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33
 
TITLE 1/6/82
Project No.______
Book No.________

From Page No. _____
   
Vehicle status

FC1 installation & elect. mate complete
2 vacuum purge & prep complete; installation due today.

IPR99 CRT 4 party error. Not repeated yet.
L oms ox burst disk integrity verified (Pressure decay CK)

IRP 127 TK set 4 O2 HTR cnter; T/S [[strikethrough]]suggests[[/strikethrough]] indicates GSE, but not isolated.

IPR 144 P/L retention latch indicators (A6)      }V1102 Mid-body DFI
150 26v @ connector output w/ cockpit switch off }

145 I/O error with DFI signal conditioner pwr down.

Pad oxidizer xfer & sampling effort halted due seized pump.

RETESTS: Pl & RHC & fwd PCA cmplt

ET/SRB: R SRB strut pull test - test load lower than spec (omrs = 43.6 klbs; applied 42.6). similar problem on STS-2. Plan to fix by upping pre-load.
[[note]]back on sked[[/note]]
R SRB - some elect/cb problem

P3D red targets for optical msmts: ~200 to install prior to rollout USAF regmt; KSC got JSC direct MCR papers/engine. not in yet

MMU 1 - current iteration = R/R (Amended 1600: Morchead & Solick opposing. 24 hr hold on work)

PCMMU 1 R/R'd. Retest yet to go. Bad unit back to Harris. Current unit is the one R/R'd prior STS-2.

TPS: Small oven fire.
11 tile revived (425 to date); 26 bonded (263 t.d.). 162 cavities.
In work: 317 step gaps to go; carrier panels [[diagonal arrow pointing to lower right corner of page]]

To Page No. 

Witnessed & Understood by me, _____________________
Date _______
Invented by _____________________
Recorded by _____________________
Date _______
 

Transcription Notes:
---------- Reopened for Editing 2023-03-29 09:29:16 ---------- Reopened for Editing 2023-03-29 09:33:47 ---------- Reopened for Editing 2023-03-29 18:30:40 ---------- Reopened for Editing 2023-03-29 19:08:00 ---------- Reopened for Editing 2023-03-30 11:01:01 ---------- Reopened for Editing 2023-03-30 11:36:05