entry checklist - nasa · ent–798 ent–799 ent–801 ent–802 multi–1599 multi–1616...
TRANSCRIPT
Lyndon B. Johnson Space CenterHouston, Texas
National Aeronautics andSpace Administration
Verify this is the correct version for the pending operation (training, simulation or flight).Electronic copies of FDF books are available. URL: http://mod.jsc.nasa.gov/fdf
JSC–48019
Entry Checklist
Mission Operations DirectorateOperations Division
Generic, Rev FApril 24, 2002
SSP Flight Data File PAGE CHANGE NOTICE JSC–48019
ENTRY C/L GENERIC Rev F (Apr 24, 2002)
PCN–1 (Oct 25, 2002) Sheet 1 of 1
List of Implemented Change Requests (482s):
ENT–798ENT–799ENT–801ENT–802
MULTI–1599MULTI–1616
Incorporate the following:
1. Replace vii thru x
2. Replace 2–3 & 2–2 (five pages each in Flt Qual only)Replace 2–3 & 2–4
3. Replace 5–1 & 5–2
4. Replace 7–3 & 7–4, 7–7 & 7–8
5. Replace CC 8–19 & CC 8–20
Prepared by:
Approved by:
Book Manager
Lead Entry GPO Chief, Ascent/Descent DynamicsBranch
Encl: 16 pages (Bond)Encl: 26 pages (Flt Qual)
File this PCN immediately behind the front cover as a permanent record
Verify this is the correct version for the pending operation (training, simulation or flight).Electronic copies of FDF books are available. URL: http://mod.jsc.nasa.gov/fdf
i ENT/ALL/GEN F
JSC–48019
MISSION OPERATIONS DIRECTORATE
ENTRY CHECKLIST
GENERIC, REVISION FApril 24, 2002
PREPARED BY:
Gwendolyn Jordan–MooreBook Manager
APPROVED BY:
Lead Entry GPO Gregory T. OliverChief, Ascent/Descent
Dynamics Branch
This document is under the configuration control of the CrewProcedures Control Board (CPCB). All proposed changes mustbe submitted on JSC Form 482 to DO3/FDF Manager.
Additional distribution of this book for official use must berequested in writing to DO3/FDF Manager. The request mustinclude justification and requester’s name, organization,position, and phone number. Contractor requests are madethrough the NASA or DOD organization supported. Deletions,reduction in quantity, or change of address may be submitted toDO3/FDF distribution manager, (713) 244–1182.
ENT/ALL/GEN F
ii ENT/ALL/GEN F
Incorporates the following:482#: ENT–794A
ENT–796
AREAS OF TECHNICAL RESPONSIBILITY
Book Manager DM43/G. Jordan–Moore 483–1261
Deorbit Burn to Entry Interface DM43/J. Patterson 483–1987
Entry Interface thru RolloutPost Landing
DM43/J. Patterson 483–1987
iii ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
iv ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
v ENT/ALL/GEN F
NOTES
1. The Wheels Stop/Egress Switch List, section 7, gives thevehicle configuration at these discrete times. If switchposition difference exists between wheels stop and crewegress, egress position will be boxed beside wheels stopposition. Section 7 contains switch configuration only forpanels that are reconfigured during crew execution ofprocedures in sections 3, 4, and 5. Refer to DEORBITPREP, section 3, for egress configuration for remainingpanels.
2. This checklist is an all–vehicle book and is not complete fora specified flight without a Flight Supplement. To obtaincomplete checklist, incorporate Flight Supplement forspecific flight of interest using instructions in FlightSupplement List of Effective Pages.
3. Entry related cue cards are contained in this document.Cue cards are listed in Entry Cue Card Config section.Some cue cards are printed in the body of checklist for MSuse and also in the Entry Cue Card Config section forreference of crop marks and fabrication instructions.
4. Velcro placement, size, and shape of cue cards arecontrolled by Cue Card Book Manager.
5. Vehicle configuration or procedural steps that areapplicable to a specific vehicle are indicated by xxx .
vi ENT/ALL/GEN F
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vii ENT/ALL/GEN F
ENTRY CHECKLIST
LIST OF EFFECTIVE PAGES
GENERIC 02/01/88REV F 04/24/02PCN–1 10/25/02
Sign Off * ALL/GEN F. . . . ii * ALL/GEN F. . . . . . . . . . iii *� ALL/GEN F. . . . . . . . . . iv *� ALL/GEN F. . . . . . . . . . v * ALL/GEN F. . . . . . . . . . vi * ALL/GEN F. . . . . . . . . . vii * ALL/GEN F,1. . . . . . . . . viii * ALL/GEN F,1. . . . . . . . . ix * ALL/GEN F,1. . . . . . . . . . x * ALL/GEN F,1. . . . . . . . . . xi *� ALL/GEN F. . . . . . . . . . xii *� ALL/GEN F. . . . . . . . . FS xiii * flt suppl. . . . . . FS xiv * flt suppl. . . . . . xv ALL/GEN F. . . . . . . . . xvi ALL/GEN F. . . . . . . . . 1–1 (3 pgs) � ALL/GEN F. 1–2 (3 pgs) � ALL/GEN F. 2–1 ALL/GEN F. . . . . . . . 2–2 (6 pgs) � ALL/GEN F. 2–3 (6 pgs) � ALL/GEN F,1. 2–4 ALL/GEN F. . . . . . . . 2–5 � ALL/GEN F. . . . . . . . 2–6 � ALL/GEN F. . . . . . . . 3–1 � ALL/GEN F. . . . . . . . 3–2 � ALL/GEN F. . . . . . . . FS 3–3 flt suppl. . . . . FS 3–4 flt suppl. . . . . 3–5 ALL/GEN F. . . . . . . . 3–6 ALL/GEN F. . . . . . . . 3–7 ALL/GEN F. . . . . . . . 3–8 ALL/GEN F. . . . . . . .
3–9 ALL/GEN F. . . . . . . . 3–10 ALL/GEN F. . . . . . . 3–11 ALL/GEN F. . . . . . . 3–12 ALL/GEN F. . . . . . . A3–13 MEDS/GEN F. . . . . A3–14 MEDS/GEN F. . . . . B3–13 NOM/GEN F. . . . . B3–14 NOM/GEN F. . . . . 3–15 ALL/GEN F. . . . . . . 3–16 ALL/GEN F. . . . . . . 3–17 ALL/GEN F. . . . . . . 3–18 ALL/GEN F. . . . . . . 3–19 ALL/GEN F. . . . . . . 3–20 ALL/GEN F. . . . . . . 3–21 ALL/GEN F. . . . . . . 3–22 ALL/GEN F. . . . . . . 3–23 ALL/GEN F. . . . . . . 3–24 ALL/GEN F. . . . . . . 3–25 ALL/GEN F. . . . . . . 3–26 ALL/GEN F. . . . . . . 3–27 ALL/GEN F. . . . . . . 3–28 ALL/GEN F. . . . . . . 3–29 � ALL/GEN F. . . . . . . 3–30 � ALL/GEN F. . . . . . . A3–31 MEDS/GEN F. . . . . A3–32 MEDS/GEN F. . . . . B3–31 NOM/GEN F. . . . . B3–32 NOM/GEN F. . . . . 3–33 � ALL/GEN F. . . . . . . 3–34 � ALL/GEN F. . . . . . . A3–35 MEDS/GEN F. . . . . A3–36 ALL/GEN F. . . . .
* – Omit from flight book� – Replace with page from Flight Supplement� – Extra pages in crew copy only
ENT/ALL/GEN F,1
viii ENT/ALL/GEN F
B3–35 NOM/GEN F. . . . . B3–36 ALL/GEN F. . . . . 3–37 ALL/GEN F. . . . . . . 3–38 ALL/GEN F. . . . . . . A3–39 MEDS/GEN F. . . . . A3–40 MEDS/GEN F. . . . . B3–39 NOM/GEN F. . . . . B3–40 NOM/GEN F. . . . . 3–41 ALL/GEN F. . . . . . . 3–42 ALL/GEN F. . . . . . . A3–43 MEDS/GEN F. . . . . A3–44 MEDS/GEN F. . . . . B3–43 NOM/GEN F. . . . . B3–44 NOM/GEN F. . . . . 4–1 ALL/GEN F. . . . . . . . 4–2 ALL/GEN F. . . . . . . . 4–3 ALL/GEN F. . . . . . . . 4–4 ALL/GEN F. . . . . . . . 4–5 ALL/GEN F. . . . . . . . 4–6 ALL/GEN F. . . . . . . . 4–7 � ALL/GEN F. . . . . . . . 4–8 � ALL/GEN F. . . . . . . . 4–9 ALL/GEN F. . . . . . . . 4–10 ALL/GEN F. . . . . . . 4–11 � ALL/GEN F. . . . . . . 4–12 � ALL/GEN F. . . . . . . 4–13 ALL/GEN F. . . . . . . 4–14 ALL/GEN F. . . . . . . 4–15 ALL/GEN F. . . . . . . 4–16 ALL/GEN F. . . . . . . 5–1 ALL/GEN F. . . . . . . . 5–2 ALL/GEN F,1. . . . . . . . A5–3 MEDS/GEN F. . . . . . A5–4 ALL/GEN F. . . . . . B5–3 NOM/GEN F. . . . . . B5–4 ALL/GEN F. . . . . . 5–5 ALL/GEN F. . . . . . . . 5–6 ALL/GEN F. . . . . . . . 5–7 ALL/GEN F. . . . . . . . 5–8 ALL/GEN F. . . . . . . . 5–9 ALL/GEN F. . . . . . . .
5–10 ALL/GEN F. . . . . . . 5–11 ALL/GEN F. . . . . . . 5–12 ALL/GEN F. . . . . . . A5–13 ALL/GEN F. . . . . A5–14 MEDS/GEN F. . . . . A5–15 MEDS/GEN F. . . . . A5–16 MEDS/GEN F. . . . . B5–13 ALL/GEN F. . . . . B5–14 NOM/GEN F. . . . . B5–15 NOM/GEN F. . . . . B5–16 NOM/GEN F. . . . . 5–17 ALL/GEN F. . . . . . . 5–18 ALL/GEN F. . . . . . . 5–19 � ALL/GEN F. . . . . . . 5–20 � ALL/GEN F. . . . . . . 5–21 ALL/GEN F. . . . . . . 5–22 ALL/GEN F. . . . . . . 5–23 ALL/GEN F. . . . . . . 5–24 ALL/GEN F. . . . . . . 6–1 ALL/GEN F. . . . . . . . 6–2 ALL/GEN F. . . . . . . . 6–3 ALL/GEN F. . . . . . . . 6–4 ALL/GEN F. . . . . . . . 7–1 * ALL/GEN F. . . . . . . . 7–2 * ALL/GEN F. . . . . . . . 7–3 * ALL/GEN F,1. . . . . . . . 7–4 * ALL/GEN F,1. . . . . . . . 7–5 * ALL/GEN F. . . . . . . . 7–6 * ALL/GEN F. . . . . . . . 7–7 * ALL/GEN F. . . . . . . . 7–8 * ALL/GEN F,1. . . . . . . . 7–9 * ALL/GEN F. . . . . . . . 7–10 * ALL/GEN F. . . . . . . 8–1 * ALL/GEN F. . . . . . . . CC 8–2 * ALL/GEN F. . . . CC 8–3 * ALL/GEN F. . . . CC 8–4 * ALL/GEN F. . . . CC 8–5 * ALL/GEN F. . . . CC 8–6 * ALL/GEN F. . . . CC 8–7 * ALL/GEN F. . . . CC 8–8 * ALL/GEN F. . . .
� – Replace with page from Flight Supplement* – Omit from flight book
ENT/ALL/GEN F,1
ix ENT/ALL/GEN F
CC 8–9 * ALL/GEN F. . . . CC 8–10 * ALL/GEN F. . . CC 8–11 * ALL/GEN F. . . . CC 8–12 * ALL/GEN F. . . CC 8–13 * ALL/GEN F. . . CC 8–14 * ALL/GEN F. . . CC 8–15 * ALL/GEN F. . . CC 8–16 * ALL/GEN F. . . CC 8–17 * ALL/GEN F. . . CC 8–18 * ALL/GEN F. . . CC 8–19 * ALL/GEN F,1. . . CC 8–20 * ALL/GEN F. . . CC 8–21 * ALL/GEN F. . . CC 8–22 * ALL/GEN F. . . 8–23 *� ALL/GEN F. . . . . . . 8–24 *� ALL/GEN F. . . . . . .
* – Omit from flight book� – Replace with page from Flight Supplement
ENT/ALL/GEN F,1
x ENT/ALL/GEN F
ENTRY CUE CARDSTitle Ref. Page Card No.
Deorbit Burn Flight Rules(Front) CC 8–2 ENT–1a/D/I. . . . . . . . . . . . . . . . . . . . . (Back) CC 8–3 ENT–1b/D/I. . . . . . . . . . . . . . . . . . . . .
Deorbit Burn (RCS)(Front) (Top) CC 8–4 ENT–3a/D/K. . . . . . . . . . . . . . . (Front) (Bottom) CC 8–5 ENT–3aa/D/K. . . . . . . . . . . . (Back) (Top) CC 8–6 ENT–3b/D/D. . . . . . . . . . . . . . . . (Back) (Bottom) CC 8–7 ENT–3bb/D/D. . . . . . . . . . . .
Deorbit Burn (2 Eng)(Front) (Top) CC 8–8 ENT–4a/D/K. . . . . . . . . . . . . . . (Front) (Bottom) CC 8–9 ENT–4aa/D/I. . . . . . . . . . . .
Deorbit Burn (1 Eng)(Back) (Top) CC 8–10 ENT–4b/D/I. . . . . . . . . . . . . . . . (Back) (Bottom) CC 8–11 ENT–4bb/D/J. . . . . . . . . . . .
Unbalanced Prplt Deorbit Burn(Front) (Top) CC 8–12 ENT–5a/D/L. . . . . . . . . . . . . . . (Front) (Bottom) CC 8–13 ENT–5aa/D/M. . . . . . . . . . . .
Deorbit Burn (Mixed Xfeed)(Back) (Top) CC 8–14 ENT–5b/D/I. . . . . . . . . . . . . . . . (Back) (Bottom) CC 8–15 ENT–5bb/D/I. . . . . . . . . . . .
Entry Maneuvers(Front) CC 8–16 ENT–6a/E/L. . . . . . . . . . . . . . . . . . . . . (Back) CC 8–17 ENT–6b/E/Q. . . . . . . . . . . . . . . . . . . . .
Entry NO–GO Checklist(Front) CC 8–18 ENT–7a/E/I. . . . . . . . . . . . . . . . . . . . .
ADTA Mgmt (Back) CC 8–19 ENT–7b/E/N. . . . . . . . . . . Mach �
(Front) CC 8–20 ENT–8a/A,E/C. . . . . . . . . . . . . . . . . . . . . (Back) CC 8–20 ENT–8b/A,E/B. . . . . . . . . . . . . . . . . . . . .
Deorbit Burn Monitor (Front) see flt suppl flt suppl. . . . . . . . . . . . . . . . . . . . .
OMS Failures (Back) see flt suppl flt suppl. . . . . . . . . . Entry Control (Front) CC 8–21 ENT–10a/A,E/A. . . . . . . . . . Entry Control (Back) CC 8–22 ENT–10b/A,E/A. . . . . . . . . .
ENT/ALL/GEN F,1
xi ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
xii ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
(Replace with pages FS xii thru FS xiv)
xv ENT/ALL/GEN F
CONTENTS PAGE
DEORBIT MNVR PADS 1–1. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OMS PRPLT AND DEL PADS 2–1. . . . . . . . . . . . . . . . . . . . . . . .
DEORBIT BURN 3–1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OMS BURN PREP (CIL) 3–9. . . . . . . . . . . . . . . . . . . . . . . . . . OMS/RCS POST BURN RECONFIG (CIL) 3–32. . . . . . . . .
ENTRY CUE CARDS 4–1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . h = 10K LES VISORS (HC) 4–5. . . . . . . . . . . . . . . . . . . . . . .
POST LANDING PROCEDURES 5–1. . . . . . . . . . . . . . . . . . . . .
1–ORBIT LATE DEORBIT PROCEDURES 6–1. . . . . . . . . . . .
SWITCH LIST AT WHEELS STOP EGRESS 7–1. . . . . . . . . .
ENTRY CUE CARD CONFIG 8–1. . . . . . . . . . . . . . . . . . . . . . . .
xvi ENT/ALL/GEN F
This Page Intentionally Blank
EN
T/A
LL
/GE
N F
1–
1
MNVRPADS
DEORBIT MNVR PAD
1OMS BOTH
2
3
4RCS SEL
6
TRIM LOAD
5TV ROLL
( )�
7 ( )�
8 ( )�
9
10 / : :�
14
TGT PEG 4
15 ( )�
16�
17�
18 ( )
24R
25P
26Y
BURN ATT
:
L OMS � RCS
R OMS � RCS
NONE
�
XVGO ( )
YVGO ( )
ZVGO ( )
�
�
�
( )TGT
HPHA
:∆VTOT
TGO
RCS I’CNCT:
NOTES
L
R
P
LY
RY
WT
TIG
C1
C2
HT
�T
PRPLT
REI
TXX
MNVRPADS
EN
T/A
LL
/GE
N F
1–
2
DEORBIT MNVR PAD
1OMS BOTH
2
3
4RCS SEL
6
TRIM LOAD
5TV ROLL
( )�
7 ( )�
8 ( )�
9
10 / : :�
14
TGT PEG 4
15 ( )�
16�
17�
18 ( )
24R
25P
26Y
BURN ATT
:
L OMS � RCS
R OMS � RCS
NONE
�
XVGO ( )
YVGO ( )
ZVGO ( )
�
�
�
( )TGT
HPHA
:∆VTOT
TGO
RCS I’CNCT:
NOTES
L
R
P
LY
RY
WT
TIG
C1
C2
HT
�T
PRPLT
REI
TXX
PR
PLT
/D
EL
PAD
S
2–1 ENT/ALL/GEN F
OMS PRPLT AND DEL PADS
PR
PLT
/D
EL
PAD
S
2–2 ENT/ALL/GEN F
BURN CARD OMS PRPLT PADDEORBITBURN(1 ENG)
OMS XFEED RETURN at �VTOT =
or at %
DEORBITBURN(RCS)
RCS I’CNCT TK SW at �VTOT =
OMS PRPLT LOW: �VTOT =
UNBALANCEDPRPLTDEORBITBURN
INITIAL CONFIG: TK ISOLs - CL
While feeding 2 OMS from 1 POD:OMS PRPLT FAIL:
Secure OMS
Secure OMS
Interconnect OMS to RCS
THC + X for :
If (XFEED) ENG ‘↓’
When OMS QTY:
5%: OMS TK ISOL (two) - OP
4%: OMS TK ISOL (two) - CL
If (STRAIGHT FEED) ENG ‘↓’
OMS ENG FAIL:At �VTOT =
or at %
TK ISOL (two) - OP
TK ISOL (two) - CL
Return to 2 ENG, 2 POD FLOW:At �VTOT = TK ISOLs - OP
OMS ENG FAIL: (XFEED CUE)
OMS QTY %L or %R
DEORBITBURN(MIXEDXFEED)
FEED FROM GOOD POD:At �VTOT =
or at %
OMS He PRESS (two) - OPTK ISOL (two) - OPXFEED (two) - OP
Secure OMSOMS PRPLT LOW:
AFT RCS RECONFIG at �VTOT =OMS ENG FAIL:
OMS He PRESS (two) - OPTK ISOL (two) - OP
OMS XFEED (two) - CL
:
EI–5 MM303 INRTL ATT
MM304 PREBANK (ENT MNVR Cue Card)
ALTM SET
CLG INIT
EXPECTED AIL TRIM
VREL 1ST REVERSAL
XCG AT TD
LAND SITE 50K
38K
28K
20K
12K
7K
3K
1K
SURFACE
∆T MACH .9 TO HAC
TOT AFT QTY 1 (%)
TOT AFT QTY 2 (%)
PREBANK/FLIP HP
FRCS: DUMP TO % (USE TIME AS CUE)
PRE–DEORBITAPU START: SINGLE APU START, ATTEMPT
APU START SEQUENCE
DEORBITBURN CUE CARD:
OMS TIG SLIP – NO EXEC > TIG +
RCS DOWNMODING
STOP/CONTINUE CUES: L OMS FAIL HP
STOP/CONTINUE CUES: R OMS FAIL HP
S FAIL HPOMS ENG FAIL XFEED QTY CUE
ENGINE FAIL HP
SAFE HP
::
APU(s)
AFT HP B/U SITE
OX FU
P YR
RL
�
OVHDL deg
STRTR TAC
MAX Nz Nz LIMIT
AIMPOINT SPEEDBRAKE
CLOSE–IN
% @ 3K
REMARKS:
THEN
%R%L
RL �
�
RWY
MLS
�
:
�
NOM
S.F.
NOM
/
/
/
/
/
/
/
/
/
ENTRY/LANDING
:
2–3 ENT/ALL/GEN F
DEL PAD
ENT/ALL/GEN F,1
2–4 ENT/ALL/GEN F
This Page Intentionally Blank
2–5 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
2–6 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
3–1 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
3–2 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
(Replace with pages FS 3–2 thru FS 3–4)
3–5 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST
TIG–46
B FINAL DEORB UPDATE/UPLINK
MCC UPDATE:DEL PADOMS PRPLT PAD
MCC UPLINK:PASS SVBFS SVPASS TGTBFS TGTBFS IMU GYRO/ACCEL
C G50 �LAND SITE per DEL PADSET TACAN tw
On MCC GO:C CRT1 LOAD – ITEM 22 EXEC
TIMER – ITEM 23 EXEC
CRT1,3 �PASS & BFS TGTs per MNVR PAD:BURN ATT∆VTOTTGOHA HP
G51 SEL ATMOSPHERE:incl ≤ 50° ITEM 22 EXECincl > 50° SEL ITEM NR (table)
Hemi Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec
N Desc 23 23 23 23 22 24 24 24 22 23 23 23
S Asc 24 24 22 23 23 23 23 23 23 23 22 24
N Asc
S Desc22
3–6 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST
C OMS TVC GMBL CHECK (Perform during S–band AOS)
CRT1 SECONDARY CHECKPerform SEC L,R then PRI L,R GMBL CK
**
If down arrow(s) or Ms:Select good GMBL
**
MS LES Pressure Integrity Check
P APU PRE–START (Perform during S–band AOS)
R4 �HYD BRAKE ISOL VLV (three) tb – CL�LG EXTEND ISOL VLV tb – CL
*****
R2R4
R2
If tb not CL:(Aff) HYD CIRC PUMP – ON(Aff) ISOL VLV – CLHold 5 sec,�tb – CLHYD CIRC PUMP – OFF
*****
R2 BLR N2 SPLY (three) – ONBL �� �PWR (three) – ONBL �� �CNTLR/HTR (three) – B
�APU AUTO SHUTDN (three) – ENAAPU CNTLR PWR (three) – ONHYD MN PUMP PRESS (three) – LO
�APU SPEED SEL (three) – NORMAP �� �OPER (three) – OFFAP �� �FUEL TK VLV (three) – CL
�cb FUEL TK VLV ENABLE (six) – CL
3: BFS, SM SYS SUMM 2P R2 APU FUEL TK VLV (three) – OP
�APU/HYD RDY tb (three) – grayAPU FUEL TK VLV (three) – CL
2: GNC 50 HORIZ SIT3: BFS, GNC 50 HORIZ SIT
3–7 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC 50 HORIZ SIT3: BFS, GNC 50 HORIZ SIT
HORIZ SIT CONFIG
ALTM – ITEM 9
PASS ITEM BFS ITEM PTI INH �1LAND SITE (DEL PAD) �41 �41RWY (DEL PAD) �3 �3
�4 �4TACAN (DEL PAD) �5 �5RA blank �46TAEM TGT
G&N OVHD �6 blankHSI blank blankXEP NEP �7 NEP �7AIM (DEL PAD) NOM
(or CLSE)�8 NOM
(or CLSE)�8
SPDBK NOM �39TAC INH �20 INH �20GPS INH �43 INH �43DRAG H AUT �22 AUT �22ADTA H INH �26 INH �26ADTA TO G&C INH �29 AUT �28DES any failed TACANs � �
TAC DELTA �35AIF G INH �48
**
If BFS engaged:Set BFS HSD ITEMs to PASS config
**
.+
3–8 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC 50 HORIZ SIT3: GNC 51 OVERRIDE
�� �ELEVON AUTO – ITEM 17 (*)�� �SSME REPOS – ITEM 19 (ENA)�� �WRAP MODE – ITEM 45 (ENA)
If PLB holding > 10K lb:FILTER ALT – ITEM 21 EXEC (*)
3: BFS, GNC 51 OVERRIDE
�� �ELEVON AUTO – ITEM 17 (*)�� �SSME REPOS – ITEM 19 (ENA)�� �WRAP MODE – ITEM 45 (ENA)
If PLB holding > 10K lb:�� �FILTER ALT – ITEM 21 (*)
**
DES any failed/comm faultedIMU, RGA, AA, or SURF feedback
**
2: GNC DEORB MNVR COAST
3: BFS, GNC DEORB MNVR COAST
�� �BFS GMBL sel config same as PASS GMBLsel config
3–9 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST
P OMS BURN PREP
CRT2 OMS ENG TRIMS2 ENG BURN:
�TRIM LOAD per MNVR PAD or:L,R – ITEM 6 +0.0 –5.7 +5.7 EXEC
1 ENG BURN:�TRIM LOAD per MNVR PAD or:
P – ITEM 6 +0.0 EXECGood eng Y:
LY – ITEM 7 +5.2 EXECRY – ITEM 8 –5.2 EXEC
XFEED: Failed engine prop togood engine
RCS DEORBIT OR RCSHe/PRPLT TK FAIL
Do not terminate OMS/RCSInterconnect
O7 AFT L,R RCSHe PRESS (four) – OP (tb–OP)TK ISOL (six) – GPC (tb–OP)XFEED (four) – GPC (tb–CL)
�MSTR RCS XFEED – OFF
O8 L,R OMS�He PRESS/VAP ISOL (four) – CL�TK ISOL (four) – OP (tb–OP)�XFEED (four) – CL (tb–CL)
FWD RCSHe PRESS (two) – OP (tb–OP)
3–10 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST
RCS BURN PREPP O8 L,R OMS
�He PRESS/VAP ISOL (four) – CL�TK ISOL (four) – OP (tb–OP)
L OMS XFEED (two) – OP (tb–OP)�R OMS XFEED (two) – CL (tb–CL)
O7 AFT L,R RCSXFEED (four) – OP (tb–OP)TK ISOL (six) – CL (tb–CL)
MS3 Remove and stow Side Hatch UV Filterand Locking Device, and Pyro BoxSafing Pin
TIG–25 VENT DOOR CLOSE
NOTEVENT DOOR CLOSE must beperformed prior to MM302 transition
2: GNC 51 OVERRIDE
CRT2 VENT DOOR CNTL CLOSE – ITEM 44 EXEC
3–11 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC 51 OVERRIDE3: BFS, GNC DEORB MNVR COAST
2: GNC DEORB MNVR COAST
B DEORB UPDATE/UPLINK (if reqd)MCC UPDATE:
DEL PADOMS PRPLT PAD
MCC UPLINK:PASS,BFS SVPASS,BFS TGT
C G50 �LAND SITE per DEL PADSET TACAN tw
MS1/MS2 SEAT INGRESS
On MCC GO:CRT1 LOAD – ITEM 22 EXEC
TIMER – ITEM 23 EXECCRT1,3 �� �PASS & BFS TGTs per MNVR PAD:
BURN ATT∆VTOTTGOHA HP
C CRT1 GNC, OPS 302 PRO
1: GNC DEORB MNVR COAST 2: GNC 51 OVERRIDE3: BFS, GNC DEORB MNVR COAST
MCC/CREW GO/NO–GO FOR DEORBITBURN
*****
P
C
R2
CRT1
IF NO–GO FOR DEORBITBURN:
HYD MN PUMP PRESS (three) –NORM
GNC, OPS 301 PRO
*****
IF 1 ORBIT DELAY:Go to section 6, 1–ORB LATE
3–12 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC DEORB MNVR EXEC
IF 24–HR EXTENSIONP O7 AFT L,R RCS
He PRESS A (two) – GPC (tb–OP)He PRESS B (two) – CL (tb–CL)TK ISOL (six) – OP (tb–OP)XFEED (four) – CL (tb–CL)
O8 FWD RCSHe PRESS A – GPC (tb–OP)He PRESS B – CL (tb–CL)
C6 Unstow ORB PKT C/LTerminate Deorbit Procedures,go to DEORB PREP, D/O PREPBACKOUT
TIG–20> MNVR TO DEORBIT BURN ATT
C C3 �DAP: AUTOB F6/F8 �ADI ATT (two) – INRTL
A �� �ERR (two) – MEDA �� �RATE (two) – MED
C MNVR to BURN ATT(�ADI ATT with CRT BURN ATT)
B Copy last DEL PAD and OMS PRPLT PADdata on DEORBIT BURN Cue Cards
F6/F8 �DEORBIT BURN and DEORBIT BURNMONITOR Cue Cards installed
A14 RCS/OMS HTRFWD RCS – OFFL POD (two) – A OFF,B OFFR POD (two) – A OFF,B OFFOMS CRSFD LINES (two) –A AUTO,B AUTO
FWD RCS JET 5 (one) – OFFAFT RCS JET 5 (one) – OFF
A3–13 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, SM SYS SUMM 2
TIG–5> P SINGLE APU START (Attempt one APU)
R2 APU FUEL TK VLV – OPAPU OPER – START/RUN
MDU �HYD PRESS ind – LO green
***
If no start, shut down APU(ENT PKT, APU/HYD)
Do not execute Deorbit Burn
***
R2 �HYD CIRC PUMP (three) – OFF
3: BFS, GNC SYS SUMM 2
C �BURN ATT � 5°
B Go to DEORBIT BURN (Cue Card)
MEDSENT/MEDS/GEN F
A3–14 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, SM SYS SUMM 2
TIG–5> P SINGLE APU START (Attempt two APUs)
R2 APU FUEL TK VLV – OPAPU OPER – START/RUN
MDU �HYD PRESS ind – LO green
************
If no start:APU OPER – OFFStart another APU
If second APU starts,shut down unstarted APU(ENT PKT, APU/HYD) >>
If neither starts,� Do not start third APU� Do not execute Deorbit Burn� Shut down unstarted APUs
(ENT PKT, APU/HYD) >>
************
R2 �HYD CIRC PUMP (three) – OFF
3: BFS, GNC SYS SUMM 2
C �BURN ATT � 5°
B Go to DEORBIT BURN (Cue Card)
MEDSENT/MEDS/GEN F
B3–13 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, SM SYS SUMM 2
TIG–5> P SINGLE APU START (Attempt one APU)
R2 APU FUEL TK VLV – OPAPU OPER – START/RUN
F8 �HYD PRESS ind – LO green
***
If no start, shut down APU(ENT PKT, APU/HYD)
Do not execute Deorbit Burn
***
R2 �HYD CIRC PUMP (three) – OFF
3: BFS, GNC SYS SUMM 2
C �BURN ATT � 5°
B Go to DEORBIT BURN (Cue Card)
ENT/NOM/GEN FNOM
B3–14 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, SM SYS SUMM 2
TIG–5> P SINGLE APU START (Attempt two APUs)
R2 APU FUEL TK VLV – OPAPU OPER – START/RUN
F8 �HYD PRESS ind – LO green
************
If no start:APU OPER – OFFStart another APU
If second APU starts,shut down unstarted APU(ENT PKT, APU/HYD) >>
If neither starts,� Do not start third APU� Do not execute Deorbit Burn� Shut down unstarted APUs
(ENT PKT, APU/HYD) >>
************
R2 �HYD CIRC PUMP (three) – OFF
3: BFS, GNC SYS SUMM 2
C �BURN ATT � 5°
B Go to DEORBIT BURN (Cue Card)
ENT/NOM/GEN FNOM
BU
RN
CA
RD
S
3–15 ENT/ALL/GEN FMS ONLY
DEORBIT BURN CARDS
BU
RN
CA
RD
S
3–16 ENT/ALL/GEN FMS ONLY
APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DPS3 RDNT fail, Split X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 1 GPC X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 GPC BITE (Multiple GPCs) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ECLS7 2 Av Bay Fans in Bay 3 X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 2 Av Bay Fans in Bay 1 or 2 X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ELEC9 H2 Manf or TK leak (not in
depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . . .
10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11 CNTL CA1 (No BFS Engage in GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12 Multi Φ AC BUS (unshorted) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
GNC13 1 MLS (if reqd), IMU, or TACAN
(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
17 3 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
21 Both OMS Eng fail X 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
22 Prplt Lk after LAST LOS . . . . . . . . . . . . . . . . . . . .
AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . . .
24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
25 1 AFT RCS PROP TK fail X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
COMM26 MCC GO for DEORBIT not rcvd X. . . . . . . . . . . . . . . . . . . . .
FAILURE
PRE TIG POST TIG
Delay (max)
OneOrbit
OneDay
StopBurn,> Safe
HP
ENT–1a/D/I
perigee adjust
1 Stop Burn > OMS PRPLT FAIL HP (Ref: DEL PAD/BURN Card)2 Stop Burn > OMS ENG FAIL HP (Ref: DEL PAD/BURN Card)
HOOKVELCRO
HOOKVELCRO
DEORBIT BURN FLIGHT RULESONE–ORBIT LATE AVAILABLE
3–17 ENT/ALL/GEN FMS ONLY
APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DPS3 RDNT fail, Split X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 1 GPC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 GPC BITE (Multiple GPCs) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ECLS7 2 Av Bay Fans in Bay 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 2 Av Bay Fans in Bay 1 or 2 X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ELEC9 H2 Manf or TK leak (not in
depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . .
10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11 CNTL CA1 (No BFS Engagein GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12 Multi ΦAC BUS (unshorted) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GNC13 1 MLS (if reqd), IMU, or TACAN
(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
17 3 ADTAs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . .
21 Both OMS Eng fail X 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
22 Prplt Lk after LAST LOS . . . . . . . . . . . . . . . . . . . .
AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . .
24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
25 1 AFT RCS PROP TK FAIL X. . . . . . . . . . . . . . . . . . . . . . . . . . .
COMM26 MCC GO for DEORBIT not rcvd X. . . . . . . . . . . . . . . . . . . . .
FAILURE
PRE TIG POST TIGDelay(max)OneDay
StopBurn,> Safe
HP
ENT–1b/D/I
perigee adjust
1 Stop Burn > OMS PRPLT FAIL HP (Ref: DEL PAD/BURN Card)2 Stop Burn > OMS ENG FAIL HP (Ref: DEL PAD/BURN Card)
HOOKVELCRO
HOOKVELCRO
DEORBIT BURN FLIGHT RULESONE–ORBIT LATE NOT AVAILABLE
3–18 ENT/ALL/GEN FMS ONLY
�MM302 �OMS BOTHEnter TGO + 5 sec
�TRIM per MNVR PAD or P +0.0, LY –5.7, RY +5.7L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OP
�DAP – AUTO(PASS)/DISCADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ON
TIG–2 OMS ENG (two) – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
If no OMS ignition: APUs – SHUT DNOMS PRPLT FAIL:
Failed OMS ENG – OFFSTOP BURN:
Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS
CONTINUE BURN:
ITEM 18 +0 EXECWhen good OMS QTY:
5%: L,R OMS XFEED (four) – OP4%: Good OMS TK ISOL (two) – CL
If OMS Pc < 80 or OMS TEMP, OMS ENG – OFF
�ADI – LVLH, center needlesRCS COMPLETION
OMS ENG FAIL:Failed OMS ENG – OFFOMS XFEED at 1/2 ∆VTOT at fail
OMS Xor OMS QTY
2nd OMS FAIL (ENG or PRPLT):
Failed OMS ENG – OFFIf PRPLT FAIL:
Secure aff OMS ITEM 18 +0 EXEC
STOP BURN:
APUs – SHUT DN
CONTINUE BURN:
�ADI – LVLH, center needlesInterconnect good OMS to RCS
THC +X (�OMS% vs RCS Burn Time)RCS I’CNCT TK SW (N/A PRPLT FAIL)RCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETION
********************************************
********************************************
DEORBIT BURN (2 ENG)
EitherPRPLT FAIL(SAFE) HP
BothENG FAIL
HP
R OMSFAIL HP
L OMSFAIL HP
ENT–4a/D/K
% R%L or
: )
3–19 ENT/ALL/GEN FMS ONLY
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP orAt AFT QTY 1 TOT AFT QTY 2
if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIPHP
AFT
HP
TGTHP
FRCS COMPLETION (if applicable):MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF+ :02 OMS ENG(s) – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
********************
********************
THC +X to TGT HP
ENT–4aa/D/I
% then
%
):
PREBANK/FRCS COMPLETION
3–20 ENT/ALL/GEN FMS ONLY
�MM302 �OMS L or R�OMS BURN CONFIG (L or R XFEED)
Enter TGO + 10 sec�TRIM per MNVR PAD or P +0.0, LY +5.2, RY –5.2
L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . .
�DAP – AUTO(PASS)/DISCADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ON
TIG–2 Good OMS ENG – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
* If no OMS ignition: APUs – SHUT DN *
OMS XFEED RETURN at ∆VTOT =
orL,R OMS TK ISOL (four) – OPL,R OMS XFEED (four) – CL
OMS PRPLT FAIL:OMS ENG – OFF
STOP BURN:APUs – SHUT DN
SAFE Secure aff OMSHP
CONTINUE BURN:Secure aff OMSITEM 18 +0 EXEC
�ADI – LVLH, center needlesInterconnect good OMS to RCS
THC +X(�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETIONOMS ENG FAIL:
OMS ENG – OFFSTOP BURN:
ENG APUs – SHUT DNFAILHP
CONTINUE BURN:�ADI – LVLH, center needles
Interconnect OMS to RCSTHC +X(�OMS% vs RCS Burn Time)RCS I’CNCT TK SWRCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETIONRCS +X JET FAIL OFF:
STOP BURN:SAFE APUs – SHUT DN
HPCONTINUE BURN:
ITEM 18 +0 EXECG23 Resel jets
**************************************
**************************************
DEORBIT BURN (1 ENG)
ENT–4b/D/I
):
%at
3–21 ENT/ALL/GEN FMS ONLY
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP orAt AFT QTY 1 TOT AFT QTY 2
if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIPHP
AFT
HP
TGTHP
FRCS COMPLETION (if applicable):MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF+ :02 OMS ENG – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
********************
********************
THC +X to TGT HP
ENT–4bb/D/J
% then
%
):
PREBANK/FRCS COMPLETION
3–22 ENT/ALL/GEN FMS ONLY
�MM302 �RCS SEL�RCS BURN CONFIG (L OMS I’CNCT)
L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . . .
�DAP – INRTL/DISCADI – LVLH(REF)/MED/MEDFLT CNTLR PWR (two) – ON
TIG THC +X (No deorbit > TIG +
Maintain PITCH ATT ERR ± 3°Monitor ∆VTOT:
RCS I’CNCT TK SW at ∆VTOT =R OMS XFEED (two) – OPL OMS XFEED (two) – CL
OMS PRPLT LOWAFT RCS RECONFIG AT ∆VTOT =RCS COMPLETION
OMS PRPLT FAIL (MULTIPLE JETS FAIL OFF):Secure aff OMS
STOP BURN:SAFE APUs – SHUT DN
HPCONTINUE BURN:
ITEM 18 +0 EXECG23 Resel jetsInterconnect good OMS to RCS
THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION
RCS +X JET FAIL OFF:STOP BURN:
SAFE APUs – SHUT DNHP
CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jets
********************
********************
DEORBIT BURN (RCS)
ENT–3a/D/K
: )
3–23 ENT/ALL/GEN FMS ONLY
PREBANK/FRCS COMPLETION
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP or
At AFT QTY 1 TOT AFT QTY 2if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIP
HP
AFTHP
TGTHP
FRCS COMPLETION (if applicable):
MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF VGOx = 0, release THC
AFT RCS RECONFIGTrim Inplane X,Z residuals < 2 fps (< 0.5 if shallow)
********************
********************
ENT–3aa/D/K
% then
%
THC +X to TGT HP
3–24 ENT/ALL/GEN FMS ONLY
�MM302 �OMS BOTHEnter TGO + 5 sec
�TRIM per MNVR PAD or P + 0.0, LY –5.7, RY +5.7�DAP – AUTO(PASS)/DISC
ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONFeed 2 ENG from 1 POD
L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OPL,R OMS TK ISOL (two) – CL (tb–CL)L,R OMS XFEED (four) – OP (tb–OP)
TIG–2 OMS ENG (two) – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
If no OMS ignition: APUs – SHUT DNWhile feeding 2 OMS from 1 POD:
OMS PRPLT FAIL:Failed OMS ENG(s) – OFF
STOP BURN:APUs – SHUT DNSecure OMS
SAFE HP
CONTINUE BURN:ITEM 18 +0 EXECIf Both ENGs ‘↓’:
Secure OMS�ADI – LVLH, center needles
Interconnect OMS to RCS
THC +X forAFT RCS RECONFIG
RCS COMPLETION If (XFEED) ENG ‘↓’:
When OMS QTY:5%: OMS TK ISOL (two) – OP4%: OMS TK ISOL (two) – CL
If OMS Pc < 80 or OMS TEMP, OMS ENG – OFF
�ADI – LVLH, center needlesRCS COMPLETION
If (STRAIGHT FEED) ENG ‘↓’: OMS ENG FAIL
OMS ENG FAIL (CONTINUE BURN):Failed OMS ENG – OFF
at ∆VTOT =or
TK ISOL(two) – OP
TK ISOL(two) – CL
Return to 2 ENG, 2 POD FLOW at ∆VTOT:L,R OMS TK ISOL (two) – OP (tb–OP)L,R OMS XFEED (four) – CL (tb–CL)
at %
***************************************
***************************************
UNBALANCED PRPLT DEORBIT BURN
ENT–5a/D/L
: )
:
3–25 ENT/ALL/GEN FMS ONLY
ENT–5aa/D/M
OMS PRPLT FAIL:Failed OMS ENG – OFF
STOP BURN:Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS
CONTINUE BURN:
ITEM 18 +0 EXECWhen good OMS QTY:
5%: L,R OMS XFEED (four) – OP4%: Good OMS TK ISOL (two) – CL
If OMS Pc < 80 or OMS TEMP, OMS ENG – OFF
�ADI – LVLH, center needlesRCS COMPLETION
OMS ENG FAIL:Failed OMS ENG – OFFOMS XFEED at 1/2 ∆VTOT at fail
or OMS QTY
2nd OMS FAIL (ENG or PRPLT):
Failed OMS ENG – OFFIf PRPLT FAIL:
Secure aff OMSITEM 18 +0 EXEC
STOP BURN:APUs – SHUT DN
CONTINUE BURN:
�ADI – LVLH, center needlesInterconnect Good OMS to RCS
THC +X (�OMS% vs RCS Burn Time)RCS I’CNCT TK SW (N/A PRPLT FAIL)RCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETIONRCS COMPLETION:
THC +X to TGT HP or TOT AFT QTY 1
At AFT QTY 1if CUR HP:
PREBANK/FLIP
HP
AFTHP
TGT
HPFRCS COMPLETION (if applicable):
MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF+ :02 OMS ENG(s) – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
***********************************************************
***********************************************************
R OMSFAIL HP
L OMSFAIL HP
EitherPRPLT FAIL(SAFE) HP
BothENG FAIL
HP
PREBANK/FRCS COMPLETION
THC +X to TGT HP
THC +X to PREBANK/FLIP HP orTOT AFT QTY 2PREBANK/FRCS COMPLETION
):
% then
%
%R%L or
3–26 ENT/ALL/GEN FMS ONLY
�MM302 �OMS L(R) or RCSEnter TGO + 10 sec
�L,R OMS TK ISOL (four) – GPCL,R OM �XFEED (four) – GPC
�tb config from table (OMS SSR–1)�DAP – AUTO(PASS)/DISC
ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONMan repress to maintain good OMS Tk Ps > 234 psi (simo)If OMS BURN INITIATION:
�TRIM per MNVR PAD or: P +0.0, LY +5.2, RY –5.2TIG–2: Good OMS ENG – ARM/PRESS
TIG–2:15 EXEC (No EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
* If no OMS ignition, APUs – SHUT DN *If RCS BURN INITIATION:
Man repress L,R OMS > L,R RCS TK PsL,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL
TIG–2:00 THC +X (No Deorbit > TIG +Maintain PITCH ATT ERR � 3°
FEED FROM GOOD POD:
at ∆VTOT =or
OMS He PRESS/VAP ISOL (two) – OPOMS TK ISOL (two) – OP (tb–OP)OMS XFEED (two) – OP (tb–OP)SECURE OMS
OMS PRPLT LOWAFT RCS RECONFIG at ∆VTOT =RCS COMPLETION
DEORBIT BURN (MIXED XFEED)
ENT–5b/D/I
at %
: )
: )
3–27 ENT/ALL/GEN FMS ONLY
OMS PRPLT FAIL:OMS ENG – OFF
STOP BURN:APUs – SHUT DN
SAFE Secure L,R OMSHP
CONTINUE BURN:Secure L,R OMSITEM 18 +0 EXEC
�ADI – LVLH, center needlesRCS COMPLETION
OMS ENG FAIL:OMS ENG – OFF
STOP BURN:ENG APUs – SHUT DN
FAILHP CONTINUE BURN:
Man repress L,R OMS > L,R RCS TK PsFEED FROM GOOD POD:
OMS HE PRESS/VAP ISOL(two) – OP
TK ISOL (two) – OP
OMS XFEED (two) – CL
L,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL
�ADI – LVLH, center needlesTHC +X (�Lowest OMS % vs
RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION
RCS +X JET FAIL OFF:STOP BURN:
SAFE APUs – SHUT DNHP
CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jet
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP orAt AFT QTY 1 TOT AFT QTY 2
if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIPHP
AFTHP
TGTHP
FRCS COMPLETION (if applicable):
MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF VGOx = 0, Release THC+ :02 OMS ENG(s) – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
:
**********************************************************
**********************************************************
ENT–5bb/D/I
PREBANK/FRCS COMPLETION
THC +X to TGT HP
)
%
% then
3–28 ENT/ALL/GEN FMS ONLY
This Page Intentionally Blank
3–29 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
3–30 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
PO
ST
BU
RN
A3–31 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC SYS SUMM 2
**********************************
C3O8
F6,F8C3
C3
O8
O7
O8
F6,F8C3
If no OMS IGNITION at TIG:OMS ENG (two) – OFF
�APU – SHUT DNMSTR MADS PWR – OFFL,R OMS
He PRESS/VAP ISOL (four) – CL�XFEED (four) – CL
GNC, OPS 301 PROFLT CNTLR PWR (two) – OFF
�DAP: AUTO�MCC at next AOS
If burn terminated with HP > SAFE HP:�OMS ENG (two) – OFF�APU – SHUT DN
MSTR MADS PWR – OFFOPS 301 PROIf I’CNCT:
DAP: INRTL/PULSEL, R OMS
He PRESS/VAP ISOL (four) – CL�XFEED (four) – CL
AFT L,R RCSHe PRESS A (two) – GPC (tb–OP)He PRESS B (two) – CL (tb–CL)TK ISOL (six) – OP (tb–OP)XFEED (four) – CL (tb–CL)
FWD RCSHe PRESS A – GPC (tb–OP)He PRESS B – CL (tb–CL)
FLT CNTLR PWR (two) – OFF�DAP: AUTO�MCC at next AOS on DEORBIT DELAY
of 24 hr
**********************************
MEDSENT/MEDS/GEN F
PO
ST
BU
RN
A3–32 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC SYS SUMM 2
MS Stow Flight Deck SpOC
B F6,F8 FLT CNTLR PWR (two) – OFFC3 �DAP: AUTO
OMS/RCS POST BURN RECONFIG
P O7 AFT L,R RCS�He PRESS (four) – OP (tb–OP)�TK ISOL (six) – GPC (tb–OP)�XFEED (four) – GPC (tb–CL)
O8 L,R OMSHe PRESS/VAP ISOL (four) – CL
�TK ISOL (four) – OP (tb–OP)
**
If OMS PRPLT FAIL,�Aff TK ISOL (two) – CL
**
XFEED (four) – CL (tb–CL)
O3 RCS/OMS PRESS sell – RCS as reqdRCS/OMS PRPLT QTY sel – RCS as reqd
MEDSENT/MEDS/GEN F
PO
ST
BU
RN
B3–31 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC SYS SUMM 2
**********************************
C3O8
F7,F8C3
C3
O8
O7
O8
F7,F8C3
If no OMS IGNITION at TIG:OMS ENG (two) – OFF
�APU – SHUT DNMSTR MADS PWR – OFFL,R OMS
He PRESS/VAP ISOL (four) – CL�XFEED (four) – CL
GNC, OPS 301 PROFLT CNTLR PWR (two) – OFF
�DAP: AUTO�MCC at next AOS
If burn terminated with HP > SAFE HP:�OMS ENG (two) – OFF�APU – SHUT DN
MSTR MADS PWR – OFFOPS 301 PROIf I’CNCT:
DAP: INRTL/PULSEL, R OMS
He PRESS/VAP ISOL (four) – CL�XFEED (four) – CL
AFT L,R RCSHe PRESS A (two) – GPC (tb–OP)He PRESS B (two) – CL (tb–CL)TK ISOL (six) – OP (tb–OP)XFEED (four) – CL (tb–CL)
FWD RCSHe PRESS A – GPC (tb–OP)He PRESS B – CL (tb–CL)
FLT CNTLR PWR (two) – OFF�DAP: AUTO�MCC at next AOS on DEORBIT DELAY
of 24 hr
**********************************
ENT/NOM/GEN FNOM
PO
ST
BU
RN
B3–32 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC SYS SUMM 2
MS Stow Flight Deck SpOC
B F7,F8 FLT CNTLR PWR (two) – OFFC3 �DAP: AUTO
OMS/RCS POST BURN RECONFIG
P O7 AFT L,R RCS�He PRESS (four) – OP (tb–OP)�TK ISOL (six) – GPC (tb–OP)�XFEED (four) – GPC (tb–CL)
O8 L,R OMSHe PRESS/VAP ISOL (four) – CL
�TK ISOL (four) – OP (tb–OP)
**
If OMS PRPLT FAIL,�Aff TK ISOL (two) – CL
**
XFEED (four) – CL (tb–CL)
O3 RCS/OMS PRESS sell – RCS as reqdRCS/OMS PRPLT QTY sel – RCS as reqd
ENT/NOM/GEN FNOM
3–33 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
3–34 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
A3–35 ENT/ALL/GEN F
1: GNC 53 ENTRY CONTROLS 2: BFS, GNC SYS SUMM 23: GNC DEORB MNVR COAST
EI–20 C SECONDARY ACTUATOR CHECK(if not previously performed and time permits)
NOTEIf port does not bypass during check, bypassaffected port after check:
SEC ACT BYPASS – ITEM 8 +X X EXECIf affected port still does not bypass:
SEC ACT RESET – ITEM 9 +X X EXEC
R2 1. HYD MN PUMP PRESS (one) – NORM
CRT3 2. SURF DRIVE ON, ITEM 39 EXEC (*)Wait at least 5 sec
MDU �SPI: Stop drive test when elevon posnswithin +12° to –27°
SURF DRIVE OFF, ITEM 40 EXEC (*)
CRT1 3. �POS STIM ENA, ITEM 7 – (no *)
C3 4. �FCS CH 1,2,3,4 – AUTO
CRT1 5. SEC ACT CK, CH 1 – ITEM 1 EXEC (*)SEC ACT CK, START – ITEM 5 EXEC (*)
6. �All CH 1 PORTS BYPASS, ‘↓’STOP – ITEM 6 EXEC (*)
C3 7. FCS CH 1 – ORIDECRT1 �All CH 1 PORTS RESET, no ‘↓’
FCS CH 1 – AUTO
8. Repeat steps 5 thru 7 for CH 2,3,4
MEDSENT/MEDS/GEN F
A3–36 ENT/ALL/GEN F
1: GNC 23 RCS 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
EI–18 P FORWARD RCS DUMP(Use for off–nominal X cg entry)
Determine FWD RCS ‘DUMP TO %’ using lowestof Ox or Fu qty (calculator or DEL PAD)
FOUR JET DUMP:
F RCS PRPLT TO BE DUMPED (%)
0 605040302010
10090807060
0:000:09
0:180:27
0:360:45
0:541:03
1:121:21
1:301:39
1:48
1:481:57
2:062:15
2:242:33
2:422:52
3:00
TIME FROM DUMP INITIATION (M:S)
NOTEDuring dump disregard FRCS qty
MEDS
B3–35 ENT/ALL/GEN F
1: GNC 53 ENTRY CONTROLS 2: BFS, GNC SYS SUMM 23: GNC DEORB MNVR COAST
EI–20 C SECONDARY ACTUATOR CHECK(if not previously performed and time permits)
NOTEIf port does not bypass during check, bypassaffected port after check:
SEC ACT BYPASS – ITEM 8 +X X EXECIf affected port still does not bypass:
SEC ACT RESET – ITEM 9 +X X EXEC
R2 1. HYD MN PUMP PRESS (one) – NORM
CRT3 2. SURF DRIVE ON, ITEM 39 EXEC (*)Wait at least 5 sec
F7 �SPI: Stop drive test when elevon posnswithin +12° to –27°
SURF DRIVE OFF, ITEM 40 EXEC (*)
CRT1 3. �POS STIM ENA, ITEM 7 – (no *)
C3 4. �FCS CH 1,2,3,4 – AUTO
CRT1 5. SEC ACT CK, CH 1 – ITEM 1 EXEC (*)SEC ACT CK, START – ITEM 5 EXEC (*)
6. �All CH 1 PORTS BYPASS, ‘↓’STOP – ITEM 6 EXEC (*)
C3 7. FCS CH 1 – ORIDECRT1 �All CH 1 PORTS RESET, no ‘↓’
FCS CH 1 – AUTO
8. Repeat steps 5 thru 7 for CH 2,3,4
ENT/NOM/GEN FNOM
B3–36 ENT/ALL/GEN F
1: GNC 23 RCS 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
EI–18 P FORWARD RCS DUMP(Use for off–nominal X cg entry)
Determine FWD RCS ‘DUMP TO %’ using lowestof Ox or Fu qty (calculator or DEL PAD)
FOUR JET DUMP:
F RCS PRPLT TO BE DUMPED (%)
0 605040302010
10090807060
0:000:09
0:180:27
0:360:45
0:541:03
1:121:21
1:301:39
1:48
1:481:57
2:062:15
2:242:33
2:422:52
3:00
TIME FROM DUMP INITIATION (M:S)
NOTEDuring dump disregard FRCS qty
NOM
3–37 ENT/ALL/GEN F
1: GNC 23 RCS 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
TWO JET DUMP:
F RCS PRPLT TO BE DUMPED (%)
0 605040302010
10090807060
0:000:18
0:350:53
1:111:28
1:462:04
2:212:39
2:563:15
3:32
3:323:50
4:084:25
4:435:01
5:185:36
5:54
TIME FROM DUMP INITIATION (M:S)
NOTEDuring dump disregard FRCS qty
CRT2 FWD RCS ARM – ITEM 36 EXECFWD RCS DUMP – ITEM 37 EXEC
(Start watch)When dump time achieved:
FWD RCS OFF – ITEM 38 EXEC
3–38 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
ENTRY SW CHECK
C L2 �CAB RELIEF A,B – ENA (tb–ENA)�ANTISKID – ON�NWS – 1�ENTRY MODE – AUTO
3: GNC 51 OVERRIDE
�ROLL MODE – AUTO
B L2/C3 �SPD BK – Full Fwd
P C3 �SRB SEP – AUTO�ET SEP – AUTO
B F6/F8 �AIR DATA – NAVADI ERR – MEDADI RATE – MED
�HSI SEL MODE – ENTRYC F6 HSI SE �� �SOURCE (two) – NAV, 1P F8 HSI SE �� �SOURCE (two) – NAV, 2
B F3 �TRIM RHC/PNL (two) – INH�PNL (two) – ON
Exercise BRAKE PEDALS
A3–39 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
NOTEIf NAVAIDS OFF due to PKT C/LPWRDN, switch ON per PWRDNprocedure
C F6 �RADAR ALTM – 1P F8 RADAR ALTM – 2
O8 �RADAR ALTM (two) – ON�MLS (three) – ON (PASS)�MLS CH (three), FS 3–2
O7 �TACAN MODE (three) – GPCRACA �� �ANT SEL (three) – AUTO
�TACAN CH (three), FS 3–2
MEDSENT/MEDS/GEN F
A3–40 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
EI–13 REMAINING APUs START
**
If an APU failed to start at TIG–5,start remaining good APU only
**
R2 APU FUEL TK VLV (two) – OP�APU/HYD RDY tb (two) – gray
* If tb – bp, attempt normal start *
APU OPER (two) – START/RUNMDU �HYD PRESS ind (two) – LO green
R2 �RDY tb (two) – bp
*****
If OIL OUT P < 25 and OIL OUTTEMP not increasing after APUstart or no start:
Shut down APU (ENT PKT,APU/HYD)
*****
MEDSENT/MEDS/GEN F
B3–39 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
NOTEIf NAVAIDS OFF due to PKT C/LPWRDN, switch ON per PWRDNprocedure
C F7 �RADAR ALTM – 1P F8 RADAR ALTM – 2
O8 �RADAR ALTM (two) – ON�MLS (three) – ON (PASS)�MLS CH (three), FS 3–2
O7 �TACAN MODE (three) – GPCRACA �� �ANT SEL (three) – AUTO
�TACAN CH (three), FS 3–2
NOMENT/NOM/GEN F
B3–40 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2
EI–13 REMAINING APUs START
**
If an APU failed to start at TIG–5,start remaining good APU only
**
R2 APU FUEL TK VLV (two) – OP�APU/HYD RDY tb (two) – gray
* If tb – bp, attempt normal start *
APU OPER (two) – START/RUNF8 �HYD PRESS ind (two) – LO greenR2 �RDY tb (two) – bp
*****
If OIL OUT P < 25 and OIL OUTTEMP not increasing after APUstart or no start:
Shut down APU (ENT PKT,APU/HYD)
*****
NOMENT/NOM/GEN F
3–41 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, SM SYS SUMM 2
*******************
If two APUs operating:�Good HYD MN PUMP PRESS
(two) – LO until EI–6, thenperform SSME HYD REPRESS atEI–6, and delete HYD FLUIDTHERMAL CONDITIONING
If only one APU operating:(Good) APU AUTO SHUTDN (one) – INH
�APU HYD MN PUMP PRESS (one) – LO
Delete SSME HYD REPRESS andHYD FLUID THERMALCONDITIONING
Delay MM304 trans until EI–2Immediately prior to MM304 trans:
(Good) HYD MN PUMP PRESS(one) – NORM
APU SPEED SEL (one) – HI
*******************
HYD MN PUMP PRESS (three) – NORMHYD PRESS ind (three) – HI green
P SSME HYD REPRESS
R2 �HYD MN PUMP PRESS (three) – NORM
**
If HYD SYS 2 or SYS 1 failed,cycle SYS 3
**
R4 HYD MPS/TVC ISOL VLV SYS 2 – OP(MA possible)
Hold 5 sec,�tb – OPWait 10 sec – CLHold 5 sec,�tb – CL
HYD MPS/TVC ISOL VLV SYS 1 – OP(MA possible)
Hold 5 sec,�tb – OPWait 10 sec – CLHold 5 sec,�tb – CL
3–42 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, SM 0 THERMAL
**************
EI–11>P HYD FLUID THERMAL CONDITIONING (MCC CALL)
CRT2 SURF DRIVE ON – ITEM 39 EXECStart TIMER
SPI Observe AEROSURFACES CYCLINGELEV U33 to D18 degRUD R5 to L5 degSPDBK 15 to 10%BDY FLP 93.6 to 3.5%
When SURF DRIVE ON (5 min),CRT2 SURF DRIVE OFF – ITEM 40 EXEC
**************
BURN REPORT (from FS 3–33)
B Stow DEORBIT BURN and DEORBITBURN MONITOR Cue Cards
�ENTRY Cue Cards installed
** ALL
If 8 psi cabin entry, �Tabs/Visor – CL/LES O2 – ON
**
*******************
*******************
A3–43 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC 50 HORIZ SIT3: BFS, GNC 50 HORIZ SIT
G SUIT INFLATION
ALL Load – 1.5 (three turns cw if reqd)
FCS CH CONFIG
If less than four PASS GPCs, config FCSCHs so that each GPC cmds equalnumber of CHs (see table)
GNC 53 CONTROLSConfig SURF FBK (see table)
AVAILABLE FCH CH CONFIG SURF FDBK
GPCs FCS CHs AUTO ORIDE OFF SEL DESEL
3 432
33
2
112
332
1 �1 �2 *
2 432
422
22
422
2 *2 *
� If CH 4 – OFF, do not desel PASS SURF FDBK
MEDSENT/MEDS/GEN F
A3–44 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST
B F6,F8 FLT CNTLR PWR (two) – ON
EI–7 If Mini–Cam Entry video reqd:MS2 O19 TV PWR – ON
V10 PWR – ONDISPLAY pb – Toggle to display tapecount
REC pb (two) – Press to beginrecording
�LCD displays RED DOT
EI–6 Go to ENTRY MANEUVERS (Cue Card)
MEDSENT/MEDS/GEN F
*******************
*******************
B3–43 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC 50 HORIZ SIT3: BFS, GNC 50 HORIZ SIT
G SUIT INFLATION
ALL Load – 1.5 (three turns cw if reqd)
FCS CH CONFIG
If less than four PASS GPCs, config FCSCHs so that each GPC cmds equalnumber of CHs (see table)
GNC 53 CONTROLSConfig SURF FBK (see table)
AVAILABLE FCH CH CONFIG SURF FDBK
GPCs FCS CHs AUTO ORIDE OFF SEL DESEL
3 432
33
2
112
332
1 �1 �2 *
2 432
422
22
422
2 *2 *
� If CH 4 – OFF, do not desel PASS SURF FDBK
NOMENT/NOM/GEN F
B3–44 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST
B F7,F8 FLT CNTLR PWR (two) – ON
EI–7 If Mini–Cam Entry video reqd:MS2 O19 TV PWR – ON
V10 PWR – ONDISPLAY pb – Toggle to display tapecount
REC pb (two) – Press to beginrecording
�LCD displays RED DOT
EI–6 Go to ENTRY MANEUVERS (Cue Card)
ENT/NOM/GEN FNOM
EN
T C
UE
CA
RD
S
4–1 ENT/ALL/GEN F MS ONLY
ENTRY CUE CARDS
EN
T C
UE
CA
RD
S
4–2 ENT/ALL/GEN F MS ONLY
This Page Intentionally Blank
4–3 ENT/ALL/GEN F MS ONLY
ENTRY NO–GO CHECKLIST
ENT–7a/E/I
AERO AUTO XWINDFAILURE OF: PTI DTO FCS DTO
MODE 1APU/HYD: 1 APU X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 APUs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISPLAYS: 2 ADIs X. . . . . . . . . . . . . . . . . . . .
CDR HUD X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTROLLERS:
RHC: 1L X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RHC: 2L & 2R X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RPTA: 2L or 2R X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GNC: 2 AAs (LAT) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 AAs (NORM) X(M < 2.5) X. . . . . . . . . . . . . . . . . . 2 RGAs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 R DDU PWR SPLY X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 IMU (or 1 IMU + BITE) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADTA NOT INCORP
OR DLMA X (M < 2). . . . . . . . . . . . . . . . . . . . . . . . . . . . MLS NOT INCORP X(< 6K ft). . . . . . . . . . . . . . . . . . . . . 2 FCS CH (same surface) X X. . . . . . . . . . . . . . . . . . . . . . . . . .
DPS: 1 GPC (not restrung) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 GPC (restrung) X. . . . . . . . . . . . . . . . 2 GPC (not restrung) X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 FF X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FF X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
RCS: LEAK (AFT – during ENT) X. . . . . . . 2 YAW JETs (same side) X. . . . . . . . . MIN RCS QTY X. . . . . . . . . . . . . . . . . .
TRIM: Ail > ± 2.0 deg X. . . . . . . . . . . . . . . . . . DOWNMODE:
FCS problem X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AOA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PLB: PLBD Latch Gang X. . . . . . . . . . . . . . . LDG/DECEL:
Tire Leak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HYD BRAKE ISOL VLV X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . < 100% Brakes X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NWS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ENERGY – OFF NOMINAL:Roll Ref Alert X. . . . . . . . . . . . . . . . . . . Above Upper Traj Line X. . . . . . . . . . . . MCC GCA, or VEL & PSN
update X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No A/L by 6K ft X. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DATA: OPS RECORDERS X(LOS). . . . . . . . . . . . XWIND:
< 10 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 15 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 10 Knots Gust X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GROUND SYSTEMS:No Runway Aim Point X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
NOTES
1 Consider runway redesignation (M > 6) to avoid Xwind landing2 GO if PAPI and BALL BAR available3 Pitch AUTO mode NO–GO for M < 2.54 GO if only string 4 affected
4
4
2
3
3
3
4–4 ENT/ALL/GEN F MS ONLY
ENTRY MANEUVERS
FLIGHTCONDITIONS MANEUVER
EI–5�LVLH ATT
GNC, OPS 304 PROIf PREBANK, R/Y – CSSRoll at 1°/sec toMaintain PREBANK ± 5°
If previous OMS OX TK or He TK or RCS OX TKleak: G51 VENT DOORS – OP
PTI – ENA at EI–5 when applicable
***
***
q = 1– (AOA) HYD MN PUMP PRESS (three) – NORM
‘GuidanceBox’ @
q ∼8or
D ∼3
–
CLOSED LOOP GUIDANCE ____:____:____If PREBANK: P,R/Y – AUTO
Begin AIL trim monitoring* *
D = 11 �DRAG H (FORCE if editing)V = 19K �MPS/TVC ISOL VLV – CLV = 15K �NAVAIDS (I/O RESET if reqd)
If ELS: UHF MODE – G T/R* *
V = 12K RAD BYP VLV MODE (two) – AUTOCNTLR LOOP (two) – AUTO B(A)
V = 10K �SPDBK to 81%
∆Az = 10.5° FIRST ROLL REVERSAL
ENT–6a/E/L
4–5 ENT/ALL/GEN F MS ONLY
ENT–6b/E/Q(Partial)
FLIGHTCONDITIONS MANEUVER
V = 7K �TACAN status
V = 5K ADTA PROBES – DEPLOY (�HEAT)Begin AIL and RUD trim monitoring
M = 2.7�APUs
HUD PWR (two) – ON
* If M < 2.5; P CSS for ADTA to G&C incorp *
M = 2.0 Ensure ADTA to G&C else �Theta limits
M = 0.9 P, R/Y – CSS as reqd�SPDBK CMD vs POS�R FLT CNTLR – ON�NWS – 1
Lock Inertia Reels
.MAX Nz
M = 0.7 �LG EXTEND ISOL VLV – OP
h = 15K �MLS
h = 10K �A/L, TABS/VISORS – CL/LES O2 – ON (KSC)
h = 2K LANDING GEAR ARM pb – ARM
h = 300 LANDING GEAR DN pb – DN
MAIN GEAR TD �SPDBK – 100%
V = 195 KEAS DRAG CHUTE pb (two) – ARM, DPY (simo)
V = 185 KEAS DEROTATE
NOSE GEAR TDSRB SEP – MAN/AUTO and depress pb
�Auto Load Relief�HYD BRAKE ISOL VLV (three) – OP
MIDFIELD andV < 140 KGS BRAKE as required (8–10 fps2, –0.25 to –0.3G)
* If 5K’ remaining and V > 140 KGS – MAX BRAKING *
V = 60 KGS DRAG CHUTE JETT pb – JETT
V = 40 KGS BRAKE < 6 fps2 (–0.2G) (Antiskid cutout)
WHEEL STOP Go to ENT C/L, POST LANDING PROCEDURES
4–6 ENT/ALL/GEN F MS ONLY
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4–7 ENT/ALL/GEN F
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4–8 ENT/ALL/GEN F
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EN
TR
YM
ISC
4–9 ENT/ALL/GEN F MS ONLY
50K
38K
28K
20K
12K
7K
/
/
/
/
/
/
/
ENT–6b/E/Q
SURF /
3K
/1K
DRAG CHUTE DEPLOYMCC Call Flight ConditionEarly Main Gear TDNOMINAL 195 KEAS
If leaking/flat tiredelay derot 10 kts
Late Post–Nose Gear TDXwind DTO
EmergencyOnly
No DeployExcept CDR call
NO DEPLOYprior to MGTD> 230 KEAS< 80 KGSXwind > 15 kts
(Partial)
EN
TR
YM
ISC
4–10 ENT/ALL/GEN F MS ONLY
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4–11 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
4–12 ENT/ALL/GEN F
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4–13 ENT/ALL/GEN F MS ONLY
ENTRY CONTROLARCS QTY (L + R) < 10%ARCS QTY = 0 & JETSFAIL OFF
1. ENTRY MODE – NO Y JET(R/Y CSS; expect sluggish control)
q ≥ 20 & M > 6 2. G51 ELEVON FIXED – ITEM 18 EXEC (*)
CONTROLPROBLEMS* &ARCS QTY > 0
3. ENTRY MODE – AUTOWhen control regained:
4. ENTRY MODE – NO Y JET5. �AIL trim
M < 6 & ARCS QTY > 0 6. ENTRY MODE – AUTOM < 5 7. TRIM/RHC PNL – ENA
8. TRIM ROLL – away from AIL trim (to < 1)*Region of least margin: M 12–8
AIL TRIM ≥ 3°TAL 1. G51 WRAP MODE – ITEM 45 EXEC (ACT)AIL trim = 5 2. BF – MAN
3. BF – UP (to 0%)NO Y JET 4. Perform roll reversals at 3°/s (expect sluggish control)M < 13 &AIL trim = 5
5. P – CSS6. Fly α per schedule:
M 12 11 10 9 8–6 5α 37 36 35 33 30 26
M < 5 7. TRIM/RHC PNL – ENA8. TRIM ROLL – away from AIL trim (to < 1)9. P – AUTO
M < 2 10. BF – AUTOENT–10a/A,E/A
HIGH–FREQ OSC OR SURF/JET CYCLEReturning PL> 10K lbs
1. G51 �FILTER ALT – ITEM 21 (*)
2. P, R/Y – CSSOsc/Cycle continues 3. ENTRY MODE – LO GAIN
Osc/Cyclestops
4. ENTRY MODE – AUTO5. P, R/Y – AUTO
ENT–10b/A,E/A
4–14 ENT/ALL/GEN F MS ONLY
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4–15 ENT/ALL/GEN F MS ONLY
RATIO < 1
MCC: AUTOor INH*
COMMOK
NOCOMM
IF BADADTA
RATIO > 1
G&CNAV
AUTO
TACANOK
MCC: INH
IF BAD NAVSTATE
MCC:FORCE
NO TACANADTA
ERRATICADTA
STEADYINH AUTO FORCE
Two or moregood ADTAs
Evaluate h,�,MMCC:
AUTO (G&C)
Evaluate h,�,MIf reasonable:
AUTO (G&C)
*(If ADTA H will degrade NAV state)
ADTA MGMT
V = 6K NO COMM TACAN MGMT
If 1st acq –FORCE
IF NOT –ZERO �STATE
RATIO< 1 RATIO > 1 ONE TACAN
LOCKED NO LOCK
AUTO TROUBLESHOOT BELOW V =5.5K
DESELECTMISSINGTACANS,then –AUTO
BELOW V =5.5K
TOGGLETACAN
IF BADTACAN
IF BAD NAVSTATE
AUTO
For � STATE UPDATES (on MCC call):P, R/Y – CSSDRAG H, TACAN, ADTA – INHOn MCC call, back to AUTO
NAV DELTA PAD
�Z 15 ( )
( )
( )
( )
( )
( )�X 10
�Y 11
�Z 12
�X 13
�Y 14
4–16 ENT/ALL/GEN F MS ONLY
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PO
ST
LD
G
5–1 ENT/ALL/GEN F
POST LANDING PROCEDURES
PO
ST
LD
G
5–2 ENT/ALL/GEN F
********************************************
LOSS OF COMMIn event of loss of comm (day or night), the following signalswill be utilized to indicate onboard status to convoy:
Crew should continue signals until acknowleged by convoyFrom Crew (with Mini Mag light stowed in ACES orSpotlight stowed in volume 3b)Crew OK Circular motionOMS/RCS & Hatch safed Circular motionAPU shutdn Circular motionCrew needs assistance;will open/blow hatch Vertical motion
Crew needs assistance;will not open/blow hatch Horizontal motion
From ConvoyConvoy will acknowledge crew signals with sequence ofthree flashes of headlights on convoy vehicle
Continuous flashing – Emer pwrdn and egress
*************************************************EXPEDITED PWRDNAccomplish for:
� Loss of all comm, including hand signals, withconvoy elements
� Loss of telemetry and onboard systems monitoringvisibility
� Fuel leak (OMS, RCS, or APU) if:– Nonisolatable, or– Leak occurs during RTLS, TAL, AOA, or
POST D/O TIG� Fire Suppression Bottle discharged during entry for
confirmed or suspected fireIf APU, OMS, RCS Fuel Leak:
APUs OFF ASAPAs time permits:
RCS,OMS SAFING (RJDs), 5–4GPC DEACT
O6 GPC MODE 1,2,3,4,5 (five) – STBY (tb–bp)O6 GPC MODE 1,2,3,4,5 (five) – HALT
ET UMBILICAL DOOR OPENING, 5–5 (RTLS/TAL only)‘MODE 5’ POST LANDING EGRESS Cue Card (CDR orMCC call) then EMER PWRDN Cue Card
NOTEBefore declaring loss of comm, attempt to contactconvoy on 259.7 using PRC–112 radio channel A
********************************************
ENT/ALL/GEN F,1
A5–3 ENT/ALL/GEN F
1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2
POST LANDING
WARNINGAPUs OFF ASAP for APUHydrazine, OMS, RCS (FWD orAFT), or MPS propellant leak
00:00 After orbiter stops:C Report, “WHEELS STOP”
Establish COMM with NCC
L2 SPD BK – MAN, full fwdNWS – OFF
P If RTLS or TAL abort:Perform ET UMBILICAL DOOROPENING, 5–5
R2 �APU AUTO SHUTDN (three) – ENAAP �� �SPEED SEL (three) – NORM
R1 �AC BUS SNSR (three) – AUTO
C F6 FLT CNTLR PWR – OFF
B F3 HUD PWR (two) – OFF
If ELS:P C3 MSTR MADS(OEX) PWR – OFF
(OEX for OV102)DoD ELS, MCC call DoD OSC onNCC
NOTEMCC will report “GO/NO–GOTO DOFF SUITS” (post safetyassessment)
ENT/MEDS/GEN FMEDS
A5–4 ENT/ALL/GEN F
1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2
CDRNOTE
CDR activities are now on evennumbered pages and PLTactivities on odd numbered pages
RCS, OMS SAFING (RJDs)C3 �OMS ENG (two) – OFFO14:F RJD DRIVER (nine) – OFFO15:F RJD LOGIC (eight) – OFFO16:F OMS ENG VLV (two) – OFF
C,P,MS DRAG CHUTE SAFING(Not performed if ELS)
O15:E cb MNB DRAG CHUTE SYS 2 – opO16:E cb MNC DRAG CHUTE SYS 1 – opF2,F3, �DRAG CHUTE PBI lts (six) – off F4
DEACT AIR DATA PROBE HTRSC3 �AIR DATA PROBE (two) – DPY
C,P,MS LANDING GEAR SAFING(Not performed if ELS)
R14:F cb ESS 1BC LDG GEAR ARM/DNRESET – cl
NOTESM0 TIRE PRESS msgs occurwhen LG ARM/DN RESETperformed
A12 LG ARM/DN RESET – RESETF6,F8 �LDG GEAR pb (four) – lt offA12 LG ARM/DN RESET – dnR14:F cb ESS 1BC LDG GEAR ARM/DN
RESET – op
Check with MS3. Report to MCC: “RJDsOFF, SIDE HATCH, DRAG CHUTE,AND LANDING GEAR SAFED” (MCCreport to NCC) MEDS
B5–3 ENT/ALL/GEN F
1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2
POST LANDING
WARNINGAPUs OFF ASAP for APUHydrazine, OMS, RCS (FWD orAFT), or MPS propellant leak
00:00 After orbiter stops:C Report, “WHEELS STOP”
Establish COMM with NCC
L2 SPD BK – MAN, full fwdNWS – OFF
P If RTLS or TAL abort:Perform ET UMBILICAL DOOROPENING, 5–5
R2 �APU AUTO SHUTDN (three) – ENAAP �� �SPEED SEL (three) – NORM
R1 �AC BUS SNSR (three) – AUTO
C F7 FLT CNTLR PWR – OFF
B F3 HUD PWR (two) – OFF
If ELS:P C3 MSTR MADS(OEX) PWR – OFF
(OEX for OV102)DoD ELS, MCC call DoD OSC onNCC
NOTEMCC will report “GO/NO–GOTO DOFF SUITS” (post safetyassessment)
NOMENT/NOM/GEN F
B5–4 ENT/ALL/GEN F
1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2
CDRNOTE
CDR activities are now on evennumbered pages and PLTactivities on odd numbered pages
RCS, OMS SAFING (RJDs)C3 �OMS ENG (two) – OFFO14:F RJD DRIVER (nine) – OFFO15:F RJD LOGIC (eight) – OFFO16:F OMS ENG VLV (two) – OFF
C,P,MS DRAG CHUTE SAFING(Not performed if ELS)
O15:E cb MNB DRAG CHUTE SYS 2 – opO16:E cb MNC DRAG CHUTE SYS 1 – opF2,F3, �DRAG CHUTE PBI lts (six) – off F4
DEACT AIR DATA PROBE HTRSC3 �AIR DATA PROBE (two) – DPY
C,P,MS LANDING GEAR SAFING(Not performed if ELS)
R14:F cb ESS 1BC LDG GEAR ARM/DNRESET – cl
NOTESM0 TIRE PRESS msgs occur whenLG ARM/DN RESET performed
A12 LG ARM/DN RESET – RESETF6,F8 �LDG GEAR pb (four) – lt offA12 LG ARM/DN RESET – dnR14:F cb ESS 1BC LDG GEAR ARM/DN
RESET – op
Check with MS3. Report to MCC:“RJDs OFF, SIDE HATCH, DRAGCHUTE, AND LANDING GEARSAFED” (MCC report to NCC)NOM
SETUP:
BF
LOAD TEST:
RELEASE:
R
BF�
�BF
�R
R�
>
�
�
��
�>
>
5–5 ENT/ALL/GEN F
1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2
PLT ET UMBILICAL DOOR OPENING
Report to MCC, “ET UMBILICALDOORS ARE COMING OPEN”
R2 ET UMB DRMODE – GPC/MANR LAT – REL (tb–bp, REL ∼6 sec)R LAT – OFFR DR – OP (tb–bp)Wait 12 sec, R DR – OFF (tb–bp)L LAT – REL (tb–bp, REL ∼6 sec)L LAT – OFFL DR – OP (tb–bp)Wait 12 sec, L DR – OFF (tb–bp)MODE – GPC
HYDRAULIC LOAD TEST (ON MCC CALL)NOTE
Minimum of two operating hydsystems is reqd for this test
F4 BDY FLP pb – MANF8 �FLT CNTLR PWR – ON
NOTEIf only two systems are operating, donot depressurize either hyd pump
R2 HYD MN PUMP PRESS 1 – LO (MA)C3 Run Full Load Test:
BDY FLP – TRAILRHC – Forward ctrRudder full left
When set, do following simo:BDY FLP – UP (to � 6%)RHC – move to aft ctrRudder full right
RHC – releaseRudder – neutralBDY FLP – reset to TRAIL
R2 HYD MN PUMPPRESS 1 – NORMPRESS 3 – LO (MA)
C3 Repeat Load TestR2 HYD MN PUMP PRESS 3 – NORM
5–6 ENT/ALL/GEN F
1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2
CDRMCC Report GO/NO–GO for DPS transition
DPS TRANSITION – GNC 9 (If PASS)
NOTEDo not perform any keyboard itementries or switch throws 10 sec beforeand after moding PASS GPCs to RUNor making OPS transition requests.
MCC will call for BFS to be taken fromRUN to STBY for OPS Recorderdumping and PL monitoring as reqd
�BFC CRT DISP – ON
CRT3 BFS, GNC, OPS 000 PRO
3: BFS, GNC BFS MEMORY
1: GNC 0 GPC MEMORY
Verify:
STR 1 12 23 34 4
PL 1/2 1CRT 1 1
2 23 34 0
L 1 12 2
MM 1 12 2
912340
CONFIGGPC
CRT1 GNC, OPS 901 PRO
5–7 ENT/ALL/GEN F
1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2
PLT SET BODY FLAP (Prior to OPS 9)F4 BODY FLAP pb – MANC3 BODY FLAP – DOWN (100%)
PLT SSME REPOSITIONING (If PASS, OPS 9,and GO from MCC)
2: GNC 105 TCS CONTROL
R4 HYD MPS/TVC ISOL VLV SYS (three) – OPHold 5 sec, �tb – OP
**
If less than two HYD MPS/TVCISOL VLVs open, �MCC
**
CRT2 CLEAR MSG – ITEM 8 EXECSELECT ID – ITEM 1 +0 2 EXEC
�NAME VFB 84 (∼60 sec)MM READ – ITEM 2 EXEC
�‘AI MODE 1(0,3) COMPLETE’ msg (∼2.5 min)�‘VFB 84 – COMPLETE’ msg
***
If any ‘AI MODE X FAILED RETEST’ msg:�MCC, report ECP ERROR
To terminate: CANCEL – ITEM 5 EXEC
***
Go to APU/HYD SHUTDN >>
PLT SPDBK REPOSITIONING (KSC only, ON MCC GO)
R4 �HYD MPS/TVC ISOL VLV SYS (three) – CL
2: GNC 113 ACTUATOR CONTROL
CRT2 Al MODE 1 MDM – ITEM 23 EXEC (*)I �ACTUATOR GIMBALING STATUS – RUN, CPLTSB – ITEM 1 EXEC (*)RATE – ITEM 29 +1 EXECFIN POS – ITEM 30 +8 EXEC
�START 31 – → ←START – ITEM 31 EXEC (*→ ←)
�STATUS – RUN, CPLT (∼30 sec)
**
If STATUS – STOP or BUSY:�MCC, (To terminate: ITEM 32 EXEC)
**
Go to APU/HYD SHUTDN >>
5–8 ENT/ALL/GEN F
1: AS DESIRED 2: AS DESIRED3: AS DESIRED
CDR RAD RECONFIG(On MCC call, unless no COMM)
O1 When FREON EVAP OUT TEMP > 40degF:
L1 RAD OUT TEMP – HIO1 When FREON EVAP OUT TEMP > 55
degF, proceed to NH3 ACT
NH3 ACTO1 When FREON EVAP OUT TEMP > 55
degF, select one of the following asspecified by MCC:
L1 NH3 CNTLR A – PRI/GPC ( )NH3 CNTLR A – SEC/ON ( )NH3 CNTLR B – PRI/GPC ( )NH3 CNTLR B – SEC/ON ( )
*******************
O1L1
O1
During NH3 ops:If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP < 32 degF:
1. FREON PUMP LOOP 1,2(two) – OFF (ASAP)
2. H2O PUMP LOOP 1 – ON3. NH3 CNTLR A(B) – OFFIf no PL H2O Loop present:
4. FLOW PROP VLV LOOP 1,2(two) – PL HX (tb–PL)
If PL H2O Loop present:5. Activate PL H2O Loop
6. FREON PUMP LOOP 1 – BWait 3 min, then:
7. FREON PUMP LOOP 2 – B8. Go to NH3 RECONFIG, 5–22 >>
If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP > 65 degF:
9. Go to NH3 RECONFIG, 5–22
*******************
5–9 ENT/ALL/GEN F
1: AS DESIRED 2: AS DESIRED3: BFS, SM SYS SUM 2
PLT APU/HYD SHUTDN
�SSME REPOS complete (if PASS)
R4 HYD MPS/TVC ISOL VLVS (1,2,3; 5 secinterval) – CL (hold each 5 sec) �tb – cl
R2 BLR PWR (three) – OFFBLR N2 SPLY (three) – OFFAPU OPER (1,2,3; 5 sec interval) – OFF (MA)
APU FUEL TK VLV (three) – CLAP �� �Shutdn (Hyd Press)APU CNTLR PWR (three) – OFF
Report to MCC, “APU/HYD SHUTDOWN”MCC Report to Convoy 1, “SSME
REPOSITIONING COMPLETE ANDAPU/HYD SHUTDOWN”
Report, “GO/NO–GO FOR VENT DOORPURGE POSITIONING”
POST LANDING MPS RECONFIG(After APU/HYD shutdn + 1 min)
R2 MPS He ISOL (six) – CL
MPS He I’CNCT L – OUT OPMPS PNEU L ENG He XOVR – CL
NOTEExpect multiple MAs for MPSHe P as regs bleed down
5–10 ENT/ALL/GEN F
1: AS DESIRED 2: AS DESIRED3: AS DESIRED
C,MSC PCS DEACTIVATION
L2 O2 SYS 1,2 SPLY (two) – CL (tb–CL)O �� �EMER tb – bp
MS GPS PWDNA13 (A12 for OV102)
****
If landing not at KSC, EDW, or NOR:GPS ENCRYPT – ZEROIZEWait 1 secGPS ENCRYPT – NORMAL
****
GPS PWR – OFFGPS PRE AMPL UPPER – OFFGPS PRE AMPL LOWER – OFF
MCC Report, “GO/NO–GO FOR EXTENDEDPWR UP”
NOTEIf GO for EXTENDED PWR UP, goto SYS DEACT FOR EXTENDEDPWR UP, 5–14.
If NO–GO for EXTENDED PWR UP,go to GPC DEACT (below)
C GPC DEACT(Perform after RCS/OMS VALVE TESTcompleted by PLT)
O6 GPC MODE 1,2,3,4,5 (five) – STBY (tb–bp)
GPC MODE 1,2,3,4,5 (five) – HALTInform MS to proceed with POSTLANDING PAYLOAD ACTIVITIES(if reqd), FS 5–19
5–11 ENT/ALL/GEN F
1: AS DESIRED 2: GNC 105 TCS CONTROL3: AS DESIRED
PLT VENT DOOR PURGE POSITIONING (PASS)(on MCC GO, not performed if ELS)
CRT2 CLEAR MSG – ITEM 8 EXECSELECT ID – ITEM 1 +0 3 EXEC
�NAME ‘VFB89’ (∼60 sec)MM READ – ITEM 2 EXECAfter ‘VFB89 – ENTERING 30 MINDELAY’ msg, CANCEL – ITEM 5 EXEC
RCS, OMS VALVE TESTPause 1 sec between each line
O7 �MSTR RCS XFEED – OFFO8 L,R OMS He PRESS/VAP ISOL (four) –
CL,GPCL OMS XFEED (two) – OP (tb–OP),then – CL (tb–CL)
R OMS XFEED (two) – OP (tb–OP),then – CL (tb–CL),GPC
L,R OMS TK ISOL(four) – CL (tb–CL),then – OP (tb–OP),GPC
L OMS XFEED (two) – OP (tb–OP),GPCFWD RCS
He PRESS (two) – CL (tb–CL),GPCTK ISOL (two) – CL (tb–CL),then – OP (tb–OP),GPC
MANF ISOL (five) – CL (tb–CL)then – OP(tb–OP),GPC
O7 L,R RCSHe PRESS (four) – CL (tb–CL),GPCMANF ISOL (ten) – CL (tb–CL),then – OP (tb–OP),GPC
TK ISOL (six) – CL (tb–CL)XFEED (four) – OP (tb–OP),then – CL (tb–CL),GPC
TK ISOL (six) – OP (tb–OP),GPC
5–12 ENT/ALL/GEN F
1: OFF 2: OFF3: OFF
C,MS,PS HATCH OPENING (Convoy)
SEAT EGRESS
C,MS,PS Pull G SUIT controller clip (if inflated)Lap Belt and Chute – ReleaseEgress seat (Helmet reqd if ELS)
MS,PS Unstow ‘Return to Houston’ Bags (exceptELS)
HATCH OPENING (ELS)
ALL �Tabs/Visor – CLGreen Apple – PULL
MS Open Hatch/Deploy Slide per decal
C Give PLT GO for VEHICLE PWRDN
C,MS,PS ORBITER UNAIDED EGRESS
Egress orbiterHand carry Landing Site Data book(if ELS) (reference ELS POSTLANDING procedures)
EX
TE
ND
PW
R U
P
A5–13 ENT/ALL/GEN F
1: OFF 2: OFF3: OFF
PLTNOTE
If GO for EXTENDED PWR UP,go to SYS DEACT FOREXTENDED PWR UP, 5–15.
If NO–GO for EXTENDED PWRUP, continue ops
HATCH OPENING (ELS)
Before hatch opening:�Tabs/Visor – CL
Green Apple – PULL
VEHICLE PWRDN (on GO from CDR)
NOTEAll vehicle lighting andorbiter O2 will be lost atpwrdn
R1 MN BUS TIE (three) – OFFFC/MN BUS (three) – OFFESS BUS SOURCE FC (three) – OFF
EGRESS
Pull G SUIT controller clip (if inflated)Egress seat, orbiter(Helmet reqd if ELS)
MCC TO KSC HANDOVER (at crew egress)
MEDS
EX
TE
ND
PW
R U
P
A5–14 ENT/ALL/GEN F
1: GNC 0 GPC MEMORY 2: AS DESIRED3: AS DESIRED
CDR SYS DEACT FOR EXTENDED PWR UP(Perform after Vent Door Purge Positioncompleted by PLT)
1: GNC 0 GPC MEMORY
STR 1 12 13 14 1
PL 1/2 1CRT 1 1
2 13 14 0
L 1 12 1
MM 1 12 1
910000
CONFIGGPC
CRT1 GNC, OPS 901 PRO
GPC PWRDN
O6 GPC MODE 2,3,4 (three) – STBYGPC MODE 2,3,4 (three) – (tb–bp)GPC MODE 2,3,4 (three) – HALT
CRT1 If no GPC failure,ERR LOG RESET – ITEM 48 EXEC
O6 GPC PWR 2,3,4 (three) – OFFLTG (five) – OFF
C2 IDP/CRT 2 PWR – OFF
Inform MS2 to proceed with MS SysDeact activities, 5–18
ENT/MEDS/GEN FMEDS
A5–15 ENT/ALL/GEN F
1: GNC 0 GPC MEMORY 2: AS DESIRED3: AS DESIRED
PLT SYS DEACT FOR EXTENDED PWR UP
F8 FLT CNTLR PWR – OFFF3 TRIM PNL – OFF
TRI �RHC – INHR4 HYD BRAKE HTR (three) – OFFO8 LTG (five) – OFFO17:A ATVC (four) – OFF
MEDSENT/MEDS/GEN F
A5–16 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
C,MS,PS
C L2 ANTISKID – OFF�NWS – OFF
C3 �FCS CH (four) – AUTOF3 TRIM PNL – OFF
TRI �RHC – INHMS If reqd, install and lock PL Bay Window
Shades
IDP/CRT 4 PWRDN
MS R12 IDP/CRT 4 PWR – OFF
EGRESS(After MS Sys Deact complete)
L1 H2O PUMP LOOP 1 – ON
C L5 L COMM PWR – OFF
C,MS,PS PULL G SUIT controller clip (if inflated)Egress seat
MS A11,A15, COMM CCU PWR – OFFMS,PS MO39M
Unstow ‘Return to Houston’ Bags
C,MS,PS Egress orbiter
MEDSENT/MEDS/GEN F
EX
TE
ND
PW
R U
P
B5–13 ENT/ALL/GEN F
1: OFF 2: OFF3: OFF
PLTNOTE
If GO for EXTENDED PWR UP,go to SYS DEACT FOREXTENDED PWR UP, 5–15.
If NO–GO for EXTENDED PWRUP, continue ops
HATCH OPENING (ELS)
Before hatch opening:�Tabs/Visor – CL
Green Apple – PULL
VEHICLE PWRDN (on GO from CDR)
NOTEAll vehicle lighting andorbiter O2 will be lost atpwrdn
R1 MN BUS TIE (three) – OFFFC/MN BUS (three) – OFFESS BUS SOURCE FC (three) – OFF
EGRESS
Pull G SUIT controller clip (if inflated)Egress seat, orbiter(Helmet reqd if ELS)
MCC TO KSC HANDOVER (at crew egress)
NOM
EX
TE
ND
PW
R U
P
B5–14 ENT/ALL/GEN F
1: GNC 0 GPC MEMORY 2: AS DESIRED3: AS DESIRED
CDR SYS DEACT FOR EXTENDED PWR UP(Perform after Vent Door Purge Position completedby PLT)
1: GNC 0 GPC MEMORY
STR 1 12 13 14 1
PL 1/2 1CRT 1 1
2 13 14 0
L 1 12 1
MM 1 12 1
910000
CONFIGGPC
CRT1 GNC, OPS 901 PRO
GPC PWRDN
O6 GPC MODE 2,3,4 (three) – STBYGPC MODE 2,3,4 (three) – (tb–bp)GPC MODE 2,3,4 (three) – HALT
CRT1 If no GPC failure,ERR LOG RESET – ITEM 48 EXEC
O6 GPC PWR 2,3,4 (three) – OFFLTG (five) – OFF
C2 CRT 2 PWR – OFF
Inform MS2 to proceed with MS SysDeact activities, 5–18
ENT/NOM/GEN FNOM
B5–15 ENT/ALL/GEN F
1: GNC 0 GPC MEMORY 2: AS DESIRED3: AS DESIRED
PLT SYS DEACT FOR EXTENDED PWR UP
F8 INST PWR – OFFFLT CNTLR PWR – OFF
F3 TRIM PNL – OFFTRI �RHC – INH
R4 HYD BRAKE HTR (three) – OFFO8 LTG (five) – OFFO17:A ATVC (four) – OFF
NOMENT/NOM/GEN F
B5–16 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
C,MS,PS
C L2 ANTISKID – OFF�NWS – OFF
C3 �FCS CH (four) – AUTOF6 INST PWR – OFFF3 TRIM PNL – OFF
TRI �RHC – INHMS If reqd, install and lock PL Bay Window
Shades
EGRESS(After MS Sys Deact complete)
L1 H2O PUMP LOOP 1 – ON
C L5 L COMM PWR – OFF
C,MS,PS PULL G SUIT controller clip (if inflated)Egress seat
MS A11,A15, COMM CCU PWR – OFFMS,PS MO39M
Unstow ‘Return to Houston’ Bags
C,MS,PS Egress orbiter
NOMENT/NOM/GEN F
MS
EX
TP
WR
UP
5–17 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
PLT EGRESS(When desired after ground support personnelestablishes comm at PS station)
R6 R COMM PWR – OFFPull G SUIT controller clip (if inflated)Egress seat, orbiter
MCC TO KSC HANDOVER(At crew egress or GSE cooling activation,whichever occurs later)
MS
EX
TP
WR
UP
5–18 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
MS MS SYS DEACT FOR EXTENDED PWR UP
MS1 Perform POST LANDING PAYLOAD ACTIVITIES (if reqd), FS 5–19
MS2 LRU DEACTIVATION(After APU/HYD SHUTDN)
O14,O15, O16 BRAKES (three) – OFF
cb GPS PRE AMPL (four) – OP(OV103,105 only)
GPS 2 PRE AMPL UPPER – opGPS 2 PRE AMPL LOWER – op(OV104 only)
RGA (four) – OFFIMU (three) – OFFASA (four) – OFFcb ADTA (four) – opcb/sw ACCEL (four) – op/OFFcb DDU (six) – opcb MNA NWS – opcb MNB NWS – op
O7 TACAN MODE (three) – OFFO8 RADAR ALTM (two) – OFF
MLS (three) – OFFC L1 IMU FAN (three) – OFF
APU HEATER DEACTIVATION(After APU/HYD SHUTDN)
A12 APU HTRTK/FU LINE H2O SYS (six) – OFFGAS GEN/FUEL PUMP (three) – OFFLUBE OIL LINE (three) – OFF
RCS/OMS HEATERS PWRDN
A14 OMS CRSFD LINE A,B (two) – OFFIf reqd, install and lock PL Bay WindowShades
MS2 Inform CDR, “POST LANDINGPROCEDURE COMPLETE”
5–19 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
5–20 ENT/ALL/GEN F
Replace this page with page(s) from Flight Supplement
AS
P E
XT
PW
R U
P
5–21 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
ASP INTEGRATED POST LANDING PROCEDURESFOR EXTENDED PWR UP
ASP 1 A15 Connect Comm (PS)PS Comm CCU PWR – ON
ASP 1 Comm ck with MCC
ASP to Report when “CREW READY TO MCC EGRESS”
ASP to Report “POST LANDING PROCEDURE MCC COMPLETE”
AS
P E
XT
PW
R U
P
5–22 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
CDR SYS DEACT FOR EXTENDED PWR UP
NH3 RECONFIG(On MCC call; Cooling Cart not ready)
L1 1. NH3 CNTLR A(B) – OFFO1 When FREON EVAP OUT TEMP
> 55 degF, select one of the following asspecified by MCC:
L1 2. NH3 CNTLR A – PRI/GPC ( )NH3 CNTLR A – SEC/ON ( )NH3 CNTLR B – PRI/GPC ( )NH3 CNTLR B – SEC/ON ( )
******************
O1L1
O1
During NH3 ops:If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP < 32 degF:
1. FREON PUMP LOOP 1,2(two) – OFF (ASAP)
2. H2O PUMP LOOP 1 – ON3. NH3 CNTLR A(B) – OFF4. If present, activate PL H2O
LOOP�MCC for steps
If no comm:5. Go to VEHICLE PWRDN,
5–13 >>6. �MCC
If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP > 65 degF:
7. Go to POST LANDING LOSSOF COOLING, 5–24
******************
5–23 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
CDR NH3 DEACT(On MCC call if Cooling Cart ready)
L1 1. NH3 CNTLR A(B) – OFF
2. RAD OUT TEMP – NORM
******************
O1L1
O1
After NH3 TERMINATION:If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP < 32 degF:
1. FREON PUMP LOOP 1,2(two) – OFF (ASAP)
2. H2O PUMP LOOP 1 – ON3. If present, activate PL H2O
LOOP�MCC for steps
If no comm:4. Go to VEHICLE PWRDN,
5–13 >>5. �MCC
If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP > 65 degFfor 5 min:
6. Go to POST LANDING LOSSOF COOLING, 5–24
******************
5–24 ENT/ALL/GEN F
1: AS DESIRED 2: OFF3: AS DESIRED
POST LANDING LOSS OF COOLING (NH3FAILED OR DEPLETED)
C L1 1. NH3 CNTLR A,B (two) – OFF
2. �RAD BYP VLV MAN SEL (two) – RADFLOW (tb–RAD, 3 sec)
3. �RAD CNTLR OUT TEMP – NORMC,P,MS 4. �Complete post landing procedures thru
ENT C/L, 5–18 & FS 5–19 ASAPAssume GO for EXTENDED PWR UP
B C3 5. �BFC CRT SEL – 3+1BFC CRT DISP – ON
3: BFS, SM SYS SUMM 2
Terminate monitoring if ground coolingestablished (Convoy commandercall) >>
CRT3 6. Monitor AV BAY TEMP (three)When AV BAY TEMP 1 or 2 > 113 orAV BAY TEMP 3 > 107 or notemperature insight:
P 7. Go to VEHICLE PWRDN,5–13 >>
A 8. Crew egress if not already complete
1–O
RB
LA
TE
6–1 ENT/ALL/GEN F
1–ORBIT LATE DEORBIT PROCEDURES
Refer to DEORBIT BURN FLIGHT RULESCue Card for failures that require 1–orbitdelay
1–O
RB
LA
TE
6–2 ENT/ALL/GEN F
1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST
1–ORBIT LATE DEORBIT PROCEDURES
TRANS B These procedures assume:DAP 1. All DEORB PREP completed
2. DEORBIT BURN completed up tobut not including SINGLE APUSTART, 3–13. If activities are notcomplete, then do them duringtroubleshooting time
C CRT1 GNC, OPS 301 PRO
R2 �HYD MN PUMP PRESS (three) – NORM
B A14 RCS/OMS HTRFWD RCS – A AUTOL POD (two) – A AUTO,B OFFR POD (two) – A AUTO,B OFFOMS CRSFD LINES (two) –A AUTO,B OFF
FWD RCS JET 5 (one) – AUTOAFT RCS JET 5 (one) – AUTO
H2O TANK CONFIG
R11L SPLY H2O TKC INLET – OP (tb–OP)SPLY H2O TKC OUTLET – OP (tb–OP)
TIG–1:10> IMU/IMU ALIGN
Perform IMU/IMU alignment using best IMU asreference. �MCC for reference IMU
1: GNC 21 IMU ALIGN
C CRT1 IMU/IMU – ITEM 14 + __ EXECALIGN IMU 1(2,3) –ITEM 10(11,12) EXEC (*)
If no comm, EXEC – ITEM 16 EXEC (*)Rcd MET ___/___:___
�EXEC, ITEM 16 – (no *) (4–6 min)
6–3 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC DEORB MNVR EXEC
C MCC UPDATE:DEL PADPRPLT PAD
MCC UPLINK:PASS TGTBFS TGT
CRT2 GNC, OPS 302 PRO
ALL FLUID LOADING: 1–ORBIT LATE
Approx 1 hr prior to new TIG, drink 8 fluidoz water plus take 2 salt tablets every15 min for total of 16 fluid oz water and4 salt tablets per crewmember
FINAL DEORB UPDATE/UPLINK
C MCC UPDATE:DEL PADPRPLT PAD
MCC UPLINK:PASS SVBFS SVPASS TGTBFS TGTBFS IMU GYRO/ACCEL
G50 �LAND SITE as reqdSET TACAN tw
On MCC GO:CRT1 LOAD – ITEM 22 EXEC
TIMER – ITEM 23 EXECCRT1,3 �PASS & BFS TGTS per MNVR PAD:
BURN ATT∆VTOTTGOHA HP
6–4 ENT/ALL/GEN F
1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC DEORB MNVR EXEC
IF WAVEOFFGo to IF NO–GO FORDEORBIT BURN, 3–11
TIG–15>B A14 RCS/OMS HTRFWD RCS – OFFL POD (two) – A OFF,B OFFR POD (two) – A OFF,B OFFOMS CRSFD LINES (two) –A AUTO,B AUTO
FWD RCS JET 5 (one) – OFFAFT RCS JET 5 (one) – OFF
TIG–10> MNVR TO 1–ORBIT LATE DEORBIT ATT
C3 �DAP: AUTOB F6,F8 �ADI ATT (two) – INRTL
A �� �ERR (two) – MEDA �� �RATE (two) – MED
C MNVR to BURN ATT(�ADI ATT with CRT BURN ATT)
B Copy last DEL PAD and OMS PRPLT PADdata on DEORBIT BURN Cue Cards
F6/F8 �DEORBIT BURN and DEORBIT BURNMONITIOR Cue Cards installed
3: BFS, SM SYS SUMM 2
R2 HYD MN PUMP PRESS (three) – LO
Return to DEORBIT BURN Cue Cards andSINGLE APU START, 3–13
SW
LIS
T
7–1 ENT/ALL/GEN F NOT FLOWN
SWITCH LIST AT WHEELS STOP EGRESS
LEFT SEAT
L5 7–2. . . . . . . . . . . . . . L1 7–2. . . . . . . . . . . . . . L2 7–2. . . . . . . . . . . . . .
F2 7–2. . . . . . . . . . . . . . F3 7–2. . . . . . . . . . . . . . F6 7–2. . . . . . . . . . . . . . F7 7–3. . . . . . . . . . . . . .
C2 7–3. . . . . . . . . . . . . C3 7–3. . . . . . . . . . . . .
O6 7–4. . . . . . . . . . . . . O7 7–4. . . . . . . . . . . . . O14 7–4. . . . . . . . . . . . O15 7–5. . . . . . . . . . . .
RIGHT SEAT
O16 7–6. . . . . . . . . . . . O17 7–6. . . . . . . . . . . . O8 7–6. . . . . . . . . . . . .
RIGHT SEAT
F4 7–6. . . . . . . . . . . . . . F8 7–6. . . . . . . . . . . . . .
R1 7–7. . . . . . . . . . . . . R2 7–7. . . . . . . . . . . . . R4 7–7. . . . . . . . . . . . . R6 7–8. . . . . . . . . . . . .
R7 7–8. . . . . . . . . . . . . R10 7–8. . . . . . . . . . . . R12 7–8. . . . . . . . . . . . R14 7–8. . . . . . . . . . . .
AFT
A11 7–9. . . . . . . . . . . . A12 7–9. . . . . . . . . . . . A13 7–9. . . . . . . . . . . . A14 7–9. . . . . . . . . . . . A15 7–9. . . . . . . . . . . .
MIDDECK – FWD
MO39M 7–10. . . . . . . . . MO42F 7–10. . . . . . . . .
NOTES
� This section contains switch configuration at egress forpanels that are reconfigured in this checklist for EXTENDPWR UP option. Refer to DEORBIT PREP, section 3, foregress configuration of remaining panels subsequent toscheduled Deorbit Prep switch verification checks.
� denotes physical break in panel structure.
� Switch list at WHEELS STOP EGRESS
SW LIST
NOT FLOWN 7–2 ENT/ALL/GEN F
LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESS
L5 L COMM PWR – ON OFF
All switches per DEORB PREP except:L1 IMU FAN B – ON OFF
H2O PUMP LOOP 1 (two) – OFF,B ON,BRAD CNTLR LOOP 1,2 (two) – AUTO BRAD BYP VLV MAN SEL 1 – ctr (tb–RAD)RAD BYP VLV MAN SEL 2 – ctr (tb–RAD or BYP)H2O BYP VLV MODE 1 – AUTOH2O BYP VLV MODE 2 – AUTO or MANNH3 CNTLR A(B) – OFF PRI/GPC or SEC/ON or OFF
L2 ANTISKID – ON OFFNWS – 1 OFFBDY FLP – AUTO/OFFENTRY MODE – AUTOTRIM R,P,Y (three) – ctrSBTC – as reqd full forwardO2 SYS 1,2 SPLY (two) – ctr (tb–OP)
ctr (tb–CL)N2 SYS 1,2 (four) – ctr (tb–OP)
F2 All pb lts – as reqd lt off
F3 L HUD PWR – ON OFFL TRIM RHC/PNL – as reqd INHL TRIM PNL – as reqd OFFR HUD PWR – ON OFFR TRIM RHC/PNL – as reqd INH
F3 R TRIM PNL – as reqd OFFDRAG CHUTE ARM 1/ARM 2 pb – as reqd lt offDRAG CHUTE DPY 1/DPY 2 pb – as reqd lt offDRAG CHUTE JETT 1/JETT 2 pb – as reqd lt off
(OV103,5)F6 INST PWR – FLT/MPS OFF
DATA BUS – 3AIR DATA – NAVADI ATT – LVLHADI ERR – as reqdADI RATE – as reqdLDG GEAR ARM pb – ARM/lt on lt offLDG GEAR DN pb – DN/lt on lt offLDG GEAR tb (three) – DNHSI SEL MODE – ENTRYHSI SEL SOURCE (two) – NAV,1BFC DISENGAGE – dnABORT MODE – OFFABORT pb – lt off(OV102,4)HUD DATA BUS – 1AIR DATA – NAVADI ATT – LVLHADI ERR – as reqdADI RATE – as reqdLDG GEAR ARM pb – ARM/lt on lt offLDG GEAR DN pb – DN/lt on lt offLDG GEAR tb (three) – DNHSI SEL MODE – ENTRY
NOT FLOWN 7–3 ENT/ALL/GEN F
LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESSF6 HSI SEL SOURCE (two) – NAV,1
BFC DISENGAGE – rtABORT MODE – OFFABORT pb – lt offFLT CNTLR POWER – ON OFFRADAR ALTM – 1
(OV103,5)F7 FLT CNTLR PWR – ON OFF
RADAR ALTM – 1
(OV103,5)C2 CRT PWR (1,3) – ON
CRT 2 PWR – ON OFFL CRT SEL – as reqdR CRT SEL – as reqd(OV102,4)IDP/CRT PWR (1,3) – ONIDP/CRT 2 PWR – ON OFFL IDP/CRT SEL – as reqdR IDP/CRT SEL – as reqd(all)1,2,3 MAJ FUNC (three) – GNCEVENT TIMER MODE – as reqdEVENT TIMER CNTL – ctrTIMER SET tw (four) – as reqdTIMER – ctr
C3 OMS ENG (two) – OFFBFC CRT DISP – ONBFC CRT SEL – 3+1FCS CH (four) – AUTOBDY FLP – AUTO/OFFAIR DATA PROBE STOW (two) – INHOV102 MN ENG VIB SHUTDN – INHMN ENG LIMIT SHUTDN – AUTOTRIM R,P,Y (three) – ctrSBTC – full forwardDAP – lts offSRB SEP – MAN/AUTOET SEP – MANAUD CTR – 1OI PCMMU PWR – 1OI PCMMU FORMAT – GPCS–BD PM CNTL – CMDS–BD PM ANT – GPCAIR DATA PROBE (two) – DPYUPLK – ENAOV103,4,5 MSTR MADS PWR – ON OFFOV102 MSTR OEX PWR – ON OFFC/W MEM – ctrC/W MODE – NORMOV102 PL SAFING (five) – SAFEOV103,4 RTG PUMP – PRIOV103 PL SAFING (2,3,4,5) – SAFEOV104 RTG SHORT PRI(SEC) ENA – DSBLOV104 RTG SHORT PRI(SEC) SHORT – OFFEMER LTG – FF/ON (as reqd)
ENT/ALL/GEN F,1
NOT FLOWN 7–4 ENT/ALL/GEN F
LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESSO6 LTG PNL (two) – BRT, as reqd OFF
LTG INST (two) – BRT, as reqd OFFLTG L GLRSHLD FLOOD (two) – BRT, as reqd OFFL SEAT/CTR CNSL FLOOD (two) – BRT, as reqd OFFSTAR TRK DR CNTL (two) – OFF (tb–CL)STAR TRR PWR (two) – OFFUHF SPLX/EVA XMIT FREQ – 259.7/414.2UHF SPLX/EVA PWR AMPL – ONUHF SPLX SQUELCH – ONUHF EVA STRING – 1UHF ENCRYPT – OFFUHF MODE – SPLXANNUN LAMP TEST – ctrANNUN BUS SEL ACA 1 – MNAANNUN BUS SEL ACA 2/3 – MNBANNUN INTEN (two) – VAR, as reqdMTU – AUTOOV103,5 DEU (four) – dnOV102,4 IDP (four) – dnMDM PL1,PL2 (two) – ONMDM PL3 – OFFMDM FA1,2,3,4 (four) – ONMDM FF1,2,3,4 (four) – ONGPC PWR 1,5 – ONGPC PWR 2,3,4 – ON OFFGPC OUTPUT 1 – NORM (tb–gray)GPC OUTPUT 2,3,4 – NORM (tb–gray) bpGPC OUTPUT 5 – BACKUP (tb–bp)IPL SOURCE – OFFGPC MODE 1,5 – RUN (tb–RUN)GPC MODE 2,3,4 – RUN (tb–RUN)
O6 GPC MODE 2,3,4 – HALT (tb–bp)
O7 TACAN 1,2,3 MODE (three) – GPC OFFTACAN 1,2,3 ANT SEL (three) – AUTOTACAN 1,2,3 CH tw (three) – 111XTACAN 1,2,3 (if Edw landing)AFT L RCS He PRESS (two) – OP (tb–OP)AFT L RCS He PRESS (two) – GPC (tb–CL)AFT L RCS TK ISOL (three) – GPC (tb–OP)AFT L RCS MANF ISOL 1,2,3,4 (four) – OPAFT L RCS MANF ISOL 1,2,3,4 (four) – (tb–OP)AFT L RCS MANF ISOL 1,2,3,4 (four) GPC (tb–OP)AFT L RCS MANF ISOL 5 – GPC (tb–OP)AFT L RCS XFEED (two) – GPC (tb–CL)MSTR RCS XFEED – OFFAFT R RCS He PRESS (two) – OP (tb–OP)AFT R RCS He PRESS (two) – GPC (tb–CL)AFT R RCS TK ISOL (three) – GPC (tb–OP)AFT R RCS MANF ISOL 1,2,3,4 (four) – OPAFT R RCS MANF ISOL 1,2,3,4 (four) – (tb–OP)AFT R RCS MANF ISOL 1,2,3,4 (four) GPC (tb–OP)AFT R RCS MANF ISOL 5 – GPC (tb–OP)AFT R RCS XFEED (two) – GPC (tb–CL)
O14:A BRAKES MNA – ON OFFRGA 1 – ON OFFIMU 1 – ON OFFFC1 CNTLR – ONAll cbs closed except:
O14:C OV102,3,5 cb MNA TACAN 1 – op
ENT/ALL/GEN F,1
NOT FLOWN 7–5 ENT/ALL/GEN F
LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESS
O14:D OV104 GPS 1 PRE AMPL UPPER – opOV104 GPS 1 PRE AMPL LOWER – opcb MNA GPS PRE AMPL (two) – op
O14 cb MNA CAB VENT – opcb MNA CAB VENT ISOL – op op
O14:E cb MNA ADTA 1 – cl opcb MNA ACCEL 1 – cl opcb MNA DDU L – cl opcb MNA CAB AFT – op opcb MNA NWS – cl
O14:F MMU 1 – ONRJD (six) – ON OFFL OMS ENG VLV – ON OFFASA 1 – ON
O15:A BRAKES MNB – ON OFFRGA (two) – ON OFFIMU 2 – ON OFFFC2 CNTLR – ON
O15:D cb MNB NWS – cl opAll cbs closed except:
O15:C OV104 GPS 2 PRE AMPL UPPER – opO15:D OV104 GPS 2 PRE AMPL LOWER – opO15:C OV102,3 cb MNB TACAN 2 – opO15:E cb MNB ADTA 2 – cl op
cb MNB ACCEL 2 – cl opcb MNB DRAG CHUTE SYS 2 – cl opDDU (two) – cl op
O15:F MMU 2 – ONRJD (four) – ON OFF
O15:F ASA 2 – ON OFFACCEL 4 – ON OFF
NOT FLOWN 7–6 ENT/ALL/GEN F
RIGHT SEAT SWITCH LIST AT WHEELS STOP EGRESSO16:A BRAKES MNC – ON OFF
RGA 3 – ON OFFIMU 3 – ON OFFFC3 CNTLR – ONAll cbs closed except:
O16:C OV102 cb MNC TACAN 3 – opO16:D OV104 GPS 3 PRE AMPL UPPER – op
OV104 GPS 3 PRE AMPL LOWER – opcb MNC GPS PRE AMPL (two) – opcb MNC GPS O2 EMER – op
O16:E cb MNC ADTA (two) – cl opcb MNC DDU R – cl opcb MNC DDU AFT – opcb MNC DRAG CHUTE SYS 1 – cl op
O16:F RJD (six) – ON OFFR OMS ENG VLV – ON OFFASA 3,4 (two) – ON OFFACCEL 3 – ON OFFRJD L5/F5/R5 DRIVER – OFF
O17:A ATVC (four) – ON OFFO17:B EIU (three) – OFFO17:C SIG CONDR FREON A – AC2
SIG CONDR FREON B – AC3SIG CONDR OL 1/2 – ONSIG CONDR OR 1/2 – ON
O17:D SIG CONDR OA 1/2/3 – ONMDM OA 1/2/3 – ONMEC (two) – OFF
O8 RADAR ALTM (two) – ON OFFO8 MLS (three) – ON OFF
O8 MLS CH tw (three) – as reqdR SEAT/CTR CNSL FLOOD (two) – as reqdLTG PNL R – BRT OFFLTG PNL R OVHD – BRT OFFLTG PNL R INST – BRT OFFLTG PNL NUMERIC – BRT OFFLT G R GLRSHLD FLOOD – OFFOMS KIT He PRESS/VAP ISOL (two) – CLOMS KIT TK ISOL (two) – CL (tb–bp)L OMS He PRESS/VAP ISOL (two) – CL GPCL OMS TK ISOL (two) – OP (tb–OP) GPC (tb–OP)L OMS XFEED (two) – CL (tb–CL) GPC (tb–OP)R OMS He PRESS/VAP ISOL (two) – CL GPCR OMS TK ISOL (two) – OP (tb–OP) GPC (tb–OP)R OMS XFEED (two) – CL (tb–CL) GPC (tb–CL)FWD RCS He PRESS (two) – OP (tb–OP)FWD RCS He PRESS (two) – GPC (tb–CL)FWD RCS TK ISOL (two) – OP (tb–OP)FWD RCS TK ISOL (two) GPC (tb–OP)FWD RCS MANF ISOL 1,2,3,4 – OP (tb–OP)FWD RCS MANF ISOL 1,2,3,4 – GPC (tb–OP)FWD RCS MANF ISOL 5 – GPC (tb–OP)ANNUN LAMP TEST – ctr
F4 All pb lts – as reqd
F8 OV103,5 INST PWR – ON OFFOV103,5 DATA BUS – 4OV102,4 HUD DATA BUS – 4AIR DATA – NAVADI ATT – LVLHADI ERR – as reqd
NOT FLOWN 7–7 ENT/ALL/GEN F
RIGHT SEAT SWITCH LIST AT WHEELS STOP EGRESS
F8 ADI RATE – as reqdLDG GEAR ARM pb – ARM/lt ON lt OFFLDG GEAR DN pb – DN/lt ON lt OFFLDG GEAR tb (three) – DNHSI SEL MODE – ENTRYHSI SEL SOURCE (two) – NAV, 2FLT CNTLR PWR – ON OFFRADAR ALTM – 2
R1 All switches and cbs per DEORB PREP except:PL PRI MNC – as reqd per FS 5–19
R2 MPS PRPLT DUMP SEQ (two) – GPCMPS ENG PWR (six) – OFFMPS He ISOL (six) – GPCMPS PNEU L ENG He XOVR – GPCMPS PNEU He ISOL – GPCMPS He I’CNECT (three) – GPCMPS LH2 ULL PRESS – AUTOAPU/HYD RDY tb (three) – bpAPU OPER (three) – START/RUN OFFAPU SPEED SEL (three) – NORMHYD MN PUMP PRESS (three) – NORMAPU CNTLR PWR (three) – ON OFFAPU AUTO SHUTDN (three) – ENABLR CNTLR/HTR (three) – BBLR PWR (three) – ON OFFBLR N2 SPLY (three) – ON OFF
R2 HYD CIRC PUMP (three) – OFFAPU FUEL TK VLV (three) – OP CLcb APU FU TK VLV ENA (six) – clET UMB DR MODE – GPCET UMB DR CTRLINE LAT – GND (tb–STO)ET UMB L DR – OFF (tb–CL)– tb–bpET UMB L LAT – OFF (tb–LAT)– tb–RELET UMB R DR – OFF (tb–CL)– tb–bpET UMB R LAT – OFF (tb–LAT)– tb–REL
R4 HYD BRAKE HTR (three) – AUTO OFFHYD BRAKE ISOL VLV 1,2,3 – GPC (tb–OP)HYD MPS/TVC ISOL VLV (three) – ctr (tb–CL)HYD MPS/TVC ISOL VLV (three) – ctr (tb–OP)LG/NWS HYD SYS – AUTO 1/2LG/EXTEND ISOL VLV – GPC (tb–op)MPS ENG CNTLR HTR (three) – OFFMPS MANF PRESS (two) – GPCMPS FILL/DRAIN LO2 OUTBD – GNDMPS FILL/DRAIN LO2 INBD – GNDMPS FILL/DRAIN LH2 OUTBD – GNDMPS FILL/DRAIN LH2 INBD – GNDMPS H2 PRESS LINE VENT – GNDMPS LO2 PREVLV (three) – GPCMPS LH2 PREVLV (three) – GPCMPS FDLN RLF ISOL (two) – GPC
NOT FLOWN 7–8 ENT/ALL/GEN F
RIGHT SEAT SWITCH LIST AT WHEELS STOP EGRESS
R6 R COMM PWR – ON
R7 (NOTE: Pnl may be deleted if spacelab not flown)All switches per DEORB PREP exceptpowered spacelab config:SS INV – ctr (lt on)SS AC/DC PWR – ctr (lt on)AV FAN ON 1 – ctr (lt on)H2O LOOP PUMP 1 – ctr (lt on)Unpowered spacelab config same as above except lts
off:
R10 MS AUD PWR – AUD/TONEMS AUD A/G (two) – T/RMS AUD A/A – T/RMS AUD ICOM (two) A – T/RMS AUD ICOM (two) B – T/RMS AUD VOX SENS – as reqdMS AUD PAGE – dnMS AUD VOL tw (five) – as reqdMS AUD XMIT/ICOM MODE – PTT/PTT
R12 OV103,5 CRT 4 PWR – ON OFFOV102,4 IDP/CRT 4 PWR – ON OFFMAJ FUNC – SM
All cbs closed except:R14:B OV102,4,5 cb MNA PALLET DSC 1A/2B – op*
OV104,5 cb MNA PALLET DSC 3A – opOV102,4,5 cb MNB PALLET DSC 1B – op*
R14:B OV104,5 cb MNB PALLET DSC 4B – opOV102,4,5 cb MNC PALLET DSC 2A – op*OV104,5 cb MNC PALLET DSC 3B/4A – op
R14:C cb MNA UHF EVA – opcb MNB KU ELEC – opcb MNB ANT HTR – opcb MNB CABLE HTR – opcb MNC KU SIG PROC – opcb MNC UHF EVA – op
R15:F cb ESS 1BC LDG GEAR ARM/DN RESET – op cl
* Closed if EDO
ENT/ALL/GEN F,1
NOT FLOWN 7–9 ENT/ALL/GEN F
AFT FLIGHT DECK SWITCH LIST AT WHEELS STOP EGRESS
A11 MS COMM CCU PWR – ON OFF
A12 APU HTR GAS GEN/FUEL PUMP (three) – B AUTOAPU HTR GAS GEN/FUEL PUMP (three) – OFFAPU HTR LUBE OIL LINE (three) – B AUTO OFFAPU HTR TK/FU LINE H2O SYS 1A,2A,3A – OFFAPU HTR TK/FU LINE H2O SYS 1B,2B,3B – AUTOAPU HTR TK/FU LINE H2O SYS 1B,2B,3B – OFFLG ARM/DN RESET – dnFC3 STRUCT RTN – ctr (tb–ON)HYD HTR (eight) – OFFHYD CIRC PUMP PWR 1 – MNAHYD CIRC PUMP PWR 2 – MNBHYD CIRC PUMP PWR 3 – MNC
A13 OS AUD MSTR SPKR VOL – as reqdSPKR PWR – OFF
A14 RCS/OMS HTR FWD RCS – OFFRCS/OMS HTR L POD (two) – OFFRCS/OMS HTR R POD (two) – OFFRCS/OMS HTR OMS KIT – OFFRCS/OMS HTR OMS CRSFD LINES (two) – A AUTORCS/OMS HTR OMS CRSFD LINES (two) – OFFRCS/OMS HTR OMS CRSFD LINES (two) – B AUTORCS/OMS HTR OMS CRSFD LINES (two) – OFFRCS/OMS HTR FWD RCS JET 1,2,3,4 (four) – AUTORCS/OMS HTR FWD RCS JET 5 – OFFRCS/OMS HTR AFT RCS JET 1,2,3,4 (four) – AUTORCS/OMS HTR AFT RCS JET 5 – OFF
A14 PYRO (twelve) – SAFERMS LAT – SAFE
A15 PS COMM CCU PWR – ON OFFDC UTIL PWR MNC – as reqdAC UTIL PWR AC3 – OFF
NOT FLOWN 7–10 ENT/ALL/GEN F
MIDDECK – FORWARD SWITCH LIST AT WHEELS STOP EGRESS
MO39M MIDDECK COMM CCU PWR – ON OFF
MO42F MIDDECK SPKR AUD PWR – OFFMIDDECK SPKR AUD A/G (two) – T/RMIDDECK SPKR AUD A/A – T/RMIDDECK SPKR AUD ICOM (two) – T/RMIDDECK SPKR AUD VOX SENS – as reqdMIDDECK SPKR AUD MSTR SPKR VOL – as reqdMIDDECK SPKR AUD PAGE – dnMIDDECK SPKR AUD VOL tw (five) – as reqdMIDDECK SPKR AUD XMIT/ICOM MOD – PTT/VOXMIDDECK SPKR AUD TONES – ACCU/BYPMIDDECK SPKR AUD SPKR PWR – OFFGPC MEM DUMP – OFFBYP TONE VOL – as reqd
CU
E C
AR
DC
ON
FIG
8–1 ENT/ALL/GEN F FAB USE ONLY
ENTRY CUE CARD CONFIG
CU
E C
AR
DC
ON
FIG
CC 8–2 ENT/ALL/GEN F FAB USE ONLY
APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DPS3 RDNT fail, Split X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 1 GPC X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 GPC BITE (Multiple GPCs) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ECLS7 2 Av Bay Fans in Bay 3 X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 2 Av Bay Fans in Bay 1 or 2 X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ELEC9 H2 Manf or TK leak (not in
depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . . .
10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11 CNTL CA1 (No BFS Engage in GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12 Multi Φ AC BUS (unshorted) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
GNC13 1 MLS (if reqd), IMU, or TACAN
(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
17 3 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
21 Both OMS Eng fail X 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
22 Prplt Lk after LAST LOS . . . . . . . . . . . . . . . . . . . .
AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . . .
24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
25 1 AFT RCS PROP TK fail X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
COMM26 MCC GO for DEORBIT not rcvd X. . . . . . . . . . . . . . . . . . . . .
FAILURE
PRE TIG POST TIG
Delay (max)
OneOrbit
OneDay
StopBurn,> Safe
HP
TOP
ENT–1a/D/I
perigee adjust
1 Stop Burn > OMS PRPLT FAIL HP (Ref: DEL PAD/BURN Card)2 Stop Burn > OMS ENG FAIL HP (Ref: DEL PAD/BURN Card)
HOOKVELCRO
HOOKVELCRO
DEORBIT BURN FLIGHT RULESONE–ORBIT LATE AVAILABLE
(reduced copy)
CC 8–3 ENT/ALL/GEN F FAB USE ONLY
TOPBACK OF ‘DEORBIT BURN FLIGHT RULES’
APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DPS3 RDNT fail, Split X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 1 GPC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 GPC BITE (Multiple GPCs) X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ECLS7 2 Av Bay Fans in Bay 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 2 Av Bay Fans in Bay 1 or 2 X. . . . . . . . . . . . . . . . . . . . . . . . . . .
ELEC9 H2 Manf or TK leak (not in
depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . .
10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11 CNTL CA1 (No BFS Engagein GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
12 Multi ΦAC BUS (unshorted) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GNC13 1 MLS (if reqd), IMU, or TACAN
(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
17 3 ADTAs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . .
21 Both OMS Eng fail X 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
22 Prplt Lk after LAST LOS . . . . . . . . . . . . . . . . . . . .
AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . .
24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
25 1 AFT RCS PROP TK FAIL X. . . . . . . . . . . . . . . . . . . . . . . . . . .
COMM26 MCC GO for DEORBIT not rcvd X. . . . . . . . . . . . . . . . . . . . .
FAILURE
PRE TIG POST TIGDelay(max)OneDay
StopBurn,> Safe
HP
ENT–1b/D/I
perigee adjust
1 Stop Burn > OMS PRPLT FAIL HP (Ref: DEL PAD/BURN Card)2 Stop Burn > OMS ENG FAIL HP (Ref: DEL PAD/BURN Card)
HOOKVELCRO
HOOKVELCRO
DEORBIT BURN FLIGHT RULESONE–ORBIT LATE NOT AVAILABLE
(reduced copy)
CC 8–4 ENT/ALL/GEN F FAB USE ONLY
HOOKVELCRO
HOOKVELCRO
�MM302 �RCS SEL�RCS BURN CONFIG (L OMS I’CNCT)
L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . . .
�DAP – INRTL/DISCADI – LVLH(REF)/MED/MEDFLT CNTLR PWR (two) – ON
TIG THC +X (No deorbit > TIG +
Maintain PITCH ATT ERR ± 3°Monitor ∆VTOT:
RCS I’CNCT TK SW at ∆VTOT =R OMS XFEED (two) – OPL OMS XFEED (two) – CL
OMS PRPLT LOWAFT RCS RECONFIG AT ∆VTOT =RCS COMPLETION
OMS PRPLT FAIL (MULTIPLE JETS FAIL OFF):Secure aff OMS
STOP BURN:SAFE APUs – SHUT DN
HPCONTINUE BURN:
ITEM 18 +0 EXECG23 Resel jetsInterconnect good OMS to RCS
THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION
RCS +X JET FAIL OFF:STOP BURN:
SAFE APUs – SHUT DNHP
CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jets
********************
********************
DEORBITBURN(RCS)
HINGE
ENT–3a/D/K
TOP
: )
(reduced copy)
CC 8–5 ENT/ALL/GEN F FAB USE ONLY
PREBANK/FRCS COMPLETION
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP or
At AFT QTY 1 TOT AFT QTY 2if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIP
HP
AFTHP
TGTHP
FRCS COMPLETION (if applicable):
MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF VGOx = 0, release THC
AFT RCS RECONFIGTrim Inplane X,Z residuals < 2 fps (< 0.5 if shallow)
********************
********************
TOPHINGED AT BOTTOM OF‘DEORBIT BURN (RCS)’
HINGE
ENT–3aa/D/K
% then
%
THC +X to TGT HP
(reduced copy)
CC 8–6 ENT/ALL/GEN F FAB USE ONLY
HOOKVELCRO
HOOKVELCRO
HINGE
ENT–3b/D/D
TOPBACK OF ‘DEORBIT BURN (RCS)’
(reduced copy)
CC 8–7 ENT/ALL/GEN F FAB USE ONLY
TOPHINGED AT BOTTOM OF
BACK OF ‘DEORBIT BURN (RCS)’
HINGE
ENT–3bb/D/D
(reduced copy)
CC 8–8 ENT/ALL/GEN F FAB USE ONLY
�MM302 �OMS BOTHEnter TGO + 5 sec
�TRIM per MNVR PAD or P +0.0, LY –5.7, RY +5.7L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OP
�DAP – AUTO(PASS)/DISCADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ON
TIG–2 OMS ENG (two) – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
If no OMS ignition: APUs – SHUT DNOMS PRPLT FAIL:
Failed OMS ENG – OFFSTOP BURN:
Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS
CONTINUE BURN:
ITEM 18 +0 EXECWhen good OMS QTY:
5%: L,R OMS XFEED (four) – OP4%: Good OMS TK ISOL (two) – CL
If OMS Pc < 80 or OMS TEMP, OMS ENG – OFF
�ADI – LVLH, center needlesRCS COMPLETION
OMS ENG FAIL:Failed OMS ENG – OFFOMS XFEED at 1/2 ∆VTOT at fail
OMS Xor OMS QTY
2nd OMS FAIL (ENG or PRPLT):
Failed OMS ENG – OFFIf PRPLT FAIL:
Secure aff OMS ITEM 18 +0 EXEC
STOP BURN:
APUs – SHUT DN
CONTINUE BURN:
�ADI – LVLH, center needlesInterconnect good OMS to RCS
THC +X (�OMS% vs RCS Burn Time)RCS I’CNCT TK SW (N/A PRPLT FAIL)RCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETION
HOOKVELCRO
HOOKVELCRO
********************************************
********************************************
DEORBITBURN (2 ENG)
TOP
EitherPRPLT FAIL(SAFE) HP
BothENG FAIL
HP
R OMSFAIL HP
L OMSFAIL HP
ENT–4a/D/KHINGE
% R%L or
: )
(reduced copy)
CC 8–9 ENT/ALL/GEN F FAB USE ONLY
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP orAt AFT QTY 1 TOT AFT QTY 2
if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIPHP
AFT
HP
TGTHP
FRCS COMPLETION (if applicable):MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF+ :02 OMS ENG(s) – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
********************
********************
TOPHINGED AT BOTTOM OF‘DEORBIT BURN (2 ENG)’
HINGE
THC +X to TGT HP
ENT–4aa/D/I
% then
%
):
PREBANK/FRCS COMPLETION
(reduced copy)
CC 8–10 ENT/ALL/GEN F FAB USE ONLY
�MM302 �OMS L or R�OMS BURN CONFIG (L or R XFEED)
Enter TGO + 10 sec�TRIM per MNVR PAD or P +0.0, LY +5.2, RY –5.2
L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . .
�DAP – AUTO(PASS)/DISCADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ON
TIG–2 Good OMS ENG – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
* If no OMS ignition: APUs – SHUT DN *
OMS XFEED RETURN at ∆VTOT =
orL,R OMS TK ISOL (four) – OPL,R OMS XFEED (four) – CL
OMS PRPLT FAIL:OMS ENG – OFF
STOP BURN:APUs – SHUT DN
SAFE Secure aff OMSHP
CONTINUE BURN:Secure aff OMSITEM 18 +0 EXEC
�ADI – LVLH, center needlesInterconnect good OMS to RCS
THC +X(�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETIONOMS ENG FAIL:
OMS ENG – OFFSTOP BURN:
ENG APUs – SHUT DNFAILHP
CONTINUE BURN:�ADI – LVLH, center needles
Interconnect OMS to RCSTHC +X(�OMS% vs RCS Burn Time)RCS I’CNCT TK SWRCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETIONRCS +X JET FAIL OFF:
STOP BURN:SAFE APUs – SHUT DN
HPCONTINUE BURN:
ITEM 18 +0 EXECG23 Resel jets
HOOKVELCRO
HOOKVELCRO
**************************************
**************************************
DEORBITBURN (1 ENG)
TOPBACK OF ‘DEORBIT BURN (2 ENG)’
ENT–4b/D/IHINGE
):
%at
(reduced copy)
CC 8–11 ENT/ALL/GEN F FAB USE ONLY
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP orAt AFT QTY 1 TOT AFT QTY 2
if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIPHP
AFT
HP
TGTHP
FRCS COMPLETION (if applicable):MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF+ :02 OMS ENG – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
********************
********************
TOPHINGED AT BOTTOM OF‘DEORBIT BURN (1 ENG)’
HINGE
THC +X to TGT HP
ENT–4bb/D/J
% then
%
):
PREBANK/FRCS COMPLETION
(reduced copy)
CC 8–12 ENT/ALL/GEN F FAB USE ONLY
�MM302 �OMS BOTHEnter TGO + 5 sec
�TRIM per MNVR PAD or P + 0.0, LY –5.7, RY +5.7�DAP – AUTO(PASS)/DISC
ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONFeed 2 ENG from 1 POD
L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OPL,R OMS TK ISOL (two) – CL (tb–CL)L,R OMS XFEED (four) – OP (tb–OP)
TIG–2 OMS ENG (two) – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
If no OMS ignition: APUs – SHUT DNWhile feeding 2 OMS from 1 POD:
OMS PRPLT FAIL:Failed OMS ENG(s) – OFF
STOP BURN:APUs – SHUT DNSecure OMS
SAFE HP
CONTINUE BURN:ITEM 18 +0 EXECIf Both ENGs ‘↓’:
Secure OMS�ADI – LVLH, center needles
Interconnect OMS to RCS
THC +X forAFT RCS RECONFIG
RCS COMPLETION If (XFEED) ENG ‘↓’:
When OMS QTY:5%: OMS TK ISOL (two) – OP4%: OMS TK ISOL (two) – CL
If OMS Pc < 80 or OMS TEMP, OMS ENG – OFF
�ADI – LVLH, center needlesRCS COMPLETION
If (STRAIGHT FEED) ENG ‘↓’: OMS ENG FAIL
OMS ENG FAIL (CONTINUE BURN):Failed OMS ENG – OFF
at ∆VTOT =or
TK ISOL(two) – OP
TK ISOL(two) – CL
Return to 2 ENG, 2 POD FLOW at ∆VTOT:L,R OMS TK ISOL (two) – OP (tb–OP)L,R OMS XFEED (four) – CL (tb–CL)
at %
HOOK VELCRO
***************************************
***************************************
UNBALANCEDPRPLT
DEORBITBURN
HINGE
TOP
ENT–5a/D/L
: )
:
HOOK VELCRO
(reduced copy)
CC 8–13 ENT/ALL/GEN F FAB USE ONLY
TOPHINGED AT BOTTOM OF ‘UNBALANCED PRPLT DEORBIT BURN’
HINGE
ENT–5aa/D/M
OMS PRPLT FAIL:Failed OMS ENG – OFF
STOP BURN:Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS
CONTINUE BURN:
ITEM 18 +0 EXECWhen good OMS QTY:
5%: L,R OMS XFEED (four) – OP4%: Good OMS TK ISOL (two) – CL
If OMS Pc < 80 or OMS TEMP, OMS ENG – OFF
�ADI – LVLH, center needlesRCS COMPLETION
OMS ENG FAIL:Failed OMS ENG – OFFOMS XFEED at 1/2 ∆VTOT at fail
or OMS QTY
2nd OMS FAIL (ENG or PRPLT):
Failed OMS ENG – OFFIf PRPLT FAIL:
Secure aff OMSITEM 18 +0 EXEC
STOP BURN:APUs – SHUT DN
CONTINUE BURN:
�ADI – LVLH, center needlesInterconnect Good OMS to RCS
THC +X (�OMS% vs RCS Burn Time)RCS I’CNCT TK SW (N/A PRPLT FAIL)RCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG
RCS COMPLETIONRCS COMPLETION:
THC +X to TGT HP or TOT AFT QTY 1
At AFT QTY 1if CUR HP:
PREBANK/FLIP
HP
AFTHP
TGT
HPFRCS COMPLETION (if applicable):
MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF+ :02 OMS ENG(s) – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
***********************************************************
***********************************************************
R OMSFAIL HP
L OMSFAIL HP
EitherPRPLT FAIL(SAFE) HP
BothENG FAIL
HP
PREBANK/FRCS COMPLETION
THC +X to TGT HP
THC +X to PREBANK/FLIP HP orTOT AFT QTY 2PREBANK/FRCS COMPLETION
):
% then
%
%R%L or
(reduced copy)
CC 8–14 ENT/ALL/GEN F FAB USE ONLY
HOOK VELCRO HOOK VELCRO
�MM302 �OMS L(R) or RCSEnter TGO + 10 sec
�L,R OMS TK ISOL (four) – GPCL,R OM �XFEED (four) – GPC
�tb config from table (OMS SSR–1)�DAP – AUTO(PASS)/DISC
ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONMan repress to maintain good OMS Tk Ps > 234 psi (simo)If OMS BURN INITIATION:
�TRIM per MNVR PAD or: P +0.0, LY +5.2, RY –5.2TIG–2: Good OMS ENG – ARM/PRESS
TIG–2:15 EXEC (No EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)
* If no OMS ignition, APUs – SHUT DN *If RCS BURN INITIATION:
Man repress L,R OMS > L,R RCS TK PsL,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL
TIG–2:00 THC +X (No Deorbit > TIG +Maintain PITCH ATT ERR � 3°
FEED FROM GOOD POD:
at ∆VTOT =or
OMS He PRESS/VAP ISOL (two) – OPOMS TK ISOL (two) – OP (tb–OP)OMS XFEED (two) – OP (tb–OP)SECURE OMS
OMS PRPLT LOWAFT RCS RECONFIG at ∆VTOT =RCS COMPLETION
DEORBITBURN
(MIXEDXFEED)
HINGE
TOPBACK OF ‘UNBALANCED PRPLT DEORBIT BURN’
ENT–5b/D/I
at %
: )
: )
(reduced copy)
CC 8–15 ENT/ALL/GEN F FAB USE ONLY
OMS PRPLT FAIL:OMS ENG – OFF
STOP BURN:APUs – SHUT DN
SAFE Secure L,R OMSHP
CONTINUE BURN:Secure L,R OMSITEM 18 +0 EXEC
�ADI – LVLH, center needlesRCS COMPLETION
OMS ENG FAIL:OMS ENG – OFF
STOP BURN:ENG APUs – SHUT DN
FAILHP CONTINUE BURN:
Man repress L,R OMS > L,R RCS TK PsFEED FROM GOOD POD:
OMS HE PRESS/VAP ISOL(two) – OP
TK ISOL (two) – OP
OMS XFEED (two) – CL
L,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL
�ADI – LVLH, center needlesTHC +X (�Lowest OMS % vs
RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION
RCS +X JET FAIL OFF:STOP BURN:
SAFE APUs – SHUT DNHP
CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jet
RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1
THC +X to PREBANK/FLIP HP orAt AFT QTY 1 TOT AFT QTY 2
if CUR HP: PREBANK/FRCS COMPLETION
PREBANK/FLIPHP
AFTHP
TGTHP
FRCS COMPLETION (if applicable):
MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)
CUTOFF VGOx = 0, Release THC+ :02 OMS ENG(s) – OFF (If < 3 IMU, at
* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)
:
**********************************************************
**********************************************************
TOPHinged at bottom of ‘DEORBIT BURN (MIXED XFEED)’
HINGE
ENT–5bb/D/I
PREBANK/FRCS COMPLETION
THC +X to TGT HP
)
%
% then
(reduced copy)
CC 8–16 ENT/ALL/GEN F FAB USE ONLY
TOP
ENTRY MANEUVERS
ENT–6a/E/LPILEVELCRO
PILEVELCRO
PILEVELCRO
PILEVELCRO
FLIGHTCONDITIONS MANEUVER
EI–5�LVLH ATT
GNC, OPS 304 PROIf PREBANK, R/Y – CSSRoll at 1°/sec toMaintain PREBANK ± 5°
If previous OMS OX TK or He TK or RCS OX TKleak: G51 VENT DOORS – OP
PTI – ENA at EI–5 when applicable
***
***
q = 1– (AOA) HYD MN PUMP PRESS (three) – NORM
‘GuidanceBox’ @
q ∼8or
D ∼3
–
CLOSED LOOP GUIDANCE ____:____:____If PREBANK: P,R/Y – AUTO
Begin AIL trim monitoring* *
D = 11 �DRAG H (FORCE if editing)V = 19K �MPS/TVC ISOL VLV – CLV = 15K �NAVAIDS (I/O RESET if reqd)
If ELS: UHF MODE – G T/R* *
V = 12K RAD BYP VLV MODE (two) – AUTOCNTLR LOOP (two) – AUTO B(A)
V = 10K �SPDBK to 81%
∆Az = 10.5° FIRST ROLL REVERSAL
(reduced copy)
CC 8–17 ENT/ALL/GEN F FAB USE ONLY
50K
38K
28K
20K
12K
7K
/
/
/
/
/
/
/
ENT–6b/E/Q
TOPBACK OF ‘ENTRY MANEUVERS’
HOOKVELCRO
HOOKVELCRO
HOOKVELCRO
HOOKVELCRO
SURF /
3K
/1K
DRAG CHUTE DEPLOYMCC Call Flight ConditionEarly Main Gear TDNOMINAL 195 KEAS
If leaking/flat tiredelay derot 10 kts
Late Post–Nose Gear TDXwind DTO
EmergencyOnly
No DeployExcept CDR call
NO DEPLOYprior to MGTD> 230 KEAS< 80 KGSXwind > 15 kts
FLIGHTCONDITIONS MANEUVER
V = 7K �TACAN status
V = 5K ADTA PROBES – DEPLOY (�HEAT)Begin AIL and RUD trim monitoring
M = 2.7�APUs
HUD PWR (two) – ON
* If M < 2.5; P CSS for ADTA to G&C incorp *
M = 2.0 Ensure ADTA to G&C else �Theta limits
M = 0.9 P, R/Y – CSS as reqd�SPDBK CMD vs POS�R FLT CNTLR – ON�NWS – 1
Lock Inertia Reels
.MAX Nz
M = 0.7 �LG EXTEND ISOL VLV – OP
h = 15K �MLS
h = 10K �A/L, TABS/VISORS – CL/LES O2 – ON (KSC)
h = 2K LANDING GEAR ARM pb – ARM
h = 300 LANDING GEAR DN pb – DN
MAIN GEAR TD �SPDBK – 100%
V = 195 KEAS DRAG CHUTE pb (two) – ARM, DPY (simo)
V = 185 KEAS DEROTATE
NOSE GEAR TDSRB SEP – MAN/AUTO and depress pb
�Auto Load Relief�HYD BRAKE ISOL VLV (three) – OP
MIDFIELD andV < 140 KGS BRAKE as required (8–10 fps2, –0.25 to –0.3G)
* If 5K’ remaining and V > 140 KGS – MAX BRAKING *
V = 60 KGS DRAG CHUTE JETT pb – JETT
V = 40 KGS BRAKE < 6 fps2 (–0.2G) (Antiskid cutout)
WHEEL STOP Go to ENT C/L, POST LANDING PROCEDURES
(reduced copy)
CC
8–
18
EN
T/A
LL
/GE
N F
FAB
US
E O
NLY
TOP
HOOKVELCRO
ENTRY NO–GO CHECKLIST
HOOKVELCRO
ENT–7a/E/I
339
343
347
351
355
359
3
7
11
15
19
23
27
31
35
39
LVLHPITCH(deg)
20
15
10
5
TIMEto EI(min)
AERO AUTO XWINDFAILURE OF: PTI DTO FCS DTO
MODE 1APU/HYD: 1 APU X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 APUs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISPLAYS: 2 ADIs X. . . . . . . . . . . . . . . . . . . .
CDR HUD X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTROLLERS:
RHC: 1L X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RHC: 2L & 2R X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RPTA: 2L or 2R X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GNC: 2 AAs (LAT) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 AAs (NORM) X(M < 2.5) X. . . . . . . . . . . . . . . . . . 2 RGAs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 R DDU PWR SPLY X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 IMU (or 1 IMU + BITE) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADTA NOT INCORP
OR DLMA X (M < 2). . . . . . . . . . . . . . . . . . . . . . . . . . . . MLS NOT INCORP X(< 6K ft). . . . . . . . . . . . . . . . . . . . . 2 FCS CH (same surface) X X. . . . . . . . . . . . . . . . . . . . . . . . . .
DPS: 1 GPC (not restrung) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 GPC (restrung) X. . . . . . . . . . . . . . . . 2 GPC (not restrung) X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 FF X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FF X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
RCS: LEAK (AFT – during ENT) X. . . . . . . 2 YAW JETs (same side) X. . . . . . . . . MIN RCS QTY X. . . . . . . . . . . . . . . . . .
TRIM: Ail > ± 2.0 deg X. . . . . . . . . . . . . . . . . . DOWNMODE:
FCS problem X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AOA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PLB: PLBD Latch Gang X. . . . . . . . . . . . . . . LDG/DECEL:
Tire Leak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HYD BRAKE ISOL VLV X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . < 100% Brakes X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NWS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ENERGY – OFF NOMINAL:Roll Ref Alert X. . . . . . . . . . . . . . . . . . . Above Upper Traj Line X. . . . . . . . . . . . MCC GCA, or VEL & PSN
update X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No A/L by 6K ft X. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DATA: OPS RECORDERS X(LOS). . . . . . . . . . . . XWIND:
< 10 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 15 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 10 Knots Gust X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GROUND SYSTEMS:No Runway Aim Point X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
HOOKVELCRO
HOOKVELCRO
HOOKVELCRO
HOOKVELCRO
NOTES
1 Consider runway redesignation (M > 6) to avoid Xwind landing2 GO if PAPI and BALL BAR available3 Pitch AUTO mode NO–GO for M < 2.54 GO if only string 4 affected
HOOKVELCRO
HOOKVELCRO
4
4
2
3
3
3
(red
uce
d cop
y)
CC
8–
19
EN
T/A
LL
/GE
N F
FAB
US
E O
NLY
POST LANDINGMODE 5
TABS – RELEASEVISOR – CLOSE/LOCKLES O2 – ONGREEN APPLE – PULLKNEEBOARDS – REMOVECOOLING – DISCONNECTRESTRAINT – RELEASEPARACHUTE (four) – RELEASE
COMM – DISCONNECT(G–SUIT CLIP – PULL)LES O2 – DISCONNECTPLT – EMER PWR DOWNEGRESS SEATSLIDE/ESCAPE PANEL
HOOKVELCRO
HOOKVELCRO
RATIO < 1
MCC: AUTOor INH*
COMMOK
NOCOMM
IF BADADTA
RATIO > 1
G&CNAV
AUTO
TACANOK
MCC: INH
IF BAD NAVSTATE
MCC:FORCE
NO TACANADTA
ERRATICADTA
STEADYINH AUTO FORCE
Two or moregood ADTAs
Evaluate h,�,MMCC:
AUTO (G&C)
Evaluate h,�,MIf reasonable:
AUTO (G&C)
*(If ADTA H will degrade NAV state)
ADTA MGMT
HOOKVELCRO
HOOKVELCRO ENT–7b/E/N
TOPBACK OF ‘ENTRY NO–GO CHECKLIST’
V = 6K NO COMM TACAN MGMT
If 1st acq –FORCE
IF NOT –ZERO �STATE
RATIO< 1 RATIO > 1 ONE TACAN
LOCKED NO LOCK
AUTO TROUBLESHOOT BELOW V =5.5K
DESELECTMISSINGTACANS,then –AUTO
BELOW V =5.5K
TOGGLETACAN
IF BADTACAN
IF BAD NAVSTATE
AUTO
For � STATE UPDATES (on MCC call):P, R/Y – CSSDRAG H, TACAN, ADTA – INHOn MCC call, back to AUTO
NAV DELTA PAD
�Z 15 ( )
( )
( )
( )
( )
( )�X 10
�Y 11
�Z 12
�X 13
�Y 14
BAILOUTMODE 8
REPORT POSITION�MACH < .95
P, R/Y – CSS
OPS 305/603 PRO (if reqd)
SB – AUTO; BF – AUTO
FLY 185–195 KEAS, Φ = 0°ABORT MODE – ATO
ABORT PBI – PUSH
P,R/Y – AUTO
FLT CNTLR PWR (two) – OFF
∼50K FT
TABS – RELEASE
VISOR – CLOSE / LOCK
LES O2 – ON
GREEN APPLE – PULL
∼40K FT
MS3 – VENT CABIN
CDR,PLT SEATS – LOWER
KNEEBOARDS – REMOVE
COOLING – DISCONNECT
RESTRAINT – RELEASE
D–RING – UNCOVER
∼30K FT
MS3 – JETTISON HATCH
COMM – DISCONNECT
(G–SUIT CLIP – PULL)
LES O2 – DISCONNECT
EGRESS SEAT
POLE – DEPLOY
D–RING – HOOK UP
BAILOUT
(red
uce
d cop
y)
EN
T/A
LL
/GE
N F,1
CC 8–20 ENT/ALL/GEN F FAB USE ONLY
�
�
�
���
TOP
�����������������
�� ��� ��
���� ���MACH/�
��
ENT/8a/A,E/C
TOP BACK
HOOKVELCRO
ENT/8b/A,E/B
HOOKVELCRO
�
��
���
CC
8–
21
EN
T/A
LL
/GE
N F
FAB
US
E O
NLY
HOOKVELCRO
TOP
HOOKVELCRO
HOOKVELCRO
HOOKVELCRO
ENT–10a/A,E/A
ENTRY CONTROL
(Continued on back for ‘HIGH–FREQ OSC OR SURF/JET CYCLE’)
ARCS QTY (L + R) < 10%ARCS QTY = 0 & JETSFAIL OFF
1. ENTRY MODE – NO Y JET(R/Y CSS; expect sluggish control)
q ≥ 20 & M > 6 2. G51 ELEVON FIXED – ITEM 18 EXEC (*)
CONTROLPROBLEMS* &ARCS QTY > 0
3. ENTRY MODE – AUTOWhen control regained:
4. ENTRY MODE – NO Y JET5. �AIL trim
M < 6 & ARCS QTY > 0 6. ENTRY MODE – AUTOM < 5 7. TRIM/RHC PNL – ENA
8. TRIM ROLL – away from AIL trim (to < 1)*Region of least margin: M 12–8
AIL TRIM ≥ 3°TAL 1. G51 WRAP MODE – ITEM 45 EXEC (ACT)AIL trim = 5 2. BF – MAN
3. BF – UP (to 0%)NO Y JET 4. Perform roll reversals at 3°/s (expect sluggish control)M < 13 &AIL trim = 5
5. P – CSS6. Fly α per schedule:
M 12 11 10 9 8–6 5α 37 36 35 33 30 26
M < 5 7. TRIM/RHC PNL – ENA8. TRIM ROLL – away from AIL trim (to < 1)9. P – AUTO
M < 2 10. BF – AUTO
(red
uce
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CC
8–
22
EN
T/A
LL
/GE
N F
FAB
US
E O
NLY
HOOKVELCRO
TOPBACK OF ‘ENTRY CONTROL’
HOOKVELCRO
HOOKVELCRO
HOOKVELCRO
ENT–10b/A,E/A
HIGH–FREQ OSC OR SURF/JET CYCLEReturning PL> 10K lbs
1. G51 �FILTER ALT – ITEM 21 (*)
2. P, R/Y – CSSOsc/Cycle continues 3. ENTRY MODE – LO GAIN
Osc/Cyclestops
4. ENTRY MODE – AUTO5. P, R/Y – AUTO
(red
uce
d cop
y)
8–23 ENT/ALL/GEN F FAB USE ONLY
Replace this page with page(s) from Flight Supplement
8–24 ENT/ALL/GEN F FAB USE ONLY
Replace this page with page(s) from Flight Supplement
ENTRYCHECKLIST
JSC–48019GENERIC, REV F
Flight Cover (trim bottom to expose tabs)
ALL