Attachment 4-Mechanical Installation Control Document.pdf

PDF 14 MB Posted Jul 22, 2026

Attached to: Geostationary Littoral Imaging and Monitoring Radiometer (GLIMR) Access to Space (ATS) “GLIMR ATS"
Solicitation number: 80LARC26R0002
Issued by: National Aeronautics and Space Administration Langley Research Center

About this file

Written by GovTribe AI · Jul 22, 2026

This is an Installation Control Drawing for the GLIMR (Global Geostationary Constellation on Low Earth Orbit for Observations of Dynamics) Instrument, a Raytheon-developed payload designed for spacecraft integration. The drawing (D4957031-500, Revision B) provides comprehensive technical specifications and installation requirements for the GLIMR Instrument assembly, including the Sensor Subsystem, Power Control Unit (PCU), and Data Electronics Box (DEB).

The document specifies critical mechanical and thermal interfaces for spacecraft integration within a NASA standard host interface coordinate system. Key requirements include: sensor subsystem mounting with 12 fasteners torqued to 47-53 ft-lbs, PCU mounting with 18 fasteners torqued to 66-73 in-lbs on thermal isolators, and DEB mounting with 4 fasteners torqued to 40-44 in-lbs. The instrument has a maximum weight exceeding two-person lift capacity and operates with a 24W average heat load to the PCU and 6W to the DEB. The drawing mandates continuous gaseous nitrogen (GN2) purging meeting MIL-PRF-27401 Type I Grade B standards through specified purge ports at bearing rings and covers, with bearing purge system elements to be removed before flight. Electrical connectivity is provided through six D38999 military connectors (J1-J6) supporting Space Wire, pulse per second signals, analog telemetry, power, launch locks, and survival heaters. The instrument features gimbal-mounted reflectors with azimuth and elevation axis control, defined optical field-of-view keep-out zones, and specific cable management requirements with first tie-down points located within 20 inches (PCU) and 12 inches (DEB) of the unit.

View the file

Other files

File	Type	Posted
EXHIBIT C - GLIMR ATSRD_Amendment 2.pdf	PDF	Aug 11, 2026
Attachment 5 - GLIMR-06-002 - GLIMR Payload to GLIMR Spacecraft IDD.pdf	PDF	Aug 11, 2026
Solicitation Amendment 80LARC26R00020002 SF 30.pdf	PDF	Aug 11, 2026
Solicitation Amendment 80LARC26R00020001 SF 30.pdf	PDF	Aug 5, 2026
Amendment Attachment 1 - RFP Questions and Answers.pdf	PDF	Aug 5, 2026
Final RFP Cover Letter.pdf	PDF	Jul 22, 2026
FINAL RFP-80LARC26R0002.pdf	PDF	Jul 22, 2026
Attachment 2 - Blackout Notice.pdf	PDF	Jul 22, 2026
Exhibit D-GLIMR Milestone Payments.xlsx	XLSX spreadsheet	Jul 22, 2026
Attachment 1-Past Performance Questionnaire.pdf	PDF	Jul 22, 2026
EXHIBIT A-GLIMR SOW.pdf	PDF	Jul 22, 2026
EXHIBIT B-GLIMR DRL_DRD.pdf	PDF	Jul 22, 2026
EXHIBIT C-GLIMR ATSRD.pdf	PDF	Jul 22, 2026
Attachment 3-Responses to DRFP Feedback and Questions.pdf	PDF	Jul 22, 2026

Show all 14

On GovTribe

Work with this file

Download the original file
Contacts named in this file
Similar government files
Ask GovTribe AI about this file

Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

REVISION HISTORY

APPROVEDDATEDESCRIPTIONREVZONE

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

THIS DRAWING SHALL BE INTERPRETED IN

ACCORDANCE WITH ASME Y14.100-2017

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

THIS DOCUMENT CONTAINS PROPRIETARY TECHNICAL DATA OR INFORMATION PERTAINING TO ITEMS, COMPONENTS, PROCESSES, OR OTHER MATTER DEVELOPED OR ACQUIRED BY RAYTHEON COMPANY USING EXCLUSIVE CUSTOMER FUNDS PURSUANT TO

CONTRACT NO. L0063.

IT IS RESTRICTED TO USE ONLY BY PERSONS AUTHORIZED BY RAYTHEON IN WRITING TO USE IT. DISCLOSURE TO UNAUTHORIZED PERSONS WOULD LIKELY CAUSE SUBSTANTIAL COMPETITIVE HARM TO RAYTHEON'S BUSINESS POSITION. THIS DOCUMENT, DATA OR INFORMATION MUST NOT BE FURNISHED, DISCLOSED TO, COPIED OR USED BY PERSONS OUTSIDE RAYTHEON WITHOUT RAYTHEON'S

EXPRESS WRITTEN APPROVAL.

THIS DOCUMENT, DATA OR INFORMATION HAS NOT BEEN FINALIZED BY RAYTHEON FOR OFFICIAL, CONTRACTUAL DELIVERY TO THE U.S. GOVERNMENT. IF/WHEN IT IS FINALIZED FOR DELIVERY DIRECTLY TO THE U.S. GOVERNMENT, RAYTHEON PERSONNEL OR OTHERS RAYTHEON AUTHORIZES IN WRITING MAY REMOVE AND REPLACE THE NON-CONFORMING MARKINGS OF TECHNICAL DATA ONLY WITH CONFORMING ONES. AT THAT TIME, THE U.S. GOVERNMENT'S RIGHTS IN AND TO THIS PROPRIETARY TECHNICAL AND/OR BUSINESS DATA OR INFORMATION ARE AS SPECIFIED IN THE FAR, DFARS OR APPLICABLE AGENCY REGULATION, WHICH WILL BE MADE PART

OF THE CONTRACT.

4U884

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA AND / OR TECHNOLOGY WHOSE EXPORT OR DISCLOSURE TO NON-U.S.

PERSONS, WHEREVER LOCATED, IS RESTRICTED BY THE INTERNATIONAL TRAFFIC IN ARMS REGULATIONS (ITAR) (22 C.F.R. SECTIONS 120-130) OR THE EXPORT ADMINISTRATION REGULATIONS (EAR) (15 C.F.R. SECTIONS 730-774). THIS DOCUMENT CANNOT BE EXPORTED (E.G., PROVIDED TO A SUPPLIER OUTSIDE OF THE UNITED STATES) OR DISCLOSED TO A NON-U.S. PERSON, WHEREVER LOCATED, UNTIL A FINAL JURISDICTION AND CLASSIFICATION DETERMINATION HAS BEEN COMPLETED AND APPROVED BY RAYTHEON, AND ANY REQUIRED U.S. GOVERNMENT APPROVALS HAVE BEEN OBTAINED. VIOLATIONS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES.

ALL SHEETS ARE THE

SAME REVISION STATUS

PARTS LIST-1

NOTES

DRAWING OR

SPECIFICATION NO

NOMENCLATURE OR

DESCRIPTION

PART OR

IDENTIFYING NUMBER

DAI

FIND

QTY

APPLICATION

USED ONNEXT ASSY

SEE PDMSEE PDM

SEE PDM

FOR APPROVAL

AUTHORIZED BY

CN1831708

CREO MAINTAINED. CHANGES SHALL BE

INCORPORATED BY THE DESIGN ACTIVITY.

D W G

N O

S H

UNLESS OTHERWISE SPECIFIED

DIM ARE IN INCHES

TOL ON ANGLE �#� 1.0

2 PL �#� .03 3 PL �#� .010

INTERPRET DIM AND TOL IAW

ASME Y14.5M-1994

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

SHEET 1 OF 9SCALE: NONE

SEE PRODUCT DATA

MANAGEMENT (PDM)

FOR APPROVAL SIGNATURES

D4957031-500E

DRAWING NODAISIZE

INSTALLATION CONTROL

DRAWING, GLIMR INSTRUMENT

TITLE

B.ADAMSDWN

L0063

CONTRACT NO

NOTES - UNLESS OTHERWISE SPECIFIED

1. INTERPRET DRAWING PER ASME-Y14.100

2. DELETED

3. DELETED

4. DELETED

5. DELETED

6 SEE TABLE I FOR CONNECTOR AND REFERENCE DESIGNATOR LIST

7. HANDLE AND PROTECT ELECTROSTATIC DISCHARGE SENSITIVE ASSEMBLY PER HP 10-00101

8. DELETED

9 SENSOR SUBSYSTEM MOUNTING INTERFACE IS LOCATED HERE

10. DELETED

11. SYMBOL DESIGNATES THE CENTER OF GRAVITY WITH A ± .500 TOLERANCE

12. REFER TO GLIMR INSTRUMENT-TO-HOST SPACECRAFT INTERFACE CONTROL DOCUMENT

ICDD4957031-020 FOR APPROXIMATE MASS MOMENT OF INERTIA ABOUT UNIT CG

13. OVERALL UNIT WEIGHT EXCEEDS TWO MAN LIFT

14 AFTER SENSOR SUBASSY UNIT HAS BEEN REGISTERED ON MOUNTING DATUM A,

TORQUE 12X NAS1351N6-16 FASTENERS WITH NAS620C6 WASHERS TO 47 - 53 FT-LBS.

DO NOT LUBRICATE. TIGHTEN USING ALTERNATING TORQUE PATTERN

15 THE PCU THERMAL AND MECHANICAL INTERFACES ARE DEFINED ON D4982950-100

16 AFTER PCU HAS BEEN REGISTERED ON MOUNTING ISOLATORS, TORQUE

18X NAS1351N3-16 FASTENERS WITH NAS620C6 WASHERS TO 66-73 IN-LBS. DO NOT

LUBRICATE. TIGHTEN USING ALTERNATING TORQUE PATTERN

17 THE DEB SHOWN HERE FOR REFERENCE ONLY. THE THERMAL AND MECHANICAL

INTERFACES ARE DEFINED ON D4954207

18 AFTER DEB HAS BEEN REGISTERED ON THERMAL AND MECHANICAL MOUNTING

SURFACE, TORQUE 4X NAS1351N08-12 FASTENERS WITH NAS620C8 WASHERS TO

40-44 IN-LBS. DO NOT LUBRICATE. TIGHTEN USING ALTERNATING TORQUE PATTERN

19 REQUESTED LOCATION AND ORIENTATION RELATIVE TO NASA STD HOST INTERFACE

COORDINATE SYSTEM. FOR REFERENCE, THIS COORDINATE SYSTEM IS ORIENTED AS

FOLLOWS:

A. +Z IN THE DIRECTION OF NADIR

B. +X IN THE DIRECTION OF ORBITAL VELOCITY

C. +Y COMPLETES THE RIGHT-HANDED SYSTEM

20 GLIMR INSTRUMENT SHOULD BE CONNECTED TO A GASEOUS NITROGEN (GN2)

SOURCE FOR CONTINUOUS PURGE AT ALL TIMES WHILE BEING INTEGRATED AT HOST

FACILITY. GN2 SOURCE TO BE CONNECTED WHERE SHOWN

21. ALL GN2 USED IN THE PURGING SHALL MEET PURITY, WATER, HYDROCARBONS AS

METHANE, AND PARTICULATE REQUIREMENTS OF MIL-PRF-27401. TYPE I. GRADE B, AT A

MINIMUM, AND SHALL BE PASSED THROUGH A 0.5 MICROMETER ABSOLUTE OR FINER

FILTER LOCATED AT THE POINT OF USE. COMPRESSED AIR SHALL NOT BE USED TO PURGE

THE ASSEMBLY OR ITS COMPONENTS

22 SUGGESTED ORIENTATION AND LOCATION FOR THE PCU DUE TO THE MAXIMUM LENGTH

OF CABLE W330A AT 50 INCHES

23 SUGGESTED ORIENTATION AND LOCATION FOR THE DEB DUE TO THE MAXIMUM LENGTH

OF CABLE W303A AT 23.7 INCHES AND CABLE W320A AT 49.4 INCHES

24 BEARING RINGS SHALL BE PURGED USING BEARING PURGE STE IN SIX LOCATIONS.

REMOVE BEARING PURGE STE BEFORE FLIGHT

25. SEE DRAWING D4954249 FOR DUST COVER DRAWING

26. UNLESS OTHERWISE SPECIFIED, ALL DIMENSIONS ARE IN INCHES [MILLIMETERS]

27 ENSURE FIRST TIE DOWN POINT FOR CABLES COMING OFF THE PCU ARE LOCATED

<20 INCHES FROM THE UNIT

28 ENSURE FIRST TIE DOWN POINT FOR CABLES COMING OFF THE DEB ARE LOCATED

<12 INCHES FROM THE UNIT

ISOMETRIC VIEW

IN STOWED ORIENTATION

FOR REFERENCE ONLY

SCALE 1/8

NADIR DECK

ORIGIN OF HOST

INTTERFACE

COORDINATE

SYSTEM

ISOMETRIC VIEW

IN STOWED ORIENTATION

FOR REFERENCE ONLY

SCALE 1/8

Developed under U.S. Govt. Contract No. 80LARC21DA002

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

40.0 1017[ ]

31.3 796[ ]

15.0 380[ ]

.1 4[ ]

.3 6[ ]

13.750 13.749 349,23 349,22[ ]

12.79 325[ ]

( )15.86 403[ ]

60.9 1548[ ]

12.1 309[ ]

16.5 420[ ]

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

C C

SHEET 2SCALE: 1/8

BD4957031-500E

REVDRAWING NODAISIZE

DWN B.ADAMS

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

D W G

N O

S H

Z3D8

Z3B6

Z3E6

AZ AXISSEE DETAIL G

DETAIL G

SCALE 1/3

2X GIMBAL REFLECTORS

SENSOR ASSEMBLY CENTER OF GRAVITY

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

.1252 3,18[ ]

.1640 4,166[ ]

3.000 76,2[ ]

3.907 99,24[ ]

1.000 25,4[ ]

23.6 600[ ]

.500 12,7[ ]

1.250 31,75[ ]

1.891 48,04[ ]

DUST COVER GAP

ALL AROUND.25

6,4[ ]

THRU

.2510 .2508 6,375 6,371[ ]

14.2°

15° .375 9,53[ ]

2X .251 6,37[ ]

( )15.74 399,9[ ]

( )15.85 402,7[ ]

( )45.2°( )45.2°

12X THRU

EQ SPACED ON A 17.75 BOLT CIRCLE

.406 10,31[ ]

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

Z X

SHEET 3SCALE: 1/8

BD4957031-500E

REVDRAWING NODAISIZE

DWN B.ADAMS

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

W G

N O

S H

VIEW D-D

SH2

VIEW C-C

SH2

SEE DETAIL H

SCALE 1/3

DETAIL H

SCALE 1/3

Developed under U.S. Govt. Contract No. 80LARC21DA002

SENSOR ASSEMBLY AND DUST COVER

INTERFACE

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

44.3 1126[ ]

49.6 1260[ ]

44.4 1128[ ]

19.8 502[ ] 24.3

616[ ]

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

SHEET 4SCALE: 1/8

BD4957031-500E

REVDRAWING NODAISIZE

DWN B.ADAMS

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

S H

SENSOR ASSEMBLY VOLUME (SWEPT)

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

.03 0,8[ ]

7.49 190,2[ ]

6.000 152,4[ ]

1.800 45,72[ ]

6.000 152,4[ ]

1.800 45,72[ ]

13.290 337,57[ ]

18.250 463,55[ ]

18X THRU MECHANICAL ISOLATOR

EQ SPACE ON PATTERN SHOWN

.219 5,56[ ]

17.54 445,4[ ]

19.25 489[ ]

8.60 218,4[ ]

3.01 76,5[ ]

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

SHEET 5SCALE: NONE

BD4957031-500E

REVDRAWING NODAISIZE

DWN B.ADAMS

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

S H

PCU INTERFACE

SCALE 1/2

THERMAL INTERFACE SURFACE

24W AVERAGE HEAT LOAD 8X .164-32 UNC-3B .250

EQ SPACED ON PATTERN SHOWN

THERMAL INTERFACE SURFACE

24W AVERAGE HEAT LOAD

8X .164-32 UNC-3B .250

EQ SPACED ON PATTERN SHOWN

PCU INTERFACE

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

7.438 188,93[ ]

1.838 46,69[ ]

MAX7.830

198,88[ ]

MAX6.125

155,58[ ]

MAX4.231

107,47[ ]

3.874 98,4[ ]

.332 8,43[ ]

4X THRU.188

+.006 -.001

4,78 +0,15 -0,02[ ]

2.733 69,42[ ]

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

SHEET 6SCALE: NONE

BD4957031-500E

REVDRAWING NODAISIZE

DWN B.ADAMS

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

S H

THERMAL INTERFACE

6 W AVERAGE HEAT LOAD

DEB INTERFACE

SCALE 1/2

ISOMETRIC VIEW

FOR REFERENCE ONLY

SCALE 1/2

DEB INTERFACE

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

19.0 483[ ]

3.1 80[ ]

11.0 279[ ]

3.1°

18.6 473[ ]

22.312 566,73[ ]

.400 10,16[ ]

20.8 527[ ]

17.7 448[ ]

45°

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

SHEET 7SCALE: 1/8

BD4957031-500E

REVDRAWING NODAISIZE

DWN B.ADAMS

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

S H

TABLE I. CONNECTORS

REFERENCE DESIGNATORS CONNECTOR PART NUMBER DESCRIPTION

J1 D38999/24GE35PN SPACE WIRE & 1 PULSE PER SECOND

J2 D38999/24GD35PN ANALOG TELEMETRY

J3 D38999/24GG35PN POWER

J4 D38999/24GG35PA LAUNCH LOCKS

J5 D38999/24GH35PN SURVIVAL HEATERS

J6 D38999/24GH35PA SURVIVAL HEATERS

AZ AXIS

DUST COVER CENTER AXIS

COALIGNED WITH THE SUNSHADE CENTER AXIS VIEW F-F

J4J6

GLIMR PAYLOAD CONNECTOR INTERFACE

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

45°

45° 45°

45°

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

SHEET 8SCALE: NONE

BD4957031-500E

REVDRAWING NODAISIZE

DWN B.ADAMS

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

S H

OPTICAL FOV KEEP OUT ZONE

VIEW ALONG GLOBAL X-AXIS

SCALE 1/8

OPTICAL FOV KEEP OUT ZONE

VIEW ALONG GLOBAL Y-AXIS

SCALE 1/8

GLIMR PAYLOAD FOV

8 7 6 5 4 3 2

C C

D D

E E

F F

G G

H H

7 6 5 4 3 2 1

RAYTHEON COMPANY

EL SEGUNDO, CA

RAYTHEON PROPRIETARY/CUSTOMER FUNDS

EXPORT CONTROLLED - SEE SHEET 1

NOTICE: DATA ON THIS SHEET IS CONTROLLED BY RESTRICTIONS LISTED ON SHEET 1

4U884

24202X

SHEET 9SCALE: 1/4

REVDRAWING NODAISIZE

DWN

SEE PDM FOR APPROVAL SIGNATURES

SEE PDM

FOR APPROVAL

SEE SHEET 1B

F I L E

N A M E

V E R

M O D

M O D E L

N O

D W G

N O

S H

PURGE PORTS TO ELEVATION BEARING RINGS

PURGE WITH 4X .125 FLEX LINE

PURGE PORTS TO AZIMUTH BEARING RING

PURGE WITH 2X .25 FLEX LINE

DUST COVER PURGE PORT

.4375-20 STRAIGHT THREAD

AFT COVER PURGE PORT

3/8 FEMALE NPT

GLIMR PAYLOAD PURGE INTERFACE

Sheet 1

Views

new_view_70

new_view_72

Zones

Sheet 2

Views

new_view_68

right_69

Zones

Sheet 3

Views

Zones

Sheet 4

Views

new_view_73

right_74

top_75

new_view_76

Zones

Sheet 5

Views

new_view_54

top_55

bottom_56

Zones

Sheet 6

Views

new_view_57

top_58

left_59

right_60

new_view_87

Zones

Sheet 7

Views

new_view_81

bottom_82

Zones

Sheet 8

Views

new_view_96

new_view_97

Zones

Sheet 9

Views

new_view_102

new_view_104

Zones

File details come from the government source that posted it. Updated Jul 22, 2026.