Apollo 13 transcript starting at 05 06 25 57 on Spacelog

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05 06 25 57
Ken Mattingly: Yes, sir. Loud and clear.
05 06 26 04
Jack Swigert (CMP): Okay. It's perform CM—CSM RCS preheat, and could you say again all after?
05 06 26 11
Ken Mattingly: Okay. I'm referring to the entry checklist, page E/1-5, steps 35 and 37.
05 06 26 33
Jack Swigert (CMP): Okay. Perform CSM RCS preheat per entry checklist, page 1-5, steps 35 and 37.
05 06 26 43
Ken Mattingly: That's affirmative. Now back to panel 5: circuit breaker CAUTION AND WARNING, MAIN B, closed.
05 06 26 59
Jack Swigert (CMP): CB CAUTION AND WARNING, MAIN B, closed.
05 06 27 02
Ken Mattingly: That's affirm. On panel 2: CAUTION AND WARNING POWER to 1.
05 06 27 15
Jack Swigert (CMP): Panel 2: CAUTION AND WARNING POWER to 1.
05 06 27 20
Ken Mattingly: That was POWER to number 1, Jack.
05 06 27 26
Jack Swigert (CMP): CAUTION AND WARNING POWER to 1.
05 06 27 29
Ken Mattingly: Okay. On panel 5: circuit breaker EPS SENSOR UNIT, DC BUS A and B, closed.
05 06 27 50
Jack Swigert (CMP): Okay, Ken. The COMM from you is awful weak—awful weak, I—I can't—it's CB EPS SENSOR UNIT. Say again, after that.
05 06 27 59
Ken Mattingly: All right, Jack. That's CB EPS SENSOR UNIT, DC, that's Delta Charlie, BUS A and B, closed.
05 06 28 16
Jack Swigert (CMP): Okay. CB EPS SENSOR UNIT, DC BUS A and B, close. And I'll give you the volts and amps.
05 06 28 27
Ken Mattingly: Okay, that's correct. Go ahead.
05 06 28 29
Jack Swigert (CMP): Okay. Volts are 39.1; amps, 1.5.
05 06 28 45
Ken Mattingly: Okay. On panel 3: MAIN BUS A and B, go to RESET and leave it in the center.
05 06 29 06
Jack Swigert (CMP): Okay, panel 3—Stand by; got to change OMNI's.
05 06 29 19
Jack Swigert (CMP): Okay. MAIN BUS A and B, RESET, then center.
05 06 29 27
Ken Mattingly: That's affirmative. Okay, now we're at EI minus 5 plus 05. And, as far as you're concerned, Jack, the command module is using this for information only. This will be the LM doing an Earth-terminator AGS alinement; and at the time of 5 plus 05 is the time they'll be going ahead and releasing their ball. And this will be covered in the LM checklist; it'll be uplinked after this one. At EI minus 5, we perform midcourse number 7. Over.
Expand selection up Contract selection down Close
05 06 30 16
Jack Swigert (CMP): Okay. At EI minus 05:05, the LM is making an Earth-terminator aline; and at EI minus 05:00, we perform MCC-7.
05 06 30 27
Ken Mattingly: That's correct. At the completion of midcourse 7, the LM will maneuver to a separation attitude. And this attitude will be sent up on one of the pads that you're going to get before all the sequence starts. And it'll be flown to the LM ball angles on that pad.
05 06 30 47
Jack Swigert (CMP): Okay. Understand.
05 06 30 50
Ken Mattingly: All right. At EI minus 4 plus 40, we want to perform page 1-6, step 39 of the entry checklist.
Expand selection down Contract selection up
05 06 31 07
Jack Swigert (CMP): Ken, I—I didn't get it. We had to change OMNI's again. Could you say it—the EI minus 4 dash—or 04:40, we do something.
05 06 31 15
Ken Mattingly: Okay. And at that time, you'll want to perform step 39 of page E/1-6. Over.
05 06 31 31
Jack Swigert (CMP): Okay. Perform step 39 of entry checklist page E/1-6.
05 06 31 39
Ken Mattingly: That's correct. Okay. The next is the command module RCS activation, and that's step 4-1 of page E/1-6.
05 06 32 13
Jack Swigert (CMP): Okay. The next is perform CSM—or CM RCS activation for step 4-1 of page E—E/1-6.
05 06 32 28
Ken Mattingly: That's correct.
05 06 32 41
Ken Mattingly: All right, Jack. The next is at EI minus 4 plus 30. We want to verify that the LM is configured for command module RCS hotfire.
05 06 33 08
Jack Swigert (CMP): Okay. Verify LM configure for RCS hotfire at EI minus 04:30.
05 06 33 16
Ken Mattingly: That's correct. Now to panel 5: circuit breaker G&N IMU HEATER, MAIN B, closed.
05 06 33 41
Jack Swigert (CMP): Okay. Panel 5: CB G&N IMU HEATER, MAIN A and MAIN B, closed.
05 06 33 49
Ken Mattingly: That's negative, Jack. That's MAIN B only.
05 06 33 59
Jack Swigert (CMP): Okay. MAIN B only.
05 06 34 02
Ken Mattingly: I'm sorry; I lost you that time. Say it again.
05 06 34 08
Jack Swigert (CMP): Okay. Let's repeat it. Stand by. Cut out. We've really got a strange attitude, so this is why we are having the COMM problem. Panel 5: CB G&N IMU HEATER, MAIN B, closed.
05 06 34 24
Ken Mattingly: That's affirmative. On panel 1: ROTATION CONTROL POWER, NORMAL. That's two of them, to AC/DC.
05 06 34 42
Jack Swigert (CMP): Okay, panel 1: RHC, NORMAL, two to AC/DC, two controllers.
05 06 34 48
Ken Mattingly: That's correct. On panel 7: SCS, LOGIC POWER 2/3, ON.
05 06 35 03
Jack Swigert (CMP): SCS, LOGIC POWER 2/3, ON, panel 7.
05 06 35 09
Ken Mattingly: That's affirm. Back to panel 2: RCS COMMAND, ON.
05 06 35 20
Jack Swigert (CMP): Panel 2: RCS COMMAND, ON.
05 06 35 25
Ken Mattingly: That's correct. Now the command module RCS check per step 4 of page E/2-1.
05 06 35 44
Jack Swigert (CMP): Okay. Perform the command module RCS check per step 4, page 2-1.
05 06 35 49
Ken Mattingly: That's correct. Okay, at this point, we want to lock the rotation hand controllers.
05 06 36 09
Jack Swigert (CMP): Okay. After that, lock both rotation hand controllers.
05 06 36 14
Ken Mattingly: That's affirm. On panel 8: SEQUENTIAL, PYRO ARM, two to ARM.
05 06 36 37
Jack Swigert (CMP): Okay. Panel 8: set PYRO ARM, two, to ARM. Do I get a MSFN GO for that?

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