Attachment 2 - X20084625-10 Drawing F-16 Gun Maintenance Trailer.pdf
PDF 3 MB Posted
- Attached to
- F-16 Maintenance Trailer Federal contract opportunity
- Solicitation number
- W50S6S24Q0020
About this file
This document is a Request for Quote (RFQ) for the procurement of an F-16 Maintenance Trailer. The solicitation is a 100% set-aside for Small Businesses under NAICS code 336413 with a 1,500 employee size standard.
The key details are:
- Solicitation Number: W50S6S24Q0020
- Agency: Department of the Army Arizona Army National Guard
- Quotes due by the date and time listed in SAM.gov, submitted via email to the provided address
- Quote should include a technical narrative, completed attachments for Section 889 representation and past performance, and vendor information
- The RFQ and associated attachments contain the detailed requirements, terms, and evaluation factors for the F-16 Maintenance Trailer. Responses will be evaluated based on the criteria outlined.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Amended RFQ W50S6S24Q0020 - F16 Maintenance Trailer.docx | DOCX document | |
| W50S6S24Q0020 - Q and A.docx | DOCX document | |
| Attachment 1 - CERT of 52.204-24 25 26.pdf | ||
| Attachment 3 - Past Performance Reference List.docx | DOCX document | |
| RFQ W50S6S24Q0020- F16 Maintenance Trailer.docx | DOCX document |
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Text version
X20084625-10_A.dft
AIR FORCE RELEASE
D
ENGINEERING DRAWING LAYOUT D
USED ONNEXT ASSEMBLY
FEB 74
FORMAF
CODE IDENT NO.
CURRENT
DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION
ENG
CHK
DR
.XXX±
.XX±
DECIMALS ANGLESFRACTIONS
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
THIRD ANGLE PROJECTION
TITLE
SIZE
SCALE:
SHEET
PARTS LIST
APPLICATION
U.S. AIR FORCE
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
- EGLIN A.F.B. FL
GENERATED USING SOLID EDGE FILENAME:
REV
UNLESS OTHERWISE SPECIFIED
QUANITY REQUIRED PER DASH NO.
SIGNATURES ARE ON FILE ON AF
FORM 2602 IN MMHE, EGLIN AFB
APPV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.
F-16 GUN MAINTENANCE
TRAILER
X20084625 A 1 / 10
N PELICAN 20110726
X2
A
FINAL FINAL
.5°.010 .03
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A
REVISED DRAWINGS X20084627, X20084628,
X20084640, X20084641 NP 20220331
20220331 B CHAMBLISS
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2018..
2. WORKMANSHIP:
ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS
AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO,
BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS,
DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS,
LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS
PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO
REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX, CHEMICAL DEPOSITS,
RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD
AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO
THE ENVIRONMENT, NOR SHALL ANY PART BE CONTAMINATED BY THE
CLEANING AGENT.
3. APPLY PRIMER (FIND NO 33) AND LOCKING COMPOUND (FIND NO 31) ON
THREADS OF SCREW (FIND NO 22) AND PRIMER (FIND NO 33) AND
LOCKING COMPOUND (FIND NO 32) ON THREADS OF SCREW (FIND NO
21) AND GREASE FITTING (FIND NO 23)
4. PERMANENTLY MARK 18894ASSYXP20084625-10 IN APPROX AREA
SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-STD-130.
5. SET MAINTENANCE STAND WELDMENT (FIND NO 1) ON TOP OF
UNDERCARRAGE ASSEMBLY (FIND NO 2) AND ALIGN OUTER EDGES.
MATCH DRILL (16X) .531 DIA MOUNTING HOLES AND INSTALL
HARDWARE (FIND NO 26-28). PROVIDE CLEARANCE CUT IN RETAINER
PLATES (PART OF XP20084627-10) AS REQUIRED TO INSTALL
HARDWARE, (FIND NO. 26 – 28).
6. ATTACH TAILGATE DOOR ASSEMBLY (FIND NO 5) TO MAINTENANCE
STAND WELDMENT (FIND NO 1) BY CENTERING DOOR ASSEMBLY IN
OPENING AS SHOWN MATCH DRILLING USING #11 DRILL BIT (23X) AND
INSTALLING RIVETS (FIND NO 24). LOCATE AND DRILL .437 DIA HOLE
(2X) TO MATCH LATCH BOLT ON DOOR ASSY.
7. ATTACH FRONT DOOR ASSEMBLY (FIND NO 6) TO MAINTENANCE STAND
WELDMENT (FIND NO 1) BY CENTERING DOOR ASSEMBLY IN OPENING AS
SHOWN MATCH DRILLING USING #11 DRILL BIT (14X) AND INSTALLING
RIVETS (FIND NO 24). LOCATE AND DRILL .437 DIA HOLE (2X) TO
MATCH LATCH BOLT ON DOOR ASSY.
8. ATTACH BARREL STOWAGE DOOR ASSEMBLY (FIND NO 7) TO
MAINTENANCE STAND WELDMENT (FIND NO 1) BY CENTERING DOOR
ASSEMBLY IN OPENING AS SHOWN MATCH DRILLING USING #11 DRILL
BIT (10X) AND INSTALLING RIVETS (FIND NO 24). LOCATE AND DRILL
.437 DIA HOLE (2X) TO MATCH LATCH BOLT ON DOOR ASSY.
9. ATTACH GUN BARREL RETAINER (FIND NO 11) TO MAINTENANCE STAND WELDMENT
(FIND NO 1) BY CENTERING RETAINER IN OPENING AS SHOWN. MATCH DRILL USING #11
DRILL BIT (7X) AND INSTALLING RIVETS (FIND NO 24).
10. ATTACH CUSHIONS (FIND NOS 12-16, 38 & 39) TO MAINTENANCE STAND WELDMENT
(FIND NO 1) APPROXIMATELY AS SHOWN, INSURING NO INTERFERENCE WITH DOOR
ASSEMBLIES. MATCH DRILL USING #11 DRILL BIT AND INSTALL RIVETS (FIND NO 44).
AND WASHER (FIND NO 19)
11. ATTACH CUSHION (FIND NO 17) TO MAINTENANCE STAND WELDMENT (FIND NO 1)
APPROXIMATELY AS SHOWN. USE CUSHION KEEPERS (FIND NO 18) TOP AND BOTTOM.
MATCH DRILL USING #11 DRILL BIT AND INSTALL RIVETS (FIND NO 25) 11 PLACES.
WRAP REMAINDER OF CUSHION AROUND CORNER AS SHOWN AND MATCH DRILL USING
#11 DRILL BIT AND SECURE WITH RIVETS (FIND NO 44) AND WASHER (FIND NO 19).
12. DELETED
13. MAY BE PURCHASED FROM MCMASTER CARR SUPPLY 6100 FULTON INDUSTRIAL
BLVD SW, ATLANTA, GA 30336-2853
14. MATCH DRILL .406 DIA HOLE THROUGH FIND NO 3 TO ALIGN BEAM WITH
UNDERCARRIAGE ASSEMBLY (FIND NO 2).
15. MATCH DRILL .272 DIA THROUGH MAINTENANCE STAND WELDMENT (FIND NO. 1) FROM
SAFETY RAIL ASSEMBLY (FIND NO. 4.
16. ATTACH HANDLE PULL (FIND NO 37) USING HARDWARE (FIND NO 34 – 36) LOCATE
HANDLE ON TALL POST TO MATCH HANDLE ON SHORT POST AS SHOWN AND MATCH
DRILL DIA .281 COMPLETELY THROUGH TALL POST.
FOR PARTS LIST SEE SHEET 2
M. LAPEE 20111212
B. CHAMBLISS 20120113
A. BUSCAVAGE 20120305
B. YOURICK 20120521
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20084625
1 / 10
X2 A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220331 20220331 B CHAMBLISS
1 DRUM STAND ASSEMBLY 20084630-10 3B1 46
1 GUN STAND ASSEMBLY 20084629-10 3A1 45
122 RIVET, BLIND OKVE6 97447A060 AL ALLOY 5000 SERIES .188 DIA X .376-.500 GRIP 3C7 44
1 SNAP, SPRING OKVE6 3764T31 316 CRES, .25 DIA , .31 EYE OPENING X 2.38 LGT 4C1 43
1 EYE BOLT, SHOULDER OKVE6 3014T201 .250-20 UNC-2A X 2.00 LG STL GALV 3C3 42
2 SLEEVE, COMPRESSION OKVE6 3883T43 COPPER, TIN COAT, .12 WIRE SIZE X .56 LG 4C2 41
1 WIRE ROPE OKVE6 8923T71 24.0 LG 7 X 19 CRES BLACK NYLON COAT 4B2 40
1 CUSHION 20084655-15 3C2 39
1 CUSHION 20084655-17 3B6 38
2 HANDLE, PULL OKVE6 5190A21 3D3 37
4 SCREW, CAP, HEX SOCKET OKVE6 92196A552 CRES STEEL, .250-20 UNC-2B X 2.50 LG 3D3 36
5 WASHER, PLAIN OKVE6 98019A360 .312 ID X .734 OD X .051 THK, CRES 35
5 NUT, SELF-LOCKING, HEXAGON OKVE6 91831A029 .250-20UNC-2B CRES, NYLON INSERT 34
A/R PRIMER, LOCK OKVE6 7614A16 LOCKTITE 7649 33
A/R LOCKING COMPOUND OKVE6 91458A13 LOCKTITE 222MS (PURPLE) 32
A/R LOCKING COMPOUND OKVE6 91458A24 LOCKTITE 242 (BLUE) 31
1 PIN, SPRING, COILED OKVE6 91598A256 STEEL PLAIN FINISH, STANDARD DUTY .125 DIA X .75 4C2 30
2 EYEBOLT, SHOULDER OKVE6 3014T491 .500-13 UNC-2A X 1.50 LG STL, GALV 8B5 29
18 NUT, HEX, CENTER LOCK OKVE6 90047A135 .500-13 UNC-2B, 18-8 CRES STEEL 1D3 28
34 WASHER, FLAT OKVE6 98019A509 .531 ID X 1.062 OD X .100 THK, CRES 1D3 27
16 SCREW, CAP OKVE6 91247A725 .500-13 UNC-2A X 3.25 LG, STEEL, ZINC PLATE GRADE 5 4D6 26
11 RIVET, BLIND OKVE6 97545A080 AL ALLOY 5056 .188 DIA X .375 - .625 MATL THK 3A3 25
54 RIVET, BLIND OKVE6 97517A050 AL ALLOY 5000 SERIES .188 DIA X .126 - .250 GRIP 4C4 24
1 GREESE FITTING OKVE6 2309K98 STEEL ZINC PLT .125 PTF MALE THD WITH BALL CHECK 3D8 23
2 SCREW, SOCKET HEAD OKVE6 90128A634 .375-16 UNC-2A X 2.500 LG, STEEL, ZINC PL 3D8 22
2 SCREW, FLAT HEAD 82 DEG OKVE6 91771A244 .190-24 UNC-2A X .625 LG, CRES 7C3 21
1 BEARING, THRUST OKVE6 60715K15 STEEL INTEGRATED BALL BEARING, SHIELDED FOR 1.00 DIA
SHAFT 1.968 OD .625 THK
7C3 20
122 WASHER, FLAT OKVE6 94744A221 .203 ID X .562 OD X .063 THK STEEL ZINC PLATE 3C7 19
2 CUSHION KEEPER 20084662-01 3B3 18
1 CUSHION 20084655-13 3B3 17
1 CUSHION 20084655-11 3B6 16
1 CUSHION 20084655-07 3B6 15
1 CUSHION 20084655-05 3B5 14
-10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN
1 CUSHION 20084655-03 4C6 13
1 CUSHION 20084655-01 3A5 12
1 RETAINER, GUN BARREL 20084635-01 4C4 11
2 BUSHING, CRANE 20084660-01 3C8 10
1 CAP, CRANE, BUSHING 20084661-01 3C8 9
6 TUBE, GUN BARREL 20084634-01 4B5 8
1 DOOR ASSY BARREL STOWAGE 20084631-10 4B4 7
1 DOOR ASSY FRONT 20084632-10 3B2 6
1 DOOR ASSY TAILGATE 20084633-10 3B6 5
1 SAFETY RAIL ASSY 20084636-10 3C4 4
1 CRANE ASSY 20084628-10 3D5 3
1 UNDERCARRIAGE ASSEMBLY 20084626-10 3A3 2
1 MAINTENANCE STAND WELDMENT 20084627-10 3C2 1
-10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
X20084625 1 / 10
X2 A
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220331 20220331 B CHAMBLISS
A
C
2 5
1 5
18 2X
17 11
25 11X
6 7
DETAIL C
19(122X) 44 (122X)
DETAIL A
222X
102X FRONT
SCALE: 1/5
SCALE: 1/5
36 4X
37 2X
35 4X
34 4X
(INSTALL RIVETS FROM TOP)
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
X20084625 1 / 10
X2 A
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220331 20220331 B CHAMBLISS
G 8 6X
16( )
14( )
13 10
DETAIL G
2616X
2732X
27 ( )
2816X
2( )
1( )
J J
B
6( )
DETAIL B
24 SECTION J-J
RIGHT SIDE VIEW
FRONT END VIEW
SCALE: 1/2
SCALE: 1/2
SCALE: 1/4
K
DETAIL K
412X
SCALE 1/5
(24 INCH LONG)
42( )
M M 8
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
X20084625 1 / 10
X2 A
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220331 20220331 B CHAMBLISS
H H
F
F
17( )
12( )
LEFT SIDE VIEW
REAR END VIEW
B
B
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
X20084625 1 / 10
X2 A
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220331 20220331 B CHAMBLISS
DETAIL E
17( )
18( )
18( )
SECTION D-D
E 8( )
29( ) 2X
27( ) 2X
28( ) 2X
D
D
TOP VIEW
ROTATED 90v CW
SCALE: 1/2
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.
SECTION F-F
20( )
3( )
SECTION H-H
21 2X
CRANE ASSY (FIND NO 3) NOT SHOWN FOR CLARITY
B
A
SCALE: 1/4 SCALE: 1/4
A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
X20084625 1 / 10
X2 A
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220331 20220331 B CHAMBLISS
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
X20084625
X2 A
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220331 20220331 B CHAMBLISS
1 / 10
SECTION M-M
292X
272X
282X
B
X20084626-10.dft
AIR FORCE RELEASE
D
ENGINEERING DRAWING LAYOUT D
USED ONNEXT ASSEMBLY
FEB 74
FORMAF
CODE IDENT NO.
CURRENT
DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION
ENG
CHK
DR
.XXX±
.XX±
DECIMALS ANGLESFRACTIONS
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
THIRD ANGLE PROJECTION
TITLE
SIZE
SCALE:
SHEET
PARTS LIST
APPLICATION
U.S. AIR FORCE
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
- EGLIN A.F.B. FL
GENERATED USING SOLID EDGE FILENAME:
REV
UNLESS OTHERWISE SPECIFIED
QUANITY REQUIRED PER DASH NO.
SIGNATURES ARE ON FILE ON AF
FORM 2602 IN MMHE, EGLIN AFB
APPV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.
UNDERCARRIAGE WELDMENT
X20084626 1 / 8
X2
20084625 20084625
.5°.010 .03
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2018.
2. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE
INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.
3. WORKMANSHIP:
ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS
AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO,
BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS,
DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS,
LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS
PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO
REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX, CHEMICAL DEPOSITS,
RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD
AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO
THE ENVIRONMENT, NOR SHALL ANY PART BE CONTAMINATED BY THE
CLEANING AGENT.
4. FINISH: UNLESS OTHERWISE SPECIFIED. PRIMER ALL
EXTERIOR SURFACES AND EDGES IAW MIL-PRF-23377, TYPE
II, CLASS C1, C2, OR N. PAINT ALL PRIMED SURFACES IAW
MIL-PRF-85285, TYPE II, COLOR GRAY, COLOR NO. 26173
IAW FED-STD-595. REMOVE WHEELS PRIOR TO PAINTING
AND MASK STUDS / THREADED HOLES, WHERE WHEELS
ATTACH.
5. PERMANENTLY MARK 18894ASSYX20084626-10 IN APPROX AREA
SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-STD-130.
6. APPLY PRIMER (FIND NO. 11) AND LOCKING COMPOUND (FIND NO. 12) TO
THREADS OF SCREW (FIND NO. 6) IAW MANUFACTURER'S INSTRUCTION
PRIOR TO INSTALLATION.
7. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE
ACCEPTABLE.
8. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE
OKVE6, PO BOX 740100, ATLANTA GA, 30374-0100.
9. STENCIL "EMPTY WEIGHT 1630 LBS" IN APPROXIMATE AREA SHOWN IN
1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-PRF-85285,
TYPE III REQUIREMENTS, COLOR NO. 37038 (BLACK) IAW FED-STD-595.
10. STENCIL "BOOM TRANSPORTATION LOCK PIN" IN APPROXIMATE AREA
SHOWN IN 1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-PRF-
85285, TYPE III REQUIREMENTS, COLOR NO. 21105 (RED) IAW FED-STD-
595.
11. LENGTHEN EXISTING BRACE PULL ROD USING ONE OF TWO EXISTING
BRAKE PULL RODS. ATTACHED WITH COUPLER (FIND NO 3) AND TWO
JAM NUTS (FIND NO 10). DIVIDE REMAINING BRAKE PULL ROD TO FORM
THE TWO SHORT REAR BRAKE PULL RODS.
7 2X
8 2X
9 2X
(BOTH SIDES)
N. PELICAN 20110726
A/R COMPOUND, LOCKING OKVE6 91458A13 LOCTITE 222MS, (PURPLE) 12
A/R PRIMER, LOCKING COMPOUND OKVE6 7614A16 LOCTITE 7649, 1.75-OZ BOTTLE 11
2 NUT, JAM OKVE6 91841A235 .375-24 UNC CRES 1C5 10
2 NUT, HEX, CENTER LOCK OKVE6 90047A135 .500-13 UNC-2B, 18-8 CRES STEEL 1D3 9
2 WASHER, FLAT OKVE6 98019A509 .531 ID X 1.062 OD X .100 THK, CRES 1D3 8
2 EYEBOLT OKVE6 3014T165 STEEL ZINC PL .500-13 UNC-2A X 3.00 LG 1D3 7
1 SCREW, MACHINE OKVE6 91400A830 .190-32 UNC-2A X .625, CRES 2C2 6
1 LANYARD OKVE6 30345T24 12 INCH WITH TAB AND LOOP 3D8 5
1 QUICK RELEASE PIN OKVE6 90302A371 .375 DIA X 5.00 GRIP, CRES 3D8 4
1 COUPLING OKVE6 90977A170 .375-24 UNC X 1.75 LG, STL, ZINC 1C5 3
1 RUNNING GEAR ASSY 20084637-10 1B5 2
1 SUB-FRAME WELDMENT 20084638-10 1B5 1
-10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN
10 2X
B. CHAMBLISS 20120113
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. X20084626
1 / 8
X2
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A
A
B
DETAIL B
CCD
DETAIL D
E E
F F
SECTION F-F
.25 2X
RELOCATE PARKING BRAKE ROD ASSY
WITH PILLOW BLOCKS,
INSTALL WITH EXISTING HARDWARE
SCALE : 1 / 4
SCALE : 1 / 4
SCALE : 1 / 4
C
C
A
G
G
C
CENTER FRONT AND REAR AXLE ASSYS UNDER SUB-FRAME WELDMENT
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
X20084626 1 / 8
X2
REVISIONS
LTR DESCRIPTION DATE APPROVED
SECTION A-A
SECTION E-E SECTION C-C
2X .25
RELOCATE HAND PARKING BRAKE
INSTALL WITH EXISTING HARDWARE
(ROTATED 90 DEGREES CW)
SCALE : 1 / 4
SCALE : 1 / 4SCALE : 1 / 4
B
B
VIEW G-G
C
B
X20084627-10_A.dft
AIR FORCE RELEASE
D
ENGINEERING DRAWING LAYOUT D
USED ONNEXT ASSEMBLY
FEB 74
FORMAF
CODE IDENT NO.
CURRENT
DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION
ENG
CHK
DR
.XXX±
.XX±
DECIMALS ANGLESFRACTIONS
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
THIRD ANGLE PROJECTION
TITLE
SIZE
SCALE:
SHEET
PARTS LIST
APPLICATION
U.S. AIR FORCE
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
- EGLIN A.F.B. FL
GENERATED USING SOLID EDGE FILENAME:
REV
UNLESS OTHERWISE SPECIFIED
QUANITY REQUIRED PER DASH NO.
SIGNATURES ARE ON FILE ON AF
FORM 2602 IN MMHE, EGLIN AFB
APPV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.
MAINTENANCE STAND
WELDMENT
X20084627 A 1 / 8
N. PELICAN 20110725
X2 A
20084625 20084625
.5°.010 .03
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A
CHNG P/L SH 2, ADD NOTE SH 6 NPELICAN
20220322
2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX
3. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.
4. WORKMANSHIP:
ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED ON THE DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO THE ENVIRONMENT, NOR SHALL ANY PART BE CONTAMINATED BY THE CLEANING AGENT.
5. FINISH: UNLESS OTHERWISE SPECIFIED. PRIMER ALL EXTERIOR SURFACES AND EDGES
IAW MIL-PRF-23377, TYPE II, CLASS C1, C2, OR N. PAINT ALL PRIMED SURFACES IAW
MIL-PRF-85285, TYPE II, COLOR GRAY, COLOR NO. 26173 IAW FED-STD-595.
6. SANDBLAST TOP SURFACE OF CENTER PLATFORM AND UPPER PLATFORM (FIND NO 43 & 44) PAINT
USING ANTI SLIP COATING IAW MANUFACTURES INSTRUCTIONS. MATERIAL MAY BE PURCHASED FROM MCMASTER CARR SUPPLY, CAGE CODE OKVE6. PO BOX 740100, ATLANTA GA, 30374-0100, PART NO 6135T37
7. PERMANENTLY MARK 18894-X20084627-10 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW
MIL-STD-130.
8. WELD IAW ANSI/AWS D1.2-2003.
9. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.
10. UNLESS OTHERWISE SPECIFIED, ALL JOINT WELDS SHALL BE CONTINUOUS .19 WELDS WITH COMPLETE
PENETRATION.
11. STENCIL “GUN” AND “DRUM” IN APPROXIMATE AREA SHOWN IN 1.00 HIGH GOTHIC CHARACTERS USING PAINT IAW MIL-PRF-85285, TYPE III REQUIREMENTS, COLOR NO. (37038 BLACK) IAW FED-STD-595.
12. ALL SEALED TUBE ASSEMBLIES SHALL HAVE A .25 DIAMETER WEEP / DRAIN HOLE TO PERMIT
CONDENSATION DRAINAGE.
13. MATERIAL MAY BE PURCHASED FROM MCMASTER CARR SUPPLY, CAGE CODE OKVE6. PO BOX 740100, ATLANTA GA, 30374-0100, PART NO 9305T78, 24 WIDE X 24 LENGTH.
DETAIL LEGEND
FIND NO DASH NUMBER SHEET AND ZONE
1 -01 9C7 2 -03 9A7
3 -05 9C3 4 -07 9A3 5 -11 10C7 6 -13 10C7 7 -15 10A7 8 -17 10C4 9 -21 10B4 10 -23 10A4 11 -25 11C6 12 -27 11B7 13 -31 11A7 14 -33 11C4 15 -35 11B5 16 -37 11A5 17 -41 11B3 18 -43 11A3 19 -45 12D7 20 -47 12B7 21 -51 12A7 22 -53 12D4 23 -55 12C4 24 -57 12A4 25 -61 13C7 26 -63 13B7 27 -65 13A7 28 -67 13D4 29 -71 13C5 30 -73 13B5 31 -75 13A4 32 -77 13C3 33 -81 13B2 34 -83 14C7 35 -85 14C7 36 -87 14B7 37 -91 14C5 38 -93 14B5 39 -95 14B5 40 -97 14C3 41 -101 14B3 42 -103 14A3 43 -105 15B6 44 -107 15A3 45 -111 16C8 46 -113 16A7 47 -115 16C5 48 -117 16B5 49 -121 16A4 50 -123 16C2 51 -125 16A3 52 -127 17D7 53 -131 17B6 54 -133 17A5 55 -135 17C4 56 -137 18C5
SEE SHEET 2 FOR PARTS LIST
M. LAPEE 20111116
B. CHAMBLISS 20120113
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
LTR DESCRIPTION DATE APPROVED
A
FN 47 WAS .250 THK, FN 1 WAS QQ-A-250/11,
FN 45-49, 51-57 WAS QQ-A-200/11
NPELICAN 20220322
20220331 B CHAMBLISS
X20084627 1 / 8
X2 A
2 TAPE, GRIP OKVE6 7781T13 EXTREME TRACTION ABRASIVE ANTISLIP TAPE 4.0 WIDE X 13.5
LONG
3D2 58*
3 PLATE, STRIKE -141 .188 THK 6061-T6 AL SHEET IAW AMS 4027 3A4 57
1 RETAINER PLATE -137 .188 THK 6061-T6 AL SHEET IAW AMS 4027 3C1 56
1 CROSS PLATE -135 .188 THK 6061-T6 AL SHEET IAW AMS 4027 3B1 55
1 RETAINER PLATE -133 .188 THK 6061-T6 AL SHEET IAW AMS 4027 3B4 54
1 RETAINER PLATE -131 .188 THK 6061-T6 AL SHEET IAW AMS 4027 3B1 53
2 GUSSET, BARREL STOP -127 .25 THK 6061-T651 AL PLATE, IAW AMS 4027 3A5 52
1 STOP, BARREL -125 .188 THK 6061-T6 AL SHEET IAW AMS 4027 3B5 51
1 BRACKET, BARREL STOP -123 2.00 X 2.00 X .125 THK 6061-T6 AL ANGLE IAW QQ-A-200/16 3A6 50
1 GUSSET, LEFT CENTER -121 .250 THK 6061-T6 AL PLATE IAW AMS 4027 6C7 49
1 GUSSET, LEFT, UPPER -117 .250 THK 6061-T6 AL PLATE IAW AMS 4027 6C5 48
1 GUSSET, AFT, UPPER -115 .375 THK 6061-T6 AL PLATE IAW AMS 4027 3C8 47
1 CAP, BUSHING -113 .750 THK 6061-T6 AL PLATE IAW AMS 4027 3C8 46
1 GUSSET, LOWER, AFT -111 .250 THK 6061-T6 AL PLATE IAW AMS 4027 3A6 45
1 PLATFORM UPPER -107 .250 THK 3003/5086-H34/6061-T6 DIAMOND TREAD AL
PLATE
3D7 44
1 PLATFORM, CENTER -105 .250 THK 3003/5086-H34/6061-T6 DIAMOND TREAD AL
PLATE
3C5 43
1 CROSSMEMBER -103 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D3 42
1 SUPPORT, VERTICAL -101 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B4 41
1 CROSSMEMBER -97 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B4 40
1 CROSSMEMBER -95 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B4 39
1 CROSSMEMBER -93 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 38
1 CROSSMEMBER -91 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 37
1 BEAM -87 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D4 36
1 SUPPORT, VERTICAL -85 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 35
1 SUPPORT, VERTICAL -83 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 34
1 SUPPORT, VERT -81 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D5 33
1 CROSSMEMBER -77 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 32
1 RETAINER -75 2.00 X 2.00 X .25 THK AL ANG 6061-T6 IAW QQ-A-200/16 4A6 31
1 SUPPORT, VERTICAL -73 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 30
-10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN
2 CROSSMEMBER -71 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D3 29
1 BEAM -67 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 28
1 CROSSMEMBER -65 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C6 27
1 SUPPORT, VERTICAL -63 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B6 26
1 CROSSMEMBER -61 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C6 25
1 BRACE, DIAGONAL -57 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B7 24
1 BRACE, DIAGONAL -55 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C7 23
1 BRACE, DIAGONAL -53 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C7 22
1 BEAM -51 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D6 21
1 BEAM -47 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D5 20
1 SUPPORT, VERTICAL -45 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D5 19
2 CROSSMEMBER -43 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D4 18
1 SUPPORT, VERTICAL -41 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D3 17
1 BRACE, DIAGONAL -37 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 16
1 SUPPORT, VERTICAL -35 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 15
1 BEAM -33 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4D6 14
1 SUPPORT, VERTICAL -31 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A4 13
1 CROSSMEMBER -27 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 12
1 BEAM -25 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B3 11
1 CROSSMEMBER -23 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A6 10
6 BEAM -21 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A5 9
1 BRACE, DIAGONAL -17 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4A6 8
1 SUPPORT, VERTICAL -15 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 7
4 SUPPORT, VERTICAL -13 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4C3 6
3 SUPPORT, VERTICAL -11 1.50 X .188 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 4B7 5
3 CROSSMEMBER, LOWER -07 2.00 X .250 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 7C3 4
2 SIDE, LOWER -05 2.00 X .250 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 7C2 3
2 END, LOWER -03 2.00 X .250 WALL 6063-T52 AL SQ TUBE IAW QQ-A-200/9 7B1 2
1 PLATFORM, LOWER -01 .188 THK AL SH 6061-T651 IAW AMS 4027 3B8 1
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
X2 A
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A
DETAIL A
52 2X
FWD
RIGHT
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1 / 8
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D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
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28 7 6 5 4 3 1
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18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NPELICAN 20220322 20220331 B CHAMBLISS
X20084627
X2 A
53X
5( )
6 4X
6( )
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9( )
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9 6X
9( )
9( )
29( )
5( ) 33
9( )
29 2X
6( )
1 / 8
(VIEW SHOWING SUPPORT STRUCTURE)
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
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18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
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5.00
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2.19
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K
SECTION K-K
( )7 57
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D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
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SHEET
28 7 6 5 4 3 1
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B
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18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A
ADD, ZONE D4 PARTIAL TOP VIEW
NP 20220322
20220331 B CHAMBLISS
X20084627
X2 A
LEFT SIDE VIEW
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47( )
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1 / 8
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D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
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SHEET
28 7 6 5 4 3 1
A
B
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18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
X2 A
70.00
28.84
24.69
TOP VIEW
47.00
8X .18 2.0-6.0
96.00
2 2X
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.18
8X .18 2.0-4.8
4 3X
.18 6X
.18
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23.50
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ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
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SHEET
28 7 6 5 4 3 1
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18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
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SECTION B-B SECTION C-C
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55( )
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D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
X2 A
48.00
96.00
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DETAIL -03
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DETAIL -05
2.00
(STK)
2.00
(STK)
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(STK)
DETAIL -07
44.00
96.00
45°2X
1 / 8
48.00
45°2X
2.00
(STK)
2.00
(STK) .25
(STK)
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
X2 A
62.941.50
(STK)
1.50
(STK)
.19
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45°
DETAIL -11
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1.50
(STK)
1.50
(STK)
.19
(STK)
19.31
DETAIL -15
1.50
(STK)
1.50
(STK) .19
(STK)
40.81
45°
1.50
(STK)
1.50
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(STK)
24.44
38° 52°
DETAIL -17
1.50
(STK)
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(STK)
45.75
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1.50
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D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
X2 A
1.50
(STK)
1.50
(STK)
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(STK)
94.50
45°
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(STK)
1.50
(STK)
.19
(STK)
45.00
1.50
(STK)
1.50
(STK)
.19
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14.31
1.50
(STK)
1.50
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(STK)
36.25
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1.50
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(STK)
19.31
1.50
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16.00
45° 45°
1.50
(STK)
1.50
(STK)
.19
(STK)
1.50
(STK)
1.50
(STK) .19
(STK)
DETAIL -37
20.00
45°
DETAIL -41
DETAIL -43
17.50
60° 60° 1.50
(STK)
.19
(STK)
1 / 8
2.50
4.578
O .2814X .752X
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
X2 A
DETAIL -45
1.50
(STK)
1.50
(STK) .19
(STK)
42.12
45°
1.50
(STK)
1.50
(STK)
11.00
.19
(STK)
45°2X
DETAIL -47
DETAIL -51
1.50
(STK)
.19
(STK)
48.75
45°2X
1.50
(STK)
1.50
(STK) .19
(STK)
62.74
42° 48°
DETAIL -53
DETAIL -55
1.50
(STK)
1.50
(STK)
.19
(STK)
54.10
32° 58°
1.50
(STK)
1.50
(STK) .19
(STK)
52.63
31°
31°
DETAIL -57
1.50
(STK)
1 / 8
MATCH DRILL AT FINAL ASSY (20084625)
MATCH DRILL AT FINAL ASSY (20084625)
D
ENGINEERING DRAWING LAYOUT D1655
FEB 74
FORMAF
DRAWING NO.AIR FORCE CODE IDENT NO.SIZE
SCALE
SHEET
28 7 6 5 4 3 1
A
B
C
D
A
B
C
D
18894
GENERATED USING SOLID EDGE FILENAME:
REV
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON: ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC. 2751, ET SEQ.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT
DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT. A
CAD MAINTAINED. CHANGES SHALL ONLY BE
INCORPORATED AT THE DIRECTION OF THE DESIGN
ACTIVITY USING A COMPATIBLE CAD SYSTEM.
REVISIONS
LTR DESCRIPTION DATE APPROVED
A SEE SHEET 1 NP 20220322 20220331 B CHAMBLISS
X20084627
X2 A
1.50
(STK)
1.50
(STK) .19
(STK)
DETAIL -61
21.00
81°
DETAIL -63
1.50
(STK)
1.50
(STK)
.19
(STK)
10.25
DETAIL -65
1.50
(STK)
1.50
(STK)
.19
(STK)
32.95
42°
1.50
(STK)
1.50
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