Apollo Lunar Surface Journal

LM-10 (Falcon)
Cabin Close Out Photos

Scans by Paul Fjeld from NASA negatives
provided by the Northrup Grumman History Center.
Last revised 9 July 2012.


Environmental Control System (ECS): see, also, LM News Reference Chapter 6 (18 Mb)

  (1) Water Management / LCG Temperature Controls (2.0 Mb)

  (2) Oxygen Control Module / Suit Flow Controls.  The CDR's hoses are on the left. (2.2 Mb)

  (3) Suit Circuit Module:  Suit Circuit Relief, Cabin Gas Return, LiOH cannisters (2.3 Mb)

  (4) LMP's ECS hoses: O2 flow from the ECS (blue connector) O2 flow return flow to the ECS (red connector). The H2O hose (with a flow path for each direction) is partly visible to the right of the O2 hoses. (2.0 Mb)


Forward Panels

  (1) Panel 1 (CDR, left), Panel 2 (LMP, right), Panel 3 (partial), armrests (2.1 Mb)

  (2) Panel 1, CDR tapemeters (2.2 Mb)

  (3) Panel 1, CDR Range/Range Rate tapemeter, Trust/Weight (T/W) tapemeter and adjacent switches (2.2 Mb)

  (4) Panel 1, Tapemeters, 8-ball, attitude rate indicators, cross-pointer at upper left, cross-pointer scale switch (2.3 Mb)

  (5) Panel 3, left section; lower part of Panel 1 (2.1 Mb)

  (6) Panel 3, center section, arm rests raised; LM Guidance Computer Display, partly hidden by a pallet covered with detailed reference data for computer operation. When the computer is in use, the pallet is swung down to horizontal, revealing a surface with more computer information. (2.0 Mb)

  (7) Panel 3, right section, LMP armrest lowered, LMP Trust/Translation Controller Assembly (TTCA) (2.1 Mb)

  (8) Panel 3, right section; lower part of Panel 2; LMP window covered (2.3 Mb)

  (9) Alignment Optical Telescope (AOT); Utility Light with Clamp on the right (2.1 Mb)

(10) Hatch opening under the DSKY (1.7 Mb)


CDR Instrument Panels: 
see, also, LM News Reference Chapter 7  (3.4 Mb)

  (1) CB(11) CDR Circuit Breaker Panel, aft end viewed from slightly forward (2.0 Mb)

  (2) CB(11) CDR Circuit Breaker Panel, forward end, viewed from slightly aft, window shade in place (2.0 Mb)

  (3) CDR Thrust/Translation Controller Assembly (TTCA) (1.9 Mb)

  (4) CDR Start/Stop button, hand grip (2.0 Mb)

  (5) Panel 5, Engine Start/Stop and X-translation push buttons, mission timer/lighting controls (1.9 Mb)

  (6) Panel 8 forward section, oblique view from inboard, Audio, COAS switch, arm rest pivot, TTCA (1.9 Mb)

  (7) Panel 8 aft end, oblique view from inboard, Descent Propulsion Vent switches, Heater Controls, Explosive Device controls (1.9 Mb)

  (8) ORDEAL (Orbital Rate Display - Earth and Lunar) (1.9 Mb)


LMP Instrument Panels: 
see, also, LM News Reference Chapter 7 (3.4 Mb)

  (1) CB(16) LMP Circuit Breaker Panel, forward end; Panel 14 (bottom), Electrical Power, Descent Power (2.0 Mb)

  (2) CB(16) LMP Circuit Breaker Panel, aft end (2.0 Mb)

  (3) Panel 12, forward section, Audio; LMP's Attitude Controller (1.9 Mb)

  (4) Panel 14 (top) aft section, Descent Power, Ascent Power, Comm; Panel 12 (bottom) Communications Antennas (1.9 Mb)

  (5) Panel 14 (top) forward section, Electrical Power, Descent Power; Panel 12 (bottom) Audio, Commentications, Communications Antennas (2.1 Mb)

  (6) Panel 12 and 14, aft sections; LMP's ECS hoses: O2 flow from the ECS (blue connector) O2 flow return flow to the ECS (red connector). The H2O hose (with a flow path for each direction) is partly visible to the right of the O2 hoses. (2.0 Mb)
 
  (7) Panel 6, Abort Guidance System, LMP TTCA, LMP's Stop pushbutton (yellow and black stripes) (1.9 Mb)

  (8) 16-mm Data Acquisition Camera (DAC) and battery, mounted over the LMP-s window (1.8 Mb)

Overhead

 (1) Rendezvous Window (covered), COAS mounting (1.9 Mb)

 (2) Utility light receptacles, switches, coli cables.  Two sets of Main Panel/Cabin Flood Lights, one on either side and just aft of the AOT.  Yellow handgrip in a recess.  The LEC pulley was hooked onto the handgrip during LEC operations. (2.2 Mb)

 (3) Docking Hatch (2.0 Mb)

Stowage


  (1) Aft bulkhead, RCU units, one visible above center on the right edge of the image (2.3 Mb)

  (2) Lefthand Side Stowage Compartment (LHSSC), immediately beneath CDR Panel 8 on the left bulkhead.  Waist tethers (2.0 Mb)

  (3) Interim Stowage Assembly (ISA) hanging from the ceiling immediately aft of the AOT.  Later, during LM checkout on the way out to the Moon, the ISA was moved to the bulkhead behind the CDR's station. (1.9 Mb)

  (4) LM Manuals left bulkhead, note the cloth compartment cover, with Velcro to hold them closed. (1.9 Mb)

  (5) View through the open hatch of LMP's PLSS secured to the floor and the CDR's helmet bag on the right (1.8 Mb)

  (6) View through the open hatch of LMP PLSS, both helmet bags, bottom of the CDR PLSS at the upper right, with more stowage below it on the midstep for the Liquid Cooled Garments and InFlight Coveralls.  ECS and hoses on the left.  The Equipment Transfer Bag is beyond the LMP PLSS and immediately forward of the grey, vertical face of the midstep. (1.9 Mb)

  (7) View through the open hatch of the RHSSC beyond the LMP helmet bag. (1.9 Mb)


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