Attachment_10d,_353-B003-MSR-C60.pdf

353-B003-MSR-60

MONTHLY STATUS REPORT

For

INTEGRATED MAINTENANCE, OPERATION & MODIFICATION SUPPORT (IMOMS)

Flight Training Devices

PERIOD COVERED:

01 – 31 March 2017

SECURITY CLASSIFICATION:

Unclassified

CONTRACT NO. HSCG38-12-C-410001

Data Item No. B003

Prepared For:

U.S. COAST GUARD

Aircraft Repair & Supply Center Elizabeth City, NC 27909-5001

Prepared By:

AERO SIMULATION, INC.

USCG ATC Mobile

8501 Tanner Williams Road Mobile, AL 33608

14 April 2017

1. Activities Summary Major contract activities that have occurred during the reporting period:

• Deficiency Reports (DRs) o Five new DRs were generated this reporting period.

o Aero Simulation, Inc. (ASI) has 19 DRs prepared for Joint Final

Inspection (JFI).

o ASI continued efforts on various other DRs.

o Additional information on specific DRs can be found in Appendix A.

• Engineering Change Proposal (ECP) o Four new ECPs were approved this reporting period.

o ASI has 18 ECPs prepared for JFI.

o ASI continued efforts on various other ECPs.

o Additional information on specific ECPs can be found in Appendix

B.

o Highlights and status of major ECPs are summarized below:

016-16, MH-60T Engine High Side Failure with loss of Np and Torque indications. ASI received notice that there has recently been a rash of interesting Engine High Side Failures in the fleet and one of the recommended actions from a mishap report was to simulate the High Side Failure in the simulator a little differently. The United States Coast Guard (USCG) provided data and an ECP was generated and approved. ASI quickly implemented the changes for evaluation by USCG Subject Matter Experts (SMEs). The changes were found to provide the required effects, and are in place on the Operational Flight Trainer (OFT) and Cockpit Procedure Trainer (CPT) as an engineering level change.

Formal Contractor Final Inspection (CFI) and JFI will still be conducted.

012-15, MH-65Dx Automatic Flight Control System (AFCS), Flight Director (FD) & Control Loader System (CLS) Integration and 001-16, MH-65D1 AFCS/FD System Problem Report (SPR) Clearance. The software efforts under these ECPs have been completed and accepted by the USCG. ASI received the final documentation from the Control Loading Original Equipment Manufacturer (OEM).

ASI is awaiting final documentation updates from the AFCS/FD OEM. ASI was informed there is additional documentation, however the AFCS/FD OEM may have data rights issues to resolve prior to delivery.

007-15, MH-60T CPT Telestra Upgrade. Site engineers have implemented the host side changes associated with the “test to speech” Automatic Terminal Information Service (ATIS) functionality on the OFT, in a development environment. ASI is in the process of documenting the hardware changes made by this upgrade. ASI began and completed the integration and CFI phases on this effort on the CPT. Site engineers will conduct JFI on the CPT and OFT with the USCG when CFI is completed on the OFT.

003-15, HC-144B OFT Forward Looking Infrared (FLIR) Universal Hand Control Unit (UHCU). The UHCU is installed in the OFT and is functional. Additional (minor) hardware is required to permanently install the cabling for the UHCU.

ASI has received all required hardware and will attempt to install the items next reporting period. Additionally, ASI is in the process of documenting the hardware changes made by this upgrade.

026-14, Update the MH-60T CPT and OFT Embedded Global Positioning (EGI), Inertial Navigation System (INS) Model. Based upon research and SME input, ASI conducted tuning of malfunction effects related to Receiver Autonomous Integrity Monitoring (RAIM) and Actual Navigation Performance (ANP) calculation and validities. As part of CFI phase, ASI noted issues with performing Stored Heading alignments. ASI engineers are currently working on addressing these issues.

014-14, HC-144A CPT Vibrations. Changes have been incorporated into the CPT Block Configuration Upgrade (BCU) software and hardware. ASI is in the process of documenting the hardware changes made by this upgrade.

ASI will attempt to schedule formal testing of this ECP once the documentation is complete.

013-14, HC-144B OFT BCU and 012-14, HC-144B RFTD

BCU.

• The Integrated Processing Computer (IPC) has been installed and in use since early November 2016 with no operational issues noted.

• Currently, three DRs remain open. The three open DRs are written up against the Enhanced Ground Proximity Warning System (EGPWS), and the same issues are present on the aircraft. These items were written up as DRs for tracking purposes and cannot be addressed until the issues are corrected on the aircraft. As of the end of this reporting period, these same discrepancies are still present on the aircraft.

• A list of open HC-144B OFT BCU DRs is included in Appendix A for tracking purposes.

• Engineering Change Notice (ECN) o No new ECNs were generated this reporting period.

o Additional information on specific ECNs can be found in Appendix

C.

• The MH-65D2 motion system has been dropping offline occasionally, due to a PLC communication timeout ever since it was installed. The motion system OEM suggested a complete motion computer replacement. The replacement computer was received and installed in December. The motion system operated without issue. However, in the last reporting period, the motion system experienced an uncommanded movement issue. This uncommanded movement was a serious safety issue. ASI troubleshot the problem and determined it to be a bad card in the new motion PC. ASI removed the same type of card from the old motion PC and installed it in the new PC. The new motion PC was placed back in the system. The motion system is fully operational and no PLC comm timeouts have been experienced. The bad card has been sent to the OEM for warrantee repair. ASI is working with the OEM to determine the course of action to take with the failed original motion computer.

• ASI is monitoring the MH-65D1 closely due to recent issues with the Input/Output (IO) system. The issue is that communication appears to be lost between the Host computer and IO system. Further research found that the driver installed on the system to communicate with the IO system has been superseded many times. ASI updated the IO system drivers on the host computer. No further issues with the IO system have occurred since the driver was updated.

• ASI continues to monitor the MH-65D1 and MH-65D2 due to what is described by instructors as an “aerodynamic lockup”. This problem requires a host reset to clear. Presently, ASI is unsure if this is related to, or the same as an issue where the airspeed seems to bleed off for no apparent reason. The scope of monitoring these devices has increased to include an AFCS/FD/Aero issue that manifests itself as bumps felt, primarily during IAS climb outs, but it has also been noted during straight and level flight on HDG/ALT mode. ASI will continue to collect data and pass along to the AFCS/FD/MH-65E OFT OEMs for evaluation.

• ASI engineers and technicians continued to support the USCG with efforts of other contractors.

o Support and assistance was provided for continuing modification efforts on the Aircrew Weapons Trainer (AWT) device.

o Support and assistance was provided for continuing modification efforts on the MH-65D1 device. This included utilization of CLIN 4006 Premium Time Support for support of weekend efforts.

• ASI has continued to purge the obsolete records, parts, and equipment from the Flight Training System (FTS) facility. The obsolete parts will be removed from the annual inventory utilization report.

A. Maintenance Status:

• Preventive Maintenance Action Forms (MAFs):

o All required preventive maintenance actions for the reporting period were accomplished.

• Unscheduled MAFs:

o Detailed Maintenance Action Data initiated this reporting period is shown in Appendix D. Additional data can be found by logging into the IMOMS issue tracker. In addition to the detailed status in Appendix D, below is a graphical representation of overall and historical MAF status and new MAFs by device and status (reporting period).

Total MAFs by Status

New MAFs by Device

New MAFs by Status

B. DR Status:

Below is a graphical representation of overall DR status and DRs by device. Detailed DR status is shown in Appendix A.

DRs by Device

DRs by Status

C. ECP Status:

Detailed and historical ECP data is shown in Appendix B.

D. Action Item Requests (AIR) Status:

No new AIRs were generated this reporting period. Detailed status and historical AIR data is shown in Appendix E.

a) AIR 019-15: In work.

b) AIR 006-16: In work.

c) AIR 007-16: In work.

d) AIR 009-16: In work.

e) AIR 014-16: Complete.

f) AIR 021-16: Closed.

g) AIR 022-16: In work.

E. Contract Line Item Number (CLIN) 4006 Activities:

• ASI was authorized to utilize Premium time in support of other contractors’ efforts on the MH-65D1. A total of 12 hours was used this reporting period

F. Contract Line Item Number (CLIN) 4010/4004 Activities:

• None.

G. Data Items:

The following submitted contract Data Items received no response and are considered accepted due to the concept of forbearance under contract law. Additional Data Item information is shown in Appendix I.

a) B003 Monthly Status Report (MSR) #57, submitted 12 January 2017;

response due 14 February 2017.

2. Action Items None.

3. Inventory Summary The Inventory Summary is shown in Appendix F.

4. Problem Areas Affecting Technical or Scheduling Elements, with Background and Any Recommendations for Solutions Beyond the Scope of the Contract

5. Problem Areas Affecting Cost Elements, with Background and Any Recommendations for Solutions Beyond the Scope of the Contract

6. Trainer Performance Summary A. The Trainer Performance Summary (Device Utilization) for the reporting period is shown in Appendix G.

a) Aircrew Weapons Trainer (AWT):

1) The AWT was off the training schedule, due to modifications by other contractors, for a portion of the reporting period.

2) There was no Chargeable Downtime (CDT) or Partial Mission Capability Quantity (PMCQ) during the reporting period.

b) HC-144 OFT:

1) There was 0.5 hours of CDT during the reporting period. The

CDT was due to a broken wire on the parking brake sensor.

The wire was repaired and the device was returned to service.

2) There was no PMCQ during the reporting period.

c) HC-144 CPT:

1) There was no CDT or PMCQ during the reporting period.

d) MH-60T OFT:

1) There was 0.5 hours of CDT during the reporting period. The CDT was due to an issue with the Image Generator (IG).

Multiple nodes required re-imaging/re-booting. Once the IG was back online the device was returned to service.

2) There was a PMCQ of 0.05 for this reporting period. The PMCQ was primarily attributed to loss of copilot communications. Communications were restored by a reset of the Telestra, Host and Instructor Operator Station (IOS).

e) MH-60T CPT:

1) There was no CDT or PMCQ during the reporting period.

f) MH-65D1:

1) There was no CDT during the reporting period.

2) There was a PMCQ of 8.17 for this reporting period. The

PMCQ was primarily attributed to issues related to the IIOC problems described above, loss of motion, FD select panel issues, loss of the #2 display and problems with the instructors’ headset cable. The motion system required a reboot to return to operations. The FD select panel issues were corrected replacing a spring and clip on the IAS-ALT button. The #2 display was restored by an IG restart. The headset cable issue has been transferred to an ECP for design correction.

g) MH-65D2:

1) There was no CDT during the reporting period.

2) There was a PMCQ of 9.54 for this reporting period. The

PMCQ was primarily attributed to numerous occurrences of pitch oscillations in flight (when there should have been any) and loss of airspeed (when it shouldn’t have decreased), problems with the copilots ADI, FD select panel issues, loss of radar display, loss of video on the copilots’ side displays and miscellaneous burnt out lights and loose hardware. See additional information in the Activities Summary section above for oscillation and airspeed issues. The copilots ADI was replaced. The FD select panel switches were cleaned. The radar system required a restart. The copilots’ side display was restored by resetting the projectors. Miscellaneous light bulbs were replaced and loose hardware was reattached.

h) Reconfigurable CPT (RCPT):

1) There was no CDT or PMCQ during the reporting period.

7. Trips and Significant Results

8. Record of All Significant Correspondence and Commitments

A summary of correspondence that took place between ASI and the Government concerning the IMOMS program during this period is contained in Appendix H.

However, if there are any comments that are not as the Government recalls or any comments missing that the Government feels are significant, please contact the ASI Program Manager (section 12.0).

9. Engineering Change Proposal (ECP) Detailed and historical ECP data is shown in Appendix B.

10. Contract Status Contract Data Requirements List (CDRLs) that have been submitted during the past month and those that have been accepted, rejected, forborne, or closed are shown in BOLD text in Appendix I.

11. Planned Activities During the Following Reporting Period The following is a list of major contract activities that are planned for the upcoming reporting period:

A. Continue and complete efforts on various AIRs, ECNs, ECPs, and DRs.

B. Continue to identify and generate ECNs, ECPs and DRs.

C. Continue working with the USCG to schedule JFI/closure of DRs and ECPs.

D. Continue to support the USCG with efforts of other contractors.

E. Perform all applicable Preventive MAFs.

F. Work off unscheduled MAFs as required.

G. The following Data Item is overdue and will be considered accepted at the end of the next reporting period if no response is received due to the concept of forbearance under contract law.

a) B003 Monthly Status Report (MSR) #58, submitted 14 February 2017;

response due 14 March 2017.

b) C002 Inventory/Utilization Data Report #6, submitted 25 January 2017;

response due 28 March 2017.

c) B007 Employee List #11, submitted 27 February 2017; response due 14

March 2017.

12. Name and Telephone Number of Preparer(s) of the Report

Robert Rodriguez 813-628-4447 ext. 162

13. Appendices for any Necessary Tables, References, Photographs, Illustrations, and Charts.

A. DR Summary

B. ECP Summary C. ECN Summary D. Corrective Maintenance Action Summary E. AIR Summary F. Inventory Summary G. Trainer Performance Summary H. Correspondence Summary I. CDRL Status

Appendix A

DR Summary

DR Summary – March 2017

AWT MH65D1 MH65D2

MH60T

CPT

MH60T

OFT CASPER

HC144

OFT

HC144

CPT RCPT Off Eq Totals

New DRs 0 5 0 0 0 0 0 0 0 0 5

CFI 0 0 0 0 0 0 0 0 0 0 0

GFI 0 0 0 0 0 0 0 0 0 0 0

Closed 0 0 0 0 0 0 0 0 0 0 0 CF DRs 0 7 5 3 5 0 0 0 4 0 24

CFI 0 0 0 0 0 0 0 0 0 0 0

GFI 0 7 5 3 3 0 0 0 1 0 19

Closed 0 0 0 0 0 0 0 0 0 0 0 Open 0 12 5 3 5 0 0 0 4 0 29

New DR Status – March 2017

Device Key DR# Summary Description Status Created Updated

MH-65D

OFT

J305-

65DOFT17006 When Copilot is in hot mic, navaids are over ridden

With the Pilot or Copilot on Hot Mic they should still hear navaid tones and Comms.

Open 23-Mar-17 23-Mar-17

MH-65D

OFT

J305-

65DOFT17005 When ATC chatter is ON, IOS station should override it when IP transmits, this is not the case

When ATC Chatter is on and the Instructor keys his mic he should override chatter side tone in his headset while transmitting.

Open 23-Mar-17 23-Mar-17

MH-65D

OFT

J305-

65DOFT17004 When observer selected at IOS both the pilot and copilot can still hear. IP on

ICS

Several problems related to the logic with the ICS and Comms system.

Open 23-Mar-17 23-Mar-17

MH-65D

OFT

J305-

65DOFT17003 IOS cannot hear ATIS tuned into FM with FM selected

With the FM radio tuned to an ATIS frequency the ATIS transmission cannot be heard at the Instructor station.

Open 23-Mar-17 23-Mar-17 https://10.0.1.102:8444/browse/J305-9005 https://10.0.1.102:8444/browse/J305-9005 https://10.0.1.102:8444/browse/J305-9003 https://10.0.1.102:8444/browse/J305-9003 https://10.0.1.102:8444/browse/J305-9001 https://10.0.1.102:8444/browse/J305-9001 https://10.0.1.102:8444/browse/J305-9000 https://10.0.1.102:8444/browse/J305-9000

Device Key DR# Summary Description Status Created Updated

MH-65D

OFT

J305-

65DOFT17002 No Audio for VOR ident at VNY (Van Nuys)

VOR-DME ident could be heard from the point the station was acquired up to 40 miles out.

Inside of 40 miles the ident could no longer be heard.

Open 23-Mar-17 23-Mar-17

CF DR Status – March 2017

Device Key DR# Summary Description Status Created Updated

HH-65C

RCPT

J305-

65RCPT15001 CDU ECMS Page Engine parameters displays (N1, N2, TOT, Q) on CDU ECMS page show a value when respective indicating system is failed. Should display "---".

In Progress 27-Feb-15 31-Aug-15

HH-65C

RCPT

J305-

65RCPT13006 IFF MON light IFF MON light should not illuminate in STANDBY mode.

In Progress 21-Nov-13 6-Dec-16

HH-65C

RCPT

J305-

65RCPT14002 EGI Failures, power off, etc.

MFD Heading fail "flags" are not representative of the aircraft with EGIs off or failed. Single EGI failures appear correct, but dual failures drop flags completely. Written up as MAF J305-4206. MAF closed due opening of DR.

In Progress 24-Jun-14 6-Dec-16

HH-65C

RCPT

J305-

Main Gearbox Overtemp EP (706)

OIL TEMP CAP light illuminates when MGB oil temp reaches 120C (should illuminate at 130C).

MGB CHIP light does not illuminate.

Ready For Customer Recheck

21-Oct-13 25-Oct-16

MH-60T

CPT

J305-

60CPT16002 Lower Cloud Level Airfield elevation gets stuck in the system which prevents proper cloud deck adjustments. Day 2 initial setting begin @ KRIV elevation 1500' we fly to KLGB which is @ sea level. Even after changing airport control to KLGB ( or any airport) the airport elevation on the environmental fog /data/wind page stays @1500'. If the aircraft is repositioned to another airport via the airport page the elevation finally changes.

Ready For Customer Recheck

4-Nov-16 21-Nov-16 https://10.0.1.102:8444/browse/J305-8999 https://10.0.1.102:8444/browse/J305-8999 https://10.0.1.102:8444/browse/J305-5466 https://10.0.1.102:8444/browse/J305-5466 https://10.0.1.102:8444/browse/J305-3220 https://10.0.1.102:8444/browse/J305-3220 https://10.0.1.102:8444/browse/J305-4261 https://10.0.1.102:8444/browse/J305-4261 https://10.0.1.102:8444/browse/J305-3028 https://10.0.1.102:8444/browse/J305-3028 https://10.0.1.102:8444/browse/J305-8361 https://10.0.1.102:8444/browse/J305-8361

Device Key DR# Summary Description Status Created Updated

MH-60T

CPT

J305-

60CPT16001 Approach Plate Disappears

The moving map spontaneously changes off of the approach plate selected to another, resulting in a blank map screen.

Ready For Customer Recheck

4-Nov-16 21-Nov-16

MH-60T

CPT

J305-

60CPT17001 P/CP ESIS Buttons Pilot and Copilot ESIS Buttons inop. They work once after each Host reset, then stop responding.

Ready For Customer Recheck

25-Jan-17 12-Feb-17

MH-60T

OFT

J305-

60OFT16002 FLIR, Display, IOS and Host PC cabinet/system documentation

Relocation of the display PC and FLIR system components into the new cabinet was never fully documented.

In Progress 13-Jul-16 30-Sep-16

MH-60T

OFT

J305-

60OFT17001 WxR Coldstart Provide WxR computer coldstart. In Progress 16-Jan-17 12-Feb-17

MH-60T

OFT

J305-

60OFT16004 Lower Cloud Level Airfield elevation gets stuck in the system which prevents proper cloud deck adjustments. Day 2 initial setting begin @ KRIV elevation 1500' we fly to KLGB which is @ sea level. Even after changing airport control to KLGB ( or any airport) the airport elevation on the environmental fog /data/wind page stays @1500'. If the aircraft is repositioned to another airport via the airport page the elevation finally changes.

Ready For Customer Recheck

4-Nov-16 21-Nov-16

MH-60T

OFT

J305-

60OFT16003 Approach Plate Disappears

The moving map spontaneously changes off of the approach plate selected to another, resulting in a blank map screen.

Ready For Customer Recheck

4-Nov-16 21-Nov-16

MH-60T

OFT

J305-

60OFT16005 DVD Burning at CADS Debrief Station

Can not burn DVD at debrief station. Ready For Customer Recheck

13-Dec-16 5-Jan-17

MH-65D

OFT

J305-

65DOFT16004 AFCS light on WCA panel

AFCS light on wca panel not illuminated during "Before Starting Engine" checklist.

Ready For Customer Recheck

21-Sep-16 30-Sep-16

MH-65D

OFT

J305-

65DOFT16005 #1 DC Bus #1 DC Bus remains powered with both generator switches off and #1 Battery RLY switch off.

Ready For Customer Recheck

21-Oct-16 25-Oct-16 https://10.0.1.102:8444/browse/J305-8359 https://10.0.1.102:8444/browse/J305-8359 https://10.0.1.102:8444/browse/J305-8687 https://10.0.1.102:8444/browse/J305-8687 https://10.0.1.102:8444/browse/J305-7782 https://10.0.1.102:8444/browse/J305-7782 https://10.0.1.102:8444/browse/J305-8633 https://10.0.1.102:8444/browse/J305-8633 https://10.0.1.102:8444/browse/J305-8360 https://10.0.1.102:8444/browse/J305-8360 https://10.0.1.102:8444/browse/J305-8358 https://10.0.1.102:8444/browse/J305-8358 https://10.0.1.102:8444/browse/J305-8512 https://10.0.1.102:8444/browse/J305-8512 https://10.0.1.102:8444/browse/J305-8147 https://10.0.1.102:8444/browse/J305-8147 https://10.0.1.102:8444/browse/J305-8287 https://10.0.1.102:8444/browse/J305-8287

Device Key DR# Summary Description Status Created Updated

MH-65D

OFT

J305-

65DOFT16006 Approach Plate Disappears

Flying within appx 10nm of KONT & KCNO, used drop down menu to select KONT ILS 26R and KCNO VOR 26R. 3 times 1 of the above plates would disappear from screen (only one selected at a time). Could recall approach immediately each time.

Ready For Customer Recheck

4-Nov-16 21-Nov-16

MH-65D

OFT

J305-

65DOFT16007 KCRQ ATIS KCRQ ATIS 120.15 w/winds 220/7 reports 27R but there is no RWY 27(only RWY24).

Ready For Customer Recheck

16-Nov-16 21-Nov-16

MH-65D

OFT

J305-

65DOFT16008 VEMD Indicated Fuel Fuel values on the VEMD Fuel page don't match up with what is inserted by the IP on the IOS.

Ready For Customer Recheck

22-Nov-16 12-Feb-17

MH-65D

OFT

J305-

65DOFT17001 IFF Mode S Check M-S code on CDU and all 0 for mode S of transponder on IFF page.

Ready For Customer Recheck

14-Feb-17 7-Mar-17

MH-65D

OFT

J305-

65DOFT16009 VEMD TOT Indication VEMD TOT indications blank when in FREEZE. Ready For Customer Recheck

28-Nov-16 7-Mar-17

MH-65D2

OFT

J305-

65D2OFT16003 H.L. Sonny Callahan

(KCQF) AWOS

AWOS-3 @ H.L. Sonny Callahan (KCQF) does not xmit on 118.425.

Ready For Customer Recheck

23-Aug-16 23-Sep-16

MH-65D2

OFT

J305-

65D2OFT16004 Heading Slew On deck in freeze unable to use heading slew or current conditions page to change aircraft heading.

Ready For Customer Recheck

13-Sep-16 21-Nov-16

MH-65D2

OFT

J305-

65D2OFT16005 Left Engine Gear Box Shaft Failure

No aural "bang" noise during left engine gear box shaft failure (EP 123L).

Ready For Customer Recheck

16-Dec-16 5-Jan-17

MH-65D2

OFT

J305-

65D2OFT17001 Airborne Targets:

Uncommanded Turns

Airborne targets would initially take heading command but after minute or so would begin uncommanded turns.

Ready For Customer Recheck

18-Jan-17 12-Feb-17

MH-65D2

OFT

J305-

65D2OFT17002 Copilot EHSI Ground Speed Vector

Copilot ground speed vector is double what it should be.

Ready For Customer Recheck

22-Feb-17 7-Mar-17 https://10.0.1.102:8444/browse/J305-8357 https://10.0.1.102:8444/browse/J305-8357 https://10.0.1.102:8444/browse/J305-8404 https://10.0.1.102:8444/browse/J305-8404 https://10.0.1.102:8444/browse/J305-8440 https://10.0.1.102:8444/browse/J305-8440 https://10.0.1.102:8444/browse/J305-8804 https://10.0.1.102:8444/browse/J305-8804 https://10.0.1.102:8444/browse/J305-8443 https://10.0.1.102:8444/browse/J305-8443 https://10.0.1.102:8444/browse/J305-7993 https://10.0.1.102:8444/browse/J305-7993 https://10.0.1.102:8444/browse/J305-8105 https://10.0.1.102:8444/browse/J305-8105 https://10.0.1.102:8444/browse/J305-8533 https://10.0.1.102:8444/browse/J305-8533 https://10.0.1.102:8444/browse/J305-8640 https://10.0.1.102:8444/browse/J305-8640 https://10.0.1.102:8444/browse/J305-8859 https://10.0.1.102:8444/browse/J305-8859

HC-144B OFT BCU (ECP 013-14) DR Status

DR # Key Summary Description Status Created Document Section

Discovery Phase

HC144B-1-

GFI-112

J724-

EGPWS TAC Mode Inop in Aircraft

EGPWS TAC mode is still not operational in the aircraft. Update TTPRR and correct RFTD software when operational and verified in the

OFT.

Open 18-Nov-15 EGPWS TAC Mode 7.6.2 Step

GFI

HC144B-1-

GFI-08

J724-

No Terrain Clearance Floor Alert

This does not currently work on aircraft, awaiting EGPWS software update.

Did not get "Too Low, Terrain" alert.

Open 18-Nov-15 EGPWS 7.6.2 Step

GFI

HC144B-1-

GFI-07

J724-

Unsafe Terrain Clearance, No Flap Warning

This does not currently work on aircraft, awaiting EGPWS software update.

When performing the Mode 4A Unsafe Terrain Clearance Gear and Flap Warnings test, got the "Too Low Gear" alert, but not the "Too Low Flaps" alert.

Open 17-Nov-15 EGPWS 7.6.2 Step

GFI

https://svn.aerosimulation.com/jira/browse/J724-247 https://svn.aerosimulation.com/jira/browse/J724-247 https://svn.aerosimulation.com/jira/browse/J724-243 https://svn.aerosimulation.com/jira/browse/J724-243 https://svn.aerosimulation.com/jira/browse/J724-242 https://svn.aerosimulation.com/jira/browse/J724-242

Appendix B

ECP Summary

ECPs Open or Closed this Reporting Period

ECP# Device Key Summary Description Status Created Updated

ECP

020-16 (E)

MH-60T

OFT

J305-

Computer Aided Debrief System (CADS) Burn to DVD function

Current functionality: Burn to DVD function will fail for events greater than approximately 2.5 hrs in length. Captured data exceeds the storage capacity of a DVD.

Desired functionality: Ability to export event data to removable media (flash drive, portable hard drive).

NOTE: This ECP also applies to the MH-65D1 & MH-65D2 devices.

Ready For Customer Recheck

2-Mar-17 29-Mar-17

ECP

019-16 (E)

Casper J305-

MX-20 Turret System Built-In-Test (BIT)

Current functionality: MX-20 Turret System BIT not simulated.

Desired functionality: Model the MX-20 Turret System to perform BIT when initiated by the operator.

Ready For Customer Recheck

2-Mar-17 29-Mar-17

ECP

018-16 (E)

AWT J305-

Capsule Lighting Current functionality: The CG-AWT Cabin lightning is insufficient for students to perform training tasks and replicate the selected time of day. The existing lighting does not adequately illuminate the cabin to safely perform required maintenance functions.

Desired functionality: Install a dimmable overhead LED lighting system in the cabin overhead to control cabin ambient lighting that coincides with time of day conditions and provides adequate lighting to perform training tasks. Upgrade the existing capsule lighting system to more adequately illuminate capsule maintenance work areas.

Open 2-Mar-17 30-Mar-17 https://10.0.1.102:8444/browse/J305-8898 https://10.0.1.102:8444/browse/J305-8898 https://10.0.1.102:8444/browse/J305-8897 https://10.0.1.102:8444/browse/J305-8897 https://10.0.1.102:8444/browse/J305-8896 https://10.0.1.102:8444/browse/J305-8896

ECP# Device Key Summary Description Status Created Updated

ECP

017-16 (E)

MH-65D

OFT

J305-

IOS NAVAID Ident Selection

Current functionality: NAVAID Idents can only be selected on or off as a group. There is no functionality to allow the Instructor Pilot to select which NAVAID he is monitoring.

Desired functionality: The ability to individually select/deselect the NAVAIDS to monitor at the instructor station.

NOTE: This ECP applies to the MH-65D2 OFT also.

Open 1-Mar-17 1-Mar-17

ECP

016-16

MH-60T

OFT

J305-

Engine High Side Failure with loss of Np and Torque Indications

Current functionality: Symptoms of Engine High Side Failure EPs do not include loss of respective Np and Torque indications.

Desired functionality: Model new Engine High Side Failure EPs that provide the symptoms of the current Engine High Side Failure EPs, but also include the loss of respective Np and Torque indications.

NOTE: This ECP also applies to the MH-60T CPT.

In Progress

2-Dec-16 28-Mar-17

ECP

014-16

MH-65D

OFT

J305-

IP & OBS ICS/COMMs Cords

Current functionality: The current IP & OBS cord connectors are not mounted, but are hanging freely on the cord that enters the IOS & OBS stations. These cords are not currently removable/swappable.

Desired functionality: To have the ICS/COMMs cord connector mounted at the IOS/OBS stations.

Reason for the change: To be able to remove and replace the cord between head set and Trainer connector.

Impact on training, if denied: When failure occurs, the Trainer is down during the repair of the cord/connection, because it is not swappable.

In Progress

19-Oct-16 10-Feb-17 https://10.0.1.102:8444/browse/J305-8887 https://10.0.1.102:8444/browse/J305-8887 https://10.0.1.102:8444/browse/J305-8469 https://10.0.1.102:8444/browse/J305-8469 https://10.0.1.102:8444/browse/J305-8268 https://10.0.1.102:8444/browse/J305-8268

ECP# Device Key Summary Description Status Created Updated

ECP

013-16

MH-60T

CPT

J305-

IOS Book Shelf Current functionality: No designated area to place ‘Trainer Book’ or A/C pubs.

Desired functionality: To have a book shelf/hutch over the IP/IOS station to place Trainer book and various pubs.

Reason for the change: To prevent these books/pubs from being scattered around the IOS, cockpit and surrounding areas.

Note: we will not be updating any drawing for this.

Ready For Customer Recheck

19-Oct-16 22-Nov-16

ECP

012-16

HU-25

OFT

J305-

Removal of the HU-25

OFT

1. Destructive disassembly of the device and associated components.

a. Majority of the effort will be done utilizing on-site employees under the normal IMOMS efforts (CLIN 4001).

b. Rental of equipment required for disassembly and transport to staging area.

c. Relocation of palletized components to USCG identified staging area.

d. Threaded studs for lower knuckles will be cut off at floor level.

e. High bay trenches and computer room subfloor shall be swept and or vacuumed.

2. USCG to remove existing cockpit air conditioner air handler.

3. Purge TDSP of all HU-25 documentation, unique spare parts, etc.

4. USCG to take lead on documentation required for turn in.

a. Assist USCG in the documentation of parts, etc., as required, for turn in.

In Progress

23-Sep-16 23-Sep-16

ECP

011-16

HC-144

OFT

J305-

HC-144B Main Battery Sealed Lead Acid Batteries (Slab)

Modify the host simulation to support the new Sealed Lead Acid Batteries.

Applicable to OFT and CPT.

In Progress

25-Aug-16 19-Dec-16 https://10.0.1.102:8444/browse/J305-8267 https://10.0.1.102:8444/browse/J305-8267 https://10.0.1.102:8444/browse/J305-8161 https://10.0.1.102:8444/browse/J305-8161 https://10.0.1.102:8444/browse/J305-8023 https://10.0.1.102:8444/browse/J305-8023

ECP# Device Key Summary Description Status Created Updated

ECP

010-16

HC-144

OFT

J305-

Custom IC Sets Current functionality: There are no custom or temporary slots available for saving IC Sets.

Desired functionality: Provide 30 slots per gaming area for IP custom and/or temporary use. Change “save ic” password to prevent saving over existing ic sets. Use existing “save ic” password for the IP custom ic sets.

Note: This ECP also applies to the HC-144 RFTD.

Ready For Customer Recheck

24-Aug-16 12-Oct-16

ECP

009-16

MH-60T

OFT

J305-

Instructor Operator Station (IOS) Emergency Procedures (EP) Descriptions

Current functionality: IOS EP descriptions are based on Emergency Operating Procedures listed in CGTO 1H-60T-1.

Desired functionality: Update IOS EP descriptions as listed in

CGTO 1H-60T-RNP-1.

Note: This ECP also applies to the MH-60T CPT.

Ready For Customer Recheck

24-Aug-16 21-Nov-16

ECP

008-16

MH-

65D2

OFT

J305-

Copilot Pitot Static Isolating Valves

Current functionality: All copilot pitot and static driven flight instruments (airspeed, barometric altimeter, and vertical speed indicators) and pilot/copilot EHSIs indications go to zero when placing the STATIC PRESS and TOTAL PRESS switches to

OFF.

Desired functionality: Copilot pitot and static driven flight instruments should operate normally as they are not affected by the STATIC PRESS and TOTAL PRESS isolating valves.

Pilot/Copilot EHSI indications and flight director inputs should remain at indications when respective isolating valve is closed.

Note: This ECP applies to MH-65D1 OFT and RCPT also.

Ready For Customer Recheck

11-Aug-16 13-Dec-16 https://10.0.1.102:8444/browse/J305-8012 https://10.0.1.102:8444/browse/J305-8012 https://10.0.1.102:8444/browse/J305-8011 https://10.0.1.102:8444/browse/J305-8011 https://10.0.1.102:8444/browse/J305-7938 https://10.0.1.102:8444/browse/J305-7938

ECP# Device Key Summary Description Status Created Updated

ECP

005-16

MH-60T

OFT

J305-

Arrival and Departure charts at Instructor Operator Station (IOS)

Current functionality: Unable to view Standard Terminal Arrival Route (STAR) and Standard Instrument Departure (SID) charts at the Instructor Operator Station (IOS).

Desired functionality: Add the capability to view STAR and SID charts at the IOS.

Note: This ECP also applies to MH-65D1, MH-65D2, MH-60T CPT, and RCPT(MH-65D).

Ready For Customer Recheck

2-Aug-16 21-Nov-16

ECP

006-16

AWT J305-

OBIOS Monitors Current functionality: OBIOS monitors are non-NVG compatible. IG Stealth View is not viewable at OBIOS.

Desired functionality: OBIOS monitors that are NVG compatible. Ability to switch left OBIOS monitor between Map View and IG Stealth View.

In Progress

2-Aug-16 6-Dec-16

ECP

004-16

MH-65D

OFT

J305-

IOS EP Flight Manual Update

Current Functionality: IOS EP titles are based on Emergency Operating Procedures listed in CGTO 1H-65C-1 Section III.

Desired Functionality: Update IOS EP descriptions as listed in CGTO 1H-65D-1 Section III. For EPs Listed in CGTO 1H-65D- 1 not currently modeled, add appropriate malfunction to simulation.

Note: This ECP also applies to MH65D2 and RCPT65 devices.

Ready For Customer Recheck

15-Jul-16 19-Oct-16

ECP

001-16

MH-65D

OFT

J305-

MH65D1 AFCS/FD

SPR Clearance

As a follow on to ECP 012-15 (Automatic Flight Control System (AFCS), Flight Director (FD) & Control Loader System (CLS) Integration), this ECP addresses SPRs as a result of the ECP 012-15 efforts.

In Progress

30-Jun-16 11-Jul-16

ECP

003-16

MH-65D

OFT

J305-

GPS Position Failure for EFB

Provide a method to fail the GPS position signal to the EFBs.

NOTE: This ECP applies to all devices with EFB capability.

Ready For Customer Recheck

30-Jun-16 21-Nov-16 https://10.0.1.102:8444/browse/J305-7896 https://10.0.1.102:8444/browse/J305-7896 https://10.0.1.102:8444/browse/J305-7895 https://10.0.1.102:8444/browse/J305-7895 https://10.0.1.102:8444/browse/J305-7792 https://10.0.1.102:8444/browse/J305-7792 https://10.0.1.102:8444/browse/J305-7732 https://10.0.1.102:8444/browse/J305-7732 https://10.0.1.102:8444/browse/J305-7730 https://10.0.1.102:8444/browse/J305-7730

ECP# Device Key Summary Description Status Created Updated

ECP

002-16

MH-

65D2

OFT

J305-

IOS Desktop modification

Relocate the simulation control panel. Ready For Customer Recheck

30-Jun-16 7-Jul-16

ECP

011-15

MH-60T

OFT

J305-

60OFT KVM upgrade Install Avocent 2015 KVM. In Progress

31-Mar-16 9-Feb-17

ECP

012-15

MH-65D

OFT

J305-

Automatic Flight Control System (AFCS), Flight Director (FD) & Control Loader System (CLS) Integration

Current functionality: The MOOG/FCS flight control loader drives the yaw axis input. The MH-65D2 OFT uses legacy AFCS/FD software models.

Desired functionality: AFCS model drives the yaw channel through commands to the control loader on both the MH-65D-1 and MH-65D-2 operational flight trainers. Integrate the MH- 65D1 OFT AFCS and FD models onto the MH-65D2 OFT.

Note: This ECP applies to both the MH-65D1 OFT and MH-

65D2 OFT.

In Progress

1-Mar-16 30-Apr-16

ECP

010-15

MH-65D

OFT

J305-

Balance power between phases

Current functionality: Power (Current utilization) is unusually high on some legs than others causing UPS to go into bypass.

Desired functionality: Balance power to more acceptable level so UPS will not go into bypass.

In Progress

19-Feb-16 25-May-16

ECP

009-15

HC-144

OFT

J305-

Daisy Chain KVMs Current functionality: User has to "jump" to a second set of KVMs when control of Aechelon computers is required.

Desired Functionality: To see all the available computers on a single dialog display.

In Progress

19-Feb-16 25-Aug-16

ECP

007-15

MH-60T

CPT

J305-

MH-60T CPT Telestra upgrade

Current functionality: The existing aural cues/communication system on the OFT is an ASTi DACS. Unsupportable.

Desired functionality: Technical Refresh. Replace DACS with Telestra.

In Progress

22-Jan-16 8-Jun-16 https://10.0.1.102:8444/browse/J305-7729 https://10.0.1.102:8444/browse/J305-7729 https://10.0.1.102:8444/browse/J305-7264 https://10.0.1.102:8444/browse/J305-7264 https://10.0.1.102:8444/browse/J305-7106 https://10.0.1.102:8444/browse/J305-7106 https://10.0.1.102:8444/browse/J305-7043 https://10.0.1.102:8444/browse/J305-7043 https://10.0.1.102:8444/browse/J305-7042 https://10.0.1.102:8444/browse/J305-7042 https://10.0.1.102:8444/browse/J305-6904 https://10.0.1.102:8444/browse/J305-6904

ECP# Device Key Summary Description Status Created Updated

ECP

006-15

MH-60T

CPT

J305-

Projector control at IOS Current functionality: Projector control is by a remote control.

Desired functionality: Provide projector control at the IOS.

Ready For Customer Recheck

22-Jan-16 29-Mar-17

ECP

003-15

HC-144

OFT

J305-

Forward Looking Infrared (FLIR) Universal Hand Control Unit (UHCU)

Current functionality: The HC-144 OFT currently utilizes the FLIR HCU Box-on-a-stick type controller.

Desired functionality: Install the new version FLIR UHCU.

In Progress

14-Oct-15 15-Nov-16

ECP

002-15

Casper J305-

CASPER Refresh Current functionality: Crystal Server not currently installed.

Desired functionality: Install Crystal Server. Perform the intent of CASPER_ATW_TCTO_Final_Draft_052915 on the CASPER Trainer. Install Crystal Server and associated hardware into trainer; stimulate Crystal Server with video from simulated sensors, and GPS position of simulated ownship.

Ready For Customer Recheck

31-Aug-15 23-May-16

ECP

025-14

HC-144

OFT

J305-

Visual Model Effects/Animations

Current functionality: The HC-144A OFT and CPT do not chain most of the effects and animations to the models, but instead they are currently independent models.

Desired functionality: Chain effect and animations to the existing virtual models.

Note: This ECP also applies to the HC-144 RFTD.

Ready For Customer Recheck

25-Feb-15 21-Nov-16

ECP

026-14

MH-60T

OFT

J305-

Update EGI Model Current functionality: The existing EGI model is sufficient for pre-RNP CAAS testing requirements but not for the aircraft RNP CAAS hardware and software recently installed on the

MH-60T CPT.

Desired functionality: Insert the existing Government-owned HC144 OFT EGI model into the MH-60T CPT & OFT to fully utilize the new RNP CAAS platform for testing and training.

Note: This ECP applies to the MH-60T CPT also.

In Progress

12-Feb-15 13-Jan-16 https://10.0.1.102:8444/browse/J305-6903 https://10.0.1.102:8444/browse/J305-6903 https://10.0.1.102:8444/browse/J305-6519 https://10.0.1.102:8444/browse/J305-6519 https://10.0.1.102:8444/browse/J305-6337 https://10.0.1.102:8444/browse/J305-6337 https://10.0.1.102:8444/browse/J305-5442 https://10.0.1.102:8444/browse/J305-5442 https://10.0.1.102:8444/browse/J305-5407 https://10.0.1.102:8444/browse/J305-5407

ECP# Device Key Summary Description Status Created Updated

ECP

022-14

HC-144

OFT

J305-

Eng Power and Condition Lever Control Knobs (SCTO HC-144A T76011.0)

Current functionality: The simulator Power and Condition Control Knobs are not compliant (labeled) with aircraft configuration.

Desired functionality: Remove and replace Power and Condition Control knobs.

Note: This ECP also applies to HC-144 CPT.

Ready For Customer Recheck

16-Dec-14 24-Feb-15

ECP

018-14

MH-60T

OFT

J305-

MH-60T Transmission EPs

Modify device to reflect the changes in Transmission EPs based upon CGTO 1H-60T-1-CL1 Revision 1 - dated 8 April 2013. This ECP applies to MH-60T CPT as well.

Ready For Internal Recheck

5-Nov-14 24-Nov-14

ECP

015-14

MH-60T

OFT

J305-

MH-60T EDECU Incorporate new EDECU model that provides the same functionality, performance and limitations as the aircraft

EDECU.

Ready For Internal Recheck

10-Oct-14 12-Aug-15

ECP

014-14

HC-144

CPT

J305-

Vibration Seat vibrations in RFTD. In Progress

10-Oct-14 18-Aug-16

ECP

013-14

HC-144

OFT

J305-

HC-144A OFT Baseline Configuration Upgrade

Convert the HC-144A OFT device to the HC-144A Ocean Sentry Refresh (OSR) baseline configuration.

Ready For Customer Recheck

1-Oct-14 11-Feb-16

ECP

009-14

MH-65D

OFT

J305-

ILS audio IDENTs Current functionality: The current ILS modeling allows you to identify ILS approaches via audio while 16 miles left or right of the inbound course. The current simulation is based on distance from transmitter and needs to be revised to a specific area in accordance with the AIM.

Desired functionality: ILS audio should only be available when within the bounded area that is given within the AIM for Localizer transmitters. Revise TTPRR to demonstrate this functionality.

Note: This ECP also applies to the MH60TOFT, MH60TCPT, MH65COFT, and RCPT65.

In Progress

29-May-14 14-Nov-16 https://10.0.1.102:8444/browse/J305-5149 https://10.0.1.102:8444/browse/J305-5149 https://10.0.1.102:8444/browse/J305-4979 https://10.0.1.102:8444/browse/J305-4979 https://10.0.1.102:8444/browse/J305-4814 https://10.0.1.102:8444/browse/J305-4814 https://10.0.1.102:8444/browse/J305-4813 https://10.0.1.102:8444/browse/J305-4813 https://10.0.1.102:8444/browse/J305-4760 https://10.0.1.102:8444/browse/J305-4760 https://10.0.1.102:8444/browse/J305-4130 https://10.0.1.102:8444/browse/J305-4130

ECP# Device Key Summary Description Status Created Updated

ECP

008-14

MH-65D

OFT

J305-

Nose Gear Weight on Wheels Switch Malfunctions (EP 606 &

EP 607)

Current functionality: AFCS, Flight Director, and Weather Radar Systems are not affected by activation of the Weight on Wheels Switch Malfunctions EP 606 (WOW Fail Open) and EP 607 (WOW Fail Closed).

Desired functionality: Weight on Wheels Switch malfunctions should affect all systems that are wired to the nosegear WOW switch in the aircraft. Change IOS Malfunction Page descriptions to EP 606 (NG WOW Fail Open) and EP 607 (NG WOW Fail Closed) to indicate these are NG WOW malfunctions.

Note: This ECP also applies to the MH65C OFT & RCPT65.

Ready For Customer Recheck

29-May-14 24-Mar-17

ECP

005-14

MH-65D

OFT

J305-

Radar Altimeter Failure

(EP 1327)

Current functionality: The ADI Radar Altitude Flag does not appear when the Radar Altimeter Failure (EP 1327) is activated.

Desired functionality: The ADI Radar Altitude Flag should appear when the Radar Altimeter Failure (EP 1327) is activated.

Note: This ECP also applies to the MH65C OFT & RCPT65.

Ready For Customer Recheck

29-May-14 3-Sep-15

ECP

031-13

MH-60T

CPT

J305-

MH-60T Visual Display System Upgrade

Current functionality: The current visual display system utilizes low resolution projectors.

Desired functionality: High resolution projectors, to take advantage of the new Aechelon IG capability.

Reason for the change: Improved training capabilities.

Impact on training, if denied: Reduced realism and situational awareness.

In Progress

8-Aug-13 25-May-16

ECP

022-13

HH-65C

OFT

J305-

VDS and IOS Update the IOS hardware design to improve desktop work area update obsolete trainer power supplies.

Update current visual display system to improve NVG focus and minimize distracting cross-cockpit FOV artifacts

Ready For Internal Recheck

19-Jul-13 23-Sep-16 https://10.0.1.102:8444/browse/J305-4129 https://10.0.1.102:8444/browse/J305-4129 https://10.0.1.102:8444/browse/J305-4126 https://10.0.1.102:8444/browse/J305-4126 https://10.0.1.102:8444/browse/J305-2694 https://10.0.1.102:8444/browse/J305-2694 https://10.0.1.102:8444/browse/J305-2627 https://10.0.1.102:8444/browse/J305-2627

ECP# Device Key Summary Description Status Created Updated

ECP

024-13

MH-60T

OFT

J305-

#1 Generator Failure and #2 Generator Failure

Note: this ECP applies to the MH-60T OFT & the MH-60T CPT.

Current functionality: During main generator failure, #1 or #2 GEN caution is displayed.

Desired functionality: Add a second #1 Generator Failure (SLOW SWITCH) and include the following symptoms: #1 GEN Caution, SAS 1 and AUTOPILOT disengaged, AFCS Degraded, SAS 2 Fail Advisory, Stabilator Caution. Also include momentary loss of #1 MFD, DCS2, V1, ICU, and ADC1. The momentary loss should appear as these items losing power for 2-3 seconds, but then coming back on line as the #2 generator picks up the #1 AC Primary and AC Essential busses.

Add a second #2 Generator Failure (SLOW SWITCH) and include the following symptoms: #2 GEN Caution. Also include momentary loss of #2 CONV, and #2 and #5 MFDs. Again, this should be a 2-3 second power loss, with the equipment coming back on line as the #1 Generator picks up the #2 AC Primary Bus and #2 DC Primary Bus.

In Progress

10-Jun-13 30-Nov-14

ECP

016-13

MH-60T

CPT

J305-

MH-60T CPT Cockpit concurrence

Install new and or modify panels, CB labels, etc., to match the current aircraft configuration. Tie DTU-7100 into the simulation and complete the installation.

In Progress

29-Apr-13 22-Nov-16

ECP

010-12

MH-60T

CPT

J305-

MH-60T CPT Image Generator and Host/IOS Computer Systems Replacement

Desired functionality: To have the same "gaming" areas and IOS visual/environmental cues control on both the CPT and

OFT.

Reason for the change: To allow the use of identical training scenarios on both the CPT and OFT. To be able to utilize the CPT as a fully functional backup device, with respect to training scenarios, for the OFT. This would also allow us to run virtually the same simulation code on the CPT that the OFT utilizes.

In Progress

4-Mar-13 25-May-16 https://10.0.1.102:8444/browse/J305-2389 https://10.0.1.102:8444/browse/J305-2389 https://10.0.1.102:8444/browse/J305-2230 https://10.0.1.102:8444/browse/J305-2230 https://10.0.1.102:8444/browse/J305-2012 https://10.0.1.102:8444/browse/J305-2012

ECP# Device Key Summary Description Status Created Updated

ECP51 HH-65C

OFT

J305-

HH-65C OFT Weather Radar Simulator Replacement

Current radar simulation is correlated to current XIG databases. New Pc Nova IG will have other gaming areas not currently covered with the existing radar simulation. Refresh the radar simulation and ensure radar database coverage provides radar capabilities in and correlates with all PC Nova IG gaming areas (except SE US). Provide an option to generate a usable radar database for the SE US gaming area.

Ready For Customer Recheck

14-Sep-11 23-Mar-16 https://10.0.1.102:8444/browse/J305-225 https://10.0.1.102:8444/browse/J305-225

Appendix C

Engineering Change Notice Summary

ECNs Open or Closed this Reporting Period – March 2017

Device Key Description Drawing Number

Status Created Updated

MH-65D2 OFT J305-8857 SWAP WIRE COLOR BETWEEN PIN 40 AND 41 185B503104 QA 22-Feb-17 22-Feb-17

HC-144 OFT J305-8836 KVM UPGRADE

ECP 009-15

315A500284 QA 16-Feb-17 17-Feb-17

HC-144 OFT J305-8835 KVM UPGRADE

ECP 009-15

315A500127 QA 16-Feb-17 16-Feb-17

HC-144 OFT J305-8834 KVM UPGRADE

ECP 009-15

315A500126 QA 16-Feb-17 16-Feb-17

HC-144 OFT J305-8833 KVM UPGRADE

ECP 009-15

315A600080 QA 16-Feb-17 17-Feb-17

MH-60T OFT J305-8797 KVM UPGRADE

ECP 014-13

307A505270 QA 13-Feb-17 13-Feb-17

MH-60T OFT J305-8796 KVM UPGRADE

ECP 014-13

204C505146 QA 13-Feb-17 13-Feb-17

MH-60T OFT J305-8794 KVM UPGRADE

ECP 014-13

185C505121 QA 13-Feb-17 13-Feb-17

MH-60T OFT J305-8784 KVM UPGRADE

ECP 011-015

204C505145 QA 9-Feb-17 10-Feb-17

MH-60T OFT J305-8783 KVM UPGRADE

ECP 011-015

204C505144 QA 9-Feb-17 10-Feb-17

MH-60T OFT J305-8765 KVM UPGRADE

ECP 011-015

204C505143 QA 7-Feb-17 15-Feb-17

MH-60T OFT J305-8757 KVM UPGRADE

ECP 011-015

707A509020 QA 6-Feb-17 9-Feb-17

MH-60T OFT J305-8747 KVM UPGRADE

ECP 011-015

204C505141 QA 3-Feb-17 3-Feb-17

MH-60T OFT J305-8746 KVM UPGRADE

ECP 011-015

204C505142 QA 3-Feb-17 3-Feb-17

MH-60T OFT J305-8736 KVM UPGRADE

ECP 011-015

204C505136 QA 2-Feb-17 16-Feb-17 https://10.0.1.102:8444/browse/J305-8857 https://10.0.1.102:8444/browse/J305-8836 https://10.0.1.102:8444/browse/J305-8835 https://10.0.1.102:8444/browse/J305-8834 https://10.0.1.102:8444/browse/J305-8833 https://10.0.1.102:8444/browse/J305-8797 https://10.0.1.102:8444/browse/J305-8796 https://10.0.1.102:8444/browse/J305-8794 https://10.0.1.102:8444/browse/J305-8784 https://10.0.1.102:8444/browse/J305-8783 https://10.0.1.102:8444/browse/J305-8765 https://10.0.1.102:8444/browse/J305-8757 https://10.0.1.102:8444/browse/J305-8747 https://10.0.1.102:8444/browse/J305-8746 https://10.0.1.102:8444/browse/J305-8736

Device Key Description Drawing Number

Status Created Updated

MH-60T OFT J305-8729 KVM UPGRADE

ECP 011-15

204C505135 QA 1-Feb-17 2-Feb-17

MH-60T OFT J305-8714 KVM UPGRADE

ECP 011-015

307A505258 QA 30-Jan-17 16-Feb-17

MH-60T OFT J305-8713 KVM UPGRADE 307A505251 QA 30-Jan-17 1-Feb-17

MH-60T OFT J305-8711 KVM UPGRADE

ECP 011-015

602001 QA 30-Jan-17 15-Feb-17

MH-60T OFT J305-8710 KVM UPGRADE

ECP 011-015

185C120000 QA 30-Jan-17 15-Feb-17

MH-60T OFT J305-8708 KVM UPGRADE

ECP 011-015

707A600005 QA 30-Jan-17 7-Feb-17

MH-60T OFT J305-8707 KVM Upgrade

ECP 011-015

307A616000 QA 30-Jan-17 10-Feb-17

MH-60T OFT J305-8678 Upgrade from DAQS to Telestra.

ECP 014-13

307A505282 QA 24-Jan-17 25-Jan-17

MH-60T OFT J305-8661 Upgrade from daqs to Telestra.

ECP 014-13

307A244000 QA 20-Jan-17 24-Jan-17

MH-60T OFT J305-8656 Change from daqs to Telestra.

ECP 014-13

307A244160 QA 19-Jan-17 24-Jan-17

MH-60T OFT J305-8643 KVM upgrade

ECP 014-13

707A620010 QA 18-Jan-17 15-Feb-17

MH-60T OFT J305-8630 KVM UPGRADE

ECP 011-15

185C505027 QA 13-Jan-17 14-Feb-17

MH-60T OFT J305-8629 KVM UPGRADE

ECP 011-15

185C505026 QA 13-Jan-17 14-Feb-17

MH-60T OFT J305-8609 KVM UPGRADE

ECP 014-13

185C505025 QA 11-Jan-17 14-Feb-17

MH-60T OFT J305-8608 Upgrade from daqs to Telestra.

ECP 014-13

185C505001 QA 11-Jan-17 24-Jan-17

MH-60T OFT J305-8607 Upgrade from daqs to Telestra.

ECP 014-13

500B003 QA 11-Jan-17 16-Feb-17 https://10.0.1.102:8444/browse/J305-8729 https://10.0.1.102:8444/browse/J305-8714 https://10.0.1.102:8444/browse/J305-8713 https://10.0.1.102:8444/browse/J305-8711 https://10.0.1.102:8444/browse/J305-8710 https://10.0.1.102:8444/browse/J305-8708 https://10.0.1.102:8444/browse/J305-8707 https://10.0.1.102:8444/browse/J305-8678 https://10.0.1.102:8444/browse/J305-8661 https://10.0.1.102:8444/browse/J305-8656 https://10.0.1.102:8444/browse/J305-8643 https://10.0.1.102:8444/browse/J305-8630 https://10.0.1.102:8444/browse/J305-8629 https://10.0.1.102:8444/browse/J305-8609 https://10.0.1.102:8444/browse/J305-8608 https://10.0.1.102:8444/browse/J305-8607

Device Key Description Drawing Number

Status Created Updated

MH-60T OFT J305-8606 Upgrade from daqs to Telestra.

ECP 014-13

185C505012 QA 11-Jan-17 24-Jan-17

MH-60T…