Appendix C1 - FRP Anchor Kit Drawings.pdf

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Attached to
Fiber-Reinforced Polymer (FRP) panel kits in support of the USAF Airfield Damage Repair Program
Solicitation number
FA8051-26-R-FRPPanelKits
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About this file

This document is a technical drawing package for the Tri-Talon Pavement Anchor System, containing detailed engineering specifications for multiple components. The drawings include technical schematics for an Anchor Bushing, Joining Bushings, Tri-Talon Anchor System, Tri-Talon Set Tool, and shipping crate designs (Crates A, B, and C). Key technical details include material specifications (primarily 1045 steel, 1020 DOM, and 1215 steel), precise dimensional measurements with tolerances of ±0.005 inches, and specific manufacturing requirements such as gold plating per AMS QQ-P-416 Rev F and hydrogen embrittlement release treatments.

The document is part of a federal contract opportunity for Fiber-Reinforced Polymer (FRP) panel kits supporting the USAF Airfield Damage Repair Program, with a Distribution Statement B limiting access to U.S. Government agencies and contractors. The drawings are dated January 2024 and were created by the Department of the Air Force Civil Engineer Center at Tyndall AFB, Florida. The technical drawings provide comprehensive manufacturing specifications for each component, including material types, dimensional tolerances, surface treatments, and assembly instructions, which would be critical for potential manufacturers responding to the sources sought announcement.

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1.50 IN

0.42 IN

0.83 IN

0.10 IN

4.00 IN 2.63 IN 2.13 IN

0.21 IN

0.63 IN

0.06 IN R

0.06 IN R

Ø Ø

A

A

SECTION A-A

NOTES:

1. ALL DIMENSIONS ARE IN INCHES. ALL

TOLERANCES ARE ±0.005

2. MADE FROM 1045 STEEL.

3. PLATED PER AMS QQ-P-416 REV F, TYPE II,

CLASS 2, GOLD HYDROGEN EMBRITTLEMENT

RELEASE. TREATED AS PER AMS QQ-P-416

REV F.

4. BREAK ALL SHARP CORNERS AND REMOVE

ALL BURRS.

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AIR FORCE CIVIL ENGINEER CENTER

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DEPARTMENT OF THE AIR FORCE

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TYNDALL AFB, FL 32403-5319

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TITLE

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ANCHOR BUSHING

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SIZE

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SHEET NO.

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DRAWN BY

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DATE

AutoCAD SHX Text Distribution Statement B. Distribution authorized to U.S. Government agencies Performance Evaluation, 15 January 2024. Other requests for this document must be referred to AFCEC/CXXM or 772 ESS, 139 Barnes Drive, Suite 1, Tyndall Air Force Base, FL 32403-5323.

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JANUARY 2024

Distribution limited to US Government agencies and their contractors; critical technology.

0.500 IN

0.375 IN

3.000 IN

2.125 IN

Ø 0.261 IN

R 0.250 IN

0.055 IN

2.500 IN

R 0.500 IN

2 plc.

33.00°

Talon Material: 1018

0.375 IN X 0.500 IN

flatbar, 3 ea.

0.160 IN 45 deg chamfer, 2 plc.

0.380 IN

120.00°

0.750 IN

Drilled for 0.250 IN x 1.0 IN roll pin, 3 plc. center of drilled hole from center of part is 0.687 IN.

Drilled 21 32 IN and threaded

4 IN-10 B7 U.N.C. (R.H.) tap

1.250 IN

Ø1.935 IN

0.750 IN

0.510 IN 0.250 IN

0.060 IN chamfer

3 plc.

Tri-Talon Body Material: 1215

2.00 IN round x 1.50 IN, 1 ea.

4 IN x1 IN spring pin, McMaster Carr #95755A404 or equivalent, 3 ea.

1.50 IN

4 IN-10

B7 R.H.

1.875 IN 1.50 IN

8 IN-11

U.N.C.

1.625 IN

5.0 IN ± .05

.50 IN

Tap 34 IN-10 B7 (R.H.)

Tap 58 IN-11 U.N.C. 2B

Tap drill

32 IN ± .005

32 IN Dia.

Tap drill

32 IN ± .005

Notes:

8 IN -11 U.N.C. SAE J429 Grade 5 Type 1 hex bolt with min 11

2 IN thread length

(1) bolt per coupling shipped threaded into coupling

4 IN-10 x 24 IN GRB7 threaded rod

(1) threaded rod per coupling.

shipped threaded into coupling and talon assembly

Special Coupling Material: 11

4 IN O.D. - GRB7 (R.H.)

4 IN - 7 GRB7 (R.H.) couple 34 IN -10 GRB7 (R.H.) to 58 IN -11 U.N.C.

3.00 IN

1.50 IN

0.06 IN Chamfer

R 0.391 IN

0.06 IN

Chamfer

Notes:

1. Tolerances unless otherwise specified: xx ± .01, .xxx ± .005

2. The 15

16 IN hex on the special coupling must accept a 15 16 IN standard socket

3. The Talon, coupling, bolt, threaded rod, and retaining ring should be assembled prior to shipment

4. The 3 4 IN -10 x 24 IN threaded rod will thread into the coupling on one end and the talon on the opposite end

5. The 5 8 IN-11 x 3 IN bolt should be threaded into coupling

6. Talons should be installed so they fold with tips pointing toward the coupling

7. A rubber band or other device should be used to hold the talons in place

8. The retaining ring should be installed approximately 3 8 IN from the end of the 3 4 IN threaded rod to prevent the tri-talon body from backing off after installation

9. All parts should be lubricated to prevent rust formation during storage

10. All machined edges should be deburred

TALON TRI-TALON BODY

SPECIAL COUPLING

0.050 IN chamfer

R .030 IN

typ 6 plc.drill point allowed beyond required dimension

Note:

Add weld stop; 8-inch from the end of the rod, to stop the talons from walking up the all-thread

16 IN HEX

Bill of Materials for Each Tri-Talon Anchor System

Item Material Description Qty

1 1018 0.375 IN x 0.500 IN flat bar 3 2 1215 2.000 IN x 1.500 IN round 1

3 1 4 IN spring pin

4 IN x 1 IN McMaster Carr

#95755A404 or equiv. 3

4 5 8 IN GR5 bolt

8 IN -11 x 3 IN Grade 5

Type 1 hex bolt with 11

2 IN

thread

5 11

4 IN GRB7

threaded rod 1 1/4 IN-7 x 5 IN GRB7 threaded rod 1

6 3/4 IN GRB7

threaded rod

3/4 IN-10 x 24 IN GRB7 threaded rod 1

3/4 IN retaining ring

E-style external retaining ring, black-finish steel, fits 3/4 IN dia. shaft, ring size 1.00 IN dia. and .050 IN thick

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AIR FORCE CIVIL ENGINEER CENTER

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DEPARTMENT OF THE AIR FORCE

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TYNDALL AFB, FL 32403-5319

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TITLE

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TRI-TALON PAVEMENT

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ANCHOR SYSTEM

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SIZE

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SHEET NO.

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DRAWN BY

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DATE

AutoCAD SHX Text Distribution Statement B. Distribution authorized to U.S. Government agencies Performance Evaluation, 15 January 2024. Other requests for this document must be referred to AFCEC/CXXM or 772 ESS, 139 Barnes Drive, Suite 1, Tyndall Air Force Base, FL 32403-5323.

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NTS

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42.250 IN

0.125 IN Chamfer typ.

0.250 IN

1.250 IN

1.500 IN

0.125 IN X 45 TYP.

Ø1.935 IN

Ø 0.875 IN

3.000 IN

0.156 IN X 45

0.125 IN X 45

Anchor Drive Tube Material: 1020 DOM

1.25 IN x 0.1875 IN wall x 42.25 IN

1 ea.

Anchor Driver Head Material: 1215

2.00 IN Round x 3.00 IN

1 ea.

Anchor Spreader Material: 1215

2.00 IN Round x 3.00 IN

1 ea.

90° IN

8 IN (316 IN)

45° IN

8 IN (316 IN)

1.500 IN 1.250 IN 7.592 IN 3.000 IN

13.342 IN

Tri-Talon Set Tool Assembly

Ø 0.875 IN

Ø 1.25 IN

N.T.S.

N.T.S.

Ø 1.935 IN Ø 1.250 IN

Ø 0.875 IN

Notes:

1. The Tri-Talon Set Tool should be welded using standard practices to complete the tool assembly

2. The exterior of the Tri-Talon Set Tool should be primed and painted with a high quality paint for protection against rust formation.

3. The paint color should be a medium (battle ship) gray.

Bill of Materials for Each Tri-Talon Set Tool Item Material Description Qty.

1 1020 DOM 1.250" x .1875" wall x 42.250" 1 2 1215 2.000" round x 3.000" 2

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AIR FORCE CIVIL ENGINEER CENTER

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DEPARTMENT OF THE AIR FORCE

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TYNDALL AFB, FL 32403-5319

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TITLE

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TRI-TALON PAVEMENT

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ANCHOR SET TOOL

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SIZE

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SHEET NO.

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DRAWN BY

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DATE

AutoCAD SHX Text Distribution Statement B. Distribution authorized to U.S. Government agencies Performance Evaluation, 15 January 2024. Other requests for this document must be referred to AFCEC/CXXM or 772 ESS, 139 Barnes Drive, Suite 1, Tyndall Air Force Base, FL 32403-5323.

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NTS

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29.00 IN

23.00 IN

20.00 IN

25.00 IN

4.00 IN

25.00 IN

29.00 IN

STENCIL FRONT SIDE:

1" BLACK INK

"[RESPECTIVE QUANTITY AND PART NUMBER]"

STENCIL ON TOP OF CRATE:

4" BLACK INK

"RETAIN FOR FUTURE USE"

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AIR FORCE CIVIL ENGINEER CENTER

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DEPARTMENT OF THE AIR FORCE

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TYNDALL AFB, FL 32403-5319

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TITLE

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CRATE A

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SIZE

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SCALE

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SHEET NO.

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DRAWN BY

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DATE

AutoCAD SHX Text Distribution Statement B. Distribution authorized to U.S. Government agencies Performance Evaluation, 15 January 2024. Other requests for this document must be referred to AFCEC/CXXM or 772 ESS, 139 Barnes Drive, Suite 1, Tyndall Air Force Base, FL 32403-5323.

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46.00 IN

24.00 IN

5.00 IN

6.00 IN 6.00 IN 4.00 IN

29.00 IN

STENCIL FRONT SIDE:

1" BLACK INK

"[RESPECTIVE QUANTITY AND PART NUMBER]"

STENCIL ON TOP OF CRATE:

4" BLACK INK

"RETAIN FOR FUTURE USE"

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AIR FORCE CIVIL ENGINEER CENTER

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DEPARTMENT OF THE AIR FORCE

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TYNDALL AFB, FL 32403-5319

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TITLE

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CRATE B

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SIZE

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SHEET NO.

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DRAWN BY

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DATE

AutoCAD SHX Text Distribution Statement B. Distribution authorized to U.S. Government agencies Performance Evaluation, 15 January 2024. Other requests for this document must be referred to AFCEC/CXXM or 772 ESS, 139 Barnes Drive, Suite 1, Tyndall Air Force Base, FL 32403-5323.

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49.00 IN

11.00 IN

12.00 IN 49.00 IN

5.00 IN

6.00 IN

2.00 IN

STENCIL ON TOP OF CRATE"

4" BLACK INK

"RETAIN FOR FUTURE USE"

STENCIL FRONT SIDE"

1" BLACK INK

"[RESPECTIVE QUANTITY AND PART NUMBER]"

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AIR FORCE CIVIL ENGINEER CENTER

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DEPARTMENT OF THE AIR FORCE

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TYNDALL AFB, FL 32403-5319

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TITLE

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CRATE C

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SIZE

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SHEET NO.

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DRAWN BY

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DATE

AutoCAD SHX Text Distribution Statement B. Distribution authorized to U.S. Government agencies Performance Evaluation, 15 January 2024. Other requests for this document must be referred to AFCEC/CXXM or 772 ESS, 139 Barnes Drive, Suite 1, Tyndall Air Force Base, FL 32403-5323.

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ANCHOR BUSHING_JAN 2024
Sheets and Views
11 X17
ANCHOR CRATE B_JAN 2024
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11 X17
ANCHOR CRATE C_JAN 2024
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11 X17
CRATE A_JAN 2024
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11 X17
TRI-TALON PAVEMENT ANCHOR SET TOOL
Sheets and Views
11 X17
TRI-TALON PAVEMENT ANCHOR SYSTEM
Sheets and Views
11 X17

File details come from the government source that posted it. Updated .