ACPRS_Environmental_Test_Report_10120-6487A.pdf

N

Arizona Operations 1155 West 23rd Street

Tempe, Arizona 85282 Tel: (480) 966-5517

Fax: (480) 966-5525 E-Mail: todd.hosier@ntscorp.com

TEST REPORT 10120-6487A

ENVIRONMENTAL TESTING OF

ACPRS

Tests Initiated: 29 July 2010

Tests Completed: 30 September 2010

20 December 2010

This report and the information contained herein represent the results of testing only those test articles identified and selected by U.S. Army PM FSS, performed to specifications and/or procedures selected by U.S. Army PM FSS. National Technical Systems (NTS) makes no representations expressed or implied that such testing is adequate (or inadequate) to demonstrate efficiency performance, reliability, or any other characteristic of the articles being tested, or similar products. This report should not be relied upon as an endorsement or certification by NTS of the equipment tested, nor does it represent any statement whatsoever as to its merchantability or fitness of the test article or similar products for a particular purpose. This report shall not be reproduced except in full, without the written approval of National Technical Systems Arizona Operations.

This report contains 142 pages including the appendices.

PREPARED FOR

US Army PM FSS R-208 1 Kansas Street Natick, Massachusetts 01760

PERFORMED BY

National Technical Systems Arizona Testing Division 1155 West 23rd Street Tempe, AZ 85282

National Technical Systems

N Test Report No. 10120-6487A Rev. –

Arizona Operations

TABLE OF CONTENTS

Section Title Page

1.0 ADMINISTRATIVE DATA 6

2.0 FACTUAL DATA 8

2.0 LOW PRESSURE (ALTITUDE) 8

3.0 HIGH TEMPERATURE 9

4.0 LOW TEMPERATURE 11

5.0 RAIN 12

6.0 HUMIDITY 13

7.0 SALT FOG 14

8.0 DUST 15

9.0 SAND 17

10.0 VIBRATION (UH-60) 18

11.0 VIBRATION (CH-47) 20

12.0 VIBRATION (LOOSE CARGO) 22

13.0 ESD 23

Tables

1 HIGH TEMPERATURE CYCLE PARAMETERS 9

2 SINE ON RANDOM VIBRATION PARAMETERS (UH-60) 18

3 SINE ON RANDOM VIBRATION PARAMETERS (CH-47) 20

Appendices

1 TEST EQUIPMENT USED 25

2 TEST CONFIGURATION PHOTOGRAPHS 34

3 LOW PRESSURE (ALTITUDE) TEST LOGS AND PLOTS 90

4 HIGH TEMPERATURE TEST LOGS AND PLOTS 93

5 LOW TEMPERATURE TEST LOGS AND PLOTS 97

TABLE OF CONTENTS (continued)

6 RAIN TEST LOGS AND PLOTS 100

7 HUMIDITY TEST LOGS AND PLOTS 103

8 SALT FOG TEST LOGS AND PLOTS 108

9 DUST TEST LOGS AND PLOTS 111

10 SAND TEST LOGS AND PLOTS 118

11 VIBRATION (UH-60) TEST LOGS AND PLOTS 123

12 VIBRATION (CH-47) TEST LOGS AND PLOTS 131

13 VIBRATION (LOOSE CARGO) TEST LOGS AND PLOTS 139

14 ESD TEST LOGS AND PLOTS 141

REVISION SUMMARY

Revision Date Affected Page (s) Affected Paragraph (s)

Initial Release 20 December 2010 N/A N/A

Note: Paragraphs affected by revisions are indicated by a superscript of the revision number appearing just after the paragraph title in the body of the report. Due to the revisions, some items may change pages.

ADMINISTRATIVE DATA

1.1 PURPOSE OF TESTS: To perform environmental testing of an ACPRS, in accordance with the procedures and specifications cited herein.

1.2 CUSTOMER: U.S. Army PM FSS

1.3 DESCRIPTION OF TEST ITEMS: ACPRS

1.4 PART NUMBER: WA25000

1.5 SERIAL NUMBER(S): 0007, 0008, 0009, 0010, 0011, 0012

1.6 QUANTITY OF ITEMS TESTED: Six (6) each (One (1) or more each per test as specified in individual test descriptions)

1.7 REFERENCES: MIL-STD-810G

IEC 61000-4-2 Edition 2.0 2008-12

1.8 SECURITY CLASSIFICATION: Unclassified

1.9 DATE TEST COMPLETED: 30 September 2010

1.10 TESTS CONDUCTED BY: National Technical Systems Arizona Operations.

1155 W. 23rd Street Tempe, AZ 85282

1.11 DISPOSITION OF TEST ITEMS: Returned To:

US Army PM FSS R-208 1 Kansas Street Natick, Massachusetts 01760

Arizona Operations

ADMINISTRATIVE DATA (continued)

1.12 TEST ABSTRACT:

TEST RESULTS

Low Pressure (Altitude) No physical anomalies were noted.

High Temperature No physical anomalies were noted.

Low Temperature No physical anomalies were noted.

Rain No physical anomalies were noted.

Humidity No physical anomalies were noted.

Salt Fog Some salt deposits and corrosion were noted post-test; customer stated units passed post-test functional test No other physical anomalies were noted.

Dust No physical anomalies were noted.

Sand No physical anomalies were noted.

Vibration (UH-60) No physical anomalies were noted.

Vibration (CH-47) No physical anomalies were noted.

Vibration (Loose Cargo) Some superficial scratches were noted on the outside of the units.

No other physical anomalies were noted.

ESD No physical anomalies were noted.

1.13 STANDARD TEST CONDITIONS: Room Ambient, unless otherwise noted

1.14 SOURCE INSPECTION: NTS - QAR, US Army - QAR

1.15 PURCHASE ORDER NUMBER: W91A2K81079040

1.16 GOVERNMENT CONTRACT NO.: W911QY-08-P-0472

FACTUAL DATA

2.0 Low Pressure (Altitude)

2.1 References

MIL-STD-810G Method 500.5 Procedure I U.S. Army PM FSS ACPRS P/N WA25000 S/N 0011

2.2 Test Assembly

The ACPRS was placed in the chamber. The chamber controls were programmed to provide the pressure equivalent of an altitude of 35,000 feet, as specified by the U.S. Army representative. The chamber door was closed and sealed.

2.3 Test Procedure

The ACPRS was placed in the chamber. The chamber controls were programmed to provide the pressure equivalent of an altitude of 35,000 feet, as specified by the U.S. Army representative. The chamber door was closed and sealed. The ACPRS was non-operational for this storage/transport test.

The chamber controls were enabled and the chamber began a ramp to the pressure equivalent of an altitude of 35,000 feet (3.47 psia) at a 1968 ft/minute rate (less than 10 meters/second). Upon reaching the required pressure conditions, the ACPRS began a one (1) hour dwell, as specified by the U.S. Army representative. Upon completion of the one (1) hour dwell, the chamber internal pressure was ramped to site ambient pressure. Upon reaching site ambient pressure, the chamber was opened, and the ACPRS was removed from the chamber and visually examined for any anomalies. No anomalies were recorded. The ACPRS was subjected to a functional check by the customer representative.

2.4 Post-Test

The ACPRS was visually inspected for any physical anomalies. No anomalies were noted. Operational checks of the ACPRS were performed as required by the customer representative.

2.5 Test Results

There were no physical anomalies noted. The customer representative reported that the ACPRS passed the post-test functional test.

2.6 Description of Test Apparatus

A log of test equipment used during ACPRS testing is located in Appendix 1.

2.7 Photographs

Photographs of the ACPRS test assembly are located in Appendix 2.

2.8 Test Data

Test logs, data and charts are located in Appendix 3.

Arizona Operations

3.0 High Temperature

3.1 References

MIL-STD-810G Method 501.5 Procedure I U.S. Army PM FSS ACPRS P/N WA25000 S/N 0008

3.2 Test Assembly

The control system for the temperature chamber was programmed to provide the environmental conditions specified in MIL- STD-810G Method 501.5 for High Temperature Cycles, Climatic Condition –Hot Dry (Induced Hot), Table 501.5-III Induced, summarized in Table 1 below.

Time of Day Temperature (ºC) 0100 33 0200 32 0300 0400 31 0500 30 0600 31 0700 34 0800 38 0900 42 1000 45 1100 51 1200 57 1300 61 1400 63 1500 1600 62 1700 60 1800 57 1900 50 2000 44 2100 38 2200 35 2300 34 2400 33

Table 1. High Temperature Cycle Parameters

The ACPRS was placed into the temperature chamber. The control system for the chamber was programmed to provide the environmental conditions summarized in Table 1.

3.3 Test Procedure

The ACPRS was placed into the thermal chamber. The chamber door was closed and sealed. The chamber controls were enabled to provide seven (7) cycles of the twenty-four (24) hour profile shown in Table 1. The chamber temperature was checked periodically during the seven (7) day period to ensure that the temperature profile was followed.

Upon completion of the seven (7) day high temperature cycling exposure, the chamber temperature was ramped to lab ambient temperature. Upon reaching lab ambient temperature, the chamber door was opened. The ACPRS was visually examined for any anomalies. No anomalies were noted.

High Temperature (continued)

3.4 Post-Test

The ACPRS was visually inspected after testing. No anomalies were noted. Operational checks of the ACPRS were performed as required by the customer representative.

3.5 Test Results

There were no physical anomalies noted. The customer representative reported that the ACPRS passed the post-test

3.6 Description of Test Apparatus

3.7 Photographs

3.8 Test Data

Test logs, data and charts are located in Appendix 4.

Arizona Operations

4.0 Low Temperature

4.1 References

MIL-STD-810G Method 502.5 Procedure I U.S. Army PM FSS ACPRS P/N WA25000 S/N 0010 and 0011

4.2 Test Assembly

The two (2) ACPRS units were placed into the temperature chamber. The chamber control system was programmed to provide the required conditions for the storage exposure per MIL-STD-810G. The U.S. Army representative specified a storage temperature of −60°F (−51.1°C), a storage duration of twenty (20) hours, and a ramp rate to not exceed 3°C per minute.

4.3 Test Procedure

The ACPRS units were placed into the temperature chamber. The chamber door was closed and sealed. The chamber controls were enabled and the chamber began to ramp to the storage temperature of −51.1°C. Upon stabilizing at the cold storage temperature, the ACPRS units began a twenty (20) hour dwell. Upon completion of the twenty (20) hour dwell, the chamber temperature was ramped to lab ambient temperature. Upon reaching lab ambient temperature, the chamber door was opened. The ACPRS units were visually examined for any anomalies. No anomalies were noted.

4.4 Post-Test

The ACPRS units were visually inspected after testing. No anomalies were noted. Operational checks of both ACPRS units were performed as required by the customer representative.

4.5 Test Results

There were no physical anomalies noted. The customer representative reported that both ACPRS units passed the post-test

4.6 Description of Test Apparatus

4.7 Photographs

4.8 Test Data

Test logs, data and charts are located in Appendix 5.

Arizona Operations

5.0 Rain

5.1 References

MIL-STD-810G Method 506.5, Procedure III U.S. Army PM FSS ACPRS P/N WA25000 S/N 0010

5.2 Test Assembly

Water flow from the drip tank was checked and measured to ensure compliance with the procedure, at a minimum of 280 liters per square meter per hour. The ACPRS was placed under the drip tank, oriented as directed by the customer representative.

The distance from the ACPRS to the drip pan was greater than 1 meter.

Prior to the exposure, the ACPRS was pre-heated in a thermal chamber to ensure the required temperature differential (10°C) was obtained between the water and the unit under test.

5.3 Test Procedure

Water flow from the drip tank was checked and measured to ensure compliance with the procedure. The water flow was stopped. The water temperature was checked, and the ACPRS was pre-heated in a thermal chamber. After pre-heating, the ACPRS was placed under the drip tank. At this point, the unit temperature was +40°C and the water temperature was +29°C.

The water flow was enabled. Water was allowed to drip on the ACPRS at a rate of at least 280 L/m2/Hr for fifteen (15) minutes.

Upon completion of the fifteen (15) minute exposure, the water flow was shut off and the drip tank allowed to drain.

The ACPRS was removed from beneath the drip tank. The unit was prepared for inspection by wiping excess water from the external surfaces of the unit. The external surfaces of the ACPRS were visually examined for any anomalies. No physical anomalies were noted. The ACPRS was subjected to a functional check by the customer representative.

5.4 Post-Test

The ACPRS was subjected to visual inspection. There were no physical anomalies noted. The customer representative performed a post-test functional test and inspected the unit for water incursion.

5.5 Test Results

No physical damage was noted during or following the exposure. The customer representative reported that the ACPRS passed the post-test functional test. The customer representative also stated that there was no water ingress to the ACPRS unit.

5.6 Description of Test Apparatus

5.7 Photographs

5.8 Test Data

Test logs and plots are located in Appendix 6.

Arizona Operations

6.0 Humidity

6.1 References

MIL-STD-810G Method 507.5, Procedure II U.S. Army PM FSS ACPRS P/N WA25000 S/N 0007

6.2 Test Assembly

The ACPRS was subjected to Humidity testing per the Aggravated Temperature-Humidity Cycle shown in Figure 507.5-7 of MIL-STD-810G. That procedure includes a conditioning period of twenty-four (24) hours at +23ºC and 50% Relative Humidity (RH), then ten (10) days with cycling between +30ºC and +60ºC while maintaining 95% RH. The ACPRS was placed on a wire rack in the temperature/humidity chamber. The chamber controls were programmed to provide the temperature and humidity profile per the procedure.

6.3 Test Procedure

The ACPRS was placed on a wire rack in the temperature/humidity chamber configured to allow humidity exposure on all sides of the unit. The chamber controls were programmed to provide the temperature and humidity profile per the procedure.

The chamber door was closed and sealed, and the controls were enabled to produce the required temperature and humidity conditions. The temperature and humidity were monitored and recorded during the test exposure. The unit began the twenty-four (24) hour soak at +23ºC and 50% RH. Upon completion of the twenty-four (24) hour soak at +23ºC and 50% RH, the chamber began a ramp to +30ºC and 95% RH. Upon reaching those conditions, the chamber began a two (2) hour ramp from +30ºC to +60ºC while maintaining 95% RH. The beginning of this ramp period marked the beginning of the first (1st) cycle.

Upon completion of the two (2) hour ramp to +60ºC, the chamber began a six (6) hour soak at +60ºC while maintaining 95% RH. Upon completion of the soak at +60ºC, the chamber began an eight (8) hour ramp down to +30ºC while maintaining 95% RH. Upon completion of the eight (8) hour ramp to +30ºC, the chamber began an eight (8) hour soak at +30ºC while maintaining 95% RH. Upon completion of the soak at +30ºC, the first (1st) cycle was complete. The chamber began a ramp up to +60ºC, beginning the second (2nd) cycle. The temperature and humidity conditions of the first (1st) cycle were repeated nine (9) times, thus completing ten (10) twenty-four (24) hour cycles. Upon completion of the tenth (10th) cycle, the chamber door was opened and the ACPRS was removed from the chamber by the customer. The ACPRS was visually examined for anomalies, and no anomalies were noted.

6.4 Post-Test

The ACPRS was visually inspected after testing. No anomalies were noted. Operational checks of the ACPRS were performed as required by the customer representative.

6.5 Test Results

There were no physical anomalies noted. The customer representative reported that the ACPRS passed the post-test functional tests. No water accumulation was noted.

6.6 Description of Test Apparatus

A log of test equipment used during testing is located in Appendix 1.

6.7 Photographs

Photographs of the test assembly are located in Appendix 2.

6.8 Test Data

Test logs, data and charts are located in Appendix 7.

Arizona Operations

7.0 Salt Fog

7.1 References

MIL-STD-810G Method 509.5 U.S. Army PM FSS ACPRS P/N WA25000 S/N 0011 and 0012

7.2 Test Assembly

The salt fog chamber was started and allowed to stabilize at +35°C. The two (2) ACPRS units were configured for the exposure and placed in the chamber, oriented as required by the procedure. The chamber was closed and sealed and the ACPRS units were subjected to salt fog exposure per the procedure.

7.3 Test Procedure

The salt fog chamber was started and allowed to stabilize at +35°C. The two (2) ACPRS units were configured for the exposure and placed in the chamber, oriented as required by the procedure. The chamber was closed and sealed and the ACPRS units were allowed to stabilize at +35°C. The salt fog was introduced to the chamber, and the ACPRS units began a twenty-four (24) hour exposure in the salt fog atmosphere. At the completion of the twenty-four (24) hour exposure, the ACPRS units were removed from the chamber. Chamber conditions at the completion of the first twenty-four (24) hour exposure period were noted as follows: temperature = +22.8°C, humidity = 39% RH, system pH = 6.89, and 24 hour fallout = 25 mL plus 35 mL in the two (2) collectors (1.25 mL/hour average). The ACPRS units were allowed to dwell for a twenty-four

(24) hour drying period. The drying conditions were measured as +23.1°C and 40% RH.

Upon completion of the twenty-four (24) hour drying period, the ACPRS units were moved back into the salt fog chamber, oriented as defined by the procedure. The salt fog was introduced to the chamber. The ACPRS units began a twenty-four (24) hour exposure in the salt fog atmosphere at +35ºC. At the completion of the twenty-four (24) hour exposure, the ACPRS units were removed from the chamber. Chamber conditions at the completion of the second twenty-four (24) hour exposure period were noted as follows: system pH = 6.97 and 24 hour fallout = 25 mL plus 35 mL in the two (2) collectors (1.25 mL/hour average). The ACPRS units were allowed to dwell for a second twenty-four (24) hour drying period. The drying conditions were measured as +23.1°C and 40% RH. Upon completion of the twenty-four (24) hour drying period, the ACPRS units were visually inspected for any salt intrusion. No anomalies were noted.

7.4 Post-Test

The two (2) ACPRS units were subjected to visual inspection. No anomalies were noted. Operational checks of the ACPRS units were performed as required by the customer representative.

7.5 Test Results

There were no physical anomalies noted. The customer representative reported that the ACPRS units passed the post-test functional tests. Some salt deposits and corrosion were noted on the units following the salt fog exposure and photographs were taken. Those photographs are included in this report.

7.6 Description of Test Apparatus

7.7 Photographs

7.8 Test Data

Test logs, data and charts are located in Appendix 8.

Arizona Operations

8.0 Dust

8.1 References

MIL-STD-810G Method 510.5 Procedure I U.S. Army PM FSS ACPRS P/N WA25000 S/N 0009

8.2 Test Assembly

The ACPRS was placed in the dust chamber. The dust chamber was closed and sealed. The chamber was charged with 140 mesh silica flour. The chamber air speed was adjusted per the procedure

8.3 Test Procedure

The ACPRS was placed in the dust chamber, oriented with one (1) side of the unit, noted as Side 1, facing the blowing dust flow, as directed by the customer representative. The ACPRS unit was grounded to the dust chamber. The chamber was charged with 140 mesh silica flour and the chamber door was closed and sealed. The air velocity was adjusted to 1750 feet per minute (fpm) ±10%, as required by the procedure. The actual wind velocity was measured as 1718 fpm at that time. Dust concentration was adjusted to be between 0.1 and 0.5 grams per cubic foot (gm/ft3) (10 ±7 g/m3). The chamber temperature was adjusted to maintain an ambient temperature condition of approximately +23°C, with a relative humidity of less than thirty

(30) percent.

Upon stabilizing at ambient temperature, the dust feeder was enabled and the ACPRS began a one (1) hour soak in the blowing dust.

Upon completion of the one (1) hour soak, the dust feeder was disabled and the air velocity was reduced to 300 fpm. The ACPRS was repositioned to expose Side 2 to the blowing dust. The chamber door was closed and sealed. Upon stabilizing at +23°C, the dust feeder was enabled and the ACPRS began a one (1) hour soak in the blowing dust. Upon completion of the Side 2 exposure, the unit was exposed to blowing dust in the same manner with Side 3, Side 4, Side 5, and Side 6 exposed for one (1) hour each.

Upon completion of the Side 6 exposure at ambient temperature, the dust feeder was disabled and the air velocity was reduced to zero. This completed the one (1) hour exposure of each of the six (6) sides of the ACPRS for a total exposure of six (6) hours at ambient temperature.

The ACPRS remained positioned in the chamber overnight at ambient temperature.

Upon restart the next morning, the chamber temperature was raised to the high operating temperature of +63°C. The air velocity was initially adjusted to 305 fpm, as required by the procedure. The ACPRS was allowed to stabilize at +63°C. Upon stabilizing at +63°C, the air velocity was increased to 1720 fpm. The dust feeder was enabled and the ACPRS, oriented to expose Side 1, began a one (1) hour soak in the blowing dust. Upon completion of the one (1) hour soak, the dust feeder was disabled and the air velocity was reduced to 300 fpm. The ACPRS was repositioned to expose Side 2 of the unit to the blowing dust. The chamber door was closed and sealed. The technician noted that the chamber fan was not operating at the start of the Side 2 exposure. The test was paused while repairs were made to the chamber fan. Then testing was resumed with the unit still in the Side 2 orientation. Upon stabilizing at +63°C, the dust feeder was enabled and the ACPRS began a one (1) hour soak in the blowing dust. Upon completion of the Side 2 exposure, the unit was exposed to blowing dust in the same manner with Side 3, Side 4, Side 5, and Side 6 exposed for one (1) hour each at +63°C.

Upon completion of the Side 6 exposure, the dust feeder was disabled and the air velocity was reduced to zero. This completed the one (1) hour exposure of each of the six (6) sides of the ACPRS, for a total exposure of six (6) hours at +63ºC.

The chamber was opened and the excess dust allowed to fall off the assembly. The ACPRS was removed from the chamber and the loose dust lightly brushed away with a soft brush.

Dust (continued)

8.4 Post-Test

The ACPRS was visually inspected after each phase of testing. No physical damage was observed. Operational checks of the ACPRS were performed as required by the customer representative.

8.5 Test Results

There were no physical anomalies noted. The customer representative reported that the ACPRS passed the post-test functional tests. No dust penetration was noted.

8.6 Description of Test Apparatus

8.7 Photographs

8.8 Test Data

Test log and charts are located in Appendix 9.

Arizona Operations

9.0 Sand

9.1 References

MIL-STD-810G Method 510.5 Procedure II U.S. Army PM FSS ACPRS P/N WA25000 S/N 0008

9.2 Test Assembly

The ACPRS was placed in the sand chamber. The sand chamber was closed and sealed. The chamber was charged with sand as defined in MIL-STD-810G. The chamber air speed was adjusted per the requirements of the procedure

9.3 Test Procedure

The ACPRS was mounted in the sand chamber, oriented to expose the first surface of the unit, noted as Axis 1. The chamber door was closed and sealed. The chamber wind speed was adjusted to 18.8 meters/second. The sand feed rate was set per the procedure. The chamber temperature was adjusted to the high operating temperature of +63°C and allowed to stabilize.

The relative humidity was measured as 18.3%.

Upon stabilizing at +63°C, the sand feed was enabled and the ACPRS began a ninety (90) minute exposure in the blowing sand. Upon completion of the ninety (90) minute exposure, the sand feeder was disabled and the air flow reduced to zero.

The ACPRS was reoriented in the chamber to expose the second surface, noted as Axis 2. Upon stabilizing at +63°C, the sand feed was enabled and the ACPRS began a ninety (90) minute exposure in the blowing sand.

Upon completion of the Side 2 exposure, the unit was exposed to blowing sand in the same manner with Axis 3, Axis 4, Axis 5, and Axis 6 exposed for ninety (90) minutes each at +63°C.

Upon completion of the ninety (90) minute exposure for Side 6, the sand feeder was disabled and the air velocity was reduced to zero. This completed the ninety (90) minute exposure of each of the six (6) sides of the ACPRS, for a total exposure of nine

(9) hours. The ACPRS was allowed to cool to ambient temperature.

The chamber door was opened. The ACPRS was removed from the chamber and the loose sand brushed away. No physical anomalies were noted during the exposure or upon removal of the AGU system from the test chamber.

9.4 Post-Test

The ACPRS was visually inspected after each phase of testing. No physical damage was observed. Operational checks of the ACPRS were performed as required by the customer representative, and a post-test inspection was performed.

9.5 Test Results

There were no physical anomalies noted. The customer representative reported that the ACPRS passed the post-test functional tests. The customer representative also stated that a post-test inspection of the ACPRS revealed no damage or anomalies from the sand exposure.

9.6 Description of Test Apparatus

9.7 Photographs

9.8 Test Data

Test logs, data and charts are located in Appendix 10.

Arizona Operations

10.0 Vibration (UH-60)

10.1 References

MIL-STD-810G Method 514.6, Annex C, Paragraph 2.6 U.S. Army PM FSS ACPRS P/N WA25000 S/N 0008 and 0010

10.2 Test Assembly

The vibration controller was programmed with the UH-60 vibration parameters specified in MIL-STD-810G Method 514.6, Annex C, Paragraph 2.6, and summarized in Table 2 which follows.

Random Sine

Frequency Bandwidth

(Hz)

P.S.D.

Level (g2/Hz)

Roll Up (dB / oct)

Roll – Off (dB / oct)

Acceleration Level (g rms)

Frequency (Hz)

Acceleration (G)

Axis Noted Duration (minutes)

3.125 – 100 0.001 +3 2.99

4.3 0.11 Lateral, Longitudinal, Vertical

60 100 – 300 0.01 17.2 1.72 300 - 500 -9 34.4 2.5

51.6 1.5

Table 2. Sine on Random Vibration Parameters (UH-60)

The two (2) ACPRS units were installed on a mounting fixture, and the mounting fixture was attached to a vibration exciter oriented for testing each of the three (3) mutually-orthogonal axes as noted in the following paragraphs. One (1) control accelerometer was mounted on the fixture for control of vibration input.

10.1 Test Procedure

The ACPRS units were installed on a mounting fixture, and the mounting fixture was attached to a vibration exciter oriented for testing in the Lateral Axis. The ACPRS units were subjected to the UH-60 sine on random vibration per the parameters shown in Table 2 for sixty (60) minutes. Upon completion of the UH-60 sine on random vibration exposure, the ACPRS units were visually inspected for any anomalies. No anomalies were noted.

Next, the ACPRS units and fixture were attached to a vibration exciter oriented for testing in the Vertical Axis. The ACPRS units were subjected to the UH-60 sine on random vibration per the parameters shown in Table 2 for sixty (60) minutes. Upon completion of the UH-60 sine on random vibration exposure, the ACPRS units were visually inspected for any anomalies. No anomalies were noted.

Next, the ACPRS units and fixture were attached to a vibration exciter oriented for testing in the Longitudinal Axis. The ACPRS units were subjected to the UH-60 sine on random vibration per the parameters shown in Table 2 for sixty (60) minutes. Upon completion of the UH-60 sine on random vibration exposure, the ACPRS units were visually inspected for any anomalies. No anomalies were noted.

10.2 Post-Test

The ACPRS units were visually inspected after the vibration exposure in each axis. No anomalies were noted.

10.3 Test Results

No physical damage or anomalies were found post-vibration testing of the ACPRS units.

10.4 Description of Test Apparatus

Vibration (UH-60) (continued)

10.5 Photographs

10.6 Test Data

The test log and plots are located in Appendix 11.

Arizona Operations

11.0 Vibration (CH-47)

11.1 References

MIL-STD-810G Method 514.6 Annex C, Paragraph 2.6 U.S. Army PM FSS ACPRS P/N WA25000 S/N 0008 and 0010

11.2 Test Assembly

The vibration controller was programmed with the CH-47 vibration parameters specified in MIL-STD-810G Method 514.6, Annex C, Paragraph 2.6, and summarized in Table 3 which follows.

Random Sine

Frequency Bandwidth

(Hz)

P.S.D.

Level (g2/Hz)

Roll Up (dB / oct)

Roll – Off (dB / oct)

Acceleration Level (g rms)

Frequency (Hz)

Acceleration (G)

Axis Duration (minutes)

3.75 – 100 0.001 +3 2.76

3.75 0.1 Lateral, Longitudinal, Vertical

60 100 – 300 0.01 11.25 1.125 300 - 500 -9 22.5 1.125

33.75 2.5

Table 3. Sine on Random Vibration Parameters (CH-47)

The two (2) ACPRS units were installed on a mounting fixture, and the mounting fixture was attached to a vibration exciter oriented for testing each of the three (3) mutually-orthogonal axes as noted in the following paragraphs. One (1) control accelerometer was mounted on the fixture for control of vibration input.

11.3 Test Procedure

The ACPRS units were installed on a mounting fixture, and the mounting fixture was attached to a vibration exciter oriented for testing in the Longitudinal Axis. The ACPRS units were subjected to the CH-47 sine on random vibration per the parameters shown in Table 3 for sixty (60) minutes. Upon completion of the CH-47 sine on random vibration exposure, the ACPRS units were visually inspected for any anomalies. No anomalies were noted.

Next, the ACPRS units and fixture were attached to a vibration exciter oriented for testing in the Vertical Axis. The ACPRS units were subjected to the CH-47 sine on random vibration per the parameters shown in Table 3 for sixty (60) minutes. Upon completion of the CH-47 sine on random vibration exposure, the ACPRS units were visually inspected for any anomalies. No anomalies were noted.

Next, the ACPRS units and fixture were attached to a vibration exciter oriented for testing in the Lateral Axis. The ACPRS units were subjected to the CH-47 sine on random vibration per the parameters shown in Table 3 for sixty (60) minutes. Upon completion of the CH-47 sine on random vibration exposure, the ACPRS units were visually inspected for any anomalies. No anomalies were noted.

11.4 Post-Test

The ACPRS units were visually inspected after the vibration exposure in each axis. No anomalies were noted.

11.5 Test Results

No physical damage or anomalies were found post-vibration testing of the ACPRS units.

11.6 Description of Test Apparatus

Vibration (CH-47) (continued)

11.7 Photographs

11.8 Test Data

The test log and plots are located in Appendix 12.

Arizona Operations

12.0 Vibration (Loose Cargo)

12.1 References

MIL-STD-810G Method 514.5 Procedure II Category 5 U.S. Army PM FSS ACPRS P/N WA25000 S/N 0010 and 0009

12.2 Test Assembly

The two (2) ACPRS units were placed in the loose cargo tester and framed per the procedure.

12.3 Test Procedure

The two (2) ACPRS units were placed in the loose cargo tester, oriented to test the Lateral Axis (labeled Fore/Aft Axis in the test log). The ACPRS units were framed per the procedure. The ACPRS units were subjected to thirty (30) minutes of loose cargo vibration per the procedure. Upon completion of the exposure, the ACPRS units were visually inspected by the customer representative. No anomalies were reported.

Then the ACPRS units were repositioned in the loose cargo tester, to expose the units to vibration along the Longitudinal Axis.

The ACPRS units were framed per the procedure. The ACPRS units were subjected to thirty (30) minutes of loose cargo vibration per the procedure. Upon completion of the Longitudinal Axis exposure, the ACPRS units were subjected to an operational check by the customer representative.

12.4 Post-Test

The ACPRS units were visually inspected after the vibration exposure in each axis. When both axes had been tested, the ACPRS units were subjected to an operational test by the customer representative.

12.5 Test Results

Visual inspection of the ACPRS units following the vibration exposure revealed some scratches on the outside of the units from movement of the loose units in the vibration bed. No other physical damage was noted. The customer representative stated that both ACPRS units passed the post-test operational test.

12.6 Description of Test Apparatus

12.7 Photographs

12.8 Test Data

Test logs, data and charts are located in Appendix 13.

Arizona Operations

13.0 ESD

13.1 References

IEC 61000-4-2 Edition 2.0 2008-12 U.S. Army PM FSS ACPRS P/N WA25000 S/N 0007 U.S. Army PM FSS ACPRS P/N WA25000 S/N 0008 (Battery packaging production intent)

13.2 Test Assembly

Each of the two (2) ACPRS units was configured for ESD testing per the procedure. ACPRS S/N 0007 was subjected to the ESD test per the procedure. ACPRS S/N 0008 was a battery packaging production intent unit subjected to ESD testing per customer direction as described in the following paragraphs.

13.3 Test Procedure

Each of the two (2) ACPRS units was configured for ESD testing per the procedure. Test points on the ACPRS were chosen in discussion with the customer representative. The Level 1 test points, which are accessible components or subassemblies, were tested with 2 kV discharges. The Level 2 test points, which are points on the ACPRS assembly, were tested with 4 kV discharges. Each test point was subjected to ten (10) positive and ten (10) negative discharges.

The Level 2 test points were:

1. Upper Suspension Link

2. Manual Lock

3. Star Wheel

4. Belt Access Cover

5. Activation Button

6. Suspension Mounting (Lower)

The Level 1 test points were:

1. Battery

2. Internal Battery Housing

3. Internal Belt Cable

ACPRS P/N WA25000 S/N 0007 was tested while unpowered. The unit was subjected to ten (10) positive and ten (10) negative discharges at the 4 kV level through direct contact of the ESD Simulator with each of the six (6) designated Level 2 test points on the unit. Upon completion of the discharges, the ACPRS was subjected to an operational test by the customer representative.

Then ACPRS P/N WA25000 S/N 0007 was tested while powered. The unit was subjected to ten (10) positive and ten (10) negative discharges at the 4 kV level through direct contact of the ESD Simulator with each of the six (6) designated Level 2 test points on the unit. Upon completion of the discharges, the ACPRS was subjected to an operational test by the customer representative.

Next, ACPRS P/N WA25000 S/N 0007 was subjected to ten (10) positive and ten (10) negative discharges at the 2 kV level through direct contact of the ESD Simulator with each of the three (3) designated Level 1 test points on the unit. Upon completion of the discharges, the ACPRS was subjected to an operational test by the customer representative.

Next, ACPRS P/N WA25000 S/N 0008 (the battery packaging production intent unit) was subjected to ten (10) positive and ten

(10) negative discharges at the 2 kV level through direct contact of the ESD Simulator with each of the three (3) designated Level 1 test points on the unit. Upon completion of the discharges, the ACPRS was subjected to an operational test by the customer representative.

13.4 Post-Test

Both ACPRS units were subjected to operational tests following each series of ESD discharges.

ESD (continued)

13.5 Test Results

The customer representative reported that ACPRS S/N 0007 passed the post-test functional tests following the Level 2 discharges (with the unit unpowered and powered) and the Level 1 discharges.

The customer representative reported that ACPRS S/N 0008 (the battery packaging production intent unit), which was only subjected to Level 1 discharges, passed the post-test functional tests following those discharges.

No physical damage was noted during or following the exposure of either unit.

13.6 Description of Test Apparatus

13.7 Photographs

13.8 Test Data

Test logs and plots are located in Appendix 14.

APPENDIX 1

TEST EQUIPMENT USED

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

TEST EQUIPMENT USED

NTS ID Description Last Cal Cal Due

LOW TEMPERATURE 29-Jul-10 TE0275 Honeywell 12-May-10 31-Oct-10 (Old ID #) ENV5039T Chart Recorder Model No: Truline 4500 Serial No: 9646I628060200001 TE0363 Thermotron 12-May-10 31-May-11 (Old ID #) ENV6040T Controller, Temperature Chamber Model No: SE-600-6-6 Serial No: 32123 HIGH TEMPERATURE 30-Jul-10 TE0275 Honeywell 12-May-10 31-Oct-10 (Old ID #) ENV5039T Chart Recorder Model No: Truline 4500 Serial No: 9646I628060200001 TE0363 Thermotron 12-May-10 31-May-11 (Old ID #) ENV6040T Controller, Temperature Chamber Model No: SE-600-6-6 Serial No: 32123

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

RAIN (DRIP) 30-Jul-10 TE0275 Honeywell 12-May-10 31-Oct-10 (Old ID #) ENV5039T Chart Recorder Model No: Truline 4500 Serial No: 9646I628060200001

TE0355 MO NCR

(Old ID #) ENV6032T Graduated Cylinder ASTM 'B' Certified Model No:

Serial No:

TE0363 Thermotron 12-May-10 31-May-11 (Old ID #) ENV6040T Controller, Temperature Chamber Model No: SE-600-6-6 Serial No: 32123 TE0480 Ultrak 27-Oct-09 30-Nov-10 (Old ID #) TE0480 Digital Stopwatch Model No: 340 Serial No:

TE0875 Omega 21-Dec-09 31-Jan-11 (Old ID #) TE0875 K-Type TC Display Model No: HH11 Serial No: 121955

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

ALTITUDE 05-Aug-10 TE0179 HP 15-Oct-09 31-Oct-10 (Old ID #) E5078T Data Acquisition System Model No: 34970A Serial No: us37002928 TE0192 Systron Donner MO NCR (Old ID #) E5099T Power Supply Model No: HB20-6 Serial No: 01004-9 TE0407 Omega Eng 24-Mar-10 30-Apr-11 (Old ID #) P5014T (-15 to 45) PSI Pressure Transducer Model No: PX203-30V45G5V Serial No: 298480 TE0535 Nor-Cal MO NCR (Old ID #) TE0535 Vacuum Chamber Model No: 970120-4 Serial No: 125797 TE0545 Watlow 21-Apr-10 31-May-11 (Old ID #) TE0545 Programmable Controller Model No: F4DH Serial No: 1596 TE0589 Hewlett-Packard 13-Oct-09 31-Oct-10 (Old ID #) E6131T 20 Channel Mux Card Model No: 34901A Serial No: US37001647 TE0891 Wallace & Tiernan 06-Apr-10 30-Apr-11 (Old ID #) TE0891 Absolute Pressure Gage 0-800mm Hg Model No: FA129 Serial No: GG 05751 TE0904 Dell MO NCR (Old ID #) TE0904 Desktop computer Model No: DIM2400 Serial No: H56JL31

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

SALT FOG 09-Aug-10 TE0244 Harshaw / Filtrol MO NCR (Old ID #) ENV174L Salt Fog Chamber Model No: N/A Serial No: N/A TE0250 Cole Parmer VAT VAT (Old ID #) ENV5002T PH Wand Model No: 05830-00 Serial No: NSN TE0286 Omega 08-Apr-10 FIO (Old ID #) ENV5052T Temperature Controller Model No: CN9000 Serial No: N/A TE0349 Omega FIO NCR (Old ID #) ENV6026T Programmable Controller Model No: CN76000 Serial No:

TE0475 Honeywell 08-Apr-10 31-Oct-10 (Old ID #) ENV6083T Chart Recorder Model No: DR45AT Serial No: 0107Y149817100001 TE0531 Oakton 01-Jun-09 01-Jun-11 (Old ID #) ENV6049T pH 7.00 Standard Solution Model No: 00654-04 Serial No: Lot # 2906508 TE0876 Westover Scientific VAT VAT (Old ID #) TE0876 Refractometer Salt Model No: RHS-10ATC Serial No: CP017387

TE0986 Graphtec 30-Apr-10 31-May-11 (Old ID #) TE0986 10 Channel Data Acquisition unit Model No: GL200A Serial No: H91215989

TE0914 Ricca Chemical Company 01-Jun-09 01-Jun-11 (Old ID #) TE0914 5% sodium chloride (salt) solution Model No: LOT 1906701 Serial No: Cat no 7215-16

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

BLOWING DUST 10-Aug-10 TE0246 Standard Environmental 04-Aug-10 31-Aug-11 (Old ID #) ENV19L Dust Chamber Model No: Dust Chamber Serial No:

TE0341 Omega 21-Apr-10 31-Oct-10 (Old ID #) ENV6017T Chart Recorder Model No: RD106A Serial No: 436006/580 TE0450 Love Controls 21-Apr-10 31-May-11 (Old ID #) ENV6075T Programmable Controller Model No: 16A Serial No: IP67022-WA8P TE0469 Vaisala 20-Nov-09 30-Nov-10 (Old ID #) TE0469 Temperature / Humidity Probe Model No: HMI41 / HMP 46 Serial No: U3930022 / Z120003 TE0504 TSI 31-Mar-10 30-Sep-10 (Old ID #) TE0504 Digital Air Velocity Meter & Temperature Indicator Model No: 9535 Serial No: T95350741010 (no no.) NCR NCR (Old ID #) no no.) 140 Silica Flour Dust Model No:

Lot No:50052710

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

BLOWING SAND 10-Aug-10 TE0290 Watlow 05-Apr-10 30-Apr-11 (Old ID #) ENV5056T Temperature Controller Model No: 922A Serial No: N/A TE0350 Standard 12-Apr-10 30-Apr-11 (Old ID #) ENV6027T Blowing Sand Chamber Model No: SD19FS Serial No: 1604 TE0469 Vaisala 20-Nov-09 30-Nov-10 (Old ID #) TE0469 Temperature / Humidity Probe Model No: HMI41 / HMP 46 Serial No: U3930022 / Z120003 TE0480 Ultrak 27-Oct-09 30-Nov-10 (Old ID #) TE0480 Digital Stopwatch Model No: 340 Serial No:

TE0504 TSI 31-Mar-10 30-Sep-10 (Old ID #) TE0504 Digital Air Velocity Meter & Temperature Indicator Model No: 9535 Serial No: T95350741010 TE0581 Omega 17-Dec-09 31-Jan-11 (Old ID #) TE0581 Data Acquisition system Model No: Multiscan 1200 Serial No: 287541 TE0581 Omega 17-Dec-09 31-Jan-11 (Old ID #) TE0581 Input Card for Multiscan 1200 Model No: MTC-24 Serial No: 285552

TE0903 HP MO NCR

(Old ID #) TE0903 Desktop computer TEDAQ01 Model No: DX2450 Serial No: MXL8220FYZ

TE0990 HP 28-Apr-10 31-May-11 (Old ID #) TE0990 Data Acquisition Model No: 34970A Serial No: US37002790 TE1016 Dell MO NCR (Old ID #) TE1016 Desktop Personal Computer Model No: Dimension 3000 Serial No: serv tag 545W461

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

HELICOPTER (UH-60 & CH-47) VIBRATION 12-Aug-10 TE0439 Spectral Dynamics 19-Mar-10 30-Sep-10 (Old ID #) D6097T Vibration Control System Model No: 2552 Serial No: 2932-7952 TE0462 PCB 02-Apr-10 31-Oct-10 (Old ID #) D6105T Accelerometer Model No: 353B04 Serial No: 108634 TE0495 Ling MO NCR (Old ID #) TE0495 Vibration Exciter (Shaker) Model No: V860 Serial No: 361

TE0507 Dytran 25-Sep-09 31-Oct-10 (Old ID #) D6101T Signal Conditioner Model No: 4121 Serial No: 368 TE0647 Unholtz-Dickie MO NCR (Old ID #) Shaker System Exciter & Amplifier Model No: R-24 Serial No: 524 LOOSE CARGO VIBRATION 13-Aug-10

D6005T M-RAD MO NCR

(Old ID #) Package Tester Model No: 3636(500)V-32-TH-AC-C Serial No: 211-166 E6092T Mitsubishi MO NCR (Old ID #) E6092T Inverter Model No: FR-A024-3.7K Serial No: N/A TE0985 Acutrak 29-Mar-10 30-Apr-11 (Old ID #) TE0985 Stop Watch Model No: SC-503 Serial No:

Arizona Operations

MO: Maintenance Only NCR: No Calibration Required VAT: Verified at Test NPCR: No Periodic Calibration Required FIO: For Indication Only

HUMIDITY 23-Aug-10 TE0325 Russels MO NCR (Old ID #) ENV6001T Temperature / Humidity Chamber Model No: GD-32-5-5 Serial No: 2987 TE0326 Watlow 05-Apr-10 30-Apr-11 (Old ID #) ENV6002T Programmable Controller Model No: F4 Serial No: 929 TE0327 Honeywell 05-Apr-10 31-Oct-10 (Old ID #) ENV6003T Chart Recorder Model No: DR 4500 Serial No: 6450002 ESD 30-Sep-10 TE0137 Electro-Tech 25-May-10 30-Jun-11 (Old ID #) E5015T Electrostatic Discharge Simulator Model No: 930C Serial No: 140 (no no.) ETS VAT VAT (Old ID #) no no.) 330 ohm/150 pF Discharge Resistor Model No:

Serial No:84-1-0140

APPENDIX 2

TEST CONFIGURATION

PHOTOGRAPHS

6 August 2010 U.S. Army PM FSS 10120-6487

ACPRS, P/N WA25000, S/N 0011

Low Pressure (Altitude) Exposure

6 August 2010 U.S. Army PM FSS 10120-6487

ACPRS, P/N WA25000, S/N 0011

Low Pressure (Altitude) Exposure

30 July 2010 U.S. Army PM FSS 10120-6487

ACPRS, P/N WA25000, S/N 0008

High Temperature Test Setup

High Temperature Test Setup

29 July 2010 U.S. Army PM FSS 10120-6487 ACPRS, P/N WA25000, S/N 0010 and 0011

Low Temperature Test Setup

ACPRS, P/N WA25000, S/N 0010

Rain Drip Test Setup

ACPRS, P/N WA25000, S/N 0010

Rain Drip Test Setup

23 August 2010 U.S. Army PM FSS 10120-6487

ACPRS, P/N WA25000, S/N 0007

Humidity Exposure

3 September 2010 U.S. Army PM FSS 10120-6487

Humidity Exposure – Post-test

9 August 2010 U.S. Army PM FSS 10120-6487 ACPRS, P/N WA25000, S/N 0011 and 0012

Salt Fog Test Setup

9 August 2010 U.S. Army PM FSS 10120-6487

Salt Fog Test Setup

13 August 2010 U.S. Army PM FSS 10120-6487

Salt Fog Post-Test

10 August 2010 U.S. Army PM FSS 10120-6487

ACPRS, P/N WA25000, S/N 0009

Blowing Dust Exposure – Side 1

Blowing Dust Exposure – Side 1 Post-Test to Show Ground on ACPRS

Blowing Dust Exposure – Side 2

Blowing Dust Exposure – Side 3

Blowing Dust Exposure – Side 4

Blowing Dust Exposure – Side 5

Blowing Dust Exposure – Side 6

11 August 2010 U.S. Army PM FSS 10120-6487

Blowing Dust Post-Test

Blowing Sand Exposure – Axis 1

Blowing Sand Exposure – Axis 2

Blowing Sand Exposure – Axis 3

Blowing Sand Exposure – Axis 4

Blowing Sand Exposure – Axis 5

Blowing Sand Exposure – Axis 5

Blowing Sand Exposure – Axis 6

12 August 2010 U.S. Army PM FSS 10120-6487 ACPRS, P/N WA25000, S/N 0008 and 0010 Vibration (UH-60 and CH-47) - Lateral Axis

Vibration (UH-60 and CH-47) - Vertical Axis

Vibration (UH-60 and CH-47) - Longitudinal Axis

ACPRS, P/N WA25000, S/N 0010 and 0009

Vibration (Loose Cargo) – Lateral Axis

ACPRS, P/N WA25000, S/N 0010 and 0009 Vibration (Loose Cargo) – Longitudinal Axis

30 September 2010 U.S. Army PM FSS 10120-6487 ACPRS, P/N WA25000, S/N 0007 and 0008

ESD Test Setup

ESD Test – ESD Simulator

ESD Test – Upper Suspension Link (typical of both units)

ESD Test – Star Wheel (typical of both units)

ESD Test – Manual Lock (typical of both units)

ESD Test – Battery Access Cover (typical of both units)

ESD Test – Activation Button (typical of both units)

ESD Test – Lower Suspension Mounting (typical of both units)

ESD Test – Battery Housing

ESD Test – Battery Housing

ESD Test – Battery (typical of both units)

ESD Test – Internal Battery Connection

ESD Test – Internal Battery Housing

ESD Test – Battery Cable

ESD Test – Internal Battery Connection

ESD Test – Internal Battery Housing

ESD Test – Battery Connection

APPENDIX 3

LOW PRESSURE (ALTITUDE)

TEST LOGS AND PLOTS

Test Report No. 10120-6487A Rev. –

20.0

25.0

30.0

35.0

40.0

45.0

50.0

‐9.00

‐7.00

‐5.00

‐3.00

‐1.00

Te m pe ra tu re

PS

IA

10120‐6487 US Army PM FSS

ACPRS unit S/N 011 Altitude Test 8/06/2010

0.0

5.0

10.0

15.0

20.0

‐15.00

‐13.00

‐11.00

9.00

APPENDIX 4

HIGH TEMPERATURE

10120‐6487 U.S. Army P/N WA‐25000 S/N 0008 High temperature 7/30‐8/6/10

45°C

:2 4:

:4 6:

:0 8:

0:

:0

3:

:0

7:

:0

:3 6:

:5 8:

:2 0:

:4 2:

0:

:0

3:

:0

6:

:0

:1 0:

:3 2:

:5 4:

:1 6:

:3 8:

3:

:0

6:

:0

9:

:0

:0 6:

:2 8:

:5 0:

:1 2:

2:

:1

5:

:1

9:

:1

:4 0:

:0 2:

:2 4:

:4 6:

2:

:1

5:

:1

8:

:1

:1 4:

:3 6:

:5 8:

:2 0:

1:

:1

5:

:1

8:

:1

:4 8:

:1 0:

:3 2:

:5 4:

1:

:1

4:

:1

8:

:1

:2 2:

Time

APPENDIX 5

LOW TEMPERATURE

APPENDIX 6

RAIN

APPENDIX 7

HUMIDITY

APPENDIX 8

SALT FOG

APPENDIX 9

DUST

APPENDIX 10

SAND

70.0

10120‐6487 US Army PM FSS Sand Test Axis 1 ‐ 4 8/10/10

60 0

65.0

0 0

55.0

60.0

45.0

50.0

°C

35.0

40.0

25.0

30.0

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M

A M PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM PM

9:

:5

9:

:2

9:

:5

9:

:2

9:

:5

9:

:2

:0 3:

:1 2:

:2 0:

9:

:3 7:

:4 6:

:5 4:

:0

1:

0:

8:

7:

5:

4:

:0 2:

9:

8:

6:

5:

:2

1:

:5

1:

:2

1:

:5

1:

:2

1:

:5

1:

:2

2:

:5

2:

:2

2:

:5

2:

:2

2:

:5

2:

:2

2:

:5

3:

:2

3:

:5

3:

:2

3:

:5

3:

:2

3:

:5

3:

:2

4:

:5

4:

:2

Time

70.0

10120‐6487 U.S. Army PM FSS Sand Test Axis 5 & 6 8/11/10

65.0

60.0

50.0

55.0

°C

45.0

35.0

40.0

:0 6:

:1 1:

:1 6:

:2 1:

:2 6:

:3 1:

:3 6:

:4 1:

:4 6:

:5 1:

:5 6:

:0 1:

:0 6:

:1 1:

:1 6:

:2 1:

:2 6:

:3 1:

:3 6:

:4 1:

:4 6:

:5 1:

:5 6:

:0 1:

:0 6:

:1 1:

:1 6:

:2 1:

:2 6:

:3 1:

:3 6:

:4 1:

:4 6:

:5 1:

:5 6:

:0 1:

:0 6:

:1 1:

:1 6:

:2 1:

:2 6:

:3 1:

:3 6:

:4 1:

:4 6:

:5 1:

:5 6:

:0 1:

:0 6:

Time

APPENDIX 11

VIBRATION (UH-60)

APPENDIX 12

VIBRATION (CH-47)

APPENDIX 13

VIBRATION (LOOSE CARGO)

APPENDIX 14

ESD