Attachment 2 - Fuselage WT Trailer Paint Package Drawings.pdf

Fuselage+WingsTails Trailer Parts and Assemblies 12 Aug 2024

P/N Set 1 Qty Material Pretreat Prime Topcoat 20141254-10 1 20141276-10 2 20141280-01 4 20141282-01 1 20141282-03 1 20141423-10 1 20141424-10 1 20141425-10 1 20141426-10 1 20141434-10 1 20141435-10 1 20141442-10 1 20141443-10 1 20141445-10 2 20141446-10 2 20141447-01 4 20141448-01 4 20141449-01 2 20141450-01 2 20141450-03 2

201443204-10 1 201443205-10 1 201443208-01 2 201443209-01 2 201443209-03 1 201443209-04 1 201443210-01 2 201443211-01 2 201443212-01 2 201443212-03 2 201443214-10 1 201443218-01 1 201443222-01 2 201443228-10 6 201443229-10 1 201443235-01 1 201443236-01 2 201443238-01 1 201443239-01 1 201443240-01 2

Description of Work

Aluminum

MIL-C-5541

Class 1A

MIL-PRF-23377

Type 1

MIL-PRF-85285

Type 1, FED-STD- 595 Color 26173

Bill/Ship to:

AFLCMC/EZPAA

5215 Thurlow Rd

WPAFB, OH 45433

Contact:

Brett Baver

937-257-7010 brett.baver.1@us.af.m

Fuselage+WingsTails Trailer Parts and Assemblies 12 Aug 2024

P/N Set 1 Qty Material Pretreat Prime Topcoat

20152203-10 1 20152209-10 1 20152212-10 1 20152216-01 1 20141397-10 1 20141302-10 1 20141315-10 1 20141330-10 1 20141331-01 3 20141333-10 2 20141335-10 2 20141336-10 2 20141341-10 1 20141345-10 1 20141347-10 1 20141354-01 3 20141435-03 2 20141360-10 1 20141362-10 1 20141369-10 1 20141383-01 1 20141383-03 1 20141385-10 1 20141389-01 2 20141394-01 1 20141395-01 1 20141281-01 2 20141378-10 20 20141381-01 3 20141384-01 1 20141384-03 1 20141413-01 4 20141414-10 4 20141418-10 4

201443219-01 2 201443219-03 2 201443248-01 4

Steel

TT-C-490 Type 1

OR

Zinc Rich Primer Mil-P-26915 and

Intermediate Primer MIL-P-

53030

MIL-PRF-23377

Type 1

MIL-PRF-85285

Type 1, , FED-STD- 595 Color 26173

ENGINEERING DRAWING LAYOUT B(PRO/ENGINEER, AFPTEF) COMPUTER GENERATEDPREVIOUS EDITIONS WILL BE USED.

FORM

AUG 72 1653AF

A�

B�

C�

D�

A�

B�

C�

D�

QUANTITY REQUIRED PER DASH NO. PARTS LIST

2X 45�$� X CHAMFER0.15

2X 0.6752X 0.150

2X 0.285

2X 0.685

( )1.50

( )0.50

1.94

1OF1SHEET1.000

SCALE

X20141450-03

DRAWING NO.A.F. CODE IDENT NO.

0B275

SIZE

B

BAR, STOP, CLAMP, SPAR

TITLE

U.S. AIR FORCE

R. L. MILLER

A.F. RELEASE

M. R. HARFF

A.F. AUTHENTICATION

M. P. BOZZUTO

ENG

A. J. RYBA

CHK

DR

CURRENT

CODE IDENT NO.

PROTOTYPE YY-MM-DD

AFPTEF PROJ NO. YY-P-000

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NOCODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

ALUMINUM BAR

6061-T6511 PER

ASTM B209

0.50 X 1.50

MATERIALS:

.XX�#�

.XXX�#�

0.03 0.015

0.5�$�

FRACTIONS DECIMALS ANGLES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

TOLERANCES ON

DISTRIBUTION STATEMENT D : DISTRIBUTION

AUTHORIZED TO THE DEPARTMENT OF DEFENSE

AND U.S. DOD CONTRACTORS ONLY;

ADMINISTRATIVE/OPERATIONAL USE;

18-MAY-2011. OTHER REQUESTS SHALL BE

REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY,

DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY

METHOD THAT WILL PREVENT DISCLOSURE OF

CONTENTS OR RECONSTRUCTION OF THE

DOCUMENT

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW ANSI/ASTM SI 10.

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT CFORM

JUN 75 1654AF

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

2.625

4.250

20.0�$�

R0.883 +0.005 -0.000

4X THRU0.323

+0.005 -0.000

0.060

2.000

2X 3.250

2X 2.000

5.750

2X 45�$� X

CHAMFER

0.06

2X 45�$� X

CHAMFER

0.13

THRU0.190

+0.004 -0.000

�x� 0.2500.375

R0.25

2X R0.19

0.738

0.525

0.38

1.375 +0.000 -0.030

( )0.250

2X 0.250

2X 1.000

1.375

2X 1.080

2.458

2X 0.750

2X 1.500 2X 0.750

2X 0.625

2X ( )0.500

R0.15

0.40

( )3.364 ( )1.771

( )1.375

1OF1SHEET0.50SCALE

201443210

DRAWING NO.AF. CODE IDENT NO.

SIZE

C

CLAMP, SPAR, LOWER

J. A. SULLIVAN

AIR FORCE RELEASE

AIR FORCE AUTHENTICATION

B. C. BAVER

L. M. GUMUCIO

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

SHOWN-01R

OPPOSITE -01-02L

APPLICATION

USED ONNEXT ASSEMBLY

20141251-10201443202-10

201444303-10

ALUMINUM

6061-T6511 PER

ASTM B221

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

MASK HOLES TO PREVENT FINISH FROM ENTERING HOLE SURFACES.

SECTION A-A

SEE SHEET 1, ZONE B2

2X DRILL AND TAP �x� 0.500

FOR #10-32 UNF HELICOIL

SECTION B-B

SEE SHEET 1, ZONE B1

2X 45�$� X 0.06

CHAMFER

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

2X THRU0.515

+0.010 -0.000

0.060

0.500

1.000

5.490

6.995

1.750

10.0�$�

15.0�$�

R0.883 +0.005 -0.000

7X R0.25

7.49

3.990

2X 45�$� X

CHAMFER

0.06

0.680 +0.010 -0.000

2X 1.413

0.135 +0.000 -0.005

2X 1.753

0.470

1.000

0.625

0.813

1.940

1.200 +0.010 -0.000

0.695

0.550 +0.030 -0.000

1.500 +0.010 -0.000

2X R0.13

( )0.500

1OF1SHEET0.50SCALE

201443211

SIZE

CLAMP, SPAR, UPPER

AIR FORCE RELEASE XX-XX-XX

L. M. GUMUCIO

CODE IDENT NO.

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

APPLICATION

USED ONNEXT ASSEMBLY

20141251-10201443202-10

201443203-10

ALUMINUM

6061-T6511 PER

ASTM B221

MATERIALS:

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

MASK HOLES TO PREVENT FINISH FROM ENTERING HOLE SURFACES.

DIMENSION APPLIES AT THE INTERSECTION OF SHARP CORNER CREATED

BY EXTENTION LINES FROM ADJACENT SURFACES. SEE EXAMPLE GRAPHIC

ON THIS DRAWING.

LIST OF CHANGES MADE SINCE DWG PACKAGE RELEASE:

1. CHANGED DESIGN COMPLETELY TO ACCOMODATE A ROD END; ELIMINATED QUICK PIN HOLE FOR

LOCK.

2. ADDED NECESSARY VIEWS TO DIMENSION PROPER NEW FEATURES.

3. ADDED NECESSARY FEATURES TO ALLOW FOR FULL FUNCTIONALITY OF THE

DESIGN CHANGE.

45�$� X 0.25 CHAMFER

SECTION A-A

SEE SHEET 1, ZONE C2

2X DRILL AND TAP �x� 0.500

FOR #10-32 UNF HELICAL

INSERT

EXTENSION LINE

DIMENSIONING

DIM1 DIM2

5 4

Plug 0.257" and 10-32 hole

A

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

A

A

B

B

2.550

2X 0.438

36.08

7.28

4.74

10.02

2X 4.12

2X 1.00

2X THRU0.500

+0.015 -0.000

2X 36.00

34.537

2X 110.0�$�

2X 152.0�$�

108.4�$�

161.6�$�

2X R0.38

4X R0.38

1.000

3.000

6.000

3X 1.000

3X 0.196 0.001

( ) TYP0.125

( )42.99

( )8.00( )12.81

( )2.41

( )2.41

( )4.87

( )7.04

1OF1SHEET0.25SCALE

201443238

SIZE

D

SHEET, CASE, LOWER

AIR FORCE RELEASE 18-08-17

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

BCB6/5/23 22A041A

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

MATERIALS:

ALUMINUM SHEET

5052-H32 PER

ASTM B209

1/8 THK

20141251-10201443237-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

VIEW B-B

NOTE:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

DIMENSION APPLIES AT THE INTERSECTION OF SHARP CORNER CREATED

BY EXTENTION LINES FROM ADJACENT SURFACES. SEE EXAMPLE GRAPHIC

A A

A

A

A

A

VIEW A-A

VIEW ROTATED 8�$� CLOCKWISE FOR CLARITY

2X

SCALE 0.13

VIEW A-A NEEDED FOR VIEW ARROWS

SECTION C-C

A

A

A

EXTENSION LINE

DIMENSIONING

DIM1 DIM2

4 4

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

A

A

B

B

2X 1.00

8.00

2X 36.40

36.48

7.00

3.270

33.130

10.98

2X 4.00

2X THRU0.500

+0.015 -0.000

2X 98.0�$�

161.6�$�

2X R0.38

2X R0.38

1.000

3.000

6.000

3X 1.000

3X THRU0.196 0.001

108.4�$�

3.00

( )43.13

( )12.09

( )2.04

( )2.04

( )0.125

( )3.98

1OF1SHEET0.25SCALE

201443239

SIZE

D

SHEET, CASE, UPPER

CODE IDENT NO.

PARTS LIST

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

BCB6/5/23 22A032A

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.03 0.015

.XX�#�

.XXX�#�

MATERIALS:

ALUMINUM SHEET

5052-H32 PER

ASTM B209

1/8 THK

20141251-10201443237-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

-01

NOTE:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

DIMENSION APPLIES AT THE INTERSECTION OF SHARP CORNER CREATED

BY EXTENTION LINES FROM ADJACENT SURFACES. SEE EXAMPLE GRAPHIC

A

A

A

A

A

A

A

VIEW A-A

VIEW ROTATED 8�$� COUNTERCLOCKWISE FOR CLARITY

2X

SCALE 0.13

VIEW A-A NEEDED FOR VIEW ARROWSSECTION C-C

A

A

VIEW B-B

EXTENSION LINE

DIMENSIONING

DIM1 DIM2

4 4 mask latch to prevent paint from entering latch plug all threaded holes no specifically marked

Plug end of tubes to prevent paint entering.

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

2OF1SHEET0.25SCALE

20141417_PAINT

SIZE

CASTER FOOT ASSEMBLY

CODE IDENT NO.

P A I N T

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

BCB6/5/23 22A045A

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10

-10-

1ASTM D5363 AN0321ADH_TLOCK_MSADHESIVE, THREAD, MED STRENGTH1

21/4-20 UNC X 1 LG, GRADE 8, ZINC PLATED STEELRHB024BOLT, REGULAR HEX2

33/8-16 UNC X 1-1/4 LG, GRADE 8, ZINC PLATED STEELRHB081BOLT, REGULAR HEX4

4S-WH-6SWC26935CASTER, SWIVEL1

51/4-20 UNC, 7/16 WD, 7/32 HT, GRADE 8, ZINC PLATED STEELRHN010NUT, HEX2

63/8-16 UNC, 9/16 WD, 21/64 HT, GRADE 8, ZINC PLATED STEELRHN012NUT, HEX4

7201443248-01PLATE, STOP, CASTER1

81/4 NOM, 11/16 OD, 0.05 MIN THK, ZINC PLATED STEELWA011WASHER, FLAT4

93/8 NOM, 13/16 OD, 0.05 MIN THK, ZINC PLATED STEELWA013WASHER, FLAT8

1020141418-10WELDMENT, FOOT, CASTER1

APPLICATION

USED ONNEXT ASSEMBLY

20141251-1020141252-10

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

A A REVISION REV STATUS

2 1 SHEET OF SHEETS

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. WELD PER AWS D1.1 WITH ER70S WELDING WIRE IAW AWS A5.18. AFTER WELDING,

ALL WELDS SHALL BE MECHANICALLY CLEANED WITH A STAINLESS STEEL WIRE

BRUSH, SANDING, GRINDING OR POLISHING AND THEN CHEMICALLY CLEANED

(I.E. ALCOHOL, ETC. ).

4. ANY HARDWARE LISTED IN THE PARTS LIST THAT HAS AN IDENTIFYING NUMBER WITHOUT A CAGE CODE SHALL BE CONSIDERED A COMMERCIALLY AVAILABLE PART. THE PART NUMBER IS AN ARBITRARY NUMBER ASSIGNED BY OUR IN-HOUSE CAD SYSTEM. THE PART DESCRIPTION IS CALLED OUT IN THE

MATERIAL/SPECIFICATION BLOCK OR IN A NOTE.

THIS ITEM SHALL BE CONSIDERED A BULK ITEM WITH QUANTITY OF "AS REQUIRED."

APPLY THREAD ADHESIVE (FIND NO. 1) PER MANUFACTURER'S RECOMMENDED PROCEDURE.

TORQUE VALUE FOR INSTALLATION OF 1/4-20 UNC HARDWARE SHALL BE 75 �#�3.0 LB-IN.

TORQUE VALUE FOR INSTALLATION OF 3/8-16 UNC HARDWARE SHALL BE 20 �#�0.8 LB-FT.

PRIOR TO PAINT, SET THE CASTER STOP PLATE (FIND NO. 7) IN FINAL POSITION.

TO ADJUST THE CASTER STOP PLATE, ATTACH THE ENTIRE CASTER FOOT ASSEMBLY

TO THE INNER JACK LEG OF THE HYDRAULIC JACK ASSEMBLY (PART NO. 20141298-10 (SHOWN) OR 20141299-10) AS SHOWN ON SHEET 2. ADJUST THE CASTER STOP PLATE SO THAT SURFACE WITH RADIUS IS TOUCHING THE INNER JACK LEG WITH THE CASTER FOOT ASSEMBLY SET AT 94.0�$� AS SHOWN IN DETAIL A. INSTALL HEX BOLT (FIND NO. 2), WASHER (FIND NO. 8), AND HEX NUT (FIND NO.

5) TO HOLD IN PLACE.

AFTER ADJUSTING THE CASTER STOP PLATE, TACK WELD TO LOCK IN PLACE.

REMOVE SWIVEL CASTER (FIND NO. 4), HEX BOLT (FIND NO. 3), WASHER (FIND NO. 9), AND

HEX NUT (FIND NO. 6) PRIOR TO PAINT. REINSTALL AFTER PAINT HAS BEEN APPLIED.

12. FINISH:

PRETREAT TT-C-490, TYPE I

ALTERNATIVE PRETREATMENT: PRETREAT USING ZINC RICH PRIMER PER

MIL-PRF-26915 AND INTERMEDIATE PRIMER PER MIL-DTL-53030.

PRIME PER MIL-PRF-23377 TYPE I CLASS C.

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595.

A

A

A

A

A

4X

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

6792X

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT C (CONTINUATION SHEET)FORM

B

A

C

D

B

A

C

D

6.03

94.0�$�

( )10.99

( )4.81

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

BCB6/5/23 22A045A

P A I N T

2OF2SHEET0.25SCALE

20141417_PAINT

SIZE

CASTER FOOT ASSEMBLY

SEE DETAIL A

SCALE 0.10

20141298-10 SHOWN IN THIS VIEW WITH CASTER FOOT ASSEMBLY

INSTALLED. SIDE GUSSETS OF CASTER FOOT WELDMENT

REMOVED FOR CLARITY

A

DETAIL A

SCALE 0.25

A

VIEW B

PROJECTED FROM DETAIL A

A

.25 0.50

Updated Drawings2