TITLE: 08/07 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
SHIFT SUMMARY:
Dust levels for H1:PEM-CS_DUST_LAB1_300NM_PCF is climbing up to 70,000 counts today. I imagine that the Dust level is goign to continues to rise with the wind this weekend.
Input Alignment team has a PLAN, which is a simple matter of just walking the mirrors.
Output Arm team has been looking for MAXIMUM_POWER through their straws in HAM7, Note: Removed yellow View Port cover and left a guillotine in place on HAM6 & Misaliging SR2 & SR3.
VAC team reports: "Cryo Traps are open to the Beam Tubes." & "The Corner station is still isolated from the Beam tubes."
End Station Y had it's PCAL Integrating sphere returned today after it was stolen for some lab measurements last night.
LOG:
| Start Time | System | Name | Location | Lazer_Haz | Task | Time End |
|---|---|---|---|---|---|---|
| 14:53 | FAC | Kim | LVEA | n | Technical cleaning. | 15:35 |
| 15:30 | VAC | Jordan | LVEA | n | Taking pics of GV6 status | 16:00 |
| 17:12 | SQZ | Sheila & Ryan S | LVEA | YES | Power measurements In HAM7 | 19:42 |
| 18:29 | VAC | Jordan & Mitchel | LVEA | y/n | opening ION pumps in the LVEA | 19:14 |
| 19:49 | PCAL | Tony, Cory | PCalLab, EY | YES | Taking Ey's PCAL Sphere back to EY's Laser Enclosure. | 21:05 |
| 20:01 | FAC | Tyler +1 | EY | - | Wellhead work | 22:01 |
| 20:24 | CDS | Marc, Caroline | CER | - | Swapping ISC power supply | 21:04 |
| 20:26 | PEM | Carlos, Shrey, Miranda | Overpass | - | Seismometer tests | 22:26 |
| 20:37 | VAC | Jordan | LVEA | - | Opening/closing GVs | 22:25 |
| 21:08 | SQZ | Sheila & Ryan | LVEA HAM7 | YES | Power Budget measurments & Beam Profiling | 23:08 |
| 22:09 | CDS | Dave | CER | N | Looking at the accelerometer.... Specifically Not Touching it | 22:25 |
| 22:35 | CDS | Dave Miranda | CER | N | Checking on more accelerometer chassis cabling | 23:15 |
| 22:43 | VAC | Jordan | LVEA HAM6 | yes | Isolating turbo pumps, and turning on the ION pump in HAM6 | 22:54 |
Both End Stations had their PCAL Reciever modules pillaged for Integrating spheres. They were taken to the lab and measured against PS4 on the lab bench for the first time in..... at least 4 years.
Preliminary Results found here: PSEYRX
And Here: PSEXRX.
Set up notes:
python pcalRRSO4_measure.py \
-DN1 PSEXRX \ <-Power Sensor from EX's Receiver side.
-DV1 8018023 \ <- This KVM is getting the signal that we usually get a temperature signal from.
-DN2 PS4 \ <---- this is nominal
-DV2 8002111 \ < - nominal
-DT2 1421891 \ <-nominal
-a yes \
-x \
-log 'PSEXRX_PS4 PSEXRX front track PS4 on the rear track' \
These measurements were ran without a temperature measurement as they do not have an AD590 to read from. But rather the script just assumes the temperatures for both spheres are the same and just used PS4 temperature sensor.
I used the PS5 Kit to set them up (Satelite box, cable, & accessories.) plugged in exactly the way I'd set up PS5.
Read the Voltage off of what would normally be the temperature KVM as it is nominally plugged in. The reason for this is because I was surprised to see that the KVM that we would normally get temperature signals from PS5 with would change voltage readings when the Sphere was exposed to Laser light.... I Also noted that this Temperature KVM had a Higher voltage reading that the normal KVM we would use to read the voltage from PS5 . Infact the normal Voltage KVM is half of the voltage read by the Temperature KVM. So I chose that one for a better signal to noise ratio. Is this the correct value. I'm not sure yet. but we will find out.
I ran this over night running multiple measurments.
Another Note: The PCAL Laser Chassis at End X has been showing a Red LED that is not normally red and Labeled "I limit" or "l limit" either way. The First time I saw it was right after a power outage so i thought it was just a weird one off sort of situation. I just powered the laser Off and back on again and the LED went away.
But I saw it had happened again yesterday, and power cycling the Chassis did NOT resolve it. I checked the MEDM screen and saw that H1:CAL-PCALX_LASERDIODECURRENT was jumping around 9.7-10.0 Amps. So I simply changed the voltage a little and brought the voltage back up and it resolved the issue. l limit was no longer lit. Checking on it today and it seems to still be functioning normally now.
All spheres are now back in their Nominal configuartion.... bolted to the IFO.
Ryan S, Sheila
In summary, after removal of the A:L2 apperture stop we still see about 4% extra losses in HAM7. We searched for the rejected beam from SFI1 in both directions with lights out, IR card, and viewer. To explain a few % loss we should expect to have 10-20urad in this beam, which should be visible with lights out an a viewer. We also noticed that the beam is off in yaw at the location where we had an iris after ZM1.
Since Ryan and Camilla aligned the beam onto the SQZT7 PD yesterday, we are noting the power on that PD here after each measurement so we can use that to account for fluctuations in power out of the OPO.
From the control room, we dithered ZM2 + ZM3 and tried to reduce the fluctuations in the SQZT7 IR PD, we were able to recover a 4% of power this way, with fairly small adjustments (+9urad ZM2 P, +19 urad ZM2 yaw, 5 urad ZM3 yaw).
One more round of power measurements:
After all of this power budgeting, OPOS rebalancing, ZM4 PSAM preloading adjustments, and alignment, this afternoon I took another (possibly the last?) ZM4/5 PSAM M^2 grid on SQZT7. Data files attached. I used different strain gauge values for ZM4 than in the past since they've shifted with the preloading change, but this still covers pretty much the whole PZT range.
This was a 26-point grid using the following PSAM strain gauge settings:
ZM4 PSAMS = [-2.6, -1.0, 1.0, 4.0]
ZM5 PSAMS = [-8.0, -6.75, -5.5, -4.5, -3.3, -1.0]
The attached plot shows the qs measured on SQZT7 propagated to SRM, with three different ZM4 preloads. Camilla has summarized the history of our ZM4 + ZM5 preloading in 91404
The blue points here are with 75 in lbs on ZM4, as adjusted in 75677. The teal points were after an attempt to lower the pre-load to 65 in lbs, which Rahul and Camilla later rechecked with the torque wrench and thought that it went to something between 40-60 in lbs. ( 91416)
On Wensday, Rahul and Camilla believed that they applied more torque to the psams (91416), but somehow the beam profiles that Ryan took show that the preload was reduced instead.
We did not repeat the OMC scans at this preload. The M^2 range is similar to previous measurements, but the astigmatism is a little better here.
K. Kawabe, E. Capote, L. Dartez
This log covers work that started yesterday. We set out to scan the IM1 pointing to see if we could find evidence of clipping and to potentially identify a preferred input pointing configuration. We applied a dither to the IM1 and IM3 suspensions to use IM4_trans and the ISS second loop QPDs as sensors. This test was laborious because each new IM1 pointing mis-centered the beam on both QPDs. Keita pointed out that we can use IM2 and IM3 to center the beam on the IM4_trans and ISS second loop QPDs, respectively. Moreover, by centering the beam on IM4_trans and the ISS second loop QPDs, we get the beam for free on the POP QPDs (even though it is not centered there). To support the argument that we can arrive on a pointing now that will be relevant once we open the arms, we note that the QPD NSUM levels for the IM4_trans, ISS second loop, REFL WFS A and B QPDs are all consistent with what we had in O4 at 2W. The NSUM levels of the POP QPDs is consistent with what we had in O4 at 2W straight shot (PRC misaligned) as well. During this test we paid particular attention to avoid moving the input alignment to a spot that would have the RMs near their actuation range to keep the beam centered on the REFL QPDs.
For each IM1 pointing trial we did the following:
1. Move IM1 alignment to new trial position
2. Walk the alignment of IM2 and IM3 to center the beam onto IM4_trans QPD and the ISS Second Loop QPD (within about 0.04 in PIT and YAW). I used IM2 to center the beam onto IM4_trans and IM3 to center it onto the ISS Second Loop QPD.
3. Check that the beam hasn't fallen off of the REFL PDs or the POP PDs and that the NSUM, PIT, and YAW signal values are at roughly the same values as they were before the IM1 adjustment.
4. Run the DC centering loops to center the beam on the REFL PDs and ensure that the RMs are not close to their actuation range.
5. Measure the transfer function from the IM1 and IM3 DAMP banks to the IM4_trans and ISS second loop QPD SUM channels while injecting an 8Hz excitation into the IM1 and IM3 SUS TEST banks.
The IM1 trials we tried are as follows:
Nominal position (the IM1 position when we began): 524.2 / -386.6 (P/Y)
Trial 1 (pink): (+30 uRad Yaw): 524.2 / -356.6 (P/Y)
Trial 2 (brown): (-50 uRad Yaw): 524.2 / -436.6 (P/Y)
Trial 3 (green): (-10 uRad Yaw): 524.2 / -396.6 (P/Y)
Trial 4 (blue): (+40 uRad PIT): 564.2 / -386.6 (P/Y)
Trial 5 (red): (-40 uRad PIT): 484.2 / -386.6 (P/Y)
The five trials for this test were split across two days. And the excitation amplitude was not necessarily constant across all 5 measurements. This made it difficult to compare today's measurements against yesterday's. In any case, we think that the position at Trial 4 is the best one so far in that it shows the lowest coherence between the dither at IM1/IM3 and the IM4 trans QPD. We do not know or think it is unilaterally the best position, but we think it is better than it was before we started this. We won't know more until we have the arms.
The new slider values for IM1, IM2, and IM3 are in IM_alignment_sliders.png. A screenshot of the TFs we took is at blueisgood.png. The colors of the traces correspond to the color next to each trial listed above. The blue trace has the best coherence for most of the measured transfer functions (and for all of the IM4_trans measurements). The DTT template we used can be found at ~keita.kawabe/IM1_moves_IM4_trans_ISS_QPD.xml.
Per WP 13497
I opened IP1/2/3/4 to the corner volume at 18:38 UTC / 11:38 PDT
GV8 Soft closed at 20:47 UTC / 13:47 PDT
GV7 opened at 21:20 UTC / 14:20 PDT
GV5 opened at 21:48 UTC / 14:48 PDT
Both GV5 & GV7 opened between 45-50 psi, and the holding pressure is set to 55 psi.
GV6 and GV8 will remain soft closed to isolate the beamtubes. CP1 and CP2 are now open to the corner volume to assist with the water pumping, water is still the dominant gas after ~22 days of pumping, see corner RGA scans in alog 91446
Corner pressure is decreasing as expected.
I've moved PR3 back to latter half of O4 based on the slider, not OSEM.
Assuming that the ITMX angle is good and the beam deflection angle through the BS is the same as before, the plan to get ready for the arm peeking is as follows.
Find a good IM4 angle where the ITMX reflection comes back to ISCT1 camera (Louis is working on it).
Once that's found, align PRM, refine PRM and IM4 alignment to have a good PRX flash.
After that we might have to walk the beam on PR2 without touching ITMX and PR3. Unless there's a convenient script to do that, you'll move IM4 a bit, change PR2 so that ITMX retro reflects, and change PRM to recover PRX.
By iterating, you'll eventually settle on the beam position on PR2 that will give you an ok signal on LSC or ASC (hopefully both) POP sensors in HAM1.
Also work on the ISCT1 alignment for the ALS beam, but this will be on Monday.
The following supplies were replaced in the CER Mezanine.
Kepco Power Supply in VDD-C6 Rack, Left Slot U31-29, ISC-R3&R5 +24V
Old S12001945
New S12001992
Kepco Power Supply in VDD-C6 Rack, Right Slot U31-29, ISC-R3&R5 -24V
Old S1201946
New S1201947
The negative supply was oscillating between 22V and 21V when measured before replacing, possibly due to failed fan. New supplies were adjusted to +/-24V at the racks.
Caroline C, Marc P.
This morning JAC lost lock due to temperature drift (temperature control was on) and at the same time WFS went crazy. After that JACK_LOCK guardian couldn't lock it, just kept scanning without success because the alignment was very much off.
When this happens, what you should do is:
For the lockloss and WFS behavior see jac_lockloss.png.
JAC lock voltage was drifting lower and lower, which meant that you must have cooled JAC down, but the temperature servo was heating it more. Ultimately we need a temperature servo to keep the lock PZT voltage constant rather than keeping the temperature sensed by the thermistor.
After the lock voltage alredy hit the bottom rail, it took about a minute for JAC to completely lose it. During this time, JAC_L error increased as the JAC slowly became off-resonant, and of course the same signal is seen by all WFS segments. Since WFS centering is not perfect, this increased WFS P and Y signal. JAC ASC tried to counter this by twisting JM1 and the PZT mirror without success.
Finally the WFS was turned off but mirrors were already heavily misaligned at that point.
RGA scans were collected for the corner volume using the new PrismaPro RGA. This RGA tree had been rebuilt and baked at high temp for 2+ weeks. Scan info below, raw data files will be posted to the DCC at T2600329.
RGA Model: Pfeiffer Prisma Pro
EM Voltage: 1200V
Dwell Time: 1s, 0-100 AMU, 10 pts/AMU
Valve States: GV5 & GV7 closed, FC2 & FC4 closed (Relay Tube removed & FCB-1 section common with corner)
Pumping: 3x 2000 l/s Turbo pumps, 1x 500 l/s turbopump (HAM6)
RGA filament has been on since 7/22 after RGA tree bakeout
Corner Pressure (8/7/26): 3.2E-7 Torr (PT120B)
Corner Pressure (7/27/26): 5.3E-7 Torr (PT120B)
Comparison plot showing partial pressure decrease after an additional ~10 days of pumping with turbo. Corner started high vacuum pumping on July 16th 2026 (22 days of pumping with turbopumps only)
Dave, Erik, Claude
Claude AI wrote a python script to plot the H1 DAQ CRC rates for the past 6 months for all frontend and both DAQ legs (see attached). This plot only shows when an individual DAQ leg recorded a CRC error from the front end. The times there were CRCs on both legs were usually due to model restarts and not spontaneous errors, so these have been removed from the plot.
The vertial lines align with Tuesdays and possible maintenance activities.
General first thoughts are: over the long term the CRCs are fairly randomly distributed over front ends and DAQ legs; in the past week they have been concentrated on the 0leg and the two frontends iscey, seib1.
TITLE: 08/07 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Planned Engineering
OUTGOING OPERATOR: None
CURRENT ENVIRONMENT:
SEI_ENV state: CALM
Wind: 3mph Gusts, 1mph 3min avg
Primary useism: 0.01 μm/s
Secondary useism: 0.06 μm/s
QUICK SUMMARY:
I came in this morning to a Vacuum Alarm on H0:VAC-EX_X2_PT524_PRESS_TORR. Wait! Dont panic! Vac Team had already put in an alog about it.
Other than that Every thing looks good.... EXCEPT: the RMS 1 & 2 are saturating for some reason. Tagging SUS
This started to happen at a round 7 UTC . I took those Suspensions to Safe.
These Saturations were caused by the DC Centering Loops being turned on about 10 seconds after the IMC unlocked. They ramped up and started to saturate the suspensions all night. The solution was to kill the DC centering loops AND clear the History.
Found PT524B cold cathode gauge tripped/off, turned it back on, now we wait for it to comeback. Gauge was tripped yesterday around 23:49 utc.
This alog was intended to be a comment on 91436
This morning we continued to use the crane that Camilla and Ryan devised to try to get more reliable power budgeting measurements on the VIP. Our previous measurements with the power meter held in a hand and hovering over the table consistently showed that we have something like 4% extra losses in HAM7, but they have not been repeatable enough for us to track down the location of the losses. The crane set up helps us set the angle of the beam profiler head by using a clamp on the post, and also gives us much more steady measurements of power, so we were able to make some progress in identifying the location of losses. However, we think that the power out of the OPO was drifting by 1-2% during these measurements, which makes the measurements less reliable for finding losses.
We do think that we have about 0..8% loss at B:L2, where the difficult to align apperture stop is. This apperture stop catches a rejected beam from B:P1 which is scattered light from the interferometer, so we need to keep it. We looked for space to move it off the lens mount onto it's own separate mount, but the platform is very crowded with bases and dog clamps in this area, so that would not be an easy solution.
For the naming of optics see: D2000021
The UPS for the EY Access system that powers the network switch a camera failed this afternoon. Power to the cameras and switch was bypassed for now.
Jenne, Wanda, Shoshana, Gizem
We started very early this morning to beat the heat, and performed 'tap tests' at various points along the length of the arms to identify positions along the length of the fiber (according to DAS) with GPS positions (according to Wanda's phone).
Spreadsheet attachment is information about where along the fiber Shoshana and Gizem identified our tapping in the data, and associated time stamps. I've also copied the spreadsheet data to a google sheet, so that we can add to it.
We tried to do more dense taps on the 'inside of the vertex' side of the arms, where the fiber actually is. This required some walking out in the sand along the arms, so we had sun hats and knee-high boots and plenty of water. We also did a few taps along the road during our drive back, to get some more coarse information along the length of the arms. At the Xend station, there were too many tumbleweeds for us to walk along the inside-vertex side of the arm, so there at EX we did our more dense taps along the road side, with the exception of the EX vault location.
In the attached photos, you can see some examples of our tap test method. Gerardo provided us with a scrap piece of steel that we used as a strike plate. We also borrowed a sledgehammer from the mechanical / vacuum parts lab. For most of the Yarm, we only did 3 heavy strikes and Gizem and Shoshana chose the strongest signal from that as our time. Once we were on the road-side of Yarm, and then for all of Xarm, we added some light tapping that seems to have helped identify which distance bin (called a "channel" in DAS terminology) we were closest to. The photos are also labeled with X/Yarm, and position number, which corresponds to the position numbers in the google sheet - I tried to capture features in the photo to help identify where exactly the strike plate was.
Wanda has added to the google sheet the GPS locations that she identified while we were at each tap point.
The last photo shows our used (but can be used again in the future!) strike plate.
I have attached some screenshots which show what the referenced path looks like for the x-arm. Further, it demonstrates how the optical metres of the fibre are now referenced to a certain co-ordinate. With this, we can now correlate any events that we detect to a physical location. In this software, a straight line is drawn between two referenced points. In picture 1, the whole arm is shown. In picture 2, it is zoomed in on the area around the corner station, showing the limitations in our technique as it is relatively rough considering we know the fibre is curving at this point. In picture 3, we see how hovering over the waterfall plot will produce a red point in the refenced fibre showing the location of this channel.
And here are some more pictures of the georeferencing.
Travis, Gerardo, Jordan
During the closing of GV6 back in May, we noticed that there was some blow-by in the pneumatic system when trying to hard close the valve, see alog 90093.
We were able to hard close the valve eventually but as preventative maintenance we wanted to replace the air cylinder seals, similar to GV7.
Prior to disassembly we measured the locations of the reed switches from the top surface of the bottom plate to the bottom surface of the reed switches:
Bottom Switch: 1 1/8"
Top Switch: 49 1/4"
We then disassembled the air cylinder and replaced the seals following procedure/notes collected during the GV7 repair. During cleaning of the old grease on the piston head, we noticed there were two burrs on the top of the piston, we did not notice any damage to the inside of the cylinder, but as a precaution we used a small flat file to remove the burrs. We also chased the threads on the four threaded rods with a die to aid with reinstallation. After cleaning and inspection of the cylinder tube, we found no issues or damage so we decided to continue to use that cylinder and keep the new one as a spare.
No other issues encountered, we removed the old seals, cleaned the grooves, added copious amounts of the supplied grease to the o-rings, seals and the inside of the air cylinder, and then re-assembled the cylinder tube. Pictures posted below and a final procedure is in progress and will be posted to the DCC.
We did not get a chance to cycle the valve after the seal replacement, so we will continue tomorrow with cycling the valve.
We were unable to fully open GV6 today after the cylinder repair. We heard the clunk of the gate camming over at 45 psi, but it did not start to raise until 55 psi, at which point we could hear air blow-by at the solenoid manifold, and up at the cylinder itself.
So we stopped trying to open the valve any further and slowly reduced the regulator output in order to bleed out the accumulated pressure on the bottom side of the piston. This lowered the gate back down and we heard the gate touch down indicating it is soft closed.
We will have to disassemble to air cylinder again and see what may be the issue. We still have 4 sets of replacement seals and one brand new air cylinder on hand if needed.
The valve remains soft closed until we are able to troubleshoot and repair the cylinder.
8/3/2026
Travis, Gerardo, Jordan
Today we again disassembled the GV6 air cylinder with the valve soft closed to try and see what may have been causing the air blow-by which prevented us from fully opening the valve last week.
We did not find anything immediately obvious such as a seal that had jumped out of the groove, so we measured the ID of the original air cylinder, which was re-used, and found that it was ~0.01" larger than the ID of the spare cylinder (original ID ~8.015", spare ID ~8.005"). We then elected to use the spare cylinder instead to make sure there is good sealing contact with the cylinder wall, so we re-distributed the grease on the new cylinder and attempted to install over the piston, but the tube seemed to be slightly out of round and would not fit over the piston. So we flipped the tube 180 degrees and measured that side of the tube and found it was better. We again added grease to that side of the cylinder and installed it over the piston, ensuring the seals and wear band stayed in place, Then we re-installed the threaded rods, torqued the nuts, installed the reed switches and installed the air lines.
To verify all the new joints/connections were ok, we put ~10 psi to the top of the cylinder and then to the bottom to see if there were any leaks. There were none so we started to open the valve by increasing air pressure at the regulator, once we got to ~25 psi we could hear and feel air coming out of the bottom plate/adapter flange below the cylinder assembly, see picture below the area where air is coming out of is circled in red, at which point we stopped trying to open the valve and closed the quarter turn isolation valve to the air line.
We spoke with a GNB rep who advised we try to to open at a higher pressure and see if the bottom seals, so we then tried to open the valve again. This time we started at 20 psi and followed our normal opening procedure with the exception of increasing by 5 psi instead of 10 and waiting 3 minutes between increases. At ~35 psi, air stopped leaking out of the bottom flange, there was no air blow-by in the cylinder and we could hear the carriage starting to move. The gate fully opened at ~48 psi and Gerardo was able to take a video where you can hear the piston incrementally move up the cylinder. We increased the holding pressure to 58 psi and verified the MEDM screen showed the valve status as green.
8/6/2026
This morning we wanted to soft close GV6 to see if the scraping/squeaking sound continued, or if grease just need to be distributed in the cylinder. Following our normal soft close procedure,we still heard the same noise as the piston moved down.
We decide to swap the cylinder one last time to the spare cylinder which removed from GV7 back in May. This cylinder had an ID of 8.004" on both ends.
During the removal of the "sticky" cylinder, we saw there were some small metal shavings on top of the piston, so we decided to remove the seals and install new ones to make sure there is no damage or debris that could cause sealing issues. We added grease to the new seals/o-rings, and the inside of the cylinder, then re-assembled the cylinder/threaded rods/nuts.
An updated cylinder repair procedure in the works at E2600176.
Once we were done with the cylinder assembly we opened the gate valve to test functionality, and see if there were any leaks in the cylinder. We again heard air coming out of the bottom flange, same as the entry above, but once we got to 35-40 psi the leak stopped and we could hear the carriage moving up. This time there was no excess noise or dragging, and the valve fully opened at 48 psi. After of ~10 minutes with the valve open, and we confirmed there were no leaks in any of the newly assembled joints, we soft closed the valve, again there was no excess noise or dragging of the piston. This is what we typically see/hear when actuating the pneumatic valves.
GV6 remains soft closed for now, closing WP 13471
(Jordan, Travis, Gerardo)
We removed and replaced the AIP for BSC6, no real complications while doing the work. However the joint at the AIP and the isolation valve has a tiny gap towards the bottom, we started pumping down on the system and it appears to be a solid union, we will go and visit tomorrow and see how the pressure is doing. On a side note we did find a flex metal hose that has a leak, it has been removed from circulation.
After checking on the pumpdown progress at BSC6 annulus system, the rest of the components were put back, controller was reinstalled, cables were connected (power supply, high voltage, and comms cable) and the annulus ion pump was powered on, it did not take long to reach good vacuum pressure. Aux-cart and can turbo will continue to pump the annulus sytem until it reaches an acceptable vacuum pressure.
(Travis S., Jordan V., Gerardo M.)
Late entry.
After a few days of pumping down the annulus system, on Monday 8/3/26, the can turbo and the aux-cart were removed from the annulus system at BSC6, the ion pump and annulus system are back to nominal.