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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 _______
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