, the wall panel, the mic and mic cable, the Trident alone.

D. Tests that decide it, in order (each under 10 minutes)

  1. Swap test. Move the mic-closet Catapult output 2 XLR into GX input 1, and Catapult output 1 into GX input 2. Buzz follows to the Trident channel of whichever line is in GX input 2 → the GX input is the asymmetric part (replacement or A&H repair is justified). Buzz stays on Trident channel 2 → the asymmetry is upstream in the Catapult path. Repeat with 20 and 16.
  2. Second grounded device. Plug mic-closet Catapult output 2 into a known-good grounded input (QSC, or a spare preamp) instead of the GX. Buzz present → Catapult/pair side. Absent → GX input.
  3. Meter the grounds. AC volts between the GX chassis and the Trident chassis (a long wire to the DMM), and between the ground pins of the two racks' outlets. Anything above about 50 mV AC is a ground difference worth killing; note the reading with lights and HVAC on and off.
  4. Temporary bond. Run a heavy wire (12 AWG) between the mic-closet rack and the Trident chassis. Buzz drops → ground potential difference confirmed; the permanent fix is the IG bus bond already recommended in the electrical project.
  5. Phantom audit. Read phantom state on the Trident, the SQ-7 and the GX LEDs for 1, 2, 16, 20. Turn all four off and listen.
  6. All-off test (T33). Original Cat6 in, buzz audible, kill circuits one at a time at the panels: lighting, HVAC, the PA amps, the camera/network switch. The circuit that silences it names the noise source.
  7. Isolate the split. Put a mic-level 1:1 isolation transformer on channel 2 between the Catapult output and the GX input (Radial TX4M/RX4M modules or a single inline iso). Buzz gone → permanent fix for every channel: replace the mic-closet RX modules with transformer-isolated ones, which is exactly what Radial builds them for.

E. Questions for Greg and Elijah

  1. Which console had phantom on for channels 2 and 20 tonight, and is it off on 1 and 16? (Trident switches, SQ-7 scene, GX PP LEDs.)
  2. In P15 (Catapult straight to the QSC), which channel number, and was anything else connected to that Catapult at the time?
  3. In P13 ("speaker directly on the A&H channel"), where exactly was the speaker connected?
  4. In T15 (Ethernet moved to other Catapult ports), did the buzz move to other channel numbers, stay on 2 and 20, or vanish?
  5. Which Catapult module and bank carries channel 20 on each end, and are 2 and 20 on the same Cat6 run or different runs? Elijah's "16 and 20 on the same route" does not match 4-channel banks.
  6. Which outlets feed the mic-closet rack and the mix-room rack, and are they IG (orange) outlets?
  7. Is the Cat6 between rooms shielded, with shielded plugs at both ends?
  8. Does the buzz change when the studio lights are dimmed, when HVAC cycles, or at a different time of day?
  9. Did the mains all-off test happen after 22:05 PDT, and what happened?
  10. Where is Elijah's paper test sheet?