SPI.pdf

PDF 1 MB Posted Dec 19, 2024

Attached to: F-16 Wing Assemblies Federal contract opportunity
Solicitation number: SPRHA4-24-R-0271
Issued by: Defense Logistics Agency Aviation

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Written by GovTribe AI · Dec 19, 2024

This is a Special Packaging Instruction (SPI) document for aircraft wing assemblies, specifically detailing the packaging requirements for F-16 wings. The document (SPI No. F01-076-8954, Code ID 98747) provides comprehensive instructions for packaging and protecting wing assemblies during shipment and storage, with both Level A and Level B protection options specified. The packaging design includes a reusable container with dimensions of 190" x 30" x 84" and a gross weight of 2482 lbs, capable of holding two wings.

The document includes detailed technical specifications for construction materials, preservation methods (using MIL-PRF-16173 and MIL-PRF-23827 preservatives), packing/unpacking procedures, and special handling requirements. Key features include metal lowering straps for crate positioning, inspection windows, sorbent material requirements for residual fuel, and specific marking instructions including "HEAVY END" markings. The package must meet international phytosanitary measures (ISPM No. 15) for wood packaging materials, requiring heat-treated and debarked wood. The document includes multiple technical drawings showing assembly details and component specifications, with distribution limited to DOD and U.S. DOD contractors only.

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DISTRIBUTION STATEMENT D: DISTRIBUTION AUTHORIZED TO DOD AND U.S. DOD CONTRACTORS ONLY, ADMINISTRATIVE OR OPERATIONAL USE, 19 AUGUST 2019. OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO 406 SCMS/GULAA, (PACKAGING

DIVISION), HILL AFB, UTAH 84056.

DESTRUCTION NOTICE: FOLLOW THE PROCEDURES IN DOD 5220.22-M, NATIONAL INDUSTRIAL SECURITY PROGRAM OPERATING MANUAL (NISPOM), SECTION 5-705, OR DOD 5200.1-R, INFORMATION SECURITY PROGRAM, CHAPTER VI. FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

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870 LBS

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ITEM WT.

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2169 MOD

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MARCH 87

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FORM

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LEVEL B:

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LEVEL A:

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CLOSURE

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IAW: ASTM D6256 AND THIS INSTRUCTION

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IAW: ASTM D6256 AND THIS INSTRUCTION

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SPI NO. F01-076-8954

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CODE ID

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DESIGN FRAGILITY G

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SPEC STYLE TYPE CL VRTY GR TR

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AS SPECIFIED BELOW AND BILL OF MATERIALS

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ILL.

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NATIONAL STOCK NO.

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PART OR DRAWING NO.

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CURRENT

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SPECIAL MARKINGS:

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A) SPI NO. F01-076-8954

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PRESERVATIVE: MIL-PRF-16173, CODE 2

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UNSERVICEABLE METHOD: 20

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CLEANING & DRYING: IAW MIL-STD-2073

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MILITARY PRESERVATION IAW MIL-STD-2073

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B) REUSABLE CONTAINER & DUNNAGE DO NOT DESTROY.

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MARKING IAW MIL-STD-129

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001 OR 002

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QUP

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ICQ

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CNTR O.D.

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LEVEL B:

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GROSS WT LBS

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PACKING

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GROSS CU FT

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ASTM D6256 (MOD)

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ASTM D6256 (MOD)

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REV

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DATE

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ORIGINAL

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CHK.

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AUTH.

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SPECIAL PACKAGING INSTRUCTION

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LENGTH WIDTH DEPTH

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LEVEL A LEVEL B

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SPI NO. (TPO)

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SHEET 1 OF 14

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K. KNIGHTON K. RESTORFF S. PEELER N. CORONADO

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1560-01-271-9172 WF

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WING ASSEMBLY, AIRCRAFT

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REVISIONS

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DESCRIPTION

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LTR

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DATE

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MARK THE SPI NUMBER ON THE IDENTIFICATION SIDE OF CONTAINER,

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SERVICEABLE METHOD: 20

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C) LIFT BY BASE ONLY

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MIL-PRF-23827, CODE 11

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D) "HEAVY END"

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UPDATED OD, ADDED DISTRIBUTION STATEMENT AND DESTRUCTION NOTICE

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ADDITIONAL SPECIAL MARKINGS:

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A) DANGEROUS GOODS IN APPARATUS

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B) TYPE AND FLASH POINT OF FUEL

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C) CLASS 9 LABEL

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UN3363

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OPPOSITE SIDE, AND INSPECTION END.

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2169C MOD

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MARCH 87

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FORM

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SPECIAL PACKAGING INSTRUCTION

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SPI NO. (TPO)

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SHEET 2 OF 14

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ITEM NOMENCLATURE

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CODE ID

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REQD

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QTY

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DESCRIPTION

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NOMENCLATURE OR

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SPECIFICATION

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MATERIAL

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AutoCAD SHX Text DATOED CLEAT DATOED CLEAT BOLT, CARRIAGE BOLT, CARRIAGE STRAP REINFCMNT BLK METAL STRAP D-RING SORBENT MATERIAL TAPE, MASKING WRAP CLEAT, MOUNTING END CLEAT, MOUNTING END CLEAT, MOUNTING SIDE CLEAT, MOUNTING SIDE CLEAT, MOUNTING SIDE REINFRCMNT, SMALL CENTER SUPPORT SMALL VERTICAL CENTER SUPPORT REINFRCMNT, SMALL VERTICAL SUPPORT SMALL VERTICAL SIDE SUPPORT REINFORCEMENT, SMALL CRADLE END CRADLE, SMALL END BRACE, CENTER, LUMBER LUMBER, SLOTTED, BRACE BOLT, CARRIAGE SUPPORT, CENTER, VERTICAL BOLT, CARRIAGE SLOTTED METAL TIE BOLT, CARRIAGE REINFORCEMENT, CRADLE CRADLE, LARGE END REINFCEMNT, LG CENTER SUPPORT LARGE VERTICAL CENTER SUPPORT BARRIER WRAP FELT RIENFCMNT, LG VERTICAL SUPPORT LARGE VERTICAL SIDE SUPPORT WASHER, PLAIN NUT, HEX BOLT, CARRIAGE BOLT, CARRIAGE BOLT, CARRIAGE SADDLE HEADER DECK SKID RUB, CENTER RUB, END RUB, END (HEAVY END)

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AutoCAD SHX Text ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASME B18.5 ASME B18.5 A-A-55057 TYPE A QQ-S-689 QQ-S-689 LOCAL PURCHASE 4235-01-308-5150 ASTM D6123 TYPE I OR II A-A-3174 TYPE I, CL 1, GRADE A, FINISH 1 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 A-A-55057 TYPE A ASTM D6199 CLASS 2 A-A-55057 TYPE A ASTM D6199 CLASS 2 A-A-55057 TYPE A ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASME B18.5 ASTM D6199 CLASS 2 ASME B18.5 MIL-S-21041 UNIT A, TYPE 4, CLASS 3 ASME B18.5 A-A-55057 TYPE A ASTM D6199 CLASS 2 A-A-55057 TYPE A ASTM D6199 CLASS 2 MIL-PRF-131 CLASS 1 ASTM D2475 A-A-55057 TYPE A ASTM D6199 CLASS 2 ASME B18.21.1 FF-N-836 TYPE II, STYLE 4 ASME B18.5 ASME B18.5 ASME B18.5 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 A-A-55057 TYPE A ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2 ASTM D6199 CLASS 2

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WING ASSEMBLY, AIRCRAFT

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PACKING AND UNPACKING METHODS:

PRIMARY METHOD: TO PACK/UNPACK-LAY CRATE DOWN USING METAL LOWERING STRAPS, REF.-43. REMOVE LAG

BOLTS, REF.-50, FROM THE SIDE DESIRED TO BE PACKED/UNPACKED AND REMOVE INNER BRACING. WINGS WILL

THEN BE LIFTED IAW ITEM T.O. 1F-16CG-3-5 TO PACK/UNPACK THE WING ON THE OPPOSITE SIDE - BLOCKING, BRACING AND CRATE WALLS ALONG WITH LAG BOLTS MUST BE IN PLACE BEFORE TURNING CRATE OVER. REPEAT THE

SAME PROCESS DESCRIBED ABOVE TO PACK/UNPACK THE SECOND WING.

ALTERNATE METHOD: APPROVED ALTERNATIVE METHOD TO PACK/UNPACK-LAY CRATE DOWN ON SIDE DESIRED TO

BE PACK/UNPACK USING METAL LOWERING STRAPS REF.-44 AND REMOVE LAG BOLTS, REF.-51, THEN REMOVE INNER

BRACING. WINGS WILL BE LIFTED WITH TEST RATED/CERTIFIED STRAPS APPROPRIATE FOR THE WEIGHT OF THE

INDIVIDUAL WING. INTERLOCK STRAPS AROUND INBOARD AND OUTBOARD REGIONS. THE PACKAGER WILL ENSURE

THAT STRAPS ARE WRAPPED SECURELY ALLOWING FOR NO MOVEMENT OR DAMAGE DURING HANDLING.

SIMULTANEOUSLY USE TWO MACHINE HOISTS TO EVENLY LIFT THE WING. TO PACK/UNPACK OPPOSITE SIDE -

BLOCKING, BRACING, CRATE WALLS, AND LAG BOLTS MUST BE IN PLACE AND SECURED BEFORE TURNING CRATE

OVER. REPEAT THE SAME PROCESS DESCRIBED ABOVE TO PACK/UNPACK THE SECOND WING.

PACKING AND UNPACKING THE WINGS MUST BE DONE WHILE THE WING IS HORIZONTAL. ONCE WINGS ARE SECURED

AND BRACED, THE CRATE CAN BE RAISED AND STORED IN A VERTICAL POSITION.

NOTES:

1. ALL CLEATS SHALL BE 1 X 4 LUMBER. THE NOTED GROSS WEIGHT IS FOR A CRATE PACKED WITH ONE RIGHT WING

AND ONE LEFT WING, FOR A TOTAL OF TWO WINGS INSIDE THE CRATE. THE GROSS WEIGHT OF THE CRATE WILL VARY

IF ONLY ONE WING IS PACKED INSIDE THE CRATE.

2. APPLY PRESERVATIVE MIL-PRF-16173, CODE 2, TO AXLES, CYLINDERS AND BUSHINGS. APPLY PRESERVATIVE

MIL-PRF-23827, CODE 11, TO BEARINGS. COVER TREATED PARTS WITH BARRIER WRAP, REF.-16, AND SECURE WITH

TAPE, REF.-40.

3. USE NAILS OR STAPLES CONFORMING TO ASTM F1667 IN ALL APPLICATIONS THAT ARE NOT SPECIFIC.

4. ALL SADDLE, CONTOURS, AND BRACES SHALL BE ADEQUATELY PROTECTED WITH FELT, REF.-15, AND BARRIER, REF.-16, TO PREVENT THE ITEM FROM COMING INTO CONTACT WITH WOOD AND TO PREVENT FELT FROM RETAINING MOISTURE

AGAINST THE WING. AFFECTED PARTS INCLUDE: REF.-7, -13, -14, -17, -18, -19, -20, -26, -28, -29, -30, -31, -32 & -33.

5. CONTAINER SIDES ARE CONSTRUCTED IN TWO (2) PIECES. THESE ARE TO BE LAG BOLTED INTO INTO THE CENTER

SUPPORT, REF.-24.

6. METAL STRAPS, REF.-43, AND THE STRAP REINFORCEMENT, REF.-44, SHALL BE LOCATED 48 INCHES FROM EACH END OF

THE CONTAINER, USING THE OUTSIDE CLEAT FOR STABILITY AS SHOWN IN ILLUSTRATIONS.

7. CUT A 10 INCH SQUARE HOLE CENTERED ON EACH END AND UP FROM BOTTOM OF END PANEL 50 INCHES FOR

INSPECTION WINDOW, REF.-49. PLACE HANDLE, REF.-50, ON INSPECTION DOOR, REF.-49, PRIOR TO INSTALLATION.

8. RUBS, REF.-1, -2, -3, SHALL BE BOLTED TO SKIDS, REF.-4, WITH BOLTS, REF.-8, APPROX. TWO INCHES FROM EACH RUB

END AND END RUBS, REF.-1 AND -2, WILL HAVE ONE ADDITIONAL BOLT PLACED NEAR THE CENTER.

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2169C MOD

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MARCH 87

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FORM

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COMPUTER GENERATED

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SPECIAL PACKAGING INSTRUCTION

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SPI NO. (TPO)

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SHEET 3 OF 14

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ITEM NOMENCLATURE

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CODE ID

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WING ASSEMBLY, AIRCRAFT

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REQD

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QTY

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DESCRIPTION

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NOMENCLATURE OR

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SPECIFICATION

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MATERIAL

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WASHER, PLAIN BOLT, LAG HANDLE INSPECTION DOOR

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1/4 2 1/2 X 1/4 1 X 2 (NOM) X 3 11 X 11 X 5/16

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ASME B18.21.1 ASME B18.2.1 ASTM D6199 CLASS 2 A-A-55057 TYPE A

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F01-076-8954

CAUTION NOTICES

NOTICE 1: ASSETS PACKAGED IN ACCORDANCE WITH PREVIOUS EDITIONS OF THIS SPI DO NOT REQUIRE

REPACKAGING IF INTEGRITY OF THE SPI IS MAINTAINED.

NOTICE 2: SEE SPIRES FOR A COMPLETE LISTING OF NSN's ASSIGNED TO THIS SPI.

NOTICE 3: PACKAGING MATERIAL MAY BE SUBSTITUTED IF IT MEETS THE REQUIREMENTS OF MIL-STD-2073, PROVIDES EQUAL OR BETTER PROTECTION AND THERE IS NO INCREASED COST TO THE GOVERNMENT.

NOTICE 4: LEVEL A PROTECTION REQUIRED TO MEET THE MOST SEVERE WORLDWIDE SHIPMENT, HANDLING, AND

STORAGE CONDITIONS. EXAMPLES OF SITUATIONS ARE: WAR RESERVE MATERIAL, MOBILIZATION, STRATEGIC AND

THEATER DEPLOYMENT, OPEN STORAGE AND DECK LOADING. SECURITY ASSISTANCE ITEMS, INCLUDING FMS, ARE

ESPECIALLY SUSCEPTIBLE TO DAMAGE DUE TO UNKNOWN AND UNFAVORABLE TRANSPORTATION, CLIMATIC, AND

STORAGE CONDITIONS. PROVIDE LEVEL B PACKING UNLESS OTHERWISE DIRECTED BY THE PROCURING COUNTRY.

CAUTION NOTES

1c. D-RINGS, REF-42, ARE FOR RAISING AND LOWERING CRATE FROM A VERTICAL POSITION TO A HORIZONTAL POSITION

AND SHALL NOT BE USED FOR LIFTING CRATE.

2c. "HEAVY END" MUST BE MARKED ON BOTH SIDES OF THE CONTAINER IN THE APPROPRIATE AREA FOR CLEAR VISIBILITY

DURING MOVEMENT.

3c. I.D. TAGS MUST BE STAMPED BY RESPONSIBLE PARTY SIGNIFYING ITEM HAS BEEN PREPARED FOR SHIPMENT/STORAGE

IAW APPLICABLE T.O.

4c. ITEMS WHICH HAVE BEEN DRAINED AND PURGED MUST BE ACCOMPANIED WITH A COMPLETED AFTO FORM 20 OR

LOCALLY PRODUCED DOCUMENTATION CERTIFYING THE ITEM HAS BEEN PROPERLY DRAINED AND PURGED.

5c. ITEMS WHICH HAVE RESIDUAL FUEL MUST BE PACKED WITH SORBENT MATERIAL, REF.-41, LINING THE BOTTOM OF

CONTAINER, THIS IS NOT A REQUIREMENT FOR (CCA) CONDITION CODE A ITEMS. SORBENT MATERIAL MUST BE

INSPECTED PRIOR TO RE-USE.

6c. IF APPLICABLE: MARK TYPE AND FLASH POINT OF PURGING FLUID IAW AFI 24-203, 4.3.3 AND AFMAN 24-204_IP.

A.3.3.9.5.4.

INTERNATIONAL STANDARDS FOR PHYTOSANITARY MEASURES

REVISION OF ISPM NO. 15

REVISION OF WOOD PACKAGING MATERIAL FOR INTERNATIONAL TRADE

THE FOLLOWING STATEMENT IS IN COMPLIANCE WITH THE UNITED NATIONS-IMPLEMENTED RESTRICTIONS ON WOOD

PACKAGING MATERIAL (WPM). THIS REQUIREMENT IS SPECIFICALLY CONCERNED WITH INVASIVE SPECIES SUCH AS THE

PINEWOOD NEMATODE. WPM IS DEFINED AS WOOD PALLETS, SKIDS, LOAD BOARDS, PALLET COLLARS, WOODEN BOXES, REELS, DUNNAGE, CRATES, FRAMES, AND CLEATS. THE STATEMENT BELOW CITES THE REQUIREMENTS IN DETAIL AND

COVERS LUMBER FOR BUILDING CONTAINERS AND PALLETS USED FOR DELIVERIES, RESULTING IN SHIPMENTS WORLDWIDE

(DIRECT, OR THROUGH AIR LOGISTICS CENTERS (ALC), CONTAINER CONSOLIDATION POINTS (CCP), OR OTHER BASES).

WOODEN LUMBER, WOODEN PALLET AND PACKAGING/CONTAINER STATEMENT:

ALL WOODEN LUMBER, WOODEN PALLETS, AND WOODEN CONTAINERS PRODUCED ENTIRELY OR IN PART OF WOOD

PACKAGING MATERIAL (WPM) SHALL BE CONSTRUCTED FROM DEBARKED WOOD IN ADDITION TO THE APPLICATION OF

HEAT-TREATED (HT) MATERIAL (HT TO 56 DEGREES CENTIGRADE OR 133 DEGREES FAHRENHEIT FOR 30 MINUTES).

CERTIFICATION/MARKING IS REQUIRED BY AN ACCREDITED AGENCY RECOGNIZED BY THE AMERICAN LUMBER STANDARDS

COMMITTEE (ALSC). FOR REFERENCE DOCUMENTATION, SEE LATEST REVISION OF "INTERNATIONAL STANDARDS FOR

PHYTOSANITARY MEASURES (ISPM NO. 15), "REGULATION OF WOOD PACKAGING MATERIAL IN INTERNATIONAL TRADE."

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DETAIL A

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DETAIL B

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2169C MOD

AutoCAD SHX Text

MARCH 87

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 7 OF 14

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text 98747

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

DETAIL D

AutoCAD SHX Text

DETAIL C

AutoCAD SHX Text

AutoCAD SHX Text I

AutoCAD SHX Text

AutoCAD SHX Text J

AutoCAD SHX Text -7

AutoCAD SHX Text -26

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

AutoCAD SHX Text

2169C MOD

AutoCAD SHX Text

MARCH 87

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 8 OF 14

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text 98747

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

1 EA. SANDWICHED WITH 5/16 PLYWOOD

AutoCAD SHX Text 30 X 11 1/2 X 5/16

AutoCAD SHX Text

1 EA. SANDWICHED WITH 5/16 PLYWOOD

AutoCAD SHX Text

DETAIL F SMALL CRADLE

AutoCAD SHX Text

DETAIL E LARGE CRADLE

AutoCAD SHX Text

AutoCAD SHX Text I

AutoCAD SHX Text

AutoCAD SHX Text I

AutoCAD SHX Text -19

AutoCAD SHX Text -20

AutoCAD SHX Text -28

AutoCAD SHX Text -29

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

AutoCAD SHX Text

2169C MOD

AutoCAD SHX Text

MARCH 87

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 9 OF 14

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text 98747

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

DETAIL G

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

AutoCAD SHX Text

7/16 SQUARE HOLES CENTERED ON PLATE

AutoCAD SHX Text

FILLET WELD BOTH SIDES

AutoCAD SHX Text

2169C MOD

AutoCAD SHX Text

MARCH 87

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 10 OF 14

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text 98747

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

AutoCAD SHX Text

62 PLCS.

AutoCAD SHX Text

62 PLCS.

AutoCAD SHX Text

8 PLCS.

AutoCAD SHX Text

2 PLCS.

AutoCAD SHX Text

2 PLCS.

AutoCAD SHX Text

2 PLCS.

AutoCAD SHX Text

8 PLCS.

AutoCAD SHX Text

8 PLCS.

AutoCAD SHX Text

8 PLCS.

AutoCAD SHX Text

14 PLCS.

AutoCAD SHX Text

4 PLCS.

AutoCAD SHX Text

DETAIL H

AutoCAD SHX Text

DETAIL I

AutoCAD SHX Text

DETAIL J

AutoCAD SHX Text

RUB PLACEMENT

AutoCAD SHX Text

BLOCKING PLACEMENT

AutoCAD SHX Text

BOLT PLACEMENT

AutoCAD SHX Text

8 PLCS.

AutoCAD SHX Text

2 PLCS.

AutoCAD SHX Text

2 PLCS.

AutoCAD SHX Text C

AutoCAD SHX Text A

AutoCAD SHX Text B

AutoCAD SHX Text E

AutoCAD SHX Text F

AutoCAD SHX Text D

AutoCAD SHX Text F01-076-8954

INSPECTION WINDOW

AutoCAD SHX Text

INSPECTION

AutoCAD SHX Text

WINDOW

AutoCAD SHX Text

AutoCAD SHX Text 84 34

AutoCAD SHX Text

DETAIL K

AutoCAD SHX Text

2169C MOD

AutoCAD SHX Text

MARCH 87

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 11 OF 14

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text 98747

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

MARCH 87

AutoCAD SHX Text

2169C MOD

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 12 OF 14

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text 98747

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

AutoCAD SHX Text B

AutoCAD SHX Text D

AutoCAD SHX Text A

AutoCAD SHX Text

AutoCAD SHX Text G

AutoCAD SHX Text

AutoCAD SHX Text C

AutoCAD SHX Text F01-076-8954

AutoCAD SHX Text

2169C MOD

AutoCAD SHX Text

MARCH 87

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 13 OF 14

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text 98747

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

AutoCAD SHX Text

ITEM ITEM REFERENCE

AutoCAD SHX Text

ITEM ITEM REFERENCE

AutoCAD SHX Text 5c

AutoCAD SHX Text

DETAIL L

AutoCAD SHX Text

SPECIAL PACKAGING INSTRUCTION

AutoCAD SHX Text 98747

AutoCAD SHX Text

2169C MOD

AutoCAD SHX Text

MARCH 87

AutoCAD SHX Text

FORM

AutoCAD SHX Text

COMPUTER GENERATED

AutoCAD SHX Text

ITEM NOMENCLATURE

AutoCAD SHX Text

SPI NO. (TPO)

AutoCAD SHX Text

SHEET 14 OF 14

AutoCAD SHX Text

CODE ID

AutoCAD SHX Text

WING ASSEMBLY, AIRCRAFT

AutoCAD SHX Text

HEAVY HEAVY END

AutoCAD SHX Text

HEAVY HEAVY END

AutoCAD SHX Text

INSPECTION WINDOW

AutoCAD SHX Text

MARK "HEAVY END" ON BOTH SIDES

AutoCAD SHX Text

AutoCAD SHX Text K

File details come from the government source that posted it. Updated Dec 19, 2024.