FA805121R3010 - L-CBA - SS 8 March 2021.docx

Attachment 4. Draft Shipping Destinations

STATEMENT OF WORK

Air Force Civil Engineer Center Rapid Explosive Hazard Mitigation (REHM) Large Clearance Blade Assembly (L-CBA) Date: DRAFT

1.0 SCOPE. This Statement of Work (SOW) defines the effort associated with the supply of large clearance blade assemblies to mount on armored front end loaders.

2.0 BACKGROUND. The Civil Engineer function has a requirement to return airfields back to a serviceable condition after an enemy attack. This solicitation is for the procurement and preposition of REHM L-CBAs and associated items to support the Airfield Damage Repair (ADR) Modernization Program. The objective of the ADR Modernization Program is to develop capabilities to rapidly asses damaged to airfield pavements, mitigate unexploded ordnance from the airfield pavement, and repair damaged airfield pavements for the full spectrum of operational scenarios including base recovery after an attack, expedient repairs at deployed locations, and sustainment of operating surfaces at forward operating bases. In all of these scenarios, time is a critical factor, either to restore flying operations or minimize airfield closures. The Large Clearance Blade Assembly (L-CBA) is required to push ordnance off airfield surfaces using an Armored Front End Loader. AFCEC/CXA has designed and tested an effective blueprint for this capability. EOD requires a five (5) year Indefinite Delivery/Indefinite Quantity ID/IQ contract to procure approximately 80 L-CBAs built to government specifications and shipped to specified locations.

3.0 REQUIREMENTS. The work required by this contract shall be performed in accordance with standards and formats identified within this SOW. The Large Clearance Blade Assemblies must be:

a. Built to the performance specifications

b. Built with specified metals

c. Incorporate ISO coupler for attachment to government armored front end loaders

d. Comply with specified schedule, data items, and other deliverables

e. Ship to specified destinations

3.1 Product/Performance Requirements.

3.1.1 The contractor shall purchase, manufacture, assemble, prepare, package, document, and deliver REHM L-CBAs, to selected worldwide locations in accordance with the detailed technical requirements of this SOW.

3.1.2 Build L-CBA(s) to government plans provided in attached technical data package specification design drawings (Attachment 1 Draft Design Specifications, Attachment 2 Draft Assembly Build Supplement, and Attachment 3 Supplemental Tool List). Paint components prior to assembly and touch up L-CBA once assembled.

3.1.2 Specified metals. Built with government specified metal alloys

a. An Astralloy-V plate 4.75”x37”x193” used for the CX1907004 blade.

b. A514 Steel Plate

c. A53 Steel Bar

d. A500 Steel Stock

e. A500 Tubing

3.1.3 Comply with ISO Standard. Large clearance blades must attach to government armored front end loader, NSN: 3805-01-686-4441 using International Organization for Standardization (ISO) 23727:2009 hydraulic quick coupler with cab mounted hydraulic attachment pressure release function. Couplers will be delivered under separate contract with the armored loader manufacture.

3.1.4 Schedule, Data Items, and Other Deliverables.

3.1.4.1 Schedule For Fully Procured REHM L-CBAs. The contractor shall commence work immediately After Receipt of each Order (ARO). The contractor shall provide production schedule plans first article for review and approval not later than 90 calendar days ARO. Once an L-CBA order is assembled the contractor shall submit an element for review and approval, and once approved, shall complete shipment of procured additional L-CBAs in accordance with Table 1. The Government requires up to a maximum of 14 calendar days to inspect and approve the submissions.

3.1.4.2 The contractor shall commence work immediately After Receipt of each Order (ARO). The contractors shall provide an estimated delivery timeline for each order.

3.1.4.3 Inspections Locations. The Government may provide on-site inspections based on the contractor’s production completion schedules. Inspections will be completed or waived by the Government prior to any L-CBA and/or items shipped. Inspections may take up to one work day to complete, per L-CBA; and include inventory of all end items and packaging. The contractor shall coordinate with the AFCEC Technical Advisors identified in Paragraph 3.1.8 for scheduling all inspections.

3.1.4.4 Inspection Details. Specific inspection details will be outlined in each Delivery Order issued against the contract.

3.1.4.5 Data Items. The contractor shall submit complete Safety Data Sheets on hazardous materials (if applicable) with the L-CBAs no later than 30 calendar days ARO to the Technical Advisors identified in Paragraph 3.1.8

3.1.4.6 Weekly Status Report. The contractor shall provide, per task order, weekly status of shipped, delivered and delivery schedules to Technical Advisors outlined in Paragraph 3.1.8. The first report shall be due seven (7) calendar days ARO and no later than 1200 CST every Monday thereafter until all deliveries are completed.

Table 1. Production and Shipment timelines

*Will be coordinated per task order

3.1.5 Packaging. The contractor shall develop a customized packaging solution for worldwide shipment and protection of the blade from the elements. Packaging shall be designed to allow heavy equipment operators to pick up and remove the blade from the packaging solution and replace it for environmental storage. (e.g. custom crating or acquiring and customizing ISO side opening shipping containers).

3.1.6 Shipment. Ship to specified destinations defined in attachment 4.

3.1.6.1 First article inspection. Obtain government physical configuration audit blade assembly inspection prior to full rate production and shipment L-CBA(s).

3.1.6.2 Loading and unloading. The Contractor shall load and unload all REHM L-CBAs, sub-kits, or individual items at their origin and at each destination (door to door). The contractor shall provide all equipment, manpower, tools, and vehicles to perform all product loading and unloading. The contractor shall offload all REHM L-CBAs in their packaged shipping/environmental protection containers, from shipping truck/containers at destinations and deliver to the installation final location per each Point of Contact (POC).

3.1.6.3 Deliveries. Deliveries under this contact are to Main Operating Base (MOB) or Forward Operating Base (FOB) destinations. The contractor shall employ packaging and shipping techniques to preclude any damage from rough transport either by land, sea, or air. The contractor shall be responsible for expenditures associated with damage incurred during shipping to include on-site repairs or replacement of damaged items. The contractor shall provide all product loading at the origin and all product offloading at the destination (door to door) as outlined above.

3.1.6.4 ISO Container Serial #s (IF APPLICABLE TO THE PACKAGING SOLUTION). The Government will provide applicable container control numbers (USFU #s) for all purchased ISO containers and track all information in the Joint Container Management System (JCMS). Contractor shall follow the specifications in the Defense Transportation Regulation – Part VI, Chapter 603, dated March 2015. The contractor shall contact the Technical Advisors identified in Paragraph 3.1.8 for assistance.

3.1.6.5 Destination POC. The contractor shall contact the applicable installation POC prior to shipment to give the installation a formal notification of an upcoming delivery and to verify the delivery address. The POCs and shipping addresses will be identified in each Delivery Order issued against the contract. The contractor shall also provide product and/or delivery schedule information to specified Technical Advisors in Paragraph 3.1.8.

3.1.6.6 External Tracking. The contractor shall make available to the Government all automated tracking information employed by the shipping agencies (i.e., web-based search engines, posted manufacture spreadsheets, etc.).

3.1.6.7 Shipping Cost. Firm fixed pricing will be negotiated on an order by order basis in accordance with the contract ordering procedures.

3.1.7 REHM L-CBA Components Verification

3.1.7.1 Classification of Inspections of REHM L-CBAS components. The inspection requirements specified herein are classified as follows:

· First article inspection.

· Conformance inspection.

3.1.7.2 First Article Inspection. The purpose of this inspection shall be to determine REHM L-CBA’S conformity with the contract. Acceptance of the First Article inspection shall not constitute a waiver by the Government of its rights under the provisions contract document or relieve the manufacturer from any requirements defined in this specification. Failure to meet inspection criteria shall constitute cause for rejection.

3.1.7.3 Conformance Inspection. The conformance inspection shall be conducted on all REHM L-CBAs prior to the vendor shipping the REHM L-CBAs.

3.1.8 AFCEC Technical Advisors

Attachment 1. Draft Design Specifications (final SOW will include complete TDP)

Attachment 2. Draft Assembly Build Supplement

Attachment 3. Draft Supplemental Tool Listing for Build

Locations

Tyndall AFB, Florida

Guam

Korea

Japan

Qatar

Kuwait

United Arab Emirates

Oman

Italy

Germany

United Kingdom

Spain image1.emf

0.

SHEET 1 OF 3

A2

WEIGHT:

A A

B B

C C

D D

E E

F F

G G

H H

DRAWN

CHK'D

APPV'D

SCALE:1:50

DWG NO.

TITLE:

REVISIONDO NOT SCALE DRAWING

MFG

Q.A

LINEAR:

ANGULAR:

FINISH:

TOLERANCES:

EDGES

NAME SIGNATURE DATE

MATERIAL:

UNLESS OTHERWISE SPECIFIED:

DIMENSIONS ARE IN INCHES

SURFACE FINISH:

DEBURR AND

BREAK SHARP

CX_1907000 Views

Distribution D Statement - Distribution authorized to Department of Defense & U.S. DoD Contractors only - (Administrative and Operational) (6 January 2020). Requests for this document must be referred to AFCEC-CXAE, 139 Barnes Drive, Suite 2, Tyndall AFB 32403

83.29

198.92

Draf t W ork ing

D oc um en t

DO NOT SCALE DRAWING

CX_1907000

Assembly

SHEET 1 OF 12

SCALE: 1:50 WEIGHT:

REVDWG. NO.

C

SIZE

NAME DATE

COMMENTS:

Q.A.

MFG APPR.

ENG APPR.

CHECKED

FINISH

MATERIAL

INTERPRET GEOMETRIC

TOLERANCING PER:

FRACTIONAL

ANGULAR: MACH BEND

TWO PLACE DECIMAL

THREE PLACE DECIMAL

APPLICATION

USED ONNEXT ASSY

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS

DRAWING IS THE SOLE PROPERTY OF

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

UNITED STATES AIRFORCE IS

PROHIBITED.

ITEM NO. PART NUMBER DESCRIPTION QTY.

11 CX_1907004 Blade Body 1

79 6 x 6 pine timber 6" x 6" x 36" 6

ITEM NO. PART NUMBER DESCRIPTION Default/

QTY.

21 CX_1907010 Tie Down Assembly 4

33 CX_1907007-A Shoe

Assembly0

SHEET 2 OF 12

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

ITEM NO. PART NUMBER DESCRIPTION Assembly1/QTY.

1 CX_1907002 Pipe Mount 1

2 CX_1907036-A 3QTR

ATTACHMENT SHIM 2

3 CX_1907001 Loader Interface 1

Use half & quarter inch shim (ref

CX_1907036-ABC)

as necesary for least clearance between parts assemblies and shims shown

SHEET 3 OF 12

SCALE: 1:20 WEIGHT:

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

2 2

SHEET 4 OF 12

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

ITEM NO. PART NUMBER DESCRIPTION Assembly 1/QTY.

2 CX_1907006 Small Support Pipe 1

24 CX_1907005 Large

25 CX_1907002-B2

MOON BOLT PLATE 8

3QTR 6in ring pattern^As Built Blade

3.00 - stage 2A

Set of 6 Fastners 4

3QTR 7in ring pattern^As Built Blade

3.00 - stage 2A

Set of 6 Fastners 4

3131313131

313131313131

313131313131

30303030

3030303030

2525Draf

Assembly0

SHEET 5 OF 12

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

4 3QTR_Bolt_6IN_Set 3QTR_Bolt_6IN_Set 8 12 3QTR_Bolt_Set_7in 3QTR_Bolt_Set_7in 12

13 CX_1907024 LARGE

BLADE MOUNT 2

14 CX_1907023 SMALL

BLADE MOUNT 4

15 CX_1907016 BLADE

PIPE INTERFACE 4

Once Assemblies are bolted together use wheeled loader to pick up and set upright

ITEM NO. PART NUMBER DESCRIPTION Default/

QTY.

2 CX_1907006 Small

24 CX_1907005 Large

25 CX_1907002-B2

MOON BOLT PLATE 8

29 CX_1907001 Loader Interface 1

SHEET 6 OF 12

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

ONCE END COLLECTORS ARE

INSTALLED, BLADE CAN REMAIN

UPRIGHT ON FLAT SURFACE

WITHOUT THE WHEELED LOADER

BEING ATTACHED

BEND

Assembly1

SHEET 7 OF 12

NEXT ASSY

USED ON

FRACTIONAL

ANGULAR: MACH

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

14 CX_1907040 Left End

Collector 1

15 CX_1907029-2 Right End Collector 1

20 CX_1907040-F End Collector Wear Edge 2

13 12

Assembly1

SHEET 8 OF 12

PROPRIETARY AND CONFIDENTIAL TOLERANCING PER:

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

10 CX_1907027 CAGE

PLATE BRACE 2

12 CX_1907028 LEFT

CAGE BRACE END 1

13 CX_1907029 RIGHT

CAGE BRACE END 1

21 CX_1907010 Tie Down

11 CX_1907015 WELDED

HOLD DOWN 4

16 CX_1907036 CAGE

ASSEMBLY 2

17 CX_1907037 CAGE

STOP ASSEMBLY 4

Remove bolt and of the cage thread through bolt hole on end assemblies last Install Cage stop

Remove bolt on blade and thread through this bolt hole on end of the cage plate

Assembly2

SHEET 9 OF 12

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

SHEET 10 OF 12

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

8 CX_1907025 UPPER

BRACING ASSEMBLY 3

9 CX_1907026 HOIST

PLATE 1 2

18 CX_1907020 DELTA

DEFLECTOR 1

CX_1907014

ADJUSTABLE

DEFLECTOR

22 3QTR_PIN_W_HAND

LE 3QTR_PIN_W_HANDLE 7

28 3QTR_Bolt_Set_3in 19

29 3QTR_Bolt_Set_7in 3QTR_Bolt_Set_7in 8

2828282828

All Fasteners #28

SHEET 11 OF 12

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

Paint Application

Primer application:

Individual sub-assemblies are to be primed after welding and cleaning. Primers are to satisfy MIL–PRF–23377 or MIL–PRF–85582. rotating components of caster wheels.

Protective coating and color coat application:

Individual sub-assemblies are to be coated prior to assembly. Protective coating is to satisfy MIL–DTL–53039 or MIL–PRF–85582. Ask customer for desired color top coat. Once LCBA is fully assembled, apply a final touch-up coat

Follow manufacturer application instructions

SHEET 12 OF 12

FRACTIONAL

ANGULAR: MACH BEND

UNITED STATES AIRFORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

36.00

48.00

1/32"

REPRODUCTION IN PART OR AS A WHOLE

2 1

WEIGHT: DO NOT SCALE DRAWINGPROHIBITED.

Blade Lift

SCALE: 1:100 SHEET 1 OF 1

B

UNITED STATES AIR FORCE IS

WITHOUT THE WRITTEN PERMISSION OF

0.5 DEG

UNITED STATES AIR FORCE. ANY

Distribution D Statement - Distribution authorized to Department of Defense & U.S. DoD Contractors only - (Administrative and Operational) (6 January 2020). Requests for this document must be referred to AFCEC-CXAE, 139 Barnes Drive, Suite 2, Tyndall AFB 32403

Each Wear-Resistant Twisted-Eye Web Sling Shackle - 2,000lb vertical lift capacity

46.56

Blade Tie Down

SCALE: 1:100 SHEET 1 OF 1

0.5 DEGANGULAR: MACH

CX_1907014 - QTY 4

CX_1907006 - QTY 1

CX_1907040 - QTY 1CX_1907029-2 - QTY 1

CX_1907015 - QTY 2

CX_1907010 - QTY 2

CX_1907040-F - QTY 2

CX_1907005 - QTY 1

CX_1907007 - QTY 4 CX_1907037 - QTY 4

CX_1907012 - QTY 2

DATE

SCALE:1:20 SHEET 1 OF 1

A3

REVISION

SIGNATURENAME

FINISH:UNLESS OTHERWISE SPECIFIED:

CX_1907000 SPARE PARTS

Part A

Part B

Threaded Bolt Washer

Lock-washer bolt

Each fastener set within the drawings consists of a bolt, washer, lock-washer & nut. Bolts heads face the collection area unless otherwise indicated

SECTION A-A

SCALE 1.5 : 1

DWG. NO.

CX_1907000_Fastener_information

SHEET 1 OF 3DO NOT SCALE DRAWING

REV

SCALE: 1:2

A

SCALE:1:10

FRACTIONAL: 1/32"

Next Assembly CX_1907001 Loader Interface

SHEET 1 OF 3

ANGULAR: 0.05 Deg

Used On

TOLERANCES: EDGES

DO NOT SCALE DRAWING REVISION

DEBURR AND UNLESS OTHERWISE SPECIFIED:

10 10

1 CX_1907001-A HOOK

REINFORCEMENT 4

CX_1907001-B

ISO23727 COUPLER

PLATE

3 CX_1907001-C

BRACE TUBING 2

CX_1907001-D

VERTICAL BRACE

CHANNEL

CX_1907001-E

ANGLED BRACE

CX_1907001-E2 REV

ANGLED BRACE

7 CX_1907012 HEAVY

DUTY CASTER 2

8 CX_1907001-F

CASTER PLATE 2

CX_1907001-G

HORIZONTAL BRACE

10 CX_1907001 5-8THS x

1&HALF ROD 2

.375

.25

TOLERANCES:

FINISH: DEBURR AND

SCALE:1:10 SHEET 2 OF 3

CX_1907001 Loader InterfaceNext Assembly

.375 .375

.375 .375

.375.375

.375.25

0.025 0.025

0.025

0.025

TOLERANCES:

SCALE:1:10 SHEET 3 OF 3

CX_1907001 Loader InterfaceNext Assembly

.4

5.50

20.64

10.38

30.75 39.25

4.25 27.75

41.50

0.50

41.00

CX_1907001-B

ISO23727 COUPLER

PLATE

CX_1907001-A

HOOK

REINFORCEMENT

2QTY

CX_1907001

Chamfer hole depth 45Degrees @ 1/2"

.5

Next Assembly detail

CX_1907001-AA Plate support weld

SCALE:1:5 SHEET 1 OF 1

to coupler plate Grind weld flush to coupler plate Grind weld flush

0.5

1.25

.1

.6

2.72

1.72

5.43

CX_1907001-AA

4QTY

T1 (A514)

Next Assembly CX_1907001-B Hook Reinforcement

SHEET 1 OF 1

SCALE:2:1

R2.19

R6.88 R

1.

R1.34

All Measurements relative to part center unless otherwise indicated

.3

15.23

Chamfer hole 45 degress - 1/4" depth each side

.0

12.25 5.00

2.

12.10

170.14°

12.10

12.85

4.

2.00

.7

5 5 .2

12.74°

14.85

6.

9.

9.72

7.

.8

15.13

Next Assembly CX_1907001-B ISO23727 PLATE

SHEET 1 OF 2

SCALE:1:5

3.37

3.59

5.

24.68

TOLERANCES:

SCALE:1:5 SHEET 2 OF 2

CX_1907001-B ISO23727 PLATENext Assembly

All measurements relative to bottom-left corner unless otherwise indicated

6.75 20.75

0 3.10 3.10

27.55

R1.24

R1.67

5.25

R3.38

0.8

2.0

R1.40

3.

25.80

CX_1907001-C BRACE TUBING

A53 or greater low-carbon steel

3" x 3" Square rod

3.00

41.00

CX_1907001-D VERTICAL BRACE

24.00

3" x 3" x 0.25" 90 Degree Steel Channel

70° ±0.05°

20° ±0.05°

4.37 24.31

25.31

0.42

3" x 3" x 0.25" 90 DEGREE STEEL CHANNEL

CX_1907001-E ANGLED BRACE

3" x 3" x 0.25" 90 Degree Steel Channel

CX_1907001-E2 REV ANGLED BRACE

24.89

25.31

1.00 20.94

20° ±0.05°

Half inch plate

Next Assembly CX_1907001-F Caster Plate

SHEET 1 OF 1WEIGHT: SCALE:1:2

0.6

0.69

9.00

8.00

Next Assembly CX_1907001-F2 QTR INCH SHIM

SCALE:1:2WEIGHT:

Quarter inch plate

Next Assembly CX_1907001-F3 HALF IN SHIM A2Q.A

SCALE:1:2

Half inch plate

3" x 3" 90 Degree Steel Channel

CX_1907001-G HORIZONTAL BRACE

SCALE:1:2 SHEET 1 OF 1

0.63

SCALE: 2:1 SHEET 1 OF 1

CX_1907001-H 5-8THS

x 1&HALF ROD

Chamfer 45 Degrees - 1/4" depth both ends

1.50

Next Assembly CX_1907002 Pipe Mount

SHEET 1 OF 2WEIGHT: SCALE:1:10

1 CX_1907002-A

STABILIZER 3

2 CX_1907002-B Pipe Mount 2

3 CX_1907002-B2

MOON BOLT PLATE 4

4 3QTR_Bolt_6IN_Set 3QTR_Bole_6IN_Set 24

5 CX_1907022 HOIST

PLATE 2 2

CX_1907000CX_1907000

SCALE 1 : 5

VIEW A

42.45 min.

Next Assembly CX_1907002 Pipe Mount

SHEET 2 OF 2

CX_1907002-A STABILIZER

SHEET 1 OF 1SCALE:1:10

Solid Rod3QTY

A500 Grade BCX_1907002

2.375

46.45

6.93

.9

6.93

16.16

26.64

8.

23.33

2 QTY

2.71

6.92

28.00

4.93

3.11

3.52

5.20

34.30

2.11

3.86

1.40

7.00

21.00

13.84

16.75

32.39

6 24.32

14.00

1.40

CX_1907002

Next Assembly CX_1907002-B Pipe Mount Plate

SHEET 1 OF 4

3.40

3.40

22.5

45°

90°

3°

45°Typical

Next Assembly CX_1907002-B Pipe Mount Plate

SHEET 2 OF 4

111.33°

10.81°

R3.40

50.52°

R1.00

3.11

R3.40

7.50

TOLERANCES:

SCALE:1:5 SHEET 3 OF 4

CX_1907002-B Pipe Mount PlateNext Assembly

2.57

0.80 0.80 0.80 0.80

0.80 0.80 0.80 0.80

0.9

R2.29

TOLERANCES:

SCALE:1:5 SHEET 4 OF 4

CX_1907002-B Pipe Mount PlateNext Assembly

T1 (A514)CX_1907002

Cut from 2-inch thick steel plate

2.00 Draf

0.40

R3.75

0°

8.94

R2.29

3.88

R4.50

3.88

0.80

4.57

22.500°

Typical

SHEET 1 OF 1SCALE:1:2

CX_1907002-B2 MOON BOLT PLATE

Next Assembly CX_1907003-A BRACING RING

SCALE:1:1 SHEET 1 OF 1

3.7

2.93 stock down with a lathe

16QTY

Waterjet from 1-inch thick steel plate Alternate - turn 3-1/2in sch 80 pipe

CX_1907005 & 06

96.00

72.00

Symetric drill pattern about the y-axis 192.00

TOLERANCES:

SCALE:1:20 SHEET 1 OF 5

CX_1907004 Blade BodyNext Assembly

An option is available to have material supplied pre-drilled from Astralloy

Y

X-Axis

Y-A x is

All Measurements relative to top left corner of material

Astralloy V CX_1907000 Sht 1

2.00

2.50

5.00

42.50 43.00 45.00

45.50

55.75 50.50 51.00

53.00

53.50 64.75 73.75

90.50 91.00

93.00 93.50

3.00 72.00

98.50 99.00

101.00

118.25

120.00 127.25

136.25 138.50

139.00 141.00

141.50

146.50

147.00 149.00

149.50

168.00 186.50 187.00 189.00

189.50

190.00 101.50

An option is available to have material supplied pre-drilled from Astralloy

Y

CX_1907000 Sht 1

TOLERANCES:

SCALE:1:20 SHEET 2 OF 5

98.50 99.00

101.00

118.25

120.00 127.25

136.25 138.50

139.00 141.00

141.50

146.50

147.00 149.00

149.50

168.00 186.50 187.00 189.00

189.50

190.00 101.50

TOLERANCES:

SCALE:1:20 SHEET 3 OF 5

CX_1907000 sht 1

TOLERANCES:

SCALE:1:20 SHEET 4 OF 5

CX_1907000 sht 1

96.00000 95.96875

96.00000 95.96875

±0

Drill Pattern is symetric about center of material

TOLERANCES:

SCALE:1:20 SHEET 5 OF 5

document must be referred to AFCEC-CXAE, 139 Barnes Drive, Suite 2, Tyndall AFB 32403 CX_1907000 sht 1

Next Assembly CX_1907005 Large Support Pipe

SCALE:1:20 SHEET 1 OF 2

EXTERIOR COMPONENTS

222 2

1 CX_1907003-A1 Long support pipe 1

2 68095K352 CX_1907034 PIPE FLANGE 4

3 CX_1907003-A2 Long

4-INCH PIPE 1

4 CX_1907003-A

Bracing Ring 9

1 INTERIOR COMPONENTS

4444444 44

NOTE: ORIENTATION OF PIPE FLANGES IS CRITICAL TO BLADE ASSEMBLY

Do not weld this side of flange Do not weld this side of flange

EXTERIOR COMPONENTS

neck side neck side neck side neck side

88.68

7.25

72.32

23.61

See DWG CX_1907034 for additional flange details

.25 .25

INTERIOR COMPONENTS

.25.25 .25.25 .25 .25 .25 .25

82.20 95.00 12.60 24.20 35.80 47.40 59.00 70.60

Next Assembly CX_1907005 Large Support Pipe

SCALE:1:20 SHEET 2 OF 2

SCALE:1:20

CX_1907005-A1 Long support pipeNext Assembly

WEIGHT: SHEET 1 OF 1

1QTY

CX_1907005

2.3

2.875

Schedule 80 2-1/2-inch seamless pipe

A500 Grade B

Schedule 80 4-inch seamless pipe

CX_1907005 Q.A

CX_1907005-A2 Long 4-INCH PIPENext Assembly

4.500

3.826

TOLERANCES:

SCALE:1:50 SHEET 1 OF 2

CX_1907006 Small Support PipeNext Assembly

1 CX_1907034 4-INCH

SLIP ON FLANGE CX_1907034 PIPE FLANGE 4

CX_1907006-A2

SMALL

REINFORCEMENT

PIPE

CX_1907003-2 Short inner bracing assembly

4 CX_1907006-A SHORT

CROSS PIPE 1

Interior components333 33333

Exterior Components

Do not weld this side of flangeDo not weld this side of flange neck sideneck side neck side neck side

.25.25

78.00

6.88 14.28 63.10 70.50

TOLERANCES:

SCALE:1:50 SHEET 2 OF 2

CX_1907006 Small Support PipeNext Assembly

See DWG CX_1907034 for additional flange details

.25 .25 .25 .25.25.25.25 .25

6.40 18.00 29.60 41.20 52.80 64.40 77.00

Schedule 80 4-inch seamless pipe

WEIGHT: SHEET 1 OF 1

CX_1907006-A SHORT CROSS PIPE

4.500

3.826

2.875

2.323

SHEET 1 OF 1SCALE:1:10

DWG NO.Q.A

CX_1907006-A2 SMALL

REINFORCEMENT PIPE

Schedule 80 2-1/2 inch seamless pipe

0.57

1.75

.2

0.90 4

3.52

3.95 0.10

4.48

1.35

0.67

0.75

5.15

3.59

0.90

T1 (A514) - A53 Alternative

CNC Construction

CX_1907007-A

Next Assembly CX_1907007 Wear Shoe

SHEET 1 OF 4

30°

30°

240°

60°

5°

CNC Construction

Acceptible short by 1/16th inch Length 48.00in (no longer)

DATE

BREAK SHARP REVISIONDO NOT SCALE DRAWING

SCALE:1:10 SHEET 2 OF 4

CX_1907007 Wear ShoeNext Assembly

NAME SIGNATURE

ANGLED VIEW (BOLTS NORMAL PROJECTION)

1.7 5T yp ical

0.90Typ ical

FRONT VIEW

45.50

43.00

5.00

45.00

42.50

SCALE:1:10 SHEET 3 OF 4

SHEET 4 OF 4

73 CX_1907007 Wear Shoe 1

74 3QTR_Bolt_6IN_Set 3QTR_Bole_6IN_Set 9

CX_1907007-A Shoe Assembly

SCALE: 1:10 WEIGHT:

FRACTIONAL

ANGULAR: MACH BEND

DRAWING IS THE SOLE PROPERTY OF

UNITED STATES AIR FORCE. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

0.25

CX_1907000 sht 10

1 CX_1907010-A AUX

PLATE 1

2 CX_1907010-B EYE

PLATE 1

3 CX_1907010-C

gussett 2

CX_1907010-C chamfer angle for both pieces

QTY 4QTY 4

REVISION

CX_1907010 Tie Down AssemblyNext Assembly

SCALE:1:2

CX_1907010

8 QTY

Next Assembly CX_1907010-A AUX PLATE

SCALE:1:1 SHEET 1 OF 1

3.00 5.00

R0 .38

3.5

2.62

R3.00

6.00

A SECTION A-A

SCALE:1:1WEIGHT:

CX_1907010-B EYE PLATE

4QTY

CX_1907010

Next Assembly CX_1907010-C GUSSET

SCALE:2:1 SHEET 1 OF 1

0 4.00

58°

4.72

2°

1.32

7.75

DUTY CASTER

SCALE: 1:5 WEIGHT:

CX_1907012 HEAVY

5.00 5.00

14.25

8.50

6.00

1.70

0 44.00

14.00 10.00 14.00

20.00 30.00

Next Assembly CX_1907014 ADJUSTABLE DEFLECTOR

R1.70

R1 .70

50.00

R1.70

1.7

0.80Typical

50.00

Short end of

CX_1907015-

A to bottom

A SECTION A-A

SCALE 1 : 2

73 CX_1907015-A - CAGE

HOLD BACK 1

74 CX_1907015-B - CAGE

HOLD CLIP SIDE 2

CX_1907000 sht

WITHOUT THE WRITTEN PERMISSION OF HOLD DOWN

SCALE: 1:5 WEIGHT:

CX_1907015 WELDED