-----------------------------------------------------------------------
  **MSFC PRACA : 2003-02-12 08:41**

  -----------------------------------------------------------------------

  -----------------------------------------------------------------------
  MSFC Problem Reporting and Corrective Action (PRACA) System

  WHOLE RECORD REPORT( + ADDENDUM)
  -----------------------------------------------------------------------

+-------------+---------------+-------------+--------+------+--------+
| **MSFC      | **In-Flight   | *           | **J    | *    |        |
| Record      | Anomaly       | *Contractor | SC#**\ | *KSC |        |
| \#**\       | Number**\     | Report      | \--    | #**\ |        |
| A16905      | \--           | Number**\   |        | \--  |        |
|             |               | P-081       |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Problem   |               |             |        |      |        |
| Title**\    |               |             |        |      |        |
| HE          |               |             |        |      |        |
| INJECTION   |               |             |        |      |        |
| FLEX HOSE   |               |             |        |      |        |
| RUPTURED    |               |             |        |      |        |
| DURING      |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| QUAL TEST   |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **EICN#**\  | **ELEMENT**\  | **Co        | **FS   | **   |        |
| \--         | ET            | ntractor**\ | CM#**\ | FCRI |        |
|             |               | LMMSS       | \--    | T**\ |        |
|             |               |             |        | 1    |        |
+-------------+---------------+-------------+--------+------+--------+
| **HCRIT**\  | **Sys_Lvl**\  | **Misc      |        |      |        |
| \--         | \--           | Codes**\    |        |      |        |
|             |               | A B C D E F |        |      |        |
|             |               | G H I J K L |        |      |        |
|             |               | M N O       |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **          | **NO          | **PART#**\  | *      | *    |        |
| HARDWARE**\ | MENCLATURE**\ | \--         | *SER/L | *MAN |        |
| EIM         | \--           |             | OT#**\ | UFAC |        |
|             |               |             | \--    | TURE |        |
|             |               |             |        | R**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **          | **NO          | **PART#**\  | *      | *    |        |
| HARDWARE**\ | MENCLATURE**\ | \--         | *SER/L | *MAN |        |
| LRU         | \--           |             | OT#**\ | UFAC |        |
|             |               |             | \--    | TURE |        |
|             |               |             |        | R**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **          | **NO          | **PART#**\  | *      | *    |        |
| HARDWARE**\ | MENCLATURE**\ | 32L20       | *SER/L | *MAN |        |
| NCA         | HE INJECTION  | 600133BA000 | OT#**\ | UFAC |        |
|             | FLEX HO       |             | 0      | TURE |        |
|             |               |             | 000026 | R**\ |        |
|             |               |             |        | TITE |        |
|             |               |             |        | FLEX |        |
|             |               |             |        | COR  |        |
+-------------+---------------+-------------+--------+------+--------+
| **Test/O    | **Prevailing  | **F / U**\  | **Fail | **   |        |
| peration**\ | Condtion**\   | F           | M      | Caus |        |
| Q - QAL     | V - VIBRATION |             | ode**\ | e**\ |        |
|             |               |             | MS -   | ET - |        |
|             |               |             | STRUCT | EI-  |        |
|             |               |             |        | TEST |        |
+-------------+---------------+-------------+--------+------+--------+
| **System**\ | **Defect**\   | **          | **Work | **   |        |
| PROPULSION  | DC - BROKEN   | Material**\ | Cont   | Fail |        |
|             |               | S - STRUCT  | act**\ | Dat  |        |
|             |               |             | D.     | e**\ |        |
|             |               |             | O      | 08   |        |
|             |               |             | \`NEAL | /13/ |        |
|             |               |             |        | 1996 |        |
+-------------+---------------+-------------+--------+------+--------+
| **Received  | **Date        | **FMEA      | **IFA: | *    |        |
| at MSFC**\  | Isolated**\   | R           | M      | *Mis |        |
| 08/16/1996  | 08/13/1996    | eference**\ | ission | sion |        |
|             |               | 2.4.9.1     | Ph     | Ela  |        |
|             |               |             | ase**\ | psed |        |
|             |               |             | \--    | Tim  |        |
|             |               |             |        | e**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **          |               | *           |        | **   |        |
| Location**\ |               | *Symptom**\ |        | Time |        |
| MSFC        |               | MS - STRUCT |        | Cycl |        |
|             |               |             |        | e**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **          |               |             |        |      |        |
| Effectivity |               |             |        |      |        |
| Text**\     |               |             |        |      |        |
| ET-80 AND   |               |             |        |      |        |
| UP          |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Vehicle   |               |             |        |      |        |
| Effectivity |               |             |        |      |        |
| Codes**     |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Vehicle   | **Vehicle     | **Vehicle   | **V    | *    |        |
| 1**\        | 2**\          | 3**\        | ehicle | *Veh |        |
| \--         | \--           | \--         | 4**\   | icle |        |
|             |               |             | \--    | 5**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **Mission   |               |             |        |      |        |
| Effectivity |               |             |        |      |        |
| Codes**     |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Mssn 1**\ | **Mssn 2**\   | **Mssn 3**\ | **Mssn | **   |        |
| \--         | \--           | \--         | 4**\   | Mssn |        |
|             |               |             | \--    | 5**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **Estimated |               |             |        |      |        |
| Completion  |               |             |        |      |        |
| Dates**     |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **MSFC      | **Contractor  | **LVL 3     | **     |      |        |
| Approved    | Req Defer     | Close**\    | Remark |      |        |
| Defer Until | Until Date**\ | \--         | /      |      |        |
| Date**\     | \--           |             | Act    |      |        |
| 03/09/1997  |               |             | ion**\ |      |        |
|             |               |             | 09/2   |      |        |
|             |               |             | 4/1996 |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **In        |               |             |        |      |        |
| vestigation |               |             |        |      |        |
| /           |               |             |        |      |        |
| Resolution  |               |             |        |      |        |
| Summary**   |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Last MSFC | **CN RSLV     | **Defer     | **Add  | *    |        |
| Update**\   | SBMT**\       | Date**\     | D      | *R/C |        |
| 02/13/2001  | 09/25/1996    | \--         | ate**\ | Code |        |
|             |               |             | 08/1   | s**\ |        |
|             |               |             | 6/1996 | 4 -  |        |
|             |               |             |        | TEST |        |
|             |               |             |        | \--  |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| *           |               |             |        |      |        |
| *Assignee** |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Design**\ | **Chief       | **S & MA**\ | **Proj | *    |        |
| J. SANFORD  | Engineer**\   | M. SMILES   | ect**\ | *Pro |        |
|             | M. PESSIN     |             | \--    | ject |        |
|             |               |             |        | MG   |        |
|             |               |             |        | R**\ |        |
|             |               |             |        | P.   |        |
|             |               |             |        | CO   |        |
|             |               |             |        | UNTS |        |
+-------------+---------------+-------------+--------+------+--------+
| *           |               |             |        |      |        |
| *Approval** |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Design**\ | **Chief       | **S & MA**\ | **Proj | *    |        |
| J. SANFORD  | Engineer**\   | M. SMILES   | ect**\ | *Pro |        |
|             | M. PESSIN     |             | \--    | ject |        |
|             |               |             |        | MG   |        |
|             |               |             |        | R**\ |        |
|             |               |             |        | P.   |        |
|             |               |             |        | CO   |        |
|             |               |             |        | UNTS |        |
+-------------+---------------+-------------+--------+------+--------+
| **PAC       | **PAC Review  | **MSFC      | **Sta  | *    |        |
| Assignee**\ | Complete**\   | Closure     | tus**\ | *F/A |        |
| R. TUCKER   | RHT           | Date**\     | C -    | C    |        |
|             |               | 10/02/1996  | CLOSED | ompl |        |
|             |               |             |        | etio |        |
|             |               |             |        | n**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **Problem   | **SEV**\      | **Program   | **R    | **O  |        |
| Type**\     | \--           | Name**\     | EVL**\ | PRIN |        |
| \--         |               | \--         | \--    | C**\ |        |
|             |               |             |        | \--  |        |
+-------------+---------------+-------------+--------+------+--------+
| **FUNC      | **Software    | **Software  |        | **SU | **So   |
| MOD**\      | E             | Fail CD**\  |        | BTYP | ftware |
| \--         | ffectivity**\ | \--         |        | E**\ | C      |
|             | \-- \-- \--   |             |        | \--  | losure |
|             | \-- \--       |             |        |      | CD**\  |
|             |               |             |        |      | \--    |
+-------------+---------------+-------------+--------+------+--------+
| **RES       | **Approval    |             |        |      |        |
| PERSON      | Signature     |             |        |      |        |
| L2**\       | L3**\         |             |        |      |        |
| \--         | \--           |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Related   | **Related     |             |        |      |        |
| Document    | Document      |             |        |      |        |
| Type**\     | ID**\         |             |        |      |        |
| \--         | N012111       |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Related   |               |             |        |      |        |
| Document    |               |             |        |      |        |
| Title**\    |               |             |        |      |        |
| \--         |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Related   | **Related     |             |        |      |        |
| Document    | Document      |             |        |      |        |
| Type**\     | ID**\         |             |        |      |        |
| \--         | \--           |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Related   |               |             |        |      |        |
| Document    |               |             |        |      |        |
| Title**\    |               |             |        |      |        |
| \--         |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Related   | **Related     |             |        |      |        |
| Document    | Document      |             |        |      |        |
| Type**\     | ID**\         |             |        |      |        |
| \--         | \--           |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Related   |               |             |        |      |        |
| Document    |               |             |        |      |        |
| Title**\    |               |             |        |      |        |
| \--         |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| *           |               |             |        |      |        |
| *Contractor |               |             |        |      |        |
| Status      |               |             |        |      |        |
| Summary**   |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Reliabil  |               |             |        |      |        |
| ity/Quality |               |             |        |      |        |
| Assurance   |               |             |        |      |        |
| Concerns,   |               |             |        |      |        |
| Recomme     |               |             |        |      |        |
| ndations:** |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **Problem   |               |             |        |      |        |
| De          |               |             |        |      |        |
| scription** |               |             |        |      |        |
|             |               |             |        |      |        |
| DURING THE  |               |             |        |      |        |
| FLEX HOSE   |               |             |        |      |        |
| DELTA       |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| TEST FOR    |               |             |        |      |        |
| SLWT        |               |             |        |      |        |
|             |               |             |        |      |        |
| BEING       |               |             |        |      |        |
| CONDUCTED   |               |             |        |      |        |
| AT MSFC,    |               |             |        |      |        |
| THE FLEX    |               |             |        |      |        |
| HOSE BROKE  |               |             |        |      |        |
| INTO TWO    |               |             |        |      |        |
| PIECES      |               |             |        |      |        |
|             |               |             |        |      |        |
| (REFERENCE  |               |             |        |      |        |
| NCD012111   |               |             |        |      |        |
| AND TEST    |               |             |        |      |        |
| PROCEDURE   |               |             |        |      |        |
| 809-2077)   |               |             |        |      |        |
|             |               |             |        |      |        |
| C           |               |             |        |      |        |
| RITICALITY: |               |             |        |      |        |
| THE FLEX    |               |             |        |      |        |
| LINE IS     |               |             |        |      |        |
| CRIT. 1;    |               |             |        |      |        |
|             |               |             |        |      |        |
| FMEA ITEM   |               |             |        |      |        |
| CODE        |               |             |        |      |        |
| 2.4.9.1,    |               |             |        |      |        |
| \"LEAKAGE\" |               |             |        |      |        |
| AND/OR      |               |             |        |      |        |
| DAMAGE      |               |             |        |      |        |
|             |               |             |        |      |        |
| INFLICTED   |               |             |        |      |        |
| TO THE      |               |             |        |      |        |
| ADJACENT    |               |             |        |      |        |
| WIRING      |               |             |        |      |        |
| HARNESS     |               |             |        |      |        |
|             |               |             |        |      |        |
| DUE TO      |               |             |        |      |        |
| STRUCTURAL  |               |             |        |      |        |
| FAILURE OF  |               |             |        |      |        |
| THE HOSE    |               |             |        |      |        |
| ASSEMBLY    |               |             |        |      |        |
|             |               |             |        |      |        |
| REV. \"C\", |               |             |        |      |        |
| REVISES     |               |             |        |      |        |
| TASKS I.A,  |               |             |        |      |        |
| B, C, AND   |               |             |        |      |        |
| D, II, III  |               |             |        |      |        |
|             |               |             |        |      |        |
| AND IV AND  |               |             |        |      |        |
| CLOSES      |               |             |        |      |        |
| CAPS. (SEE  |               |             |        |      |        |
| ASTERISKS)  |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| *           |               |             |        |      |        |
| *Contractor |               |             |        |      |        |
| Inve        |               |             |        |      |        |
| stigation/R |               |             |        |      |        |
| esolution** |               |             |        |      |        |
|             |               |             |        |      |        |
| GENERAL:    |               |             |        |      |        |
|             |               |             |        |      |        |
| \- THIS     |               |             |        |      |        |
| FLEX HOSE   |               |             |        |      |        |
| CONNECTS    |               |             |        |      |        |
| HELIUM      |               |             |        |      |        |
| INJECTION   |               |             |        |      |        |
| TUBE        |               |             |        |      |        |
| ASSEMBLIES  |               |             |        |      |        |
| LOCATED     |               |             |        |      |        |
|             |               |             |        |      |        |
| IN THE LH2  |               |             |        |      |        |
| CABLE TRAY  |               |             |        |      |        |
| AND         |               |             |        |      |        |
| VERTICAL    |               |             |        |      |        |
| STRUT CABLE |               |             |        |      |        |
| TRAY AT     |               |             |        |      |        |
|             |               |             |        |      |        |
| STATION     |               |             |        |      |        |
| 2033. THE   |               |             |        |      |        |
| HOSE IS     |               |             |        |      |        |
| FABRICATED  |               |             |        |      |        |
| USING       |               |             |        |      |        |
| CORRUGATED  |               |             |        |      |        |
| STEEL,      |               |             |        |      |        |
|             |               |             |        |      |        |
| BRAID WIRE  |               |             |        |      |        |
| RE          |               |             |        |      |        |
| INFORCEMENT |               |             |        |      |        |
| AND END     |               |             |        |      |        |
| FITTINGS.   |               |             |        |      |        |
| ALL HOSE    |               |             |        |      |        |
| MATERIAL IS |               |             |        |      |        |
|             |               |             |        |      |        |
| CORROSION   |               |             |        |      |        |
| RESISTANT   |               |             |        |      |        |
| STEEL       |               |             |        |      |        |
|             |               |             |        |      |        |
| \- THE TEST |               |             |        |      |        |
| REQUIRES    |               |             |        |      |        |
| FLIGHT      |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| RANDOM      |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| AND FLIGHT  |               |             |        |      |        |
|             |               |             |        |      |        |
| DYNAMIC     |               |             |        |      |        |
| SINE        |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| TESTING TO  |               |             |        |      |        |
| BE          |               |             |        |      |        |
| PERFORMED   |               |             |        |      |        |
| IN Y-AXIS,  |               |             |        |      |        |
| X-AXIS      |               |             |        |      |        |
|             |               |             |        |      |        |
| AND Z-AXIS  |               |             |        |      |        |
|             |               |             |        |      |        |
| \- THE      |               |             |        |      |        |
| FAILURE     |               |             |        |      |        |
| OCCURRED 2  |               |             |        |      |        |
| MINUTES AND |               |             |        |      |        |
| 52 SECONDS  |               |             |        |      |        |
| INTO THE 3  |               |             |        |      |        |
| MINUTE      |               |             |        |      |        |
|             |               |             |        |      |        |
| RANDOM      |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| TEST BEING  |               |             |        |      |        |
| CONDUCTED   |               |             |        |      |        |
| IN THE      |               |             |        |      |        |
| Y-AXIS.     |               |             |        |      |        |
| BOTH THE    |               |             |        |      |        |
|             |               |             |        |      |        |
| Z-AXIS AND  |               |             |        |      |        |
| X-AXIS      |               |             |        |      |        |
| TESTS       |               |             |        |      |        |
| (RANDOM AND |               |             |        |      |        |
| FLIGHT      |               |             |        |      |        |
| DYNAMIC)    |               |             |        |      |        |
| HAD BEEN    |               |             |        |      |        |
|             |               |             |        |      |        |
| S           |               |             |        |      |        |
| UCCESSFULLY |               |             |        |      |        |
| COMPLETED   |               |             |        |      |        |
|             |               |             |        |      |        |
| TASK I.     |               |             |        |      |        |
| FAILURE     |               |             |        |      |        |
| /PROBLEM    |               |             |        |      |        |
| IN          |               |             |        |      |        |
| VESTIGATION |               |             |        |      |        |
|             |               |             |        |      |        |
| A. REVIEW   |               |             |        |      |        |
| TEST DATA   |               |             |        |      |        |
| AND VERIFY  |               |             |        |      |        |
| ALL TEST    |               |             |        |      |        |
| PARAMETERS  |               |             |        |      |        |
| WERE WITHIN |               |             |        |      |        |
|             |               |             |        |      |        |
| SP          |               |             |        |      |        |
| ECIFICATION |               |             |        |      |        |
| DURING THE  |               |             |        |      |        |
| TEST        |               |             |        |      |        |
|             |               |             |        |      |        |
| RESP        |               |             |        |      |        |
| ONSIBILITY: |               |             |        |      |        |
| J.          |               |             |        |      |        |
| BLE         |               |             |        |      |        |
| VINS/4410 - |               |             |        |      |        |
| J. DYE/4400 |               |             |        |      |        |
|             |               |             |        |      |        |
| \*          |               |             |        |      |        |
| COMPLETE:   |               |             |        |      |        |
| 8/29/96     |               |             |        |      |        |
|             |               |             |        |      |        |
| \* CLOSURE  |               |             |        |      |        |
| STATEMENT   |               |             |        |      |        |
|             |               |             |        |      |        |
| A REVIEW OF |               |             |        |      |        |
| TEST DATA   |               |             |        |      |        |
| HAS SHOWN   |               |             |        |      |        |
| THAT THE X  |               |             |        |      |        |
| AND Z-AXIS  |               |             |        |      |        |
|             |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| EXPOSURES   |               |             |        |      |        |
| REMAINED IN |               |             |        |      |        |
| TOLERANCE   |               |             |        |      |        |
| FOR BOTH    |               |             |        |      |        |
| VEHICLE     |               |             |        |      |        |
|             |               |             |        |      |        |
| DYNAMICS    |               |             |        |      |        |
| SINE        |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| AND FLIGHT  |               |             |        |      |        |
| RANDOM      |               |             |        |      |        |
| VIBRATION.  |               |             |        |      |        |
| THE         |               |             |        |      |        |
|             |               |             |        |      |        |
| Y-AXIS      |               |             |        |      |        |
| FLIGHT      |               |             |        |      |        |
| RANDOM      |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| TEST,       |               |             |        |      |        |
| HOWEVER,    |               |             |        |      |        |
| CONTAINED   |               |             |        |      |        |
| HIGH        |               |             |        |      |        |
|             |               |             |        |      |        |
| FREQUENCY   |               |             |        |      |        |
| HARMONICS   |               |             |        |      |        |
| WHICH       |               |             |        |      |        |
| EXCEEDED    |               |             |        |      |        |
| THE UPPER   |               |             |        |      |        |
| TOLERANCE.  |               |             |        |      |        |
| AN          |               |             |        |      |        |
|             |               |             |        |      |        |
| EVALUATION  |               |             |        |      |        |
| DETERMINED  |               |             |        |      |        |
| THAT THE    |               |             |        |      |        |
| HOSE        |               |             |        |      |        |
| ASSEMBLY    |               |             |        |      |        |
| WAS NOT     |               |             |        |      |        |
| AFFECTED BY |               |             |        |      |        |
|             |               |             |        |      |        |
| THIS Y-AXIS |               |             |        |      |        |
| TOLERANCE   |               |             |        |      |        |
| EXCEEDANCE. |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| IOM         |               |             |        |      |        |
| 4410-96-042 |               |             |        |      |        |
|             |               |             |        |      |        |
| B. PERFORM  |               |             |        |      |        |
| FAILURE     |               |             |        |      |        |
| ANALYSIS ON |               |             |        |      |        |
| FAILED FLEX |               |             |        |      |        |
| HOSE        |               |             |        |      |        |
|             |               |             |        |      |        |
| RESP        |               |             |        |      |        |
| ONSIBILITY: |               |             |        |      |        |
| J.          |               |             |        |      |        |
| RUS         |               |             |        |      |        |
| SELL/3741 - |               |             |        |      |        |
| D.          |               |             |        |      |        |
| WE          |               |             |        |      |        |
| STPHAL/3740 |               |             |        |      |        |
|             |               |             |        |      |        |
| J.          |               |             |        |      |        |
| MATTHEE     |               |             |        |      |        |
| SSEN/3741 - |               |             |        |      |        |
| D.          |               |             |        |      |        |
| WE          |               |             |        |      |        |
| STPHAL/3740 |               |             |        |      |        |
|             |               |             |        |      |        |
| R.          |               |             |        |      |        |
| LEB         |               |             |        |      |        |
| OEUF/4643 - |               |             |        |      |        |
| E.          |               |             |        |      |        |
| HORAK/4600  |               |             |        |      |        |
|             |               |             |        |      |        |
| \*          |               |             |        |      |        |
| COMPLETE:   |               |             |        |      |        |
| 9/6/96      |               |             |        |      |        |
|             |               |             |        |      |        |
| CLOSURE     |               |             |        |      |        |
| STATEMENT   |               |             |        |      |        |
|             |               |             |        |      |        |
| SEM AND     |               |             |        |      |        |
| P           |               |             |        |      |        |
| HOTOGRAPHIC |               |             |        |      |        |
| EXAMINATION |               |             |        |      |        |
| SHOWS       |               |             |        |      |        |
| EVIDENCE    |               |             |        |      |        |
| CONSISTENT  |               |             |        |      |        |
| WITH        |               |             |        |      |        |
|             |               |             |        |      |        |
| FATIGUE     |               |             |        |      |        |
| FAILURE; NO |               |             |        |      |        |
| UNEXPECTED  |               |             |        |      |        |
| CONDITIONS  |               |             |        |      |        |
| WERE NOTED. |               |             |        |      |        |
| CHEMICAL    |               |             |        |      |        |
|             |               |             |        |      |        |
| ANALYSIS OF |               |             |        |      |        |
| ASSEMBLY\'S |               |             |        |      |        |
| COMPONENTS  |               |             |        |      |        |
| SHOW THEM   |               |             |        |      |        |
| TO BE OF    |               |             |        |      |        |
| THE PROPER  |               |             |        |      |        |
|             |               |             |        |      |        |
| MATERIALS.  |               |             |        |      |        |
| A           |               |             |        |      |        |
| COMPARATIVE |               |             |        |      |        |
| ANALYSIS    |               |             |        |      |        |
| WITH AN     |               |             |        |      |        |
| UNDAMAGED   |               |             |        |      |        |
| HOSE SHOW   |               |             |        |      |        |
|             |               |             |        |      |        |
| NO          |               |             |        |      |        |
| ABNORMAL    |               |             |        |      |        |
| /UNEXPECTED |               |             |        |      |        |
| CONDITIONS. |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| LAB         |               |             |        |      |        |
|             |               |             |        |      |        |
| REPORT NO.  |               |             |        |      |        |
| 96A196      |               |             |        |      |        |
|             |               |             |        |      |        |
| C. EVALUATE |               |             |        |      |        |
| LWT         |               |             |        |      |        |
| E           |               |             |        |      |        |
| NVIRONMENTS |               |             |        |      |        |
| VS. SLWT    |               |             |        |      |        |
| E           |               |             |        |      |        |
| NVIRONMENTS |               |             |        |      |        |
| RELATIVE TO |               |             |        |      |        |
| THE         |               |             |        |      |        |
|             |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| R           |               |             |        |      |        |
| EQUIREMENTS |               |             |        |      |        |
| FOR THIS    |               |             |        |      |        |
| FLEX HOSE.  |               |             |        |      |        |
| DETERMINE   |               |             |        |      |        |
| IF          |               |             |        |      |        |
|             |               |             |        |      |        |
| THIS        |               |             |        |      |        |
| FAILURE     |               |             |        |      |        |
| IMPACTS LWT |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
|             |               |             |        |      |        |
| RESP        |               |             |        |      |        |
| ONSIBILITY: |               |             |        |      |        |
| L.          |               |             |        |      |        |
| PAL         |               |             |        |      |        |
| ERMO/4410 - |               |             |        |      |        |
| J. DYE/4400 |               |             |        |      |        |
|             |               |             |        |      |        |
| \*          |               |             |        |      |        |
| COMPLETE:   |               |             |        |      |        |
| 9/23/96     |               |             |        |      |        |
|             |               |             |        |      |        |
| CLOSURE     |               |             |        |      |        |
| STATEMENT   |               |             |        |      |        |
|             |               |             |        |      |        |
| AN          |               |             |        |      |        |
| INSPECTION  |               |             |        |      |        |
| OF THE SLWT |               |             |        |      |        |
| ENVIRONMENT |               |             |        |      |        |
| SHOWED AN   |               |             |        |      |        |
| EXCEEDANCE  |               |             |        |      |        |
| OVER        |               |             |        |      |        |
|             |               |             |        |      |        |
| THE         |               |             |        |      |        |
| HISTORIC    |               |             |        |      |        |
| LWT TEST.   |               |             |        |      |        |
| TRANSLATING |               |             |        |      |        |
| THE SLWT    |               |             |        |      |        |
| ENVIRONMENT |               |             |        |      |        |
| TO THE      |               |             |        |      |        |
|             |               |             |        |      |        |
| LWT LEVEL   |               |             |        |      |        |
| SHOWED A    |               |             |        |      |        |
| LOW         |               |             |        |      |        |
| FREQUENCY   |               |             |        |      |        |
| EXCEEDANCE  |               |             |        |      |        |
| STILL       |               |             |        |      |        |
| EXISTED     |               |             |        |      |        |
|             |               |             |        |      |        |
| AFTER       |               |             |        |      |        |
| EVALUATION  |               |             |        |      |        |
| BY          |               |             |        |      |        |
| E           |               |             |        |      |        |
| NGINEERING, |               |             |        |      |        |
| A DECISION  |               |             |        |      |        |
| WAS MADE TO |               |             |        |      |        |
| ADJUST      |               |             |        |      |        |
|             |               |             |        |      |        |
| THE TEST    |               |             |        |      |        |
| E           |               |             |        |      |        |
| NVIRONMENTS |               |             |        |      |        |
| AND UPDATE  |               |             |        |      |        |
| THE LWT     |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| FOR THIS    |               |             |        |      |        |
|             |               |             |        |      |        |
| HOSE AS     |               |             |        |      |        |
| WELL AS     |               |             |        |      |        |
| RETEST FOR  |               |             |        |      |        |
| SLWT        |               |             |        |      |        |
| EN          |               |             |        |      |        |
| VIRONMENTS. |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| TEST        |               |             |        |      |        |
|             |               |             |        |      |        |
| PLANS       |               |             |        |      |        |
| 809-2080    |               |             |        |      |        |
| (LWT) AND   |               |             |        |      |        |
| 809-2078    |               |             |        |      |        |
| (SLWT).     |               |             |        |      |        |
| BOTH HOSES  |               |             |        |      |        |
| WERE        |               |             |        |      |        |
|             |               |             |        |      |        |
| S           |               |             |        |      |        |
| UCCESSFULLY |               |             |        |      |        |
| PASSED.     |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| IOM         |               |             |        |      |        |
| 4410-96-045 |               |             |        |      |        |
|             |               |             |        |      |        |
| D. REVIEW   |               |             |        |      |        |
| THE BUILD   |               |             |        |      |        |
| DATA        |               |             |        |      |        |
| RELATIVE TO |               |             |        |      |        |
| THIS FLEX   |               |             |        |      |        |
| HOSE AND    |               |             |        |      |        |
| EVALUATE    |               |             |        |      |        |
|             |               |             |        |      |        |
| FOR         |               |             |        |      |        |
| COMPLIANCE  |               |             |        |      |        |
| TO          |               |             |        |      |        |
| R           |               |             |        |      |        |
| EQUIREMENTS |               |             |        |      |        |
|             |               |             |        |      |        |
| RESP        |               |             |        |      |        |
| ONSIBILITY: |               |             |        |      |        |
| F.          |               |             |        |      |        |
| RA          |               |             |        |      |        |
| MSEY/3761 - |               |             |        |      |        |
| S.          |               |             |        |      |        |
| PARIKH/3760 |               |             |        |      |        |
|             |               |             |        |      |        |
| J.          |               |             |        |      |        |
| RUS         |               |             |        |      |        |
| SELL/3741 - |               |             |        |      |        |
| D.          |               |             |        |      |        |
| WE          |               |             |        |      |        |
| STPHAL/3740 |               |             |        |      |        |
|             |               |             |        |      |        |
| \*          |               |             |        |      |        |
| COMPLETE:   |               |             |        |      |        |
| 9/12/96     |               |             |        |      |        |
|             |               |             |        |      |        |
| CLOSURE     |               |             |        |      |        |
| STATEMENT   |               |             |        |      |        |
|             |               |             |        |      |        |
| ATTEMPTS TO |               |             |        |      |        |
| LOCATE THE  |               |             |        |      |        |
| BUILD DATA  |               |             |        |      |        |
| AT TITEFLEX |               |             |        |      |        |
| WERE        |               |             |        |      |        |
| U           |               |             |        |      |        |
| NSUCCESSFUL |               |             |        |      |        |
|             |               |             |        |      |        |
| THIS HOSE   |               |             |        |      |        |
| WAS         |               |             |        |      |        |
| M           |               |             |        |      |        |
| NAUFACTURED |               |             |        |      |        |
| IN JULY     |               |             |        |      |        |
| 1989;       |               |             |        |      |        |
| TITEFLEX IS |               |             |        |      |        |
|             |               |             |        |      |        |
| CO          |               |             |        |      |        |
| NTRACTUALLY |               |             |        |      |        |
| REQUIRED TO |               |             |        |      |        |
| RETAIN THE  |               |             |        |      |        |
| DATA FOR A  |               |             |        |      |        |
| PERIOD OF   |               |             |        |      |        |
| SEVEN       |               |             |        |      |        |
|             |               |             |        |      |        |
| YEARS. AS   |               |             |        |      |        |
| THE SEVEN   |               |             |        |      |        |
| YEARS       |               |             |        |      |        |
| LIMITATION  |               |             |        |      |        |
| HAS PASSED, |               |             |        |      |        |
| THE SEARCH  |               |             |        |      |        |
|             |               |             |        |      |        |
| FOR DATA    |               |             |        |      |        |
| WAS         |               |             |        |      |        |
| DI          |               |             |        |      |        |
| SCONTINUED. |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| CCMAIL FROM |               |             |        |      |        |
| F. RAMSEY,  |               |             |        |      |        |
|             |               |             |        |      |        |
| PROCUREMENT |               |             |        |      |        |
| QUALITY;    |               |             |        |      |        |
| DATED       |               |             |        |      |        |
| 9/12/96     |               |             |        |      |        |
|             |               |             |        |      |        |
| E. REVIEW   |               |             |        |      |        |
| THE         |               |             |        |      |        |
| NON         |               |             |        |      |        |
| CONFORMANCE |               |             |        |      |        |
| DATABASE    |               |             |        |      |        |
| FOR SIMILAR |               |             |        |      |        |
| FAILURES    |               |             |        |      |        |
|             |               |             |        |      |        |
| RESP        |               |             |        |      |        |
| ONSIBILITY: |               |             |        |      |        |
| J.          |               |             |        |      |        |
| RUS         |               |             |        |      |        |
| SELL/3741 - |               |             |        |      |        |
| D.          |               |             |        |      |        |
| WE          |               |             |        |      |        |
| STPHAL/3740 |               |             |        |      |        |
|             |               |             |        |      |        |
| COMPLETE:   |               |             |        |      |        |
| 8/20/96     |               |             |        |      |        |
|             |               |             |        |      |        |
| CLOSURE     |               |             |        |      |        |
| STATEMENT   |               |             |        |      |        |
|             |               |             |        |      |        |
| A SEARCH    |               |             |        |      |        |
| WAS         |               |             |        |      |        |
| CONDUCTED   |               |             |        |      |        |
| FOR ALL     |               |             |        |      |        |
| NONC        |               |             |        |      |        |
| ONFORMANCES |               |             |        |      |        |
| WRITTEN     |               |             |        |      |        |
| AGAINST     |               |             |        |      |        |
|             |               |             |        |      |        |
| 32L2XXX AND |               |             |        |      |        |
| 32L1XXX     |               |             |        |      |        |
| FLEX HOSE   |               |             |        |      |        |
| ASSEMBLIES, |               |             |        |      |        |
| BOTH        |               |             |        |      |        |
| FLEXIBLE    |               |             |        |      |        |
| METALLIC    |               |             |        |      |        |
|             |               |             |        |      |        |
| ASSEMBLIES. |               |             |        |      |        |
| NO SIMILAR  |               |             |        |      |        |
| FAILURES,   |               |             |        |      |        |
| I.E.        |               |             |        |      |        |
| STRUCTURAL  |               |             |        |      |        |
| FAILURE OF  |               |             |        |      |        |
| THE         |               |             |        |      |        |
|             |               |             |        |      |        |
| LINE        |               |             |        |      |        |
| ASSEMBLIES, |               |             |        |      |        |
| WERE FOUND  |               |             |        |      |        |
|             |               |             |        |      |        |
| NOTE: ON    |               |             |        |      |        |
| ET-4 A      |               |             |        |      |        |
| FINAL LEAK  |               |             |        |      |        |
| CHECK ON    |               |             |        |      |        |
| THE HE      |               |             |        |      |        |
| INJECTION   |               |             |        |      |        |
| SYSTEM      |               |             |        |      |        |
|             |               |             |        |      |        |
| FAILED AS A |               |             |        |      |        |
| RESULT OF A |               |             |        |      |        |
| LEAKING     |               |             |        |      |        |
| 32L         |               |             |        |      |        |
| 206026AA000 |               |             |        |      |        |
| HOSE        |               |             |        |      |        |
| ASSEMBLY    |               |             |        |      |        |
|             |               |             |        |      |        |
| THE CAUSE   |               |             |        |      |        |
| WAS FOUND   |               |             |        |      |        |
| TO BE A     |               |             |        |      |        |
| HIGH CYCLE  |               |             |        |      |        |
| FATIGUE     |               |             |        |      |        |
| CRACK WHICH |               |             |        |      |        |
|             |               |             |        |      |        |
| ORIGINATED  |               |             |        |      |        |
| FROM A      |               |             |        |      |        |
| SHARP ROOT  |               |             |        |      |        |
| RADIUS OF   |               |             |        |      |        |
| THE FLEX    |               |             |        |      |        |
| HOSE        |               |             |        |      |        |
| CONVOLUTE   |               |             |        |      |        |
|             |               |             |        |      |        |
| AND A       |               |             |        |      |        |
| SERIES OF   |               |             |        |      |        |
| CIRC        |               |             |        |      |        |
| UMFERENTIAL |               |             |        |      |        |
| GROOVES ON  |               |             |        |      |        |
| THE OUTSIDE |               |             |        |      |        |
| SURFACE     |               |             |        |      |        |
|             |               |             |        |      |        |
| PROPAGATION |               |             |        |      |        |
| STRESSES    |               |             |        |      |        |
| WERE CAUSED |               |             |        |      |        |
| BY HIGH     |               |             |        |      |        |
| FREQUENCY   |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
|             |               |             |        |      |        |
| THAT        |               |             |        |      |        |
| OCCURRED    |               |             |        |      |        |
| DURING THE  |               |             |        |      |        |
| LEAK CHECK. |               |             |        |      |        |
| NO          |               |             |        |      |        |
| STRUCTURAL  |               |             |        |      |        |
| FAILURE OF  |               |             |        |      |        |
|             |               |             |        |      |        |
| THE         |               |             |        |      |        |
| ASSEMBLY    |               |             |        |      |        |
| OCCURRED.   |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| MATERIALS   |               |             |        |      |        |
| ENGINEERING |               |             |        |      |        |
| F/A         |               |             |        |      |        |
|             |               |             |        |      |        |
| REPORT NO.  |               |             |        |      |        |
| ETFA-50     |               |             |        |      |        |
|             |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| CCMAIL FROM |               |             |        |      |        |
| J. RUSSELL, |               |             |        |      |        |
| DATED       |               |             |        |      |        |
| 8/20/96     |               |             |        |      |        |
|             |               |             |        |      |        |
| CAUSE:      |               |             |        |      |        |
|             |               |             |        |      |        |
| FATIGUE     |               |             |        |      |        |
| FAILURE DUE |               |             |        |      |        |
| TO OVER     |               |             |        |      |        |
| TEST        |               |             |        |      |        |
|             |               |             |        |      |        |
| \* TASK II. |               |             |        |      |        |
| CORRECTIVE  |               |             |        |      |        |
| ACTION      |               |             |        |      |        |
|             |               |             |        |      |        |
| \- TEST     |               |             |        |      |        |
| E           |               |             |        |      |        |
| NVIRONMENTS |               |             |        |      |        |
| WERE        |               |             |        |      |        |
| EVALUATED   |               |             |        |      |        |
| AND         |               |             |        |      |        |
| ADJUSTED    |               |             |        |      |        |
| AND THE     |               |             |        |      |        |
| HOSE        |               |             |        |      |        |
|             |               |             |        |      |        |
| ASSEMBLY    |               |             |        |      |        |
| S           |               |             |        |      |        |
| UCCESSFULLY |               |             |        |      |        |
| RETESTED    |               |             |        |      |        |
|             |               |             |        |      |        |
| \- NO       |               |             |        |      |        |
| FURTHER     |               |             |        |      |        |
| ACTION      |               |             |        |      |        |
| REQUIRED.   |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| TEST        |               |             |        |      |        |
| E           |               |             |        |      |        |
| NVIRONMENTS |               |             |        |      |        |
| ARE         |               |             |        |      |        |
|             |               |             |        |      |        |
| UNIQUE AND  |               |             |        |      |        |
| DETERMINED  |               |             |        |      |        |
| ON A CASE   |               |             |        |      |        |
| BY CASES    |               |             |        |      |        |
| BASIS       |               |             |        |      |        |
|             |               |             |        |      |        |
| TASK III.   |               |             |        |      |        |
| CLEARANCE   |               |             |        |      |        |
| OF          |               |             |        |      |        |
| EF          |               |             |        |      |        |
| FECTIVITIES |               |             |        |      |        |
|             |               |             |        |      |        |
| ET-80 AND   |               |             |        |      |        |
| UP:         |               |             |        |      |        |
| REQU        |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| OF THE      |               |             |        |      |        |
| 32L2        |               |             |        |      |        |
| 060133BA000 |               |             |        |      |        |
| HOSE WAS    |               |             |        |      |        |
|             |               |             |        |      |        |
| SUCCESSFUL  |               |             |        |      |        |
| FOR BOTH    |               |             |        |      |        |
| LWT AND     |               |             |        |      |        |
| SLWT        |               |             |        |      |        |
| E           |               |             |        |      |        |
| NVIRONMENTS |               |             |        |      |        |
|             |               |             |        |      |        |
| REFERENCE   |               |             |        |      |        |
| MSFC MEMO   |               |             |        |      |        |
| EE31(53-96) |               |             |        |      |        |
|             |               |             |        |      |        |
| NOTE: THIS  |               |             |        |      |        |
| IS ALSO     |               |             |        |      |        |
| DEFERRAL    |               |             |        |      |        |
| RATIONALE   |               |             |        |      |        |
|             |               |             |        |      |        |
| \* TASK IV. |               |             |        |      |        |
| CAPS        |               |             |        |      |        |
| CLOSURE     |               |             |        |      |        |
| SUMMARY     |               |             |        |      |        |
|             |               |             |        |      |        |
| DURING THE  |               |             |        |      |        |
| FLEX HOSE   |               |             |        |      |        |
| DELTA       |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| TEST FOR    |               |             |        |      |        |
| SLWT        |               |             |        |      |        |
|             |               |             |        |      |        |
| BEING       |               |             |        |      |        |
| CONDUCTED   |               |             |        |      |        |
| ON THE HE   |               |             |        |      |        |
| INJ FLEX    |               |             |        |      |        |
| HOSE        |               |             |        |      |        |
| ASSEMBLY,   |               |             |        |      |        |
| THE HOSE    |               |             |        |      |        |
| BROKE       |               |             |        |      |        |
|             |               |             |        |      |        |
| INTO TWO    |               |             |        |      |        |
| PIECES. THE |               |             |        |      |        |
| TEST        |               |             |        |      |        |
| REQUIRES    |               |             |        |      |        |
| FLIGHT      |               |             |        |      |        |
| QU          |               |             |        |      |        |
| ALIFICATION |               |             |        |      |        |
| RANDOM      |               |             |        |      |        |
|             |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| AND FLIGHT  |               |             |        |      |        |
| DYNAMIC     |               |             |        |      |        |
| SINE        |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| TESTS TO BE |               |             |        |      |        |
| PERFORMED   |               |             |        |      |        |
|             |               |             |        |      |        |
| IN THE      |               |             |        |      |        |
| Y-AXIS,     |               |             |        |      |        |
| X-AXIS AND  |               |             |        |      |        |
| Z-AXIS. THE |               |             |        |      |        |
| FAILURE     |               |             |        |      |        |
| OCCURRED    |               |             |        |      |        |
| WHILE       |               |             |        |      |        |
|             |               |             |        |      |        |
| THE TEST    |               |             |        |      |        |
| WAS BEING   |               |             |        |      |        |
| CONDUCTED   |               |             |        |      |        |
| IN THE      |               |             |        |      |        |
| Y-AXIS, THE |               |             |        |      |        |
| LAST AXIS   |               |             |        |      |        |
| TO BE       |               |             |        |      |        |
|             |               |             |        |      |        |
| TESTED,     |               |             |        |      |        |
| DURING      |               |             |        |      |        |
| RANDOM      |               |             |        |      |        |
| VIBRATION   |               |             |        |      |        |
| TESTING.    |               |             |        |      |        |
| THE FAILURE |               |             |        |      |        |
| CAUSE WAS   |               |             |        |      |        |
|             |               |             |        |      |        |
| DETERMINED  |               |             |        |      |        |
| TO BE       |               |             |        |      |        |
| FATIGUE     |               |             |        |      |        |
| FAILURE DUE |               |             |        |      |        |
| TO OVER     |               |             |        |      |        |
| TESTING THE |               |             |        |      |        |
| ASSEMBLY    |               |             |        |      |        |
|             |               |             |        |      |        |
| AFTER       |               |             |        |      |        |
| EVALUATION  |               |             |        |      |        |
| BY          |               |             |        |      |        |
| E           |               |             |        |      |        |
| NGINEERING, |               |             |        |      |        |
| IT WAS      |               |             |        |      |        |
| DETERMINED  |               |             |        |      |        |
| THAT A LOW  |               |             |        |      |        |
|             |               |             |        |      |        |
| FREQUENCY   |               |             |        |      |        |
| EXCEEDANCE  |               |             |        |      |        |
| EXISTED FOR |               |             |        |      |        |
| BOTH THE    |               |             |        |      |        |
| SLWT TEST   |               |             |        |      |        |
| E           |               |             |        |      |        |
| NVIRONMENTS |               |             |        |      |        |
|             |               |             |        |      |        |
| AND THE     |               |             |        |      |        |
| PREVIOUS    |               |             |        |      |        |
| LWT TEST    |               |             |        |      |        |
| EN          |               |             |        |      |        |
| VIRONMENTS. |               |             |        |      |        |
| CORRECTIVE  |               |             |        |      |        |
| ACTION      |               |             |        |      |        |
|             |               |             |        |      |        |
| CONSISTED   |               |             |        |      |        |
| OF          |               |             |        |      |        |
| ADJUSTING   |               |             |        |      |        |
| THE         |               |             |        |      |        |
| ENVIRONMENT |               |             |        |      |        |
| FOR BOTH    |               |             |        |      |        |
| LWT AND     |               |             |        |      |        |
| SLWT AND    |               |             |        |      |        |
|             |               |             |        |      |        |
| RETESTING.  |               |             |        |      |        |
| BOTH TEST   |               |             |        |      |        |
| WERE        |               |             |        |      |        |
| SUCCESSFUL. |               |             |        |      |        |
| NO FURTHER  |               |             |        |      |        |
| ACTION WAS  |               |             |        |      |        |
|             |               |             |        |      |        |
| NECESSARY   |               |             |        |      |        |
|             |               |             |        |      |        |
| THIS CAPS   |               |             |        |      |        |
| IS CLOSED.  |               |             |        |      |        |
| NO FURTHER  |               |             |        |      |        |
| ACTION      |               |             |        |      |        |
| REQUIRED    |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+
| **MSFC      |               |             |        |      |        |
| Response/Co |               |             |        |      |        |
| ncurrence** |               |             |        |      |        |
+-------------+---------------+-------------+--------+------+--------+

  -----------------------------------------------------------------------
  MSFC Problem Reporting and Corrective Action (PRACA) System

  ASSESSMENT ADDENDUM REPORT
  -----------------------------------------------------------------------

  ------------------ ----------------- ---------------- ----------- ----------- ------------
  **MSFC Report#**\  **IFA#**\         **Contractor     **JSC#**\   **KSC#**\   **EICN#**\
  A16905             \--               RPT#**\          \--         \--         \--
                                       P-081                                    

  **Asmnt Part#**\   **Asmnt Part      **Asmnt                                  
  32L20602133BA000   Name**\           Serial/Lot#**\                           
                     FLEX HOSE ASSY    0000026                                  

  **HCRIT CD**\      **FCRIT CD**\     **CAUSE CD**\    **FAIL                  
  \--                1                 ET - EI-TEST     MODE**\                 
                                                        MS - STRUCT             

  **Asmnt FMEA**\    **Asmnt FM**\     **FMEA CSE**\    **FMEA                  
  2.4.9.1            1                 \--              SCSE**\                 
                                                        \--                     

  **Asmnt FMEA**\    **Asmnt FM**\     **FMEA CSE**\    **FMEA                  
  \--                \--               \--              SCSE**\                 
                                                        \--                     

  **Asmnt FMEA**\    **Asmnt FM**\     **FMEA CSE**\    **FMEA                  
  \--                \--               \--              SCSE**\                 
                                                        \--                     

  **Correlated       **Correlated      **Correlated                             
  Part#**\           Part#**\          Part#**\                                 
  \--                \--               \--                                      

  **Associated       **Associated      **Associated                             
  LRU#**\            LRU#**\           LRU#**\                                  
  \--                \--               \--                                      

  **MAJOR DESIGN                                                                
  CHANGES**                                                                     

  **APRV DATE**\     **DESCRIPTION OF                                           
  \--                CHANGES**\                                                 
                     \--                                                        

  **ASSESSMENT                                                                  
  TEXT**                                                                        
  ------------------ ----------------- ---------------- ----------- ----------- ------------