Sounds like the Big 14 list is on the way 
And thanks to James Oberg....
What’s the list of “Big 14” International Space Station EVA Tasks?
(Excerpt from Increment Definition and Requirements Document)
ISS critical maintenance tasks as follows. This list is not in order of priority. The criteria for tasks being added to this list are that the failure of the function provided by the ORU causes a situation placing the ISS in a configuration that is zero tolerant, or effectively zero fault tolerant, to survival.
1. Maintain ISS Primary Electrical Power System (EPS) Survivability
a. External (EXT) Multiplexer/Demultiplexer (MDM) Remove and Replace (R&R)
b. Battery Charge/Discharge Unit (BCDU) Backout
c. Main Bus Switching Unit (MBSU) R&R
d. Sequential Shunt Unit (SSU) R&R
e. Direct Current Switching Unit (DCSU) R&R
f. R&R of DC to DC Converter Units (DDCUs) 1A, 1B, 2A, 2B, 3A, 3B, 4A, 4B, S01A, S02B
g. Solar Array Wing (SAW) Manual Positioning
h. Pump Flow Control Subassembly (PFCS) R&R
i. Photovoltaic Controller Unit (PVCU) MDM R&R
j. R&R of External Remote Power Control Modules (RPCMs) S01A_C, S02B_C, S01A_A, S11A_D, S02B_A, and P12B_D
2. Maintain ISS Thermal Control System (TCS) Survivability
a. Interface Heat Exchanger (IFHX) R&R
b. External Thermal Control System (ETCS) Pump Module (PM) R&R
c. Flex Hose Rotary Coupler (FHRC) R&R
d. Ammonia (NH3) Leak Isolation and Recovery
The DDCUs listed provide power to the ORUs on this list. The RPCMs listed provide power to the EXT MDMs and ETCS PMs). The loss of these Secondary Power System (SPS) ORUs would be equivalent to the loss of function of the downstream ORUs themselves. Thus these SPS ORUs are critical to ISS survivability. All other ORUs on this list either receive power from ORUs already on this list (e.g. PVCU MDM receives power from DCSU) or does not require power (e.g. FHRC or NH3 Leak Isolation and Recovery).
For additional information on these systems, visit:
http://www.nasa.gov/pdf/167129main_Systems.pdfWhat is the cost of each PM ORU?
TBD
What are the actual dimensions of PM ORU?
Each pump module weighs 780 pounds and is 5 ½ feet long (69 inches) by 4 feet wide (50 inches), and is 3 feet tall (36 inches).
Number of electrical connections required for R&R?
The spacewalkers will need to disconnect and reconnect five electrical connectors, four fluid quick-disconnect devices, one fixed grapple bar and four bolts.
Describe functions of two jumpers crew put in place?
Contingency jumper from S3 to P3 for additional electrical loads.
American to Russian Converter Unit 53 – 54 power jumper to give some redundancy for powering Russian Segment.
What were the PM failure’s impacts on station research?
MELFI 1 had to be shut down because we lost Low Temp Loop capability in the JEM. The crew transferred all samples to MELFI 2 in US Destiny Lab. No science lost.
Express Rack 4 in Japanese Experiment Module “Kibo” was turned off because JAXA lost smoke detection capability for JEM Express Racks. No science loss here as the rack was only on to power a SAMS sensor at the time.
JAXA SEDA-AP and SMILES external payloads had to powered down to standby mode and are currently not collecting science data.
Many planned payload operations (MDCA/Flex experiment maintenance [CIR Rack], SPHERES, VO2Max) were cancelled this week to make room for EVA preparation tasks. Crew time off between and following EVAs will result in additional postponements.
In general, many racks and experiments can’t be activated because either crew time or other resources are not available.
When did this PM spare fly to ISS?
The spare pump module that will be used to replace the failed unit was delivered to the station on the STS-121/Utilization Logistics Flight-1 mission in July 2006.