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

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

+--------------+---------------+-----------+---------+------+--------+
| **MSFC       | **In-Flight   | **C       | **      | *    |        |
| Record \#**\ | Anomaly       | ontractor | JSC#**\ | *KSC |        |
| A08081       | Number**\     | Report    | \--     | #**\ |        |
|              | \--           | Number**\ |         | \--  |        |
|              |               | E-001     |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Problem    |               |           |         |      |        |
| Title**\     |               |           |         |      |        |
| LH2 ULLAGE   |               |           |         |      |        |
| PRESSURE     |               |           |         |      |        |
| TRANSDUCER   |               |           |         |      |        |
| FAILED ATP   |               |           |         |      |        |
| TEMP TEST    |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **EICN#**\   | **ELEMENT**\  | **Cont    | **F     | **   |        |
| \--          | ET            | ractor**\ | SCM#**\ | FCRI |        |
|              |               | MMMSS     | \--     | T**\ |        |
|              |               |           |         | 1    |        |
+--------------+---------------+-----------+---------+------+--------+
| **HCRIT**\   | **Sys_Lvl**\  | **Misc    |         |      |        |
| \--          | N             | Codes**\  |         |      |        |
|              |               | A B C D E |         |      |        |
|              |               | F G H I J |         |      |        |
|              |               | K L M N O |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| *            | **NO          | *         | **SER/  | *    |        |
| *HARDWARE**\ | MENCLATURE**\ | *PART#**\ | LOT#**\ | *MAN |        |
| EIM          | N/A           | N/A       | N/A     | UFAC |        |
|              |               |           |         | TURE |        |
|              |               |           |         | R**\ |        |
|              |               |           |         | N/A  |        |
+--------------+---------------+-----------+---------+------+--------+
| *            | **NO          | *         | **SER/  | *    |        |
| *HARDWARE**\ | MENCLATURE**\ | *PART#**\ | LOT#**\ | *MAN |        |
| LRU          | N/A           | N/A       | N/A     | UFAC |        |
|              |               |           |         | TURE |        |
|              |               |           |         | R**\ |        |
|              |               |           |         | N/A  |        |
+--------------+---------------+-----------+---------+------+--------+
| *            | **NO          | *         | **SER/  | *    |        |
| *HARDWARE**\ | MENCLATURE**\ | *PART#**\ | LOT#**\ | *MAN |        |
| NCA          | LH2 ULL PRES  | PD74      | 0000036 | UFAC |        |
|              | TRNSDCR       | 00098-019 |         | TURE |        |
|              |               |           |         | R**\ |        |
|              |               |           |         | GU   |        |
|              |               |           |         | LTON |        |
+--------------+---------------+-----------+---------+------+--------+
| **Test/      | **Prevailing  | **F /     | **Fail  | **   |        |
| Operation**\ | Condtion**\   | U**\      | Mode**\ | Caus |        |
| A - ATP      | \--           | F         | \--     | e**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **System**\  | **Defect**\   | **Ma      | **Work  | **   |        |
| ELECTRICAL   | \--           | terial**\ | Con     | Fail |        |
|              |               | \--       | tact**\ | Dat  |        |
|              |               |           | R.      | e**\ |        |
|              |               |           | JACKSON | 04   |        |
|              |               |           |         | /11/ |        |
|              |               |           |         | 1977 |        |
+--------------+---------------+-----------+---------+------+--------+
| **Received   | **Date        | **FMEA    | **IFA:  | *    |        |
| at MSFC**\   | Isolated**\   | Ref       | Mission | *Mis |        |
| 07/01/1979   | \--           | erence**\ | P       | sion |        |
|              |               | 3.1.1.9   | hase**\ | Ela  |        |
|              |               |           | \--     | psed |        |
|              |               |           |         | Tim  |        |
|              |               |           |         | e**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| *            |               | **S       |         | **   |        |
| *Location**\ |               | ymptom**\ |         | Time |        |
| GULTON       |               | EV -      |         | Cycl |        |
|              |               | NO        |         | e**\ |        |
|              |               | T-TO-SPEC |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| *            |               |           |         |      |        |
| *Effectivity |               |           |         |      |        |
| Text**\      |               |           |         |      |        |
| NONE         |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Vehicle    |               |           |         |      |        |
| Effectivity  |               |           |         |      |        |
| Codes**      |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Vehicle    | **Vehicle     | **Vehicle | **      | *    |        |
| 1**\         | 2**\          | 3**\      | Vehicle | *Veh |        |
| \--          | \--           | \--       | 4**\    | icle |        |
|              |               |           | \--     | 5**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **Mission    |               |           |         |      |        |
| Effectivity  |               |           |         |      |        |
| Codes**      |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Mssn 1**\  | **Mssn 2**\   | **Mssn    | **Mssn  | **   |        |
| \--          | \--           | 3**\      | 4**\    | Mssn |        |
|              |               | \--       | \--     | 5**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **Estimated  |               |           |         |      |        |
| Completion   |               |           |         |      |        |
| Dates**      |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **MSFC       | **Contractor  | **LVL 3   | *       |      |        |
| Approved     | Req Defer     | Close**\  | *Remark |      |        |
| Defer Until  | Until Date**\ | \--       | /       |      |        |
| Date**\      | \--           |           | Ac      |      |        |
| \--          |               |           | tion**\ |      |        |
|              |               |           | \--     |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **I          |               |           |         |      |        |
| nvestigation |               |           |         |      |        |
| / Resolution |               |           |         |      |        |
| Summary**    |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Last MSFC  | **CN RSLV     | **Defer   | **Add   | *    |        |
| Update**\    | SBMT**\       | Date**\   | Date**\ | *R/C |        |
| 10/07/1987   | 07/01/1979    | \--       | \--     | Code |        |
|              |               |           |         | s**\ |        |
|              |               |           |         | 1 -  |        |
|              |               |           |         | DES  |        |
|              |               |           |         | \--  |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **Assignee** |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Design**\  | **Chief       | **S &     | **Pro   | *    |        |
| G. PLATT     | Engineer**\   | MA**\     | ject**\ | *Pro |        |
|              | \--           | D. NEWMAN | R.      | ject |        |
|              |               |           | ABRAHAM | MG   |        |
|              |               |           |         | R**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **Approval** |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Design**\  | **Chief       | **S &     | **Pro   | *    |        |
| N/A          | Engineer**\   | MA**\     | ject**\ | *Pro |        |
|              | \--           | N/A       | N/A     | ject |        |
|              |               |           |         | MG   |        |
|              |               |           |         | R**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **PAC        | **PAC Review  | **MSFC    | **St    | *    |        |
| Assignee**\  | Complete**\   | Closure   | atus**\ | *F/A |        |
| M. GLASS     | MG            | Date**\   | C -     | C    |        |
|              |               | 0         | CLOSED  | ompl |        |
|              |               | 7/01/1979 |         | etio |        |
|              |               |           |         | n**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **Problem    | **SEV**\      | **Program | **      | **O  |        |
| Type**\      | \--           | Name**\   | REVL**\ | PRIN |        |
| \--          |               | \--       | \--     | C**\ |        |
|              |               |           |         | \--  |        |
+--------------+---------------+-----------+---------+------+--------+
| **FUNC       | **Software    | *         |         | **SU | **So   |
| MOD**\       | E             | *Software |         | BTYP | ftware |
| \--          | ffectivity**\ | Fail      |         | E**\ | C      |
|              | \-- \-- \--   | CD**\     |         | \--  | losure |
|              | \-- \--       | \--       |         |      | CD**\  |
|              |               |           |         |      | \--    |
+--------------+---------------+-----------+---------+------+--------+
| **RES PERSON | **Approval    |           |         |      |        |
| L2**\        | Signature     |           |         |      |        |
| \--          | L3**\         |           |         |      |        |
|              | \--           |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Related    | **Related     |           |         |      |        |
| Document     | Document      |           |         |      |        |
| Type**\      | ID**\         |           |         |      |        |
| \--          | \--           |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Related    |               |           |         |      |        |
| Document     |               |           |         |      |        |
| Title**\     |               |           |         |      |        |
| \--          |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Related    | **Related     |           |         |      |        |
| Document     | Document      |           |         |      |        |
| Type**\      | ID**\         |           |         |      |        |
| \--          | \--           |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Related    |               |           |         |      |        |
| Document     |               |           |         |      |        |
| Title**\     |               |           |         |      |        |
| \--          |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Related    | **Related     |           |         |      |        |
| Document     | Document      |           |         |      |        |
| Type**\      | ID**\         |           |         |      |        |
| \--          | \--           |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Related    |               |           |         |      |        |
| Document     |               |           |         |      |        |
| Title**\     |               |           |         |      |        |
| \--          |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Contractor |               |           |         |      |        |
| Status       |               |           |         |      |        |
| Summary**    |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Reliabi    |               |           |         |      |        |
| lity/Quality |               |           |         |      |        |
| Assurance    |               |           |         |      |        |
| Concerns,    |               |           |         |      |        |
| Recomm       |               |           |         |      |        |
| endations:** |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Problem    |               |           |         |      |        |
| D            |               |           |         |      |        |
| escription** |               |           |         |      |        |
|              |               |           |         |      |        |
| THE          |               |           |         |      |        |
| TRANSDUCERS  |               |           |         |      |        |
| FAILED       |               |           |         |      |        |
| DURING THE   |               |           |         |      |        |
| TEMP CYCLING |               |           |         |      |        |
| ACCEPTANCE   |               |           |         |      |        |
| PORTION OF   |               |           |         |      |        |
|              |               |           |         |      |        |
| THE GULTON   |               |           |         |      |        |
| AT           |               |           |         |      |        |
| P-3031-13801 |               |           |         |      |        |
| \"C\" WHILE  |               |           |         |      |        |
| UNDERGOING   |               |           |         |      |        |
| ACCEPTANCE   |               |           |         |      |        |
| TESTING AT   |               |           |         |      |        |
|              |               |           |         |      |        |
| GULTON       |               |           |         |      |        |
| SERVONICS.   |               |           |         |      |        |
| S/N 0000036  |               |           |         |      |        |
| HAD AN       |               |           |         |      |        |
| OUTPUT       |               |           |         |      |        |
| READING OF   |               |           |         |      |        |
| -3.3% AT     |               |           |         |      |        |
| 16.0         |               |           |         |      |        |
|              |               |           |         |      |        |
| PSIA DURING  |               |           |         |      |        |
| DITHER       |               |           |         |      |        |
| CALIBRATION; |               |           |         |      |        |
| SHOULD BE    |               |           |         |      |        |
| +/- 3.0%,    |               |           |         |      |        |
| PARA.        |               |           |         |      |        |
| 6.1.4.1. S/N |               |           |         |      |        |
|              |               |           |         |      |        |
| 0000038 HAD  |               |           |         |      |        |
| AN OUTPUT    |               |           |         |      |        |
| READING OF   |               |           |         |      |        |
| -0.85% AT    |               |           |         |      |        |
| 3.5 PSIA     |               |           |         |      |        |
| DURING       |               |           |         |      |        |
| DITHER       |               |           |         |      |        |
|              |               |           |         |      |        |
| CALIBRATION; |               |           |         |      |        |
| SHOULD BE    |               |           |         |      |        |
| +/-.075%,    |               |           |         |      |        |
| PARA.        |               |           |         |      |        |
| 6.1.4.1. S/N |               |           |         |      |        |
| 0000041 READ |               |           |         |      |        |
| 4,705        |               |           |         |      |        |
|              |               |           |         |      |        |
| OHMS; SHOULD |               |           |         |      |        |
| BE 5000 +/-  |               |           |         |      |        |
| 250 OHMS,    |               |           |         |      |        |
| PARA.        |               |           |         |      |        |
| 6.3.4.2      |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **Contractor |               |           |         |      |        |
| In           |               |           |         |      |        |
| vestigation/ |               |           |         |      |        |
| Resolution** |               |           |         |      |        |
|              |               |           |         |      |        |
| CAUSE - 1.   |               |           |         |      |        |
| S/N 0000041  |               |           |         |      |        |
| WAS CAUSED   |               |           |         |      |        |
| BY A LOW     |               |           |         |      |        |
| RESISTANCE   |               |           |         |      |        |
| OF THE ELE   |               |           |         |      |        |
|              |               |           |         |      |        |
| DURING       |               |           |         |      |        |
| INITIAL      |               |           |         |      |        |
| BUILD. 2.    |               |           |         |      |        |
| S/N 0000036  |               |           |         |      |        |
| & S/N        |               |           |         |      |        |
| 0000038 WAS  |               |           |         |      |        |
| CAUSED BY    |               |           |         |      |        |
| NOT          |               |           |         |      |        |
|              |               |           |         |      |        |
| CHECKING THE |               |           |         |      |        |
| NITIAL SETUP |               |           |         |      |        |
| PRIOR TO     |               |           |         |      |        |
| FINAL ASSY.  |               |           |         |      |        |
| CLOSURE      |               |           |         |      |        |
| ACTION - 1.  |               |           |         |      |        |
| S/N          |               |           |         |      |        |
|              |               |           |         |      |        |
| 0000041      |               |           |         |      |        |
| (RESISTANCE  |               |           |         |      |        |
| CHANGE). THE |               |           |         |      |        |
| RESISTANCE   |               |           |         |      |        |
| WIRE         |               |           |         |      |        |
| UTILIZED IN  |               |           |         |      |        |
| THE          |               |           |         |      |        |
|              |               |           |         |      |        |
| RESISTANCE   |               |           |         |      |        |
| ELE. IS      |               |           |         |      |        |
| SIGMOND COHN |               |           |         |      |        |
| ALLOY 479    |               |           |         |      |        |
| WHICH HAS A  |               |           |         |      |        |
| TEMP         |               |           |         |      |        |
| COEFFICIENT  |               |           |         |      |        |
|              |               |           |         |      |        |
| OF           |               |           |         |      |        |
| RESISTANCE   |               |           |         |      |        |
| OF 0.000133  |               |           |         |      |        |
| O            |               |           |         |      |        |
| HMS/OHMS/DEG |               |           |         |      |        |
| F, AT -170   |               |           |         |      |        |
| DEGS: R =    |               |           |         |      |        |
| 4,927        |               |           |         |      |        |
|              |               |           |         |      |        |
| (0.00013)    |               |           |         |      |        |
| (170 + 70) = |               |           |         |      |        |
| 157 OHMS.    |               |           |         |      |        |
| THE WEAR-IN  |               |           |         |      |        |
| OF THE UNIT  |               |           |         |      |        |
| CAUSES THE   |               |           |         |      |        |
|              |               |           |         |      |        |
| WIPER TO BE  |               |           |         |      |        |
| IN CONTACT   |               |           |         |      |        |
| WITH MORE    |               |           |         |      |        |
| WIRE TURNS   |               |           |         |      |        |
| WHICH        |               |           |         |      |        |
| ACCOUNTS FOR |               |           |         |      |        |
|              |               |           |         |      |        |
| ADDITIONAL   |               |           |         |      |        |
| 30 OHMS      |               |           |         |      |        |
| DELTA.       |               |           |         |      |        |
| ADDITIONAL   |               |           |         |      |        |
| INVESTI-     |               |           |         |      |        |
| GATION       |               |           |         |      |        |
| REQ\'D TO    |               |           |         |      |        |
| DETERMINE    |               |           |         |      |        |
|              |               |           |         |      |        |
| LOSS OF 55   |               |           |         |      |        |
| OHMS. THE    |               |           |         |      |        |
| ADDITIONAL   |               |           |         |      |        |
| 55 OHMS      |               |           |         |      |        |
| CANNOT BE    |               |           |         |      |        |
| EXPLAINED    |               |           |         |      |        |
| DIRECTLY     |               |           |         |      |        |
|              |               |           |         |      |        |
| BUT THE      |               |           |         |      |        |
| FOLLOWING    |               |           |         |      |        |
| FACTORS      |               |           |         |      |        |
| SHOULD BE    |               |           |         |      |        |
| CO           |               |           |         |      |        |
| NSIDERED. 1. |               |           |         |      |        |
| A LINEAR     |               |           |         |      |        |
| FUNCTION     |               |           |         |      |        |
|              |               |           |         |      |        |
| CANNOT BE    |               |           |         |      |        |
| ASSUMED FOR  |               |           |         |      |        |
| THE SIGMOND  |               |           |         |      |        |
| COHN ALLOY   |               |           |         |      |        |
| 479 TEMP     |               |           |         |      |        |
| COEFFICIENT. |               |           |         |      |        |
| 2            |               |           |         |      |        |
|              |               |           |         |      |        |
| TELECON WITH |               |           |         |      |        |
| SIGMOND COHN |               |           |         |      |        |
| DISCLOSED    |               |           |         |      |        |
| THAT ACTUAL  |               |           |         |      |        |
| DATA ON      |               |           |         |      |        |
| ALLOY 479 IS |               |           |         |      |        |
|              |               |           |         |      |        |
| NOT          |               |           |         |      |        |
| AVAILABLE AT |               |           |         |      |        |
| TEMPS BELOW  |               |           |         |      |        |
| -100 DEGS F  |               |           |         |      |        |
| & IS NOT     |               |           |         |      |        |
| PREDICTABLE  |               |           |         |      |        |
| & COULD      |               |           |         |      |        |
|              |               |           |         |      |        |
| POSSIBLY     |               |           |         |      |        |
| ENTER THE    |               |           |         |      |        |
| AREA OF      |               |           |         |      |        |
| SUPER        |               |           |         |      |        |
| C            |               |           |         |      |        |
| ONDUCTIVITY. |               |           |         |      |        |
| 3. THE       |               |           |         |      |        |
| RESISTANCE   |               |           |         |      |        |
| CHANGE       |               |           |         |      |        |
|              |               |           |         |      |        |
| FOR          |               |           |         |      |        |
| IDENTICAL    |               |           |         |      |        |
| UNITS S/N    |               |           |         |      |        |
| 0000034, S/N |               |           |         |      |        |
| 0000037, S/N |               |           |         |      |        |
| 0000043 &    |               |           |         |      |        |
| S/N 0000045  |               |           |         |      |        |
|              |               |           |         |      |        |
| SHOWED A     |               |           |         |      |        |
| RESISTANCE   |               |           |         |      |        |
| CHANGE OF    |               |           |         |      |        |
| 180 TO 240   |               |           |         |      |        |
| OHMS. 4. THE |               |           |         |      |        |
| PREDICTED    |               |           |         |      |        |
|              |               |           |         |      |        |
| OPERATING    |               |           |         |      |        |
| ENVIRONMENT  |               |           |         |      |        |
| FOR THE      |               |           |         |      |        |
| PD7400098 IS |               |           |         |      |        |
| -155 DEGS F  |               |           |         |      |        |
| & THE UNITS  |               |           |         |      |        |
| ARE          |               |           |         |      |        |
|              |               |           |         |      |        |
| TESTED TO    |               |           |         |      |        |
| -170 DEGS F. |               |           |         |      |        |
| GULTON       |               |           |         |      |        |
| SERVONICS    |               |           |         |      |        |
| STD          |               |           |         |      |        |
| PRODUCTION   |               |           |         |      |        |
| I            |               |           |         |      |        |
| NSTRUCTIONS, |               |           |         |      |        |
|              |               |           |         |      |        |
| RELATING TO  |               |           |         |      |        |
| RESISTANCE   |               |           |         |      |        |
| ELE. BUILD,  |               |           |         |      |        |
| HAVE BEEN    |               |           |         |      |        |
| CHANGED FROM |               |           |         |      |        |
| +/- 250 OHMS |               |           |         |      |        |
|              |               |           |         |      |        |
| TO +200, OR  |               |           |         |      |        |
| -0 OHMS. 2.  |               |           |         |      |        |
| S/N 0000036  |               |           |         |      |        |
| & S/N        |               |           |         |      |        |
| 0000038. THE |               |           |         |      |        |
| CALIBRATION  |               |           |         |      |        |
|              |               |           |         |      |        |
| CURVES       |               |           |         |      |        |
| INDICATE THE |               |           |         |      |        |
| THE DRIVE    |               |           |         |      |        |
| BAND WAS     |               |           |         |      |        |
| SIDE LOADED  |               |           |         |      |        |
| CAUSING      |               |           |         |      |        |
| FRICTION AT  |               |           |         |      |        |
|              |               |           |         |      |        |
| THE 16 & 52  |               |           |         |      |        |
| PSIA POINTS. |               |           |         |      |        |
| DESIGN OF    |               |           |         |      |        |
| THE UNIT     |               |           |         |      |        |
| WOULD        |               |           |         |      |        |
| INDICATE     |               |           |         |      |        |
| THAT THE     |               |           |         |      |        |
|              |               |           |         |      |        |
| CAPSULE      |               |           |         |      |        |
| WOULD HAVE   |               |           |         |      |        |
| THE LEAST    |               |           |         |      |        |
| AMOUNT OF    |               |           |         |      |        |
| TORQUE WHEN  |               |           |         |      |        |
| APPROACHING  |               |           |         |      |        |
| OR GOING     |               |           |         |      |        |
|              |               |           |         |      |        |
| INTO THESE 2 |               |           |         |      |        |
| POINTS. ANY  |               |           |         |      |        |
| FRIC- TION   |               |           |         |      |        |
| OF SIDE      |               |           |         |      |        |
| LOADING ON   |               |           |         |      |        |
| THE DRIVE    |               |           |         |      |        |
| BAND         |               |           |         |      |        |
|              |               |           |         |      |        |
| WOULD CAUSE  |               |           |         |      |        |
| A REDUCED    |               |           |         |      |        |
| OUTPUT AS    |               |           |         |      |        |
| INDICATED ON |               |           |         |      |        |
| THE CALIBRA- |               |           |         |      |        |
| TION CURVES  |               |           |         |      |        |
|              |               |           |         |      |        |
| THE 33 PSIA  |               |           |         |      |        |
| SETPOINT WAS |               |           |         |      |        |
| SET          |               |           |         |      |        |
| CORRECTLY    |               |           |         |      |        |
| BUT THE      |               |           |         |      |        |
| FRICTION     |               |           |         |      |        |
| CAUSED THE   |               |           |         |      |        |
| OUT          |               |           |         |      |        |
|              |               |           |         |      |        |
| OF TOL.      |               |           |         |      |        |
| CONDITION.   |               |           |         |      |        |
| GULTON       |               |           |         |      |        |
| SERVONICS    |               |           |         |      |        |
| HAS          |               |           |         |      |        |
| INCORP\'D A  |               |           |         |      |        |
| ROOM TEMP    |               |           |         |      |        |
| DITHERED     |               |           |         |      |        |
|              |               |           |         |      |        |
| CALIBRATION  |               |           |         |      |        |
| TO CHECK     |               |           |         |      |        |
| BAND SIDE    |               |           |         |      |        |
| LOADING      |               |           |         |      |        |
| FRICTION &   |               |           |         |      |        |
| THE CURVE IS |               |           |         |      |        |
| LIMITED      |               |           |         |      |        |
|              |               |           |         |      |        |
| TO +/- 1% OF |               |           |         |      |        |
| FULL SCALE.  |               |           |         |      |        |
| ON THE       |               |           |         |      |        |
| INCREASING   |               |           |         |      |        |
| PRESS. RUN   |               |           |         |      |        |
| THE 33 PSIA  |               |           |         |      |        |
| POINT        |               |           |         |      |        |
|              |               |           |         |      |        |
| INTERCEPT    |               |           |         |      |        |
| WILL BE HELD |               |           |         |      |        |
| TO A -0.3%   |               |           |         |      |        |
| MAX. BELOW   |               |           |         |      |        |
| 0%. THE      |               |           |         |      |        |
| INCORP\'D    |               |           |         |      |        |
| CHANGES      |               |           |         |      |        |
|              |               |           |         |      |        |
| WILL ENSURE  |               |           |         |      |        |
| THAT         |               |           |         |      |        |
| FRICTION     |               |           |         |      |        |
| SETUP &      |               |           |         |      |        |
| SLOPE PROBS  |               |           |         |      |        |
| WILL BE      |               |           |         |      |        |
| CORRECTED    |               |           |         |      |        |
| PRIOR        |               |           |         |      |        |
|              |               |           |         |      |        |
| TO FINAL     |               |           |         |      |        |
| ASSY &       |               |           |         |      |        |
| THEREFORE    |               |           |         |      |        |
| ELIMINATE    |               |           |         |      |        |
| THE OUT OF   |               |           |         |      |        |
| TOL.         |               |           |         |      |        |
| EXPERIENCED  |               |           |         |      |        |
| DURING       |               |           |         |      |        |
|              |               |           |         |      |        |
| ATP          |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+
| **MSFC       |               |           |         |      |        |
| Response/C   |               |           |         |      |        |
| oncurrence** |               |           |         |      |        |
+--------------+---------------+-----------+---------+------+--------+

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

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

  ---------------- ----------------- ---------------- ------------- ----------- ------------
  **MSFC           **IFA#**\         **Contractor     **JSC#**\     **KSC#**\   **EICN#**\
  Report#**\       \--               RPT#**\          \--           \--         \--
  A08081                             E-001                                      

  **Asmnt Part#**\ **Asmnt Part      **Asmnt                                    
  \--              Name**\           Serial/Lot#**\                             
                   \--               \--                                        

  **HCRIT CD**\    **FCRIT CD**\     **CAUSE CD**\    **FAIL                    
  \--              \--               \--              MODE**\                   
                                                      EV -                      
                                                      NOT-TO-SPEC               

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