706E001 TDP 05SEP2024.pdf

PDF 15 MB Posted Sep 5, 2024

Attached to: SHIPPING AND STORAG Federal contract opportunity
Solicitation number: N0038324QC543
Issued by: Department of the Navy Naval Supply Systems Command

About this file

Written by GovTribe AI · Sep 5, 2024

This document is a Request for Proposal (RFP) for a federal contract opportunity to provide shipping and storage containers. The key details are:

The solicitation is for the procurement of an inner-frame and outer-shell container for the T56 QECA engine. The contract will be awarded to the responsible offeror whose proposal is most advantageous to the government, with non-price factors (relevant past performance and technical capability) being significantly more important than price. Offerors must demonstrate their ability to manufacture and test the containers per the applicable drawings, specifications, and requirements. A first article test will be required for new manufacturers, with the cost of testing to be added to the offeror's price. Alternate offers may be submitted requesting a waiver of the first article test requirement if certain criteria are met. The period of performance and delivery schedule will be adjusted if the first article requirement is waived. All costs related to the first article testing and shipping are the responsibility of the contractor.

View the file

On GovTribe

Work with this file on GovTribe

Download the original file
Contacts named in this file
Similar government files
Ask GovTribe AI about this file

Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

DPB

RMS

FCL

02/97

SEALING FLANGE

EXTRUSION

02/19/97

13C099

SEE NOTE 3ALUM 6061-T6COVER TUBE EXTRUSION13C099-1

FSCM

NO.

QTY

REQ'D

PART NO.

IDENTIFY NUMBER

DATA: SPECIFICATION

NOTES, VENDORSNO.

ITEM

LENGTH

OD/ID

WIDTH

GAUGE

THICK

MATERIAL

NOMENCLATURE

OR DESCRIPTION

PARTS LIST

A REDRAWN & ADDED ITEMS 3 & 4 01/13/04 DPB/RMS

ZONE REV DESCRIPTION

REVISIONS

DATE APPROVED

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

ARE IN INCHES

SPECIFIED DIMS

UNLESS OTHERWISE

USED ON

APPLICATION

NEXT ASSEMBLY

REVSIZE

DATE

DATEAPPROVED BY

GOV'T APVD BY

CHECKED BY

DRAWN BY

DATE:

CONTRACT NUMBER

SHEET:WEIGHT:SCALE:

CODE IDENT NO. DWG NO.

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

C 05259

D D

4 3 2 1

2 SEE NOTE 3ALUM 6061-T6BASE EXTRUSION13C099-2

STANDARD ALUM

ASSOC TOL. APPLY

PER ANSI H35.2,

UNLESS OTHERWISE

SPECIFIED

3 SEE NOTE 3ALUM 6061-T6COVER TUBE EXTRUSION, WELDED13C099-3

4 SEE NOTE 3ALUM 6061-T6BASE EXTRUSION, WELDED13C099-4

5 SEE NOTE 3ALUM 6061-T6BASE EXTRUSION13C099-5

B ADDED ITEM 5 01/13/09 GC

NOTES:

1. ALL EDGES AND CORNERS TO BE BROKEN BY .015 R,

UNLESS OTHERWISE SPECIFIED.

2. IDENTIFY IN ACCORDANCE WITH MIL-STD-130.

3. ALUM ALLOY 6061-T6 SHALL CONFORM TO ASTM B221.

4. ESTIMATED WEIGHT FOR ITEM 1 = 6.59 LBS/FT.

ESTIMATED WEIGHT FOR ITEM 2 = 5.74 LBS/FT.

ESTIMATED WEIGHT FOR ITEM 3 = 6.62 LBS/FT.

ESTIMATED WEIGHT FOR ITEM 4 = 5.77 LBS/FT.

ESTIMATED WEIGHT FOR ITEM 5 = 5.00 LBS/FT.

ISOMETRIC VIEW -1ISOMETRIC VIEW -2

.52

.63 2.06R .256X

3.00

3.382X .502X

.092X

.502X

3.125 +.030 -.0002X

.252X

.062X

R .062X

.31

.79

1.65

R .50

R .290.728.78

.617

.75

2.69

1.58

.44

R FULL

4.442X

105°4X

45°2X

.382X

.06 .06 X 45v CHAMFER

1.97

R .50

R .12 1.279

R .25

R .50

.31

R .122X

1.605

.420

3.63

R .092X

110°2X

.31

5.19

5.50

.062X

.502X

R .062X

3.125 +.030 -.000

.252X

.092X

45°2X

6.942X

.255.000 +.015 -.000

.06 X 45v CHAMFER

.06

5.872X

.502X

105°2X

DETAIL A

R .09

.400

.800

R .024X

R .062X

.6882X.1402X

70°2X

R .25

1.812

.350

.700 CL

DESTRUCTION NOTICE:

DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS OR

RECONSTRUCTION OF THE DOCUMENT.

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 EXECUTIVE

ORDER 12470. VIOLATIONS OF THESE EXPORT LAWS ARE SUBJECT TO SEVERE CRIMINAL

PENALTIES.

DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THERE

CONTRACTORS, ADMINISTRATION / OPERATIONAL USE, OTHER REQUESTS FOR THIS

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

13C099 B

2RMSDPD

02/19/97

DWG NO.FSCM NO.

05259C

SIZE

CHK BY:DWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

SCALE: WEIGHT: SHEET:

REV

ZONE REV DESCRIPTION

REVISIONS

DATE APPROVED

D D

4 3 2 1

6.712XR .06

4 SAME AS ITEM 2, EXCEPT AS SHOWN

4.262X

3 SAME AS ITEM 1, EXCEPT AS SHOWN

ISOMETRIC VIEW -3ISOMETRIC VIEW -4

R .06

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

.382X

.06 .06 X 45v CHAMFER

1.97

R .50

R .12 1.279

R .25

R .50

.31

R .122X

1.605

.420

3.63

R .092X

110°2X

.31

5.19

5.50

.255.000 +.015 -.000

.06 X 45v CHAMFER

.06

1.03

RED

RMS

FCL

01/97

JOINT, ANGLED PANEL

EXTRUSION

01/22/97

13C102

CODE

IDENT

QTY

REQ'D

PART NO.

IDENTIFY NUMBER

DATA: SPECIFICATION

NOTES, VENDORSNO.

ITEM

LENGTH

OD/ID

WIDTH

GAUGE

THICK

MATERIAL

NOMENCLATURE

OR DESCRIPTION

PARTS LIST

B REDRAWN & ADDED -2 01/14/04 DPB/RMS

ZONE REV DESCRIPTION

REVISIONS

DATE APPROVED

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

ARE IN INCHES

SPECIFIED DIMS

UNLESS OTHERWISE

USED ON

APPLICATION

NEXT ASSEMBLY

REVSIZE

DATE

DATEAPPROVED BY

GOV'T APVD BY

CHECKED BY

DRAWN BY

DATE:

CONTRACT NUMBER

SHEET:WEIGHT:SCALE:

CODE IDENT NO. DWG NO.

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

C 05259

D D

4 3 2 1

SEE NOTE 4ALUM 6061-T6JOINT, ANGLED PANEL EXTRUSION13C102-11

STANDARD ALUM

ASSOC TOL. APPLY

PER ANSI H35.2,

UNLESS OTHERWISE

SPECIFIED

SEE NOTE 4ALUM 6061-T6JOINT, ANGLED PANEL EXTR WELDED13C102-21

NOTES:

1. ALL EDGES AND CORNERS TO BE BROKEN BY .015 R..

UNLESS OTHERWISE SPECIFIED.

2. IDENTIFY IN ACCORDANCE WITH MIL-STD-130.

3. ESTIMATED WEIGHT = 4.51 LBS/FT.

4. AREA = 3.83 IN SQ.

5. ALUM ALLOY 6061-T6 SHALL CONFORM TO ASTM B221.

ISOMETRIC VIEW FOR -1

DETAIL A

45°

R .375

R .625

R .187

.252X

3.125 +.030 -.0002X

.252X

.064X

.504X

.2502X

.3754X

R .25

1.4382X

R .064X

R .50

R .045

45°

105°2X .09

.50

1.9384X

1.7524X

1.2522X R .064X

ISOMETRIC VIEW FOR -2

DESTRUCTION NOTICE:

RED

RMS

FCL

01/97

JOINT, ANGLED PANEL

EXTRUSION

01/22/97

13C102

CODE

IDENT

QTY

REQ'D

PART NO.

IDENTIFY NUMBER

DATA: SPECIFICATION

NOTES, VENDORSNO.

ITEM LENGTHOD/ID

WIDTH

GAUGE

THICKMATERIALNOMENCLATURE

OR DESCRIPTION

PARTS LIST

B REDRAWN & ADDED -2 01/14/04 DPB/RMS

ZONE REV DESCRIPTION

REVISIONS

DATE APPROVED

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

ARE IN INCHES

SPECIFIED DIMS

UNLESS OTHERWISE

USED ON

APPLICATION

NEXT ASSEMBLY

REVSIZE

DATE

DATEAPPROVED BY

GOV'T APVD BY

CHECKED BY

DRAWN BY

DATE:

CONTRACT NUMBER

SHEET:WEIGHT:SCALE:

CODE IDENT NO. DWG NO.

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

C 05259

D D

4 3 2 1

SEE NOTE 4ALUM 6061-T6JOINT, ANGLED PANEL EXTRUSION13C102-11

STANDARD ALUM

ASSOC TOL. APPLY

PER ANSI H35.2,

UNLESS OTHERWISE

SPECIFIED

SEE NOTE 4ALUM 6061-T6JOINT, ANGLED PANEL EXTR WELDED13C102-21

NOTES:

1. ALL EDGES AND CORNERS TO BE BROKEN BY .015 R..

UNLESS OTHERWISE SPECIFIED.

2. IDENTIFY IN ACCORDANCE WITH MIL-STD-130.

3. ESTIMATED WEIGHT FOR ITEM 1 = 4.64 LBS/FT.

ESTIMATED WEIGHT FOR ITEM 2 = 4.72 LBS/FT.

4. ALUM ALLOY 6061-T6 SHALL CONFORM TO ASTM B221.

ISOMETRIC VIEW FOR -1

DETAIL A

45°

R .375

R .625

R .187

.252X

3.125 +.030 -.0002X

.252X

.064X

.504X

.2502X

.3754X

R .25

1.4382X

R .064X

R .50

R .045

45°

105°2X .09

.50

1.9384X

1.7524X

1.2522X R .064X

ISOMETRIC VIEW FOR -2

DESTRUCTION NOTICE:

DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS OR

RECONSTRUCTION OF THE DOCUMENT.

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 EXECUTIVE

ORDER 12470. VIOLATIONS OF THESE EXPORT LAWS ARE SUBJECT TO SEVERE CRIMINAL

PENALTIES.

DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THERE

CONTRACTORS, ADMINISTRATION / OPERATIONAL USE, OTHER REQUESTS FOR THIS

RMS 08/03

08/03

8/15/07

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CAGE CODE

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015 ±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16 2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

8 7 6 5 4

2 13

DPB

RMS

LATCH ASSEMBLY

17E070 B

-1

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CAGE

CODE OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST

10/18/06 FCLA REMOVED WELD SYMBOL AND INSTEAD

REFERRED LATCH WELDING TO THE

APPLICABLE WELDMENT DRAWING(S)

T-56 QECA

1 17E070-1 LATCH ASSEMBLY

CAD MAINTAINED BY SOLID EDGE; CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

ASTM B221, SEE NOTE 15.503.002.44ALUM 6061-T6BRACKET17E070-221

McMASTER CARR OR EQUIV18-8 SSSHOULDER SCREW90298A7073942832

10 GAGE, SEE NOTES 4 & 59.257.576.134ASTM A569 STEELHANDLE17E070-441

ASTM B2114.4201.0 ODALUM 2017-T451HANDLE PIN17E070-551

ASTM A5644.370.50 ODSS 17-4 PHSWING PIN17E070-661

SEE NOTE 51.751.501.004140 STEELSWING NUT17E070-771

SEE NOTE 52.502.25.8754140 STEELCLAMP17E070-881

ASTM A5645.00.50 DSS 17-4 PHCLAMP BOLT17E070-991

ASTM A2101.22.63 D x .058 WALUM 6061-T6SPACER17E070-10102

McMASTER CARR OR EQUIV.51 ID x .88 OD.062UHMW POLYFLAT WASHER95649A24439428112

FLAT WASHERAN960C816122

18-8 SSHEX NUT1/2-13 UNC132

18-8 SSLOCK NUT WITH NYLON INSERT3/8-16 UNC142

CIBA, SEE NOTES 2 & 3ARALDITE METAL BONDING201315AR

8/13/07 GCB MINOR CHANGES PER CUSTOMER

COMMENTS. ADDED SECTION VEIW,

REMOVED HIDDEN LINES, MOVED

BALLOONS AROUND, AND ADDED BRAKE

AWAY LINES TO BOTTOM LEFT VIEW.

ADDED 3 PLS TO DIMENSION ON ITEM 22.

DESTRUCTION NOTICE:

BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OR EXECUTIVE ORDER 12470. VIOLATIONS OF THESE EXPORT LAWS ARE SUBJECT

TO SEVERE CRIMINAL PENALTIES.

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

ITEM 2 REMOVED FOR CLARITY

PEAN OR ROLL FORM AS

REQUIRED (BOTH SIDES)

6ROLL FORM AS REQUIRED

(BOTH SIDES)

32X

9 SEE NOTE 2

14 2X

11 LOCATE BETWEEN ITEMS 2 & 4 (BOTH SIDES)

TYPICAL INSTALLATION TO EXTRUSTIONS

.50

(13C099-1)

(13C099-2)

NOTES:

1. STANDARD ALUMINUM ASSOCIATION TOLERANCES APPLY PER

ANSI H35.2 FOR ITEM 2.

2. ITEM 15 TO BE APPLIED IN ACCORDANCE WITH MANUFACTURER’S

INSTRUCTIONS WITH ONE DROP APPLIED TO BOTH THREADS.

3. ALTERNATE HYSOL 9460 STRUCTURAL ADHESIVE.

4. HOT ROLLED, PICKLED AND OILED.

5. ZINC NICKEL PLATE PER ASTM-B841, CLASS 1, TYPE B, GRADE 3.

2.875

THREADS IN ITEM 9

15 APPLY TO ITEMS 7 & 9 PRIOR TO ENGAGEMENT

4.38

ITEM 9 FULLY THREADED IN ITEM 7

WELD PER APPLICABLE WELDMENT DRAWING

ASECTION A-A

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

8/15/07

DWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

CHK BY:

SIZE CAGE CODE

05259

DWG NO.

WEIGHT:SCALE: SHEET:

REV

8 7 6 5 4

2 13

17E070 B

DPB RMS

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

1.062

3.000

1.520

R .5004XO .502

+.005

- .000 IN LINE DRILL

(BOTH WALLS)

2.4382X

.548 4.404 ±.005

5.500

R .2504X

.288 .288

.2502X .187

HOLES REMOVED FOR CLARITY

.375

3.250

.2572X

R .5002X

.4382X

2.1882X

.4382X

.7502X

.4382X

1.9382X

8.0002X

4.250

9.2502X

45°45°

.375

7.625

.625 ±.005

.344 ±.005

.375 ±.005

1.344

O .375 +.005

- .000 THRU BOTH WALLS

s O.500 X 82v (BOTH ENDS)

O .375 +.005

- .000 THRU BOTH WALLS

s O .500 X 82v BOTH ENDS

R .2504X

.500

R .1254X

R .285

R .231 15°

.541

4X .062 X 45v CHAMFER

.634

.200

30°

O .530 THRU

.630

1.250

4.000 ±.005

1.000O

1.500

1.750

R .500

O .502 THRU

.500

1.000

O .417 ` .750

1/2-13 UNC ` .625

.500

.750

2.88 +.50

- .00

.75 +.50

- .00

5.000

1/2-13 UNC

.050 X 45v CHAMFER

.370 +.005

- .0052X O

.500 +.000

- .005O

.200 ±.0052X

.125 ±.0052X.370 +.000

- .0052X O

.875

2.500

1.470

1.976

2.250

2X .200 X 45v CHAMFER

1.250

1.219 ±.005

.625O

O .509

R .2502X

2X UNDERCUT

O .502 +.005

- .000 IN LINE DRILL AFTER

THE ASSEMBLY OF ITEMS 4, 5 & 6.

O .468 BOTH WALLS

.1345 STK

R .5004X

.707 .896 .896 .707

3.981

T-56 QECA

DPB

RMS

08/03

HEAVY DUTY I-BEAM

10/17/03

706B009

ASTM B221ALUM 6061-T6EXTRUSION - HEAVY DUTY I BEAM706B009-1

CAGE

CODE

QTY

REQ'D

PART NO.

IDENTIFY NUMBER

DATA: SPECIFICATION

NOTES, VENDORSNO.

ITEM

LENGTH

OD/ID

WIDTH

GAUGE

THICK

MATERIAL

NOMENCLATURE

OR DESCRIPTION

PARTS LIST

ZONE REV DESCRIPTION

REVISIONS

DATE APPROVED

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

ARE IN INCHES

SPECIFIED DIMS

UNLESS OTHERWISE

USED ON

APPLICATION

NEXT ASSEMBLY

REVSIZE

DATE

DATEAPPROVED BY

GOV'T APVD BY

CHECKED BY

DRAWN BY

DATE:

CONTRACT NUMBER

SHEET:WEIGHT:SCALE:

CAGE CODE DWG NO.

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

B 05259

TOLERANCES ON:

.01 - .03RBREAK EDGES:

-.001 +.007

±.010 ±.015

HOLE SIZES:

BEND R .00 TO .09:

.091 AND ABOVE:

FRACTIONS: 1/16

ANGLES: 1/2°

DECIMALS:

.XX

.XXX

.X ±

.06

.010

EXTRUSION

6.022 +.044 -.000

1.0002X

.375

3.330

3.500

R .187

ISOMETRIC VIEW -A-

1.500

.2502X

2.0002X R .14010X

90° ±0.5

10°4X i .032 A

2.80 ±.03

SEE NOTE 2

SYM

X X

2.0° PER 15 FT MAX.

0v 15 MINUTES PER FT MAX

ALLOWABLE TWIST

NOTES:

1. INTERPRET DRAWING IN ACCORDANCE WITH DOD-STD-100.

2. LENGTH TO BE STRAIGHT WITHIN .006 PER FT.

3. REF DWG 343AS311 REV B, EXTRUSION - I BEAM HEAVY DUTY

FROM THE DEPARTMENT OF THE NAVY, NAVAL AIR SYSTEMS

COMMAND

DESTRUCTION NOTICE:

BY THE ARMS EXPORT COTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OR EXECUTIVE ORDER 12470. VOOLATIONS OF THESE EXPORT LAWS ARE SUBJECT

TO SEVERE CRINMINAL PENALTIES.

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

Ryy

Rxx

Iyy

Ixx

0.78 IN

2.22 IN

5.02 IN

40.7 IN

SECTION PROPERTIES

Zxx TON 12.7 IN

Zyy 2.87 IN

A 8.40 IN

Wt 10.20 LBS/FT

REF INFORMATION

8/16/07

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CAGE CODE

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

1345678

12345678

FCL

CLAMP WELDMENT

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CAGE

CODE OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST

10/19/06 FCLA

ADDED CHAMFER TO ITEM 31.

T-56 QECA

7/28/2011

12/04

CLAMP WELDMENT706D010-1-1-

706D010

ASTM B20910.503.002.00AL 6061-T651CLAMP706D010-2-22

ASTM B22123.593.0OD0.50WAL 6061-T6511TUBE706D010-3-32

ASME B18.6.4; NOTE 7.38#8STEELDRIVE SCREWMS21318-36-42

NASM 35307; NOTE 72.255/8-11GRADE 5 SSHEX HEAD BOLT- MODIFIEDMS35307-465-54

CABLE ASSEMBLYSTD-360-B-8-5-64

NASM 35338; NOTE 75/818-8 SSLOCK WASHERMS35338-145-74

1.502.00D304 SSBOSS706D010-8-81

1.502.00D304 SSBOSS706D010-9-91

10.001.50D17-4 SSTURNBUCKLE706D010-10-101

McMASTER-CARR, NOTE 7.750.250D416 SSDOWEL PIN98380A54039428116

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

ADDED NOTES 9 & 102.

8/13/07 GCB

ADDED T-56 QECA TO "USED ON" SEC. IN

TITLE BLOCK

ADDED MS HARDWARE CALLOUTS FOR

ITEMS 4, 5, & 7

DELETED NOTE 7 & RENUMBERED3.

4X - WRAP CORNERS

NOTE 9.25

2X, WELD MUST NOT

EXTEND BELOW BOTTOM OF ITEM 2

NOTE 9

.19

6X -DRILL O.250 THRU ONE WALL

OF ITEMS 8 AND 9

USING PILOT HOLES IN ITEM 3

FOR ITEM 11

ISOMETRIC VIEW

ITEMS 4-7 REMOVED FOR CLARITY

4. CHEMICAL TREATMENT

AN ACID DEOXIDIZING TREATMENT SHALL BE APPLIED BY

EITHER IMMERSION OR BRUSHING/WIPING. DEOXIDIZERS

ACCEPTABLE FOR USE SHALL INCLUDE NITRIC ACID, SULFURIC

CHROMIC, PHOSPHORIC CHROMIC OR EQUIVALENT

SOLUTIONS. SODIUM HYDROXIDE SOLUTIONS SHALL NOT BE

USED. CARE SHALL BE TAKEN TO ASSURE 100% SOLUTION

COVERAGE OF THE AREA TO BE WELDED. TO ALLOW AN

ADEQUATELY SIZED DEOXIDIZED AREA FOR GOOD WELDING,

THE SOLUTION SHALL BE APPLIED TO AN AREA EXTENDING AT

LEAST 2 INCHES FROM THE WELD SITE, OR ENDING AT ANY

CLOSER ADJACENT EDGE.

5. MECHANICAL MEANS

IMMEDIATELY PRIOR TO WELDING, MECHANICAL CLEANING

METHODS SHALL BE APPLIED TO THE WELD AREA PREVIOUSLY

CHEMICALLY TREATED TO ASSURE REMOVAL OF RESIDUAL OR

REFORMED OXIDES, IF ANY. ACCEPTABLE METHODS OF

MECHANICAL CLEANING INCLUDE STAINLESS STEEL WIRE

BRUSHING, SCRAPING, FILING, OR SANDING. HOWEVER,

ABRASIVES CONTAINING IRON AND ITS OXIDES, STEEL WOOL

AND WIRE, AND COPPER ALLOY BASED WIRE, WHICH MAY

BECOME EMBEDDED WITH GALVANICALLY ACTIVE METALS

AND ACCELERATE CORROSION OF ALUMINUM ALLOYS SHALL

NOT BE USED. MECHANICAL METHODS SHALL BE VIGOROUS

ENOUGH TO ADEQUATELY REMOVE ANY RESIDUAL OXIDE

FILMS, BUT GENTLE ENOUGH TO AVOID FORMING AN

EXCESSIVELY ROUGH SURFACE IN THE COMPARATIVELY SOFT

METAL UNDERNEATH.

6. BREAK ALL SHARP EDGES .020 - .050 RADIUS.

7. ITEM TO BE AS SPECIFIED OR FUNCTIONALLY EQUIVALENT.

8. LIQUID DYE PENETRANT INSPECT WELDS PER ASTM E1417.

9. STEEL STAMP ASSEMBLY PART NUMBER IN .50” LETTERS/

NUMBERS.

1. ALUMINUM WELDING:

WELDING AND WELD INSPECTION SHALL BE IN

ACCORDANCE WITH MIL-W-22248, CLASS 4

EXCEPT THAT:

(1) VISUAL INSPECTION SHALL INCLUDE 5X

(5 POWER) MAGNIFICATION WHEN SUSPECT

CONDITION IS TO BE EXAMINED BEYOND THE

CAPABILITY OF NORMAL VISION.

(2) CRITICAL AND MAJOR WELDS MAY BE

SUBJECTED TO FURTHER NON-DESTRUCTIVE

TESTING (SUCH AS DYE PENETRANT INSPECTION) AS

PRESCRIBED BY THE BUYING ACTIVITY.

PROPER CONTROLS SHALL BE USED TO PREVENT MELT

THROUGH OR BURN THROUGH. WELDER

QUALIFICATION SHALL BE TO AMS-STD-1595. FILLER

FOR WELDING 6061 ALLOY SHALL BE ER-4043 PER AWS

A5.10 FILLER FOR WELDING 5000 SERIES TO

THEMSELVES OR TO 6061 SHALL BE 5356 OR 5556.

2. CLEANING

PARTS TO BE WELDED SHALL BE CHEMICALLY

CLEANED TO REMOVE SURFACE SOILS SUCH AS OILS,

WAXES, GREASE, INKS, ETC. PER MIL-C-5541, EXCEPT

THAT UNINHIBITED ALKALINE SOLUTION SHALL NOT

BE USED.

3. DEOXIDIZING

THE CLEANED PARTS SHALL BE CHEMICALLY

DEOXIDIZED NO MORE THEN 10 DAYS PRIOR TO

WELDING TO REMOVE THICK SURFACE OXIDE FILMS.

(IF THE MATERIAL OR WORK IS EXPOSED TO AN

OUTDOOR ENVIRONMENT, THIS TIME LIMIT SHALL BE

REDUCED TO A MAXIMUM OF 3 DAYS TO ACCOUNT FOR

ATMOSPHERIC EFFECTS). MECHANICAL CLEANING

METHODS SHALL BE APPLIED JUST PRIOR TO THE

ACTUAL START OF WELDING, TO REMOVE ANY

REOXIDATION OR RESIDUAL THIN OXIDE FILMS.

NOTE 10

8/16/07

DWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

CHK BY:

SIZE CAGE CODE

05259

DWG NO.

WEIGHT:SCALE: SHEET:

REV

1345678

12345678

706D010 B

FCL 2

7/28/2011

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

FCL

O .144

1.502X

3.00

2.00

1.00

10.00

1.00

FLAT

.7503X

3X - O.187 THRU ONE WALL

EQUALLY SPACED

1 1/4-7 UNC

4.002X

1 1/4-7 UNC LH

1 1/4-7 UNC

1.00

2.00

1.125

.38R

3.000

.50

.56

1.12

MIN. UNDERCUT

10.50

1.750

2.750

.19 X 45v CHAMFER

ALL AROUND CUTOUT - 2X

1.50 CUTOUT IN TUBE

2.25

.75

REMOVE THREADS/TURN

SHANK TO MINOR O

O 2.00

PRESS FIT WITH ITEM 3 O 2.00

PRESS FIT WITH ITEM 3

1.50 1.50

23.59

1.502X

R .56

2.0655.500

3.00 CUTOUT IN TUBE

1.5003X

O .6562X

145°

3.71

1 OF 11/2

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CAGE CODE

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

1345678

12345678

FCL

IFAA RESTRAINT

BELT ASSEMBLY

-1

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CAGE

CODE OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST

10/19/06 FCLA

ADDED NOTES 3 & 41.

T-56 QECA

7/28/2011

12/04

IFAA RESTRAINT BELT ASSEMBLY706D012-1-1

706D012

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

ITEMS 3 & 4 WERE .187 THICK2.

SLOT TO SLOT LENGTH WAS 60.003.

2/19/07 FCLB

ADDED NOTES 5 & 61.

ADDED PULL TEST DIAGRAM2.

8/13/07 GCC

ADDED ADDITIONAL INFO. TO NOTE 31.

ADDED T-56 QECA TO "USED ON" SEC. IN

TITLE BLOCK

ADDED SCALE INFO TO BMI3.

8/10/07 GCD

ADDED RADIUS CALLOUT - WAS: NONE1.

ADDED RADIUS CALLOUT - WAS: NONE2.

C4 SH 1

D8 SH1

11/19/10 CMHE ADDED NOTE 7A8 SH 1

12/7/10 CMHF ADDED NOTE 81.A8 SH 1

CMHADDED NOTE2.B5 SH 1

CMHADDED TOLERANCE3.B4 SH 1

NOTE 5, NOTE 7-1

6'' u .50 OVERLAP - STITCHING

TO BE AS REQUIRED TO MEET

NOTE 3

5000 LB BREAKING STRENGTH2.00NYLONBELT - WEBBING706D012-2-21

NOTE 24.943.250.25ASTM A36RAIL HOOK END706D012-3-31

NOTE 25.563.250.25ASTM A36RAIL HOOK END706D012-4-41

6'' u .50 OVERLAP - STITCHING

TO BE AS REQUIRED TO MEET

NOTE 3

NOTES:

1) BREAK ALL SHARP EDGES .020 - .050 RADIUS.

2) ZINC-NICKEL PLATE PER ASTM B841, CLASS 1, TYPE B,

GRADE 3.

3) BELT ASSEMBLY TO BE PULL TESTED TO 6,900 LBS AFTER

END CLIPS ARE SEWN. PULL TEST TAG TO BE ATTACHED

WITH DATE OF TEST AND LOAD.

4) STEEL STAMP ASSEMBLY PART NUMBER IN .50”

LETTERS/NUMBERS.

5) APPROVED SOURCE OF SUPPLY: I & I SLING INC.

2626 MARKET STREET

ASTON, PA 19104

610-485-8500

WWW.IANDISLING.COM

USE OF ANY OTHER SOURCE REQUIRES A FIRST ARTICLE

PULL TEST PER NOTES 3 & 6.

6) PULL TEST REQUIREMENTS:

A) HOOK END MUST ENGAGE A “T” SHAPED

STRUCTURE WITH A 3.33” WIDE X .25” THICK

FLANGE WITH A .50” THICK STEM.

B) BOLT PLATE END TO BE BOLTED IN PLACE

C) STRAP SHALL BE TAUT, NOT JERKED.

D) PULL ANGLE/DIMENSIONS MUST BE MAINTAINED.

E) FORCE TO BE APPLIED AS SHOWN

7) DIMENSION LENGTH IS PRIOR TO PROOF TEST. AFTER

TEST, LENGTH MAY INCREASE UP TO .75”

8) SLEEVE PROTECTION OPTIONAL

VIEW B-B

3.25

.50

2.25

.88

.25

1.25 .75

.62

.50 +.06 -.00

.25 STK

R .12

R .132X

1.00

150° 150°

1.62

1.00

O .75

VIEW A-A

.88

.25

R .122X

.19 STK

21.00

SLOT TO SLOT

1.50 2.50

.64

NOTE 4

BOLT PLATE END

HOOK END

21.00

8.25

R .254X

SLEEVE PROTECTION

OPTIONAL

SLEEVE PROTECTION

OPTIONAL

3.25

4.00

1.50

2.25

.50

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CAGE CODE

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

1345678

12345678

FCL

IFAA COWLING

CUSHION ASSEMBLY

-1

10/19/06 FCLA ADDED NOTES 4, 5 & 61.

T-56 QECA

7/28/2011

12/04

706D013

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CAGE

CODE OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST-1

QTY

REQ'D

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

ADDED "AND REV" WORDING TO NOTE 61. 8/13/07 GCB

CHANGED DIM ON ITEM 3 TO INSIDE DIM

INSTEAD TO THE OUTSIDE OF MATERIAL

2.SH 2

IFAA COWLING CUSHION ASSEMBLY - LH706D013-1-1

FWD

R H

IFAA COWLING CUSHION ASSEMBLY - RH706D013-2-2

ZINC PLATE OR PRIME COAT22.5312.000.187ASTM A36BRACKET706D013-3-31

NOTES 2 & 312.012.06.5POLYETHYLENECUSHION706D013-4-41

1 AS SHOWN (RH)

2 OPP. HAND (LH)

4 5

3MADHESIVE1357049635ARAR

2.50

1. BREAK ALL SHARP EDGES .020 - .050 RADIUS.

2. MATERIAL TO BE PER A-A 59136 CLASS 1, GRADE C,

TYPE I.

3. ITEM 4 MAY BE MADE UP OF MULTIPLE LAYERS

LAMINATED TOGETHER USING ITEM 5.

4. PRIME WITH ONE COAT PRIMER PER TT-P-1757, TY II,

CLASS N. FINISH WITH TWO COATS TT-E-527 COLOR

NUMBER 37925 PER FED-STD-595.

5. STENCIL LETTERING AND ARROWS USING PAINT

CONFORMING TO A-A-56032, COLOR BLACK PER FED-

STD-595, COLOR NO. 27038 OR 27040.

6. STEEL STAMP ASSEMBLY PART NUMBER AND REV

USING .50” LETTERS/NUMBERS.

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

1" X 5" ARROW

.75" LETTERS

-1 LH

-2 RH

NOTE 6

8/16/07

DWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

CHK BY:

SIZE CAGE CODE

05259

DWG NO.

WEIGHT:SCALE: SHEET:

REV

1345678

12345678

706D013 B

FCL FCL 2

7/28/2011

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

14.50

7.62

1.00

12.00

.188 STK

R .122X

SEE NOTE 3,

REQUIRED ORIENTATION OF LAYERS

3.00

12.00

5.00

3.00

6.00

1.442X

O .5622X STK

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CAGE CODE

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

1345678

12345678

FCL

IFAA TRUNNION

CROSS TUBE ASSEMBLY

-1

10/19/06 FCLA

ADDED NOTES 5, 6 & 71.

T-56 QECA

7/28/2011

12/04

706D014

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CAGE

CODE OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST-2

QTY

REQ'D

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

SPECIFIED WELDS FOR NDT2.

8/13/07 GCB

ADDED T-56 QECA TO "USED ON" SEC. IN

TITLE BLOCK

ADDED MS HARDWARE CALLOUTS FOR

ITEMS 6, 7, & 9

ADDED "AND REV" WORDING TO NOTE 63.

IFAA TRUNNION CROSS TUBE ASSEMBLY706D014-1-1

101.442.00D0.12WASTM A513 GRBTUBE706D014-3-3

6.007.00.375ASTM A36PLATE706D014-4-4

CROSS TUBE WELDMENT706D014-2-21

17.002.500.25ASTM A36GUSSET706D014-5-5

NASM 35307; NOTE 31.751/2-13GRADE 5 SSHEX HEAD BOLT-MODIFIEDMS35307-414-68

NASM 35338; NOTE 3 & 41/2SSLOCK WASHERMS35338-143-78

CABLE ASSEMBLYSTD-360-B-8-1-88

1. STEEL WELDING TO BE IN ACCORDANCE WITH

MIL-STD-278, WELDER QUALIFICATION TO BE IN

ACCORDANCE WITH MIL-STD-248., VISUAL INSPECTION

SHALL BE IN ACCORDANCE WITH MIL-STD-271.

GRIT BLAST MEDIA MAY BE USED BEFORE WELDING &

SHALL BE DONE PRIOR TO PAINTING.

3. SURFACE FINISHING

STEEL SURFACES SHALL BE CLEANED IN ACCORDANCE

WITH TT-C-490, ANY TYPE AND METHOD ACCEPTABLE.

PRIMER SHALL CONSIST OF TWO COATS IN ACCORDANCE

WITH TT-P-664. TOTAL THICKNESS SHALL BE 1.5 MILS AS A

MINIMUM.

PAINT SHALL CONSIST OF TWO COATS OF TT-E-527 COLOR

LUSTERLESS GRAY NO. 36622 OF FED-STD-595 FOR A

TOTAL THICKNESS OF 1.6 TO 2.4 MILS.

.375#6STLDRIVE SCREWMS21318-29-94 ASME B18.6.4; NOTE 3 & 4

8 7

5. MAGNETIC PARTICLE INSPECT WELDS PER ASTM

E709.

6. STEEL STAMP ASSEMBLY PART NUMBER AND REV

IN .50” LETTERS/NUMBERS.

7. PRIME ASSEMBLY WITH ONE COAT OF TT-P-1757, TY

II, CLASS N PRIMER. TOP COAT WITH TWO COATS OF

TT-E-527 COLOR NUMBER 37925 PER FED-STD-595.

2. BREAK ALL SHARP EDGES .020 - .050 RADIUS.

3. ZINC-NICKEL PLATE PER ASTM B841, CLASS 1, TYPE

B, GRADE 3.

4. HARDWARE TO BE AS SPECIFIED OR FUNCTIONALLY

EQUIVALENT.

NOTE 6

8/16/07

DWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

CHK BY:

SIZE CAGE CODE

05259

DWG NO.

WEIGHT:SCALE: SHEET:

REV

1345678

12345678

706D014 B

FCL 2

7/28/2011

FCL

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

56.63

50.88

1.002X

1.622X

7.00

1.75

WRAP CORNERS.25

2X - NOTE 5

.19

2.88

8/16/07

DWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

CHK BY:

SIZE CAGE CODE

05259

DWG NO.

WEIGHT:SCALE: SHEET:

REV

1345678

12345678

706D014 B

FCL FCL

7/28/2011

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

7.00

6.00

2.5002X

2.7502X

1.0002X4.0002X

.38 STK

O .5624X

2X - R.11

55°

32.43

1.75

TURN DOWN THREAD

TO MINOR DIAMETER

.75

3.02X

.52X O .1202X

17.00

.25 STK

135°2X

2.50

2.00 STK

50.88

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CAGE CODE

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

1345678

12345678

FCL

DOOR HOLD

BAR ASSEMBLY

-1

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CAGE

CODE OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST

10/19/06 FCLA ADDED PART MARKING1.

T-56 QECA

7/28/2011

12/04

706D020

HOLE IN ITEM 3 WAS .190D2.

2/21/07 FCLB ITEM 2 WAS 71.751.

8/13/07 GCC

ADDED ADDITIONAL INFO. TO DETAIL A1.

ADDED T-56 QECA TO "USED ON" SEC. IN

TITLE BLOCK

CHANGED NOTE CALLOUT FOR ITEM3.

ADDED ADDITIONAL INFO IN BMI FOR

ITEM 4

DOOR HOLD BAR ASSEMBLY706D020-1-1

65.00.625D304 SSROD706D020-2-21

2.001.001.00304 SSCLEVIS706D020-3-32

McMASTER CARR; MILL 165550.383/16416 SSDOWEL PIN98380A5033942844

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

DETAIL A1.00 STK

1.00 STK

1.500

R .500

.295

.410

.5003X

.312

O .185 THRU

O .250 THRU

O .631 X .750`

.3332X

.2102X

.3752X O

2X - .06 X 45v

CHAMFER

3 2X

44X

.875

.625O

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

STEEL STAMP OR STENCIL ASSEMBLY PART

NUMBER IN .25" LETTERS/NUMBERS

65.00

ITEM 4 TO BE PRESSED FLUSH WITH

OUTSIDE SURFACES OF COMPONENT

3. DO NOT BOTTOM ITEM 3 ON ITEM 2

EACH END

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CAGE CODE

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

1345678

12345678

FCL

INSTALLATION

INSTRUCTIONS

T-56 QECA

12/04

706D021

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CAGE

CODE OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

8/13/07 GCA ADDED T-56 QECA TO "USED ON" SEC. IN

TITLE BLOCK

11.008.5BOND PAPERINSTALLATION INSTRUCTIONS706D021-11

706D021-1 SHEET 1 OF 2

INSTALLATION INSTRUCTIONS FOR

T56 QUICK ENGINE CHANGE ASSEMBLY SHIPPING & STORAGE CONTAINER

IFAA with or without QEC removal from container:

• Release ambient pressure from container.

• Open both Doors:

o Release latches (recommend alternating).

o Remove latch pin on single hinge, left side of door.

o Swing open doors.

o Install door brace on end to be exited.

• Attach rail extensions located in bottom of container, to container rails on end to be used as exit for IFAA.

• Align and attach 4000 series trailer to rail extensions.

o Install two pins connecting extensions to trailer.

o ONLY USE PROPER SIZE BALL-LOCK PINS

• Remove spreader bar “706E010-1” on end to be used for exit.

o Undo four bolts.

• Remove four pins through rollers.

o Two forward, one each side & two aft, one each side.

• MAKE SURE TRANSPORT TRAILER STOP PINS ON RAILS ARE “UP” AT

NON-CONNECTED END OF TRAILER.

• Lower stop pins on transport trailer rails connected to extensions.

• Ensure all personnel are aware of possible personal injury and/or damage to the

QECA due to clearance while moving the IFAA into or out of the container.

• Roll IFAA out of container.

o WATCH FOR INTERFERENCE OF FOAM PADS WITH

CONNECTION PINS BETWEEN TRAILERS.

• Tighten brake pads on IFAA to rail of Trailer (12 places) o Tighten Jam nut to secure brakes. (12 places)

• Raise stop pins on trailer.

• Separate trailer from container extensions.

• Install IFAA restraint straps.

• Replace Spreader Bar “706E010-1” on container rails.

o Install four bolts, adjustment of width may be necessary.

• Remove Exhaust Pipe and Rear Vibration Isolator from shipping holder in aft end of container.

• Return extensions to storage position if not in immediate use and close container.

• Close container both ends.

o Remove door brace.

o Closed door.

o Install latch pin on single hinge, left side.

o Secure latches (recommend alternating).

11.00

8.50

706D021-1 SHEET 2 OF 2

INSTALLATION INSTRUCTIONS FOR

T56 QUICK ENGINE CHANGE ASSEMBLY SHIPPING & STORAGE CONTAINER

IFAA with or without Engine installation to container:

• Release pressure from container.

• Open Doors:

o Release latches (recommend alternating).

o Remove latch pin on left side hinge..

o Swing open doors.

o Install door brace.

• Attach rail extensions to container rails.

• Remove safety straps from ends of transport trailer rails.

• Align and attach transport trailer to rail extensions.

o Install two pins connecting extensions to trailer.

o ONLY USE PROPER SIZE BALL-LOCK PINS.

• Remove spreader bar on end of entrance.

o Undo four bolts.

• Loosen brake pads on IFAA.

o Loosen Jam nut, then raise pad (12 places).

• MAKE SURE SPREADER BAR IS INPLACE AT FAR END OF CONTAINER.

• MAKE SURE HANDWHEEL IS IN STOWED FOR TRANSPORT POSITION.

• REMOVE EXHAUST PIPE FROM AFT OF ENGINE.

• Lower stop pins on transport trailer rail connecting to extensions.

• Roll IFAA into container.

o PAY ATTENTION TO DIRECTION OF ENGINE o WATCH FOR INTERFERENCE OF FOAM PADS WITH

CONNECTION PINS BETWEEN TRAILERS.

• Install four pins through rollers.

o Two forward, one each side & two aft, one each side.

• Install spreader bar.

o Install 4 bolts.

• Raise stop pins on trailer.

• Separate trailer from extensions.

• Return extensions to storage position in container.

• Install exhaust pipe in shipping holder in aft end of container.

• Place packaged Rear Vibration Isolator inside exhaust pipe in shipping holder in aft end of container.

• Check desiccant and humidity indicator. Replace as needed.

• Close container.

o Remove door brace.

o Closed door.

o Install latch pin on left side hinge.

o Secure latches (recommend alternating).

1. INSTRUCTIONS TO BE LAMINATED IN CLEAR PLASTIC.

2. CODE IDENT

REV LETTER: F

DATE REVISED: 10/20/11

SHEET: 1

OF: 3

9 10 11 12 13

CODE DRAWING DOCUMENT NUMBER SHEET REVISION

IDENT SIZE NUMBER LETTER

05259 E 706E001 1 B

05259 E 706E001 2 B

05259 E 706E001 3 B

T-56 QECA ENGINE CONTAINER

5. LIST TITLE 6. AUTHENTICATION

T-56 QECA ENGINE CONTAINER ASSEMBLY

CONTAINER RESEARCH CORPORATION

N00140-98-D-K155/0020

NOMENCLATURE OF DESCRIPTION

T-56 QECA ENGINE CONTAINER ASSEMBLY

GLEN RIDDLE, PA 19037

05259 DL-706E001

7. REVISION AUTHENTICATION NUMBER 8

DATA LIST

1. AGENCY (CONTRACTOR IDENTIFICATION) 1A. CONTRACT NUMBER 3. DATA LIST DRAWING NUMBER 4. REVISION

DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE

DOCUMENT.

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 EXECUTIVE ORDER 12470. VIOLATIONS OF THESE EXPORT

LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES.

DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT

AGENCIES AND THERE CONTRACTORS, ADMINISTRATION /

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 E 706E001 3 B

05259 E 706E002 1 B

05259 E 706E002 2 B

05259 E 706E002 3 B

05259 E 706E002 4 B

05259 E 706E002 5 B

05259 E 706E002 6 B

05259 E 706E002 7 B

05259 E 706E002 8 B

05259 E 706E002 9 B

05259 E 706E002 10 B

BASE ASSEMBLY

T-56 QECA ENGINE CONTAINER ASSEMBLY

BASE ASSEMBLY

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 E 706E002 10 B

05259 E 706E002 11 B

05259 E 706E002 12 B

05259 E 706E003 1 B

05259 E 706E003 2 B

05259 E 706E003 3 B

05259 E 706E003 4 B

05259 E 706E003 5 B

05259 E 706E004 1 C

05259 E 706E004 2 C

05259 E 706E004 3 C INNER FRAME ADAPTER ASSEMBLY

HINGED DOOR ASSEMBLY

INNER FRAME ADAPTER ASSEMBLY

BASE ASSEMBLY

HINGED DOOR ASSEMBLY

BASE ASSEMBLY

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 E 706E004 3 C

05259 E 706E004 4 C

05259 E 706E005 1 C

05259 E 706E005 2 C

05259 E 706E005 3 C

05259 E 706E005 4 C

05259 E 706E005 5 C

05259 E 706E005 6 C

05259 E 706E005 7 C

IFAA SIDE RAIL ASSEMBLIES

INNER FRAME ADAPTER ASSEMBLY

IFAA SIDE RAIL ASSEMBLIES

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

DATE REVISED: 10/20/11

SHEET: 2

OF: 3

9 10 11 12 13

CODE DRAWING DOCUMENT NUMBER SHEET REVISION

IDENT SIZE NUMBER LETTER

05259 E 706E005 8 C

05259 E 706E005 9 C

05259 E 706E005 10 C

T-56 QECA ENGINE CONTAINER

NOMENCLATURE OF DESCRIPTION

IFAA SIDE RAIL ASSEMBLIES

7. REVISION AUTHENTICATION NUMBER

DL - 706E001GLEN RIDDLE, PA 19037

DATA LIST

85. LIST TITLE 6. AUTHENTICATION

1. AGENCY (CONTRACTOR IDENTIFICATION) 1A. CONTRACT NUMBER 3. DATA LIST DRAWING NUMBER

IFAA SIDE RAIL ASSEMBLIES

4. REVISION

CONTAINER RESEARCH CORPORATION

NOO140-98-D-K155/0020 05259

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 E 706E005 10 C

05259 E 706E005 11 C

05259 E 706E006 1 B

05259 E 706E006 2 B

05259 E 706E007 1 B

05259 E 706E007 2 B

05259 E 706E007 3 B

05259 E 706E008 1 B

05259 E 706E008 2 B

05259 E 706E008 3 B

05259 B 706B009 1

DESICCANT BASKET ASSEMBLY

IFAA SIDE RAIL ASSEMBLIES

DOOR HINGE ASSEMBLY

HEAVY DUTY I-BEAM EXTRUSION

DOOR HINGE ASSEMBLY

IFAA AFT ENGINE MOUNT ASSEMBLY

DESICCANT BASKET ASSEMBLY

DOOR HINGE ASSEMBLY

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 B 706B009 1

05259 D 706D010 1 B

05259 D 706D010 2 B

05259 E 706E011 1 B

05259 E 706E011 2 B

05259 D 706D012 1 F

05259 D 706D013 1 B

05259 D 706D013 2 B

05259 D 706D014 1 B

05259 D 706D014 2 B

05259 D 706D014 3 B IFAA TRUNNION CROSS TUBE ASSEMBLY

IFAA COWLING CUSHION ASSEMBLY

CLAMP WELDMENT

IFAA TRUNNION CROSS TUBE ASSEMBLY

CLAMP WELDMENT

TAIL CONE STORAGE ASSEMBLY

HEAVY DUTY I-BEAM EXTRUSION

IFAA COWLING CUSHION ASSEMBLY

TAIL CONE STORAGE ASSEMBLY

IFAA RESTRAINT BELT ASSEMBLY

IFAA TRUNNION CROSS TUBE ASSEMBLY

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 D 706D014 3 B

05259 E 706E015 1 C

05259 E 706E015 2 C

05259 E 706E015 3 C

05259 E 706E016 1 E

05259 E 706E016 2 E

05259 E 706E016 3 E

05259 E 706E016 4 E

05259 E 706E016 5 E

05259 E 706E017 1 B

IFAA TRUNNION CROSS TUBE ASSEMBLY

IFAA GEARBOX SUPPORT ASSEMBLY

IFAA FORWARD CROSS MEMBER

IFAA GEARBOX SUPPORT ASSEMBLY

IFAA GEARBOX ADJUSTMENT ASSEMBLY

IFAA FORWARD CROSS MEMBER

IFAA GEARBOX SUPPORT ASSEMBLY

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

DATE REVISED: 10/20/11

SHEET: 3

OF: 3

9 10 11 12 13

CODE DRAWING DOCUMENT NUMBER SHEET REVISION

IDENT SIZE NUMBER LETTER

05259 E 706E017 2 B

05259 E 706E017 3 B

05259 E 706E018 1 B

3. DATA LIST DRAWING NUMBER 4. REVISION

CONTAINER RESEARCH CORPORATION

NOO140-98-D-K155/0020

T-56 QECA ENGINE CONTAINER

GLEN RIDDLE, PA 19037

5. LIST TITLE 6. AUTHENTICATION 7. REVISION AUTHENTICATION NUMBER 8

DATA LIST

1. AGENCY (CONTRACTOR IDENTIFICATION) 1A. CONTRACT NUMBER

05259 DL - 706E001

IFAA TRUNNION MOUNT ASSEMBLY

IFAA GEARBOX ADJUSTMENT ASSEMBLY

NOMENCLATURE OF DESCRIPTION

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 E 706E018 1 B

05259 E 706E018 2 B

05259 E 706E018 3 B

05259 E 706E018 4 B

05259 E 706E019 1 B

05259 E 706E019 2 B

05259 E 706E019 3 B

05259 E 706E019 4 B

05259 D 706D020 1 C

05259 D 706D021 1 A

05259 C 706C022 1 - PROPELLER SHAFT PRESERVATION QECA

IFAA TRUNNION MOUNT ASSEMBLY

IFAA BRIDGE RAIL ASSEMBLY

IFAA TRUNNION MOUNT ASSEMBLY

IFAA BRIDGE RAIL ASSEMBLY

DOOR HOLD BAR ASSEMBLY

IFAA TRUNNION MOUNT ASSEMBLY

INSTALLATION INSTRUCTIONS

IFAA TRUNNION MOUNT ASSEMBLY

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 C 706C022 1 -

05259 D STD-225 1

05259 B STD-228 1

05259 C STD-295 1

05259 C STD-295 2

05259 C STD-295 3

05259 C STD-295 4

05259 D STD-360 1

05259 D 13D097 1

05259 C 13C099 1

05259 C 13C099 2

CAPTIVATING TAB

PROPELLER SHAFT PRESERVATION QECA

NAMEPLATE

CABLE ASSEMBLY

CAPTIVATING TAB

SEALING FLANGE EXTRUSIONS

SEALING FLANGE EXTRUSION

RECORDS RECEPTACLE

CAPTIVATING TAB

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

WARFARE CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ

08733-5000

05259 C 13C099 2

05259 C 13C102 1

05259 E 17E070 1

05259 E 17E070 2

ECO #1 1 B - C

ECO #2 1 - 2 C - D

ECO #3 1 D - E

ECO #4 1 E - F

ECO #4 2 E - F

ACTIVE: 706E015 - DRILL SIZE & TAP CALLOUT INCORRECT FOR INSERTION OF ITEM #9

ACTIVE: 706D012 - ADDED TOLERANCE

ACTIVE: 706D012 - ADD RADIUS TO ITEMS #3 & #4

JOINT, ANGLED PANEL EXTRUSION

LATCH ASSEMBLY

SEALING FLANGE EXTRUSION

ACTIVE: 706D012 - ADDED NOTE 7

ACTIVE: 706D012 - ADDED NOTE 8

LATCH ASSEMBLY

CONTROL ACT (TITLE 22, U.S.C. SEC 2751 ET SEQ.)

OPERATIONAL USE, OTHER REQUESTS FOR THIS DOCUMENT

SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR

CAD MAINTAINED BY SOLID EDGE; CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

A 1. UPDATED TO REFLECT CHANGES IN

LOWER LEVEL DRAWINGS

FCL10/19/06

706E001 B

T-56 QECA

ENGINE CONTAINER

ASSEMBLY

RMS 08/03

08/03DPB

10/17/03

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CODE

IDENT OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

CODE IDENT NO.

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.XX

.XXX

± .015

.06

FRACTIONS:

ANGLES:

DECIMALS:

8 7 6 5 4

2 13

T-56 QECA ENGINE CONTAINER706E001-1

1 BASE ASSEMBLY706E002-1

1 HINGED DOOR ASSEMBLY - FWD706E003-1

1 INNER FRAME ADAPTER ASSEMBLY706E004-1

2 288.0 NOTE 6GASKET706E001-5

6 AGM, NOTE 13HUMIDITY INDICATOR W/O CARDTA-45608992

2 AGM, NOTE 13HUMIDITY INDICATOR ELEMENTTA-37808992

4 AGM, NOTE 13RELIEF VALVETA770-025C-025C-R08992

1 HINGED DOOR ASSEMBLY - AFT706E003-19

4 FLEXTRON, NOTE 13DESICCANT PORT17C057-321106

1 NOTE 7NAME PLATESTD-228-1

3 NOTE 8INSTALLATION INSTRUCTIONS706D021-1

2 AGM, NOTE 13AIRFILL VALVETA-32208992

142 CLAMP WELDMENT706D010-1

152 DOOR HOLD ASSEMBLY706D020-1

164 .250 ASME B18.6.4, NOTE 12STLDRIVE SCREWMS 21318-27

17AR 3MADHESIVE135704963

182 LABEL706C022-1

B 1. ADDED ITEM 18 FCL1/19/06

1. CONTAINER WEIGHT: 4,496 LBS.

GROSS WEIGHT: 7,040 LBS.

OVERALL DIMENSIONS LENGTH 180.38

WIDTH 87.38

HEIGHT 96.22

2. ALUMINUM SHALL BE CLEANED IN ACCORDANCE WITH MIL-C-5541.

3. LEAK TEST:

THE CONTAINER SHALL BE PERPARED FOR TESTING BY REMOVING

ALL BREATHING DEVICES AND INSERTING SUITABLE PRESSURIZING

FITTINGS. AFTER THE CONTAINER HAS BEEN CLOSED AND SEALED

IN THE NORMAL MANNER THE PNEUMATIC PRESSURE TECHNIQUE

SHALL BE USED PER METHOD 5009 OF FED. TEST METHOD STD. NO.

101 TO DETECT LEAKAGE, AN INITIAL PRESSURE SETTING OF 0.50

PSIG SHALL BE USED FOR 1 HOUR. AFTER STABILIZATION,

PRESSURE SHALL BE MONITORED WITH PARTICULAR ATTENTION

GIVEN TO THE SEALING FLANGES AND WELD AREAS. ANY

PERMANENT DEFORMATION OF THE CONTAINER WHICH IS

GREATER THEN THREE-QUARTERS OF AN INCH BEYOND ITS

NORMAL POSITION SHALL BE CAUSE FOR REJECTION.

WARNING

CONTAINER MAY EXPLODE OR FASTENERS MAY FAIL DURING THIS

TEST. USE PROTECTIVE BARRIERS TO AVOID INJURY TO

PERSONNEL.

4. SEALING OF FAYING SURFACES:

ALL FAYING SURFACES WHERE ATMOSPHRIC LIQUIDS MAY BE

RETAINED BY CAPILLARY ACTION, THE CREVICE, SHALL BE SEALED

USING COMPOUND MIL-PRF-81733 OR EQUIVLENT.

5. STENCILING PAINT CONFORMING TO A-A-56032, COLOR BLACK PER

FED-STD-595, COLOR NO. 27038 OR 27040. UNLESS OTHERWISE

SPECIFIED, LETTERS SHALL BE 1.00 INCHES HIGH. STENCILING ON

SIDE OF CONTAINER IS TYPICAL FOR OTHER SIDE.

10. 8.5 X 11 AREA TO BE SOLID BLACK (REFER TO NOTE 5).

11. KEEP DOORS CLOSED WHEN CONTAINER IS NOT IN USE. SUNLIGHT

AND OZONE WILL DETERIORATE GASKETS PREMATURELY. THE

DESICCANT CAN BE REACTIVATED IN 12 HOURS

AT 245 DEGREES FAHRENHEIT.

12. ZINC- NICKEL PLATE PER ASTM-B841, CLASS 1, TYPE B, GRADE 3.

13. ITEM TO BE AS SPECIFIED OR FUNCTIONALLY EQUIVALENT.

14. DOOR INSTALLATION: MUST USE AN OVERHEAD CRANE AND

APPROPRIATE SLING. ATTACH SLING SO DOOR HANGS PERFECTLY

VERTICAL. REMOVE BOLT AND LOCK NUT FROM EACH OF THE

DOOR HINGES AND BALL LOCK PINS FROM EACH OF THE DOOR

LOCKS ON THE BASE. SLOWLY MOVE DOOR TOWARDS BASE AND

ALIGN THE MALE CLEVIS OF COVER HINGE SECTIONS WITH THE

FEMALE CLEVIS OF BASE HINGE SECTIONS. PUSH EACH CLEVIS

TOGETHER AND ALIGN HOLES. INSERT BOLTS AND LOCK NUTS.

6. GASKET TO BE PER MIL-R-6855, CLASS 2, TYPE A, GRADE 60

(.75 O.D. X .38 I.D.) BOND GASKET SPLICE JOINT WITH (01666)

PERMABOND 105.

7. THE FOLLOWING DATA WILL BE STAMPED ON THE NAME PLATE

PRIOR TO INSTALLATION ONTO THE CONTAINER

CONTAINER, SHIPPING AND STORAGE FOR T-56 QECA ENGINE

NAVY P/N: (80132) 15832

NSN: 6KH 8145-01-522-3940

MANUFACTURES P/N: (05259) 706E001-1

CONTRACT NO. *

• CONTRACT NO. WILL BE ASSIGNED PER CURRENT CONTRACT

8. INSTALLATION INSTRUCTIONS TO BE LAMINATED IN PLASTIC WITH

ONE SET BONDED TO THE INSIDE OF EACH DOOR AND ONE SET

PLACED IN THE RECORDS BOX.

9. STEEL STAMP CONTAINER SERIAL NUMBER IN .50 HIGH

CHARACTERS ON NAMEPLATE.

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

B706E001

10/17/03

RMSDPBDWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

CHK BY:

SIZE FSCM NO.

05259

DWG NO.

WEIGHT:SCALE:

REV

SHEET:

8 7 6 5 4

2 13

HUMIDITY

INDICATOR

VIEW PORTVIEW PORT

FUEL VAPOR

TEST

RELIEF

VALVE

RELIEF

VALVE

DESICCANT BASKET

256 UNITS REQUIRED

IN EACH BASKET

F W D

I N T A K E

C A U T I O N

R E L E A S E

P R E S S U R E

B E F O R E

O P E N I N G

C O N T A I N E R

RECORDS

BOX

FWD (INTAKE) END VIEW

TIE DOWN TOW HERE TIE DOWN TOW HERE

FORK POCKETS

TIE DOWN TIE DOWN

REUSABLE CONTAINER

DO NOT DESTROY

RETURN TO SUPPLY WHEN NOT IN USE

DESICCANT COMPARTMENT

256 UNITS REQUIRED

IN EACH BASKET

CENTER OF GRAVITY

A F T

E X H A U S

TDOOR HINGE

DOOR HINGE

DOOR HINGE LATCH

CAUTION: RELEASE PRESSURE BEFORE OPENING CONTAINER

SHIPPING INFORMATION ONLY

TEST FOR FUEL VAPERS

BEFORE OPENING

VERTREP

2644390 SLING LEG

LIFT HERE

VERTREP

2644390 SLING LEG

LIFT HERE

LIFTING POINT -

USE ONLY FOR

DOOR REMOVAL

138.25

BOTH SIDES OF DOOR

2 INCH HIGH STENCIL

BOTH SIDES OF DOOR

2 INCH HIGH STENCIL

BOTH SIDES OF DOOR

2 INCH HIGH STENCIL

96.22

34.25

SEE NOTE 10

22X ARROWS TO BE

5.00 LONG X 1.00 WIDE

8.50

AFT (EXHAUST) END VIEW

6 6X

72X

1084X

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

69.1

87.38

3.00

2.75

.124X

.254X

33.6

52X

15 2X

13 2X

16 4X

180.37

69.19

BOTH SIDES OF DOOR

12 17 2X

DRILL O.120 HOLE - 4X

USE ITEM 11 AS TEMPLATE

LOCATE APPROX. AS SHOWN

INSIDE OF BOTH DOORS

18 17

B706E001

08/11/03

RMSDPBDWN BY:

DATE:

GLEN RIDDLE, PENNSYLVANIA

CONTAINER RESEARCH CORP.

CHK BY:

SIZE FSCM NO.

05259

DWG NO.

WEIGHT:SCALE:

REV

SHEET:

8 7 6 5 4

2 13

DOOR REMOVED FOR CLARITY

1:8

DESTRUCTION NOTICE:

DOCUMENT SHALL BE REFERRED TO COMMANDING OFFICER, NAVAL AIR WARFARE

CENTER, AIRCRAFT DIVISION, LAKEHURST, NJ 08733-5000

14 2X, 1 AT EACH END OF ITEM 4

4 NOTE ORIENTATION

DEPARTMENT OF THE NAVY

NAVSUP WEAPON SYSTEMS SUPPORT

CODE P0771 PACKAGING ENGINEERING TEAM

BUILDING 1, ROOM 2500

700 ROBBINS AVENUE

PHILADELPHIA PA 19111-5098

ENGINEERING CHANGE ORDER 1. ECO NO.:

2. DRAWING/PART NO.: 3. PART NOMENCLATURE: 4. REVISION:

5. CONTAINER NSN: 6. CONTAINER NOMENCLATURE: 7. DATE:

8. NEXT HIGHER ASSEMBLY: 9. REQUESTED BY:

10. DESCRIPTION OF CHANGE (WAS/IS):

11. REASON FOR CHANGE [INCLUDE JUSTIFICATION AND BACKUP DATA (IF AVAILABLE)]:

VALUE ENGINEERING SPEC CHANGE CORRECTIONS IN-SERVICE SAFETY NEW DRAWING

12. COMMENTS:

13. ECO ORIGINATOR SIGNATURE: 14. DATE:

15. ENGINEERING CHECK SIGNATURE: 16. DATE:

1. ECO NO.:

2. DRAWING/PART NO. 3. NOMENCLATURE 4. CURRENT REVISION

5. CONTINUATION ITEMS:

ENGINEERING CHANGE ORDER

(CONTINUATION SHEET)

12/6/22, 1:31 PM Nickel-Coated Steel Hoist Ring for Lifting, Machined, 3/4"-10 Thread Size, 8-1/8" Overall Height | McMaster-Carr https://www.mcmaster.com/3145T73/ 1/2

180° Pivot

360° Swivel

Nickel-Coated Steel Hoist Ring for Lifting Machined, 3/4"-10 Thread Size, 8-1/8" Overall Height

$360.05 Each 3145T73

Application For Lifting

Fabrication Machined

Thread Size 3/4"-10

Thread Length 1 1/2"

Inside Width 2 3/4"

Overall Height 8 1/8"

Material Nickel-Coated Steel

Vertical

Capacity 7,000 lbs.

Movement 180° Pivot and 360° Swivel

Includes Proof Test Certificate

Specifications

Met

ASME B30.26, CE Marked, MIL-STD-1365, MIL-

STD-209

RoHS RoHS 3 (2015/863/EU) Compliant

REACH REACH (EC 1907/2006) (07/08/2021, 219 SVHC)

Compliant

DFARS Specialty Metals COTS-Exempt

Country of

Origin United States

USMCA

Qualifying Yes

Schedule B 732690.8695

ECCN EAR99

Designed for angular lifting, hoist rings resist stresses that would bend or break…

This is the start of the file's text. The full file is on GovTribe.

File details come from the government source that posted it. Updated Sep 5, 2024.