Gray Eagle RTS - RFQ EZPAA 2025-08-13.pdf

PDF 5 MB Posted Aug 21, 2025

Attached to: FA8604 MQ-IC RR Trailer Paint / Gray Eagle Trailers Federal contract opportunity
Solicitation number: FA860425QB005
Issued by: Department of the Air Force Materiel Command Lifecycle Management Center Wright Patterson Air Force Base

About this file

Written by GovTribe AI · Aug 21, 2025

This document is a series of engineering drawings and parts lists for various components of a Gray Eagle RTS (Readiness Test Set) assembly, dated 29 May 2025, for the U.S. Air Force. The drawings cover multiple assemblies including a trailer assembly, wing assembly, tail assembly, surrogate spar assembly, capture arm assembly, forward link assembly, forward saddle assembly, mid saddle assembly, upper lift assembly, and bracket for a screw jack.

The technical drawings specify detailed coating requirements using MIL-DTL-5541 pretreatment, MIL-PRF-23377 primer, and MIL-DTL-53039 topcoat in black color (37030 per SAE AMS-STD-595). Each assembly has specific masking and plugging instructions for various holes, surfaces, and components to ensure proper painting. The drawings are part of a prototype project (AFPTEF Proj No. 19-P-118) with multiple components for what appears to be an aerospace or defense system, likely related to the Gray Eagle unmanned aerial vehicle platform. The bill/ship-to address is AFLCMC/EZPAA at Wright-Patterson Air Force Base in Ohio, with a point of contact named Mike Harff.

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Other files for this federal contract opportunity

Other files attached to FA8604 MQ-IC RR Trailer Paint / Gray Eagle Trailers, newest first.
File	Type	Posted
QA Set 2 Paint Buy Solicitation FA860425QB005.pdf	PDF	Sep 3, 2025
QA Paint Buy Solicitation FA860425QB005.pdf	PDF	Aug 25, 2025
Solicitation - FA860425QB005.pdf	PDF	Aug 21, 2025
Synopsis FA8604-25-Q-B005 MQ-IC RR Trailer Paint - Gray Eagle.docx	DOCX document	Aug 21, 2025
Painting Performance Work Statement Updated 2025-08-19 FINAL.pdf	PDF	Aug 21, 2025

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Bill/Ship to: AFLCMC/EZPAA 5215 Thurlow Rd, Suite 5

WPAFB, OH 45433

29 MAY 2025

GRAY EAGLE RTS SNs 002/003

POC Mike Harff 937-257-4519

P/N Lot 1 QTY Lot 2 QTY Material Pretreat Prime Topcoat 202114751-10 1 1

202114752-10/20 BASE ASSY 2 2

202114752-10/20 INBOARD CLAMP ASSY 2 2

202114752-10/20 OUTBOARD CLAMP ASSY 2 2

202114753-10/20 BASE ASSY 2 2

202114753-10/20 CLAMP ASSY 2 2

202114754-10/20 2 2 202114763-10/20 2 2 202114766-10/20 2 2 202114767-10/20 2 2 202114768-10 1 1 202114865-10/20 2 2 202236503-10 2 2

Description of Work

Aluminum Substrate /

Stainless Fasteners / Zn Coated Fasteners

MIL-DTL-5541

CLASS 1A

MIL-PRF-23377

Type 1 Class C

MIL-DTL-53039, BLACK

37030 PER SAE AMS-

STD-595

12345678

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

JUN 73AF 1656 PREVIOUS EDITION WILL BE USED.

202.88

20.85

16.69

12.25

9.19

29.19

22.00

61.25

REVISIONS

APPROVEDDATEDESCRIPTIONLTRPROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

2OF2SHEET0.100SCALE

X202114751-10_PAINT

DRAWING NO.AIR FORCE IDENT NO.

0B275

SIZE

TRAILER ASSEMBLY

TITLE

U.S. AIR FORCE

X P A I N T

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

MASK ALL FOAM CUSHIONS, IF PRESENT. 5 LOCATIONS. 5X TOTAL.

MASK ALL PLASTIC LINERS. 26 LOCATIONS. 26X TOTAL.

MASK 3/8-24 UNF FLOATING NUT PLATES. 2 LOCATIONS. 2X TOTAL

MASK SWIVEL TIE DOWNS. 8 LOCATIONS. 8X TOTAL.

MASK 3/8 DOWEL PINS. 2 LOCATIONS. 4X TOTAL.

MASK 3/8 OBLONG HOLES. 4X TOTAL.

PLUG 1/2-13 TAPPED HOLES. 5 LOCATIONS. 20X TOTAL.

PLUG 5/16-18 TAPPED HOLES. 4 LOCATIONS. 44X TOTAL.

PLUG 1/2 BUSHING HOLES. 6 LOCATIONS. 20X TOTAL.

PLUG 1/2 BOLT HOLES. 4 LOCATIONS. 8X TOTAL.

PLUG 5/8 HOLES. 4 LOCATIONS. 4X TOTAL.

MASK INDICATED METAL SURFACES. 2 LOCATIONS. 2X TOTAL.

MASK 1.00 INCH COUNTERBORES. 4 LOCATIONS. 8X TOTAL.

SECTION AA-AA

SCALE 0.25

SEE SHEET 1, ZONE D4

10 8X

1116X

124X

58X

144X

168X

104X

7 7

8 9 4X

132X

1114X

1114X12

5 15

12345678

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

JUN 73AF 1656 PREVIOUS EDITION WILL BE USED.

213.50

17.31

0.00

20.56

22.06

54.72

2.01

REVISIONS

APPROVEDDATEDESCRIPTIONLTRPROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

3OF2SHEET0.100SCALE

X202114752-10_20_PAINT

DRAWING NO.AIR FORCE IDENT NO.

0B275

SIZE

WING ASSEMBLY

TITLE

U.S. AIR FORCE

X P A I N T

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

MASK ALL FOAM CUSHIONS, IF PRESENT. BASE ASSY: 7 LOCATIONS. 7X TOTAL.

INBOARD/OUTBOARD CLAMP ASSYS: 1 LOCATION EACH. 2X TOTAL.

MASK 1/2 OBLONG BUSHING HOLES. 4X TOTAL.

PLUG 1/2 BUSHING HOLES. BASE ASSY: 4 LOCATIONS. 8X TOTAL.

INBOARD/OUTBOARD CLAMP ASSYS: 2 LOCATIONS EACH. 4X TOTAL.

MASK ENTIRE INNER SLIDING SURFACE ADJACENT TO 1/2 BUSHINGS. 4 LOCATIONS. 8X TOTAL.

PLUG 3/8 THRU HOLES. 4 LOCATIONS. 16X TOTAL.

PLUG 1/4-20 TAPPED HOLES. 6 LOCATIONS. 12X TOTAL.

PLUG 10-32 TAPPED HOLES. 7 LOCATIONS. 17X TOTAL.

PLUG 10-32 THRU HOLES. 5 LOCATIONS. 7X TOTAL.

MASK CONTOURED SLIDING SURFACE OF 0.190 THK HOOKS. 4 LOCATIONS. 4X TOTAL.

PLUG 3/4 HOLE. 1X.

MASK INNER SLIDING SURFACES OF 0.190 THK HOOKS. 2 LOCATIONS. 4X TOTAL.

MASK OUTER SLIDING SURFACES ON INBOARD/OUTBOARD CLAMP ASSYS. 2 LOCATIONS EACH.

8X TOTAL.

SCALE 0.050

BASE ASSY

SEE DETAIL B

SEE DETAIL A

DETAIL A

SCALE 0.50

DETAIL B

SCALE 0.50

11 2X 112X

104X 10 4X

4 4

10 3X 10 3X

9 2X

109 2X

9 2X

5 5

8 4X

6 2X

6 4X

72X

7 2X

7 4X

12345678

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

JUN 73AF 1656 PREVIOUS EDITION WILL BE USED.

42.25

2.00

7.50

18.80

15.29

31.96

7.50 2.00

REVISIONS

APPROVEDDATEDESCRIPTIONLTRPROTOTYPE 22-07-22

AFPTEF PROJ NO. 19-P-118

3OF3SHEET0.200SCALE

X202114752-10_20_PAINT

DRAWING NO.AIR FORCE IDENT NO.

0B275

SIZE

WING ASSEMBLY

TITLE

U.S. AIR FORCE

X P A I N T

INBOARD CLAMP ASSY

OUTBOARD CLAMP ASSY

152X

92X

12345678

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

JUN 73AF 1656 PREVIOUS EDITION WILL BE USED.

38.50

48.00

27.00

38.26

13.04

2.09

4.97

38.02

32.02

33.45

10.86

REVISIONS

APPROVEDDATEDESCRIPTIONLTRPROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

2OF2SHEET0.100SCALE

X202114753-10_20_PAINT

DRAWING NO.AIR FORCE IDENT NO.

0B275

SIZE

TAIL ASSEMBLY

TITLE

U.S. AIR FORCE

X P A I N T

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

MASK ALL FOAM CUSHIONS, IF PRESENT. 6 LOCATIONS. 6X TOTAL.

MASK ENTIRE INNER SURFACE ADJACENT TO CLAMP CLEVIS 3/8 THRU HOLES. 4 LOCATIONS. 8X TOTAL.

MASK ENTIRE OUTER SURFACE ADJACENT TO CLAMP EYE 3/8 THRU HOLES. 4 LOCATIONS. 8X TOTAL

PLUG 3/8 THRU HOLES IN CLAMP EYES AND CLEVISES. 8 LOCATIONS. 12X TOTAL.

PLUG 1/4 THRU HOLES. 1 LOCATIONS. 2X TOTAL.

MASK ALL PLASTIC LINERS. 6 LOCATIONS. 10X TOTAL.

PLUG 10-32 TAPPED HOLES. 2 LOCATIONS. 2X TOTAL.

MASK ENTIRE DRAW LATCH. 1 LOCATION. 1X TOTAL.

CLAMP

BASE

SECTION A-A

CLAMP

8 2X

54X

7 4X

102X

7 2X

102X

12345678

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

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

21.13

9.54

38.00

6.70

3.24

1OF1SHEET0.20SCALE

X202114754-10_20_PAINT

DRAWING NO.AF. CODE IDENT NO.

0B275

SIZE

SURROGATE SPAR ASSEMBLY

TITLE

U.S. AIR FORCE

R.L. MILLER

AIR FORCE RELEASE

M. R. HARFF

AIR FORCE AUTHENTICATION

ENG

M. P. BOZZUTO

CHK

CURRENT

CODE IDENT NO.

X P A I N T

PARTS LIST

PROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

1202114846-01SPAR1

2202114782-101

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

MASK 2.00 BUSHING HOLES INCLUDING OUTER SURFACES ON BOTH SIDES. 2X TOTAL.

PLUG 1/2 THRU HOLES. 2 LOCATIONS. 2X TOTAL.

MASK EVERYTHING BELOW INDICATED PLANE. 2 LOCATIONS.

PLUG 1/4-20 TAPPED HOLES IN UPPER CLAMP. 4 LOCATIONS. 8X TOTAL.

5 2X

12345678

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

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

25.86

6.00

8.50

28.53

9.50

25.53

1OF1SHEET0.10SCALE

X202114763-10_20_PAINT

SIZE

CAPTURE ARM ASSY

CODE IDENT NO.

X P A I N T

PARTS LIST

PROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

1CSEE311CAP SCREW, FLAT HEAD SOCKET20

2202114764_REFCAPTURE ARM WELDMENT, FWD1

3202114848-01CLEVIS, CAPTURE ARM, INNER1

4202114848-03CLEVIS, CAPTURE ARM, OUTER1

5202114855-01EYE, CAPTURE ARM, LOWER1

6202114851FLANGE, CAPTURE ARM1

7202114853-03HINGE, AFT CAPTURE ARM, PRESS FIT2

8202114853-01HINGE, AFT CAPTURE ARM, SLIP FIT2

91185-5CN312INSERT, HELICAL20

10202114854-01LATERAL STOP, CAPTURE ARM1

11202236477-03POST, CAPTURE ARM, AFT1

12202114858-011

13UPPER_CAPTURE_ARM_L_SKEL1

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 ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

PLUG 5/8 BUSHING HOLES AND MASK INNER SLIDING SURFACES ON BOTH SIDES. 2X TOTAL.

PLUG 1/2 BUSHING HOLE AND MASK OUTER SLIDING SURFACES.

PLUG 1/2 BUSHING HOLE.

MASK HINGE COMPLETELY. NO PAINT SHALL ENTER CROSS-HATCHED AREA.

42X

12345678

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

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

11.31

20.84

2.00

1OF1SHEET0.50SCALE

X202114766-10_20_PAINT

SIZE

FWD LINK ASSY

CODE IDENT NO.

X P A I N T

PARTS LIST

PROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

1202114849-01CLEVIS, FWD LINK, LOWER2

2202114849-03CLEVIS, FWD LINK, UPPER1

3202114852-01FWD LINK1

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

PLUG 1/2 BUSHING HOLES AND MASK INNER SLIDING SURFACES ON BOTH SIDES. 3 LOCATIONS. 6X TOTAL.

4 4

42X

44X

12345678

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

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

16.09

20.00

7.00

1OF1SHEET0.25SCALE

X202114767-20_PAINT

SIZE

FWD SADDLE ASSEMBLY, R

J. A. SULLIVAN

B. C. BAVER

CODE IDENT NO.

X2 P A I N T

PARTS LIST

PROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

1202114802-05ANGLE, SADDLE, LOWER, AFT R1

2202114802-07ANGLE, SADDLE, LOWER, FWD R1

3202114802-03ANGLE, SADDLE, UPPER, AFT1

4202114802-01ANGLE, SADDLE, UPPER, FWD1

5CSEE284CAP SCREW, FLAT HEAD SOCKET38

6202114806-04FLANGE, FWD SADDLE, AFT, R1

7202114806-02FLANGE, FWD SADDLE, FWD, R1

8202114804-03FLANGE, FWD SADDLE, LOWER, R1

9202114805-02FLANGE, FWD SADDLE, UPPER, R1

1098381A617_DOWELPINPIN, DOWEL4

11202114803-03RIB, FWD SADDLE, R1

1295105A147RIVET NUT38

13FWD_L_SADDLE_FOAM_INST1

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

MASK FOAM CUSHION, IF PRESENT. 1X TOTAL.

MASK 3/8 DOWEL PINS. 4X TOTAL.

MASK 3/8 OBLONG HOLES. 4X TOTAL.

56 6

12345678

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

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

22.125

26.000

2X 3.500

7.500

1.000

2OF1SHEET0.20SCALE

X202114768

SIZE

MID SADDLE ASSEMBLY

J. A. SULLIVAN

B. C. BAVER

CODE IDENT NO.

PARTS LIST

PROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

202114750-10202114751-10

USED ONNEXT ASSEMBLY

APPLICATION

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

1AN0321ADHESIVE, THREAD, MED STRENGTH1

2202114809-01ANGLE, MID SADDLE, L1

3202114809-02ANGLE, MID SADDLE, R1

4202114833-01BRACE, LATERAL LINK, L1

5202114833-02BRACE, LATERAL LINK, R1

610-32 X 0.625 L, 18-8 SSCSEE258CAP SCREW, FLAT HEAD SOCKET8

75/16-18 X 0.75 L, 18-8 SSCSEE309CAP SCREW, FLAT HEAD SOCKET4

85/16-18 X 1.00 L, 18-8 SSCSEE311CAP SCREW, FLAT HEAD SOCKET30

9202114856-01EYE, FWD LINK, INNER2

10202114810-01EYE, LATERAL LINK2

11202114814-05FLANGE, MID SADDLE, AFT1

12202114814-01FLANGE, MID SADDLE, LOWER1

13202114814-03FLANGE, MID SADDLE, UPPER1

14RHN012HEX NUT2

155/16-18 X 0.312 L, SS1185-5CN312INSERT, HELICAL12

16202114769-10MID SADDLE WELDMENT1

17202114811-01PLATE, MID SADDLE1

18202236493-01POST, LATERAL LINK2

19202114815-01RIB, MID SADDLE, AFT L1

20202114815-02RIB, MID SADDLE, AFT R1

21202114815-03RIB, MID SADDLE, FWD L2

22202114814-04RIB, MID SADDLE, FWD R2

23202114815-05RIB, MID SADDLE, MAIN1

24202114815-11RIB, MID SADDLE, OFFSET, AFT L1

25202114815-12RIB, MID SADDLE, OFFSET, AFT R1

26202114815-07RIB, MID SADDLE, OFFSET, FWD2

27202114815-09RIB, MID SADDLE, OFFSET, MAIN1

285/16-18 X 0.150 MAX GRIP, KNURLED, YZ PLT95105A151_RIVNUT516X150RIVET NUT30

29 3/16 X .500 MAX GRIP, 100 °CSK, AL98778A361RIVET, BLIND, HIGH-STRENGTH36

30 1/4 X .725 MAX GRIP, 100 °CSK, AL98778A363RIVET, BLIND, HIGH-STRENGTH48

31 3/16 X .438 MAX GRIP, STD HEAD, AL98778A502RIVET, BLIND, HIGH-STRENGTH384

325/16-18 X 0.625L, 18-8 SSHCS_5_16X625SCREW, HEX HEAD CAP8

335/16 SCREW, 18-8 SSWA011WASHER, PLAIN8

34WA013WASHER, PLAIN2

35MID_SADDLE_CUSHION1

NOTE:

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. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK PER SAE-AMS-STD-595.

MASK FOAM CUSHION, IF PRESENT. 1 LOCATION. 1 TOTAL.

MASK 3/8 THRU HOLES. 2 LOCATIONS. 2 TOTAL. LATERAL LINK POST

(FIND NO. 18) SHALL BE REMOVED PRIOR TO PAINTING.

MASK BOTTOM AND INSIDE SURFACES OF LOWER MID SADDLE FLANGE

(FIND NO. 12)

MASK BOTTOM SURFACE OF MID SADDLE ANGLES (FIND NOS. 2 & 3)

PLUG 3/8 HOLES IN BOTTOM LEG OF MID SADDLE ANGLES (FIND NOS. 2 & 3).

2 LOCATIONS. 16X TOTAL.

MASK INNER SLIDING SURFACES OF INNER FWD LINK EYE (FIND NO. 9).

2 LOCATIONS. 4X TOTAL.

PLUG 1/2 BUSHING HOLES. 4 LOCATIONS. 4X TOTAL.

PLUG 3/8-16 TAPPED HOLES. 2 LOCATIONS. 2X TOTAL.

102X

102X 11 2X

52X

11 11

88X

12345678

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

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

10.00

10.75

15.19

20.44

4.25 5.25

X202114865_PAINT

SIZE

UPPER LIFT ASSY

CODE IDENT NO.

X2 P A I N T

PARTS LIST

PROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

1202114865-01CHANNEL, JACK, UPPER, L1

2202114856-03EYE, FWD LINK, OUTER L1

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

PLUG 1/2 AND 5/8 BUSHINGS, INCLUDING HOLES AND SLIDING SURFACES ON BOTH SIDES. 4 LOCATIONS. 4X TOTAL.

PLUG 5/16-18 TAPPED HOLES. 8X.

PLUG 10-32 TAPPED HOLES. 10X.

MASK 10 X 4.25 CHANNEL ALL BOTTOM AND INNER SURFACES. NO PAINT SHALL COVER INDICATED SURFACES.

42X

6 6

12345678

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

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

5.50

10.25

7.002.50

12.00

13.50

8.50

10.25

X202236503-10_PAINT

SIZE

BRACKET, SCREW JACK

CODE IDENT NO.

X2 P A I N T

PARTS LIST

PROTOTYPE 22-07-29

AFPTEF PROJ NO. 19-P-118

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM

1202114882-03GUSSET, JACKSCREW, INNER1

2202114882-01GUSSET, JACKSCREW, OUTER L1

3202114882-02GUSSET, JACKSCREW, OUTER R1

NOTES:

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

2. ALL CONVERSIONS FROM METRIC TO ENGLISH

UNITS SHALL BE IAW ANSI/ASTM SI 10.

3. COATING SYSTEM:

PRETREAT PER MIL-DTL-5541

PRIME PER MIL-DTL-53022

TOPCOAT PER MIL-DTL-53039, COLOR BLACK 37030 PER SAE-AMS-STD-595.

PLUG 5/16 HOLES. 6 LOCATIONS. 26X TOTAL.

MASK INDICATED CROSSHATCHED SURFACES. 2 LOCATIONS.

6. ASSEMBLY SHALL BE PAINTED AS THREE SEPARATE PARTS LISTED IN THE PARTS LIST

(FIND NOS. 1, 2, AND 3).

48X

412X

46X

Painted parts list - 2025-05-29

Sheet1

Gray Eagle RTS - RFQ EZPAA 2025-05-29

202114751-10_paint

Sheet 2

Views

new_view_3

right_4

left_5

top_6

bottom_7

new_view_8

202114752-10_20_paint

Sheet 2

Views

new_view_11

new_view_12

top_13

bottom_14

left_15

right_16

Sheet 3

Views

new_view_20

new_view_21

left_23

new_view_24

new_view_25

left_26

right_27

202114753-10_20_paint

Sheet 2

Views

new_view_19

new_view_23

right_24

left_25

left_26

new_view_27

new_view_28

left_29

202114754-10_20_paint

Sheet 1

Views

new_view_19

bottom_20

left_21

202114763-10_20_paint

Sheet 1

Views

new_view_31

left_32

right_33

top_34

202114766-10_20_paint

Sheet 1

Views

new_view_35

new_view_36

left_37

202114767-20_paint

Sheet 1

Views

new_view_38

new_view_39

left_40

bottom_41

202114768_PAINT

Sheet 1

Views

new_view_4

new_view_7

left_8

top_9

bottom_14

202114865_paint

Sheet 1

Views

new_view_38

new_view_39

top_40

left_42

202236503-10_paint

Sheet 1

Views

new_view_44

new_view_45

top_46

left_47

MQ-1C TRAILER Paint List 2025-08-13.pdf

Sheet1

File details come from the government source that posted it. Updated Aug 21, 2025.