Attachments.pdf

REV:

ENGINEERING DATA REQUIREMENTS/INSTRUCTIONS

(ATTACHMENT ‘A’)

NOTE: MILITARY SPECIFICATIONS / STANDARDS WILL NOT BE FURNISHED IN THE BID SET.

1. THE FOLLOWING INSTRUCTIONS ARE FURNISHED FOR THE MANUFACTURE OF:

DRAG BRACE ASSY, NOSE GEAR (E-3 LG) “2012 RIGHTS GUARD”

2. PART NUMBER:

65-3693-27

3. NATIONAL STOCK NUMBER:

1620-01-098-2808

PREPARED BY:

JAMES HUMPHERYS

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

20140721

HILL AFB FORM 462 Page 1 of 19

4. THE FOLLOWING SPECIFICATIONS/STANDARDS, ETC. WILL BE USED IN LIEU OF THE DATA INDICATED. THE

SUPERSEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.

5. MATERIAL REVIEW BOARD:

6. OO-ALC LANDING GEAR ENGINEERING RETAINS ALL RIGHTS TO REVIEW AND ACCEPT MATERIAL REVIEW BOARD

(MRB’S) DISPOSITIONS PRIOR TO SHIPMENT OF DISCREPANT ITEM. ALL DEVIATIONS, MINOR AND MAJOR, FROM THE

ENGINEERING DRAWING PACKAGE SHALL BE SUBMITTED FOR MRB DISPOSITION.

7. PRIOR TO CONTRACT AWARD, THE CONTRACTOR SHALL CERTIFY TO THE GOVERNMENT IN WRITING FULL

COMPLIANCE WITH MANUALS, SPECIFICATIONS AND STANDARDS CALLED OUT AND REQUIRED FOR THE MANUFACTURE OF THIS CONTRACTED LANDING GEAR COMPONENT/ASSEMBLY. CONTRACTOR IS RESPONSIBLE TO COMPLETELY SEARCH THESE MANUALS, SPECIFICATIONS AND STANDARDS AND FULLY UNDERSTAND THE REQUIREMENTS NECESSARY TO MANUFACTURE LANDING GEAR COMPONENTS. ANY QUESTIONS CAN BE

FORWARDED TO OO-ALC LANDING GEAR ENGINEERING.

8. “2012 RIGHTS GUARD LICENSING AGREEMENT” APPLIES - THE DATA REQUIRED TO MANUFACTURE THIS ITEM IS

CLAIMED TO BE PROPRIETARY TO BOEING. THE RIGHT OF THE GOVERNMENT TO USE THE DATA TO PURCHASE THIS PART FROM ADDITIONAL SOURCES HAS BEEN ESTABLISHED UNDER THE "2012 RIGHTS GUARD LICENSING AGREEMENT” CONTRACT # FA8119-12-D-0015, TO PROVIDE DOD PROCURING AGENCIES THE USE OF DATA FOR

COMPETITIVE RE-PROCUREMENT OF REPLENISHMENT SPARES.

9. GENERAL REQUIREMENTS:

10. DRILLING, REAMING AND HONING TO MEET DRAWING SPECIFICATIONS USING BEST AIRCRAFT INDUSTRY

STANDARDS. CHEMICAL, ELECTRICAL, OR ELECTROCHEMICAL HOLE PRODUCING METHODS SHALL NOT BE USED AS A FINAL SURFACE PRODUCING METHOD ON HOLES NOT INSPECTABLE WITH NITAL ETCH WITHOUT PRIOR

APPROVAL FROM OO-ALC LANDING GEAR ENGINEERING.

11. DIMENSION AND TOLERANCING PER ASME Y14.5 IN LIEU OF ANSI Y14.5.

12. SURFACE ROUGHNESS PER ASME B46.1 IN LIEU OF BACD 2097.

13. FORM, PUNCH AND FIT METAL PARTS PER BEST AIRCRAFT INDUSTRY PRACTICES IN LIEU OF BAC5300.

14. BOLT AND NUT INSTALLATION PER BEST AIRCRAFT INDUSTRY STANDARDS IN LIEU OF BAC 5009.

15. MARKING PER DRAWING REQUIREMENTS AND MIL-STD-130.

16. (CSI) MAGNETIC PARTICLE INSPECTION PER ASTM E 1444 IN LIEU OF BAC5424 AND AN-I-32. USE FLUORESCENT TYPE, FULL WAVE DIRECT CURRENT (FWDC), AND WET CONTINUOUS METHOD. THE FOLLOWING ACCEPTANCE/REJECTION CRITERIA MAY BE USED AS AN ALTERNATE TO THE ORIGINAL MANUFACTURER CRITERIA: NO RELEVANT INDICATIONS ALLOWED. THE INTENT OF NO RELEVANT INDICATIONS ALLOWED IS THAT THE INSPECTION IS CONDUCTED AT THE REQUIRED SENSITIVITY LEVEL AND THERE SHALL BE NO DEFECTS ALLOWED. THE INSPECTOR PERFORMING THE INSPECTIONS SHALL BE CERTIFIED TO LEVEL II WITH THE INSPECTION PROCEDURE DEVELOPED

BY A LEVEL III AS SPECIFIED IN AIA/NAS-410.

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 2 of 19

17. (CSI) SHOT PEEN TO MEET DRAWING REQUIREMENTS PER SAE AMS 2430. SHOT PEENING INTENSITY SHALL BE AS SPECIFIED BY THE DRAWING. THE SIZE OF THE SHOT SHALL BE AT THE OPTION OF THE CONTRACTOR, WITHIN THE REQUIREMENTS OF SAE AMS 2430 (UNLESS OTHERWISE SPECIFIED ON THE DRAWING). THE FOLLOWING CRITERIA SHOULD BE USED IN SELECTING THE SHOT MATERIAL (UNLESS OTHERWISE SPECIFIED ON THE DRAWING): STEEL PARTS HEAT TREATED TO VALUES BELOW 200 KSI, USE STANDARD HARDNESS STEEL SHOT (PER SAE AMS 2431/1, 2431/3, OR 2431/4).

18. MACHINING, GRINDING AND HOLE PREPARATION AFTER HEAT TREATMENT TO MEET DRAWING REQUIREMENTS

SHALL BE PER BAC5440. GRINDING PER MIL-STD-866 IN LIEU OF BAC5440.

19. PROCEDURES AND PROCESSES PER DRAWING NOTES AS SUPPLEMENTED BY THIS ENGINEERING DATA

REQUIREMENTS/INSTRUCTIONS (ATTACHMENT “A”) IN LIEU OF D-18462.

20. INSTALL BEARINGS PER THE FOLLOWING IN LIEU OF BAC5435.

21. THE BEARINGS INSTALLATIONS SHALL BE ACCOMPLISHED IN SUCH A MANNER AS TO AVOID DAMAGE TO THE

FINISH ON THE I.D. OF THE HOUSING INTO WHICH THE BUSHING IS INSTALLED, OR THE FINISH OF THE O.D. OF THE BEARINGS. FORCED INSTALLATION OF SUB-ZERO INSTALLATIONS, SUCH AS THE USE OF A PRESS OR HAMMER IS NOT PERMITTED, AND IS NOT ACCEPTABLE. A SMALL NON-METALLIC HAMMER MAY BE USED TO TAP THE

BEARINGS INTO ALIGNMENT WITH THE HOUSING BORE, OR TO SEAT THE BEARINGS.

21.1. PRIOR TO BEARINGS INSTALLATION, THE PARTS AND HOUSING BORE SHALL BE CLEANED WITH CLEANING

SOLVENT TO REMOVE ALL CONTAMINATION.

21.2. LIQUID NITROGEN SHALL BE USED FOR ALL SUB-ZERO INSTALLATIONS UNLESS SOME OTHER SUB-ZERO COOLANT IS SPECIFIED AND APPROVED BY OO-ALC LANDING GEAR ENGINEERING. THE SOAK TIME OF THE BUSHING IN THE LIQUID NITROGEN SHALL BE SUFFICIENT TO ALLOW THE BUSHING TO REACH THE SAME

TEMPERATURE AS THE COOLANT.

21.3. THE BEARINGS SHALL BE INSTALLED INTO THE HOUSING IMMEDIATELY UPON REMOVAL FROM THE COOLANT

WITH AN ABSOLUTE MINIMUM OF LOST TIME. TRIAL RUNS SHALL BE ACCOMPLISHED AS NECESSARY TO MINIMIZE INSTALLATION TIME WHICH SHOULD BE IN THE ORDER OF ABOUT SEVEN (7) SECONDS MAXIMUM.

21.4. IT MAY OCCASIONALLY BE NECESSARY TO HEAT THE HOUSING INTO WHICH THE BEARINGS IS TO BE

INSTALLED IN ADDITION TO SUB-ZERO COOLING OF THE BEARINGS. DETAIL PARTS IN PROCESS WILL NOT HAVE PAINT, SEALANT OR OTHER ORGANIC MATERIAL APPLIED PRIOR TO HEATING. THE PARTS SHALL BE HEATED BY THE USE OF RADIANT HEAT TECHNIQUES SUCH AS THERMAL BLANKETS, INFRARED LAMPS ETC., TO NO MORE THAN A MAXIMUM TEMPERATURE OF 250 F. TEMPERATURE MEASURING DEVICES SHALL BE USED TO MONITOR HEAT AND SHALL BE LOCATED ON AREAS OF THE PART EXPECTED TO REACH MAXIMUM TEMPERATURE. NO

SCALING, OXIDATION OR CORROSION SHALL BE PERMITTED.

21.5. COR-BAN 27L (ZIP-CHEM ZC-027L), HEREAFTER REFERRED TO AS CORROSION INHIBITING COMPOUND, PER BMS

3-38 (BOEING CAGE 81205), MANUFACTURED BY ZIP-CHEM PRODUCTS, 400 JARVIS DR., MORGAN HILL, CA 95037

(CAGE 8E913), SHALL BE USED AS NOTED IN PARAGRAPHS (G) AND (H).

21.6. BEARINGS WITHOUT FLANGES SHALL BE INSTALLED INTO HOUSING BORE WHICH HAS RECEIVED A LIGHT

COAT OF CORROSION INHIBITING COMPOUND. CORROSION INHIBITING COMPOUND SHALL NOT OBSTRUCT

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 3 of 19

GREASE ZERK PASSAGES. INSTALL SHRUNKEN BEARINGS AND WIPE OFF ANY EXCESS COMPOUND THAT MAY

HAVE EXTRUDED AROUND THE PERIPHERY OF BOTH ENDS OF THE BEARINGS.

21.7. BEARINGS WITH FLANGES SHALL BE INSTALLED IN A SIMILAR MANNER AS PARAGRAPH (G), EXCEPT

CORROSION-INHIBITING COMPOUND SHALL ALSO BE APPLIED TO FACE OF LUG UNDER FLANGE. THE COMPOUND SHALL BE APPLIED IN SUCH A MANNER AS TO ENSURE COMPLETE COVERAGE OF INSIDE FACE OF BEARINGS FLANGE WHEN BEARINGS IS INSTALLED. WIPE OFF ANY EXCESS COMPOUND AROUND PERIPHERY OF BEARINGS

FLANGE FORMING A BEAD. WIPE ANY EXCESS COMPOUND FROM OTHER END OF BEARINGS ALSO.

22. THE FOLLOWING DOCUMENTS ARE NOT REQUIRED FOR MANUFACTURE AND WILL NOT BE PROVIDED: BAC5307, BAC5424, BAC5617, BAC 5048, BAC5730, D2-5000, D6-5000, BAC5845, BAC5423 BACD2074 AND BAC5435.

23. MATERIAL SUBSITUTIONS SHALL BE PER OO-ALC LANDING GEAR ENGINEERING APPROVAL IN LIEU OF GUIDANCE

PER BAC5005.

24. MARKING AND IDENTIFICATION TO MEET DRAWING REQUIREMENTS PER MIL-STD-130 IN LIEU OF BAC 5307.

25. FINISH AS REQUIRED BY THE DRAWING SHALL BE PER THE FOLLOWING IN LIEU OF FINISH CODE PER D2-5000.

25.1. APPLY ONE COAT EPOXY WATERBORNE PRIMER PER MIL-PRF-85582 TYPE I CLASS C2 OR N. ALTERNATE ONE

COAT OF EPOXY POLYAMIDE PRIMER PER MIL-PRF-23377 TYPE I CLASS C2 OR N.

25.2. APPLY TWO TOPCOATS POLYURETHANE PER MIL-PRF-85285 TYPE I CLASS H. USE COLOR NUMBER 17925 (WHITE)

PER FED-STD-595 IN LIEU OF COLOR NUMBER 17875.

26. DRAWING 65-3693 (-27) DRAG BRACE ASSY-NOSE GEAR

27. MARKING AND UNIQUE IDENTIFICATION (UID) TO MEET DRAWING REQUIREMENTS PER MIL-STD-130 AND THE

FOLLOWING IN LIEU OF BAC 5307.

27.1. TESA TAPE LABEL APPLIED DIRECTLY TO PART AND HRI ETCHED DIRECTLY ON PART: UNIQUE IDENTIFICATION (UID) SHALL BE APPLIED TO EACH PART PER MIL-STD-130. THE UID SHALL CONTAIN HUMAN- READABLE INFORMATION (HRI) AND MACHINE-READABLE INFORMATION (MRI) MARKINGS. QUALITY AND TECHNICAL REQUIREMENTS FOR BOTH THE MRI AND HRI SHALL BE IN ACCORDANCE WITH SAE AS9132. THE METHOD OF MARKING FOR THE HRI SHALL BE LIMITED TO ELECTRO-CHEMICAL ETCHING, DOT PEEN, VIBRO PEEN, OR MICRO-MILL. THE DEPTH OF EACH MARK SHALL BE FROM .003 - .005 INCHES. THE HRI MARK SHALL INCLUDE BOTH THE PART NUMBER AND THE SERIAL NUMBER. THE SERIAL NUMBER WILL BE LIMITED TO 16 ALPHANUMERIC CHARACTERS INCLUDING THE VENDOR CAGE (FSCM) OF THE CONTRACTOR NAMED ON THE CONTRACT, DATE OF MANUFACTURE IN THE FORMAT MMYY, AND A UNIQUE 4-DIGIT NUMBER STARTING WITH 0001 IN NUMERICAL ORDER OF MANUFACTURE. THE HRI SHALL APPEAR AS “SN 9874701040001”. THE HEIGHT OF EACH ALPHANUMERIC CHARACTER IN THE HRI SHALL BE A MAXIMUM OF .125 INCHES. THE METHOD OF MARKING FOR THE MRI SHALL BE IN ACCORDANCE WITH DRAWING 200827953-11. APPLY TWO TOPCOATS POLYURETHANE OVER LABEL PER MIL-PRF-85285, TYPE I, CLEAR PER FED-STD-595.THE LOCATION OF THE UID SHALL IN ACCORDANCE WITH EO 13C0141-H. TESA TAPE LABEL SHALL ONLY BE PLACED ON THE TOP COAT OF

THE PAINTED COMPONENTS.

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 4 of 19

28. LUBRICATE PER BEST AIRCRAFT INDUSTRY STANDARDS IN LIEU OF BAC5008 USING GREASE PER MIL-G-81322 OR

MIL-PRF-81322 IN LIEU OF MIL-G-3728 OR MIL-G-21164.

29. INSTALL FASTENERS PER AIA/NAS NASM 47196 IN LIEU OF BAC 5004 AND BAC 5047.

30. FUNCTION TEST DRAWING 65-6625 IS NOT REQUIRED FOR MANUFACTURE AND WILL NOT BE PROVIDED.

31. DRAWING 3-98799 (-1 & -2) SPRING-TORSION

32. USE STEEL MUSIC WIRE MATERIAL TO MEET DRAWING REQUIREMENTS PER ASTM A228/A228M IN LIEU OF MIL-W-

6101.

33. IN LIEU OF FINISH CODE F-1.20 (SPRINGS): CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870

TYPE II CLASS 2. DO NOT FLEX SPRINGS PRIOR TO BAKING.

34. DRAWING 3-99400 PLUG

35. USE 4130 STEEL BAR MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS-S-6758 IN LIEU OF MIL-S-6758

36. OR USE 4140 STEEL ALLOY MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6349 OR SAE AMS 6382 IN

LIEU OF MIL-S-5626

37. HEAT-TREAT STEEL PER SAE AMS-H-6875 (160-180 KSI ) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875.

(BAC5617)

38. IN LIEU OF FINISH CODE F-1.20: CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870 TYPE II

CLASS 2.

39. LUBRICANT, SOLID FILM PER MIL-PRF-46010 IN LIEU OF BMS3.3.

40. DRAWING: 3-99413 BOLT

41. USE 4130 STEEL BAR MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS-S-6758 IN LIEU OF MIL-S-6758.

42. OR USE 4140 STEEL ALLOY MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6349 OR SAE AMS 6382 IN

LIEU OF MIL-S-5626.

43. HEAT-TREAT STEEL PER SAE AMS-H-6875 (160-180 KSI ) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875.

(BAC5617).

44. IN LIEU OF FINISH CODE F-1.20: CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870 TYPE II

CLASS 2.

45. DRAWING: 3-99448 ROLLER

46. USE STEEL MATERIAL (SAE 52100) TO MEET DRAWING REQUIREMENTS PER SAE AMS 6444 IN LIEU OF AMS 6444.

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 5 of 19

47. HEAT-TREAT STEEL PER SAE AMS-H-6875 TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875. (BAC5617)

48. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT

WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE PERFORMED WITHOUT A WAIVER FROM OO-ALC LANDING GEAR ENGINEERING. GRINDING WILL BE PER MIL-STD- 866.

49. FORM, PUNCH AND FIT METAL PARTS PER BEST AIRCRAFT INDUSTRY PRACTICES AND THE FOLLOWING IN LIEU OF

BAC5300: BREAK SHARP EDGES 0.002-0.003 OR AS SPECIFIED ON DRAWING PER BEST AIRCRAFT INDUSTRY PRACTICES IN LIEU OF BAC5300. BROKEN EDGES SHALL NOT EXHIBIT BURRS DETECTABLE BY TOUCH.

STRAIGHTENING OF PART IS PROHIBITED. BAC5300 WILL NOT BE PROVIDED.

50. HOLE PREPARATION, MACHINING, AND GRINDING PER BEST AIRCRAFT INDUSTRY PRACTICES/STANDARDS AND THE

FOLLOWING IN LIEU OF BAC5440.

51. DRAWING: 4-80140 LINK ASSY. SIDE BRACE, TIP PROTECTION GEAR

52. FINISH PER THE FOLLOWING IN LIEU OF IN LIEU OF FINISH CODES IN DRAWINGS D2-5000:

52.1. IN LIEU OF FINISH CODE F-1.10: NO FINISH IS REQUIRED EXCEPT THAT TEMPORARY CORROSION PROTECTION DURING HANDLING, TRANSPORTATION AND STORAGE MAY BE APPLIED PER MIL-PRF-16173 CLASS II GRADE 3 OR

MIL-C-11796 CLASS 3.

52.2. IN LIEU OF FINISH CODE F-12.43: APPLY A LIGHT FILM OF MIL-PRF-7870 OIL TO ALL SURFACES AT TIME OF

INSTALLATION.

53. MARKING AND UNIQUE IDENTIFICATION (UID) TO MEET DRAWING REQUIREMENTS PER MIL-STD-130 AND THE

53.1. TESA TAPE LABEL APPLIED DIRECTLY TO PART AND HRI ETCHED DIRECTLY ON PART: UNIQUE IDENTIFICATION (UID) SHALL BE APPLIED TO EACH PART PER MIL-STD-130. THE UID SHALL CONTAIN HUMAN-READABLE INFORMATION (HRI) AND MACHINE-READABLE INFORMATION (MRI) MARKINGS. QUALITY AND TECHNICAL REQUIREMENTS FOR BOTH THE MRI AND HRI SHALL BE IN ACCORDANCE WITH SAE AS9132. THE METHOD OF MARKING FOR THE HRI SHALL BE LIMITED TO ELECTRO-CHEMICAL ETCHING, DOT PEEN, VIBRO PEEN, OR MICRO- MILL. THE DEPTH OF EACH MARK SHALL BE FROM .003 - .005 INCHES. THE HRI MARK SHALL INCLUDE BOTH THE PART NUMBER AND THE SERIAL NUMBER. THE SERIAL NUMBER WILL BE LIMITED TO 16 ALPHANUMERIC CHARACTERS INCLUDING THE VENDOR CAGE (FSCM) OF THE CONTRACTOR NAMED ON THE CONTRACT, DATE OF MANUFACTURE IN THE FORMAT MMYY, AND A UNIQUE 4-DIGIT NUMBER STARTING WITH 0001 IN NUMERICAL ORDER OF MANUFACTURE. THE HRI SHALL APPEAR AS “SN 9874701040001”. THE HEIGHT OF EACH ALPHANUMERIC CHARACTER IN THE HRI SHALL BE A MAXIMUM OF .125 INCHES. THE METHOD OF MARKING FOR THE MRI SHALL BE IN ACCORDANCE WITH DRAWING 200827953-01A. APPLY TWO TOPCOATS POLYURETHANE OVER LABEL PER MIL-PRF-85285, TYPE I, CLEAR PER FED-STD-595.THE LOCATION OF THE UID SHALL BE IDENTIFIED ON THE DRAWING (REF ENGINEERING ORDER 09A0330). TESA TAPE LABEL SHALL ONLY BE PLACED

ON THE TOP COAT OF THE PAINTED COMPONENTS.

54. DRAWING: 4-80142 BEARING, SIDE BRACE TIP PROTECTION

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 6 of 19

55. IN LIEU OF FINISH CODE F-12.40: APPLY NO FINISH.

56. DRAWING: 4-80143 (-1 LINK-SIDE BRACE)

57. (CSI) HEAT-TREAT STEEL PER SAE AMS-H-6875 (180-200 KSI) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-

6875. (BAC5617)

58. (CSI) ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT

WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

59. HOLE PREPARATION, MACHINING, AND GRINDING PER BEST AIRCRAFT INDUSTRY PRACTICES/STANDARDS AND THE

60. (CSI) CADMIUM PLATE PER MIL-STD-870, TYPE II, CLASS 2 IN LIEU OF F-1.181, (D2-5000).

61. (CSI) MAKE FROM FORGING 69-59128-1 OR MACHINE FROM 4340 STEEL MATERIAL TO MEET DRAWING

REQUIREMENTS PER SAE AMS 6415 OR SAE AMS 6484 IN LIEU OF MIL-S-5000.

62. DRAWING: 69-59128 (-1 LINK FORGING, OPTIONAL PER NOTE 60)

63. TOOLING POINTS PER ASME Y14.5 IN LIEU OF BAC5482.

64. (CSI) USE 4340 STEEL MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6415 OR SAE AMS 6484 IN LIEU OF

MIL-S-5000.

65. FORGE STEEL PER SAE AMS-F-7190 TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-F-7190. CONTRACTOR SHALL

PROCURE FORGINGS AND DEVELOP FORGING DIES IN ACCORDANCE WITH FORGING DIE QUALIFICATION DOCUMENT

ENCLOSED IN THIS TECHNICAL DATA PACKAGE.

65.1. THE CONTRACTOR MAY PROCURE FORGINGS FROM SOURCES PRE-APPROVED BY LANDING GEAR ENGINEERING

PER PARAGRAPH (A), OR MAY ELECT TO DEVELOP SOURCES PER PARAGRAPH (B).

65.2. IF FORGINGS ARE PROCURED FROM TOOLING APPROVED BY OO-ALC LANDING GEAR ENGINEERING, ORIGINAL CERTIFIED FORGING PROCEDURES AND DIES/TOOLING OR EQUIVALENT (E.G., REFURBISHED/RESUNK BY APPROVED FORGING SOURCE AND HAVING THE SAME DIE NUMBER DESIGNATION) SHALL BE USED. NEW TOOLING AT AN EXISTING SOURCE WILL BE QUALIFIED PER PARAGRAPH (B). PRIOR TO CONTRACT AWARD, THE DETAILED PART BIDDER SHALL PROVIDE VERIFICATION (E.G., FORGING QUOTE) TO THE GOVERNMENT THAT THE CERTIFIED DIES AND PROCEDURES ARE AVAILABLE FOR THEIR USE IN THE EVENT THEY ARE THE SUCCESSFUL

BIDDER.

65.2.1. FORGING DRAWING: (69-59128)

65.2.2. DIE #: UNKNOWN

65.2.3. LOCATION OF FORGING DIES: UNKNOWN

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 7 of 19

65.2.4. PHONE:

65.2.5. CAGE CODE:

65.3. IF THE FORGING SOURCE IS LISTED AS UNKNOWN OR THE CONTRACTOR WISHES TO DEVELOP ADDITIONAL

SOURCES OR NEW TOOLING AT AN EXISTING FORGING SOURCE, THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE PRIOR TO CONTRACT AWARD. THE CONTRACTOR SHALL NOT PROCEED TO OBTAIN NEW DIES WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT-PROCURING AGENCY (SEE OO-ALC LANDING GEAR ENGINEERING FORGING SQS FOR FURTHER INFORMATION ON FORGING TOOLING QUALIFICATION REQUIREMENTS). THE GOVERNMENT SHALL HAVE UNLIMITED USE OF THE DIES DEVELOPED UNDER THIS CONTRACT. THE CONTRACTOR SHALL INFORM THE FORGING HOUSE IN WRITING, AT THE SAME TIME THE ORDER FOR THE DIES IS PLACED, THAT THE GOVERNMENT HAS UNLIMITED USE RIGHTS OF THE DIES AND FORWARD A COPY OF THIS

LETTER TO THE GOVERNMENT CONTRACTING OFFICER.

65.4. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE

FORGING DRAWING AND SAE AMS-F-7190 FOR STEEL FORGINGS. THE DETAILED PART CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE FORGING SOURCE AND RETAIN IN THEIR RECORDS FOR NO LESS THAN 10 YEARS. LANDING GEAR ENGINEERING RESERVES THE RIGHT TO REVIEW THIS DOCUMENTATION

AS NEEDED.

66. DRAWING: 4-80141 (-1 LINK ASSEMBLY SIDE BRACE)

67. FINISH PER THE FOLLOWING IN LIEU OF IN LIEU OF FINISH CODES IN DRAWINGS D2-5000:

67.1. IN LIEU OF FINISH CODE F-1.10: NO FINISH IS REQUIRED EXCEPT THAT TEMPORARY CORROSION PROTECTION DURING HANDLING, TRANSPORTATION AND STORAGE MAY BE APPLIED PER MIL-PRF-16173 CLASS II GRADE 3 OR

MIL-C-11796 CLASS 3.

67.2. IN LIEU OF FINISH CODE F-12.43: APPLY A LIGHT FILM OF MIL-PRF-7870 OIL TO ALL SURFACES AT TIME OF

INSTALLATION.

68. DRAWING: 4-80144 (-1 LINK SIDE BRACE)

69. MAKE FROM FORGING 69-59128-1 OR MACHINE FROM 4340 STEEL MATERIAL TO MEET DRAWING REQUIREMENTS PER

SAE AMS 6415 OR SAE AMS 6484 IN LIEU OF MIL-S-5000.

70. HEAT-TREAT STEEL PER SAE AMS-H-6875 (180-200 KSI) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875.

(BAC5617)

71. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT

WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 8 of 19

72. HOLE PREPARATION, MACHINING, AND GRINDING PER BEST AIRCRAFT INDUSTRY PRACTICES/STANDARDS AND THE

73. CADMIUM PLATE PER MIL-STD-870, TYPE II, CLASS 2 IN LIEU OF F-1.181, (D2-5000).

74. DRAWING: 69-66127 (-1 LINK ASSY, OPTIONAL TO 4-80141-1)

75. USE 4340 STEEL MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6414 IN LIEU OF BMS 7-26.

76. HEAT-TREAT STEEL PER SAE AMS-H-6875 (270-300 KSI ) TO MEET DRAWING REQUIREMENTS IN LIEU OF BAC5617.

77. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT

WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

78. ON STEEL PARTS HEAT-TREATED TO 180 KSI UTS OR ABOVE, CHROMIUM PLATE PER MIL-STD-1501, TYPE II CLASS 2.

79. THE MAXIMUM ALLOWABLE DELAY FOR THE 4-HOUR BAKE BETWEEN CHROMIUM PLATE AND CADMIUM PLATE

OPERATIONS AS REFERENCED IN MIL-STD-1501 SHALL BE 4 HOURS.

80. IN LIEU OF FINISH CODE F-15.01: CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870 TYPE II

CLASS 2 IN LIEU OF TITANIUM CADMIUM PLATE. BAKE 12 HOURS MINIMUM AT 375 +/- 25 F AND APPLY CHROMATE

POST PLATE TREATMENT PER SAE AMS-QQ-P-416 TYPE II.

81. DRAWING: 4-80145 (WASHER)

82. MATERIAL: USE SAE 8630 STEEL PER SAE AMS 6280 (NORMALIZED) IN LIEU OF MIL-S-6050.

83. USE 4130 STEEL BAR MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS-S-6758 IN LIEU OF MIL-S-6758.

84. HEAT-TREAT STEEL PER SAE AMS-H-6875 (150-170 KSI) TO MEET DRAWING REQUIREMENTS.

85. PER F-1.10, D2-5000: APPLY NO FINISH EXCEPT TEMPORARY PROTECTION MAY BE APPLIED FOR HANDLING, TRANSPORTATION AND STORAGE MAY BE APPLIED PER MIL-PRF-16173 CLASS II GRADE 3 OR MIL-C-11796 CLASS 3.

86. DRAWING: 6-68013 (-2 ARM-DRAG BRACE)

87. THIS COMPONENT/ASSEMBLY IS CRITICAL SAFETY ITEM (CSI). THE FOLLOWING FEATURES AND PROCESSES ARE

SAFETY CRITICAL. ASSOCIATED TOLERANCES, LOCATIONS, PERPENDICULARITIES, CONCENTRICITY’S, ETC. OF THE REFERENCED FEATURES ARE ALSO SAFETY CRITICAL. THE PROCESSED REFERENCED MUST COMPLY STRICTLY WITH

THE SPECIFICATIONS REQUIRED BY CONTRACT. REFER TO IN LIEU ITEMS.

CSI HEAT TREAT PER SAE AMS-H-6875

CSI INSPECT FOR BURNS PER MIL-STD-867

CSI GRINDING PER MIL-STD-867

CSI MPI PER ASTM E 1444

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 9 of 19

CSI CADMIUM PLATE PER MIL-STD-870 TYPE II CLASS 2

CSI MATERIAL PER SAE AMS 6349 OR SAE AMS 6382

CSI AMERICAN STANDARD INVOLUTE SPLINE, SHEET 1

88. USE 4140 STEEL ALLOY MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6349 OR SAE AMS 6382 IN LIEU

OF MIL-S-5626.

89. HEAT-TREAT STEEL PER SAE AMS-H-6875 (180-200 KSI) TO MEET DRAWING REQUIREMENTS.

90. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

91. FORGE STEEL PER SAE AMS-F-7190 TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-F-7190. CONTRACTOR SHALL

PROCURE FORGINGS AND DEVELOP FORGING DIES IN ACCORDANCE WITH FORGING DIE QUALIFICATION DOCUMENT

ENCLOSED IN THIS TECHNICAL DATA PACKAGE.

91.1. THE CONTRACTOR MAY PROCURE FORGINGS FROM SOURCES PRE-APPROVED BY LANDING GEAR ENGINEERING

PER PARAGRAPH (A), OR MAY ELECT TO DEVELOP SOURCES PER PARAGRAPH (B).

91.2. IF FORGINGS ARE PROCURED FROM TOOLING APPROVED BY OO-ALC LANDING GEAR ENGINEERING, ORIGINAL CERTIFIED FORGING PROCEDURES AND DIES/TOOLING OR EQUIVALENT (E.G., REFURBISHED/RESUNK BY APPROVED FORGING SOURCE AND HAVING THE SAME DIE NUMBER DESIGNATION) SHALL BE USED. NEW TOOLING AT AN EXISTING SOURCE WILL BE QUALIFIED PER PARAGRAPH (B). PRIOR TO CONTRACT AWARD, THE DETAILED PART BIDDER SHALL PROVIDE VERIFICATION (E.G., FORGING QUOTE) TO THE GOVERNMENT THAT THE CERTIFIED DIES AND PROCEDURES ARE AVAILABLE FOR THEIR USE IN THE EVENT THEY ARE THE SUCCESSFUL

BIDDER.

91.2.1. FORGING DRAWING: (6-68013)

91.2.2. DIE #: 2817

91.2.3. LOCATION OF FORGING DIES: UNKNOWN

91.2.4. PHONE:

91.2.5. CAGE CODE:

91.3. IF THE FORGING SOURCE IS LISTED AS UNKNOWN OR THE CONTRACTOR WISHES TO DEVELOP ADDITIONAL

GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE PRIOR TO CONTRACT AWARD. THE CONTRACTOR SHALL NOT PROCEED TO OBTAIN NEW DIES WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT-PROCURING AGENCY (SEE OO-ALC LANDING GEAR ENGINEERING FORGING SQS FOR FURTHER INFORMATION ON FORGING TOOLING QUALIFICATION REQUIREMENTS). THE GOVERNMENT SHALL HAVE UNLIMITED USE OF THE DIES DEVELOPED UNDER THIS CONTRACT. THE CONTRACTOR SHALL INFORM THE FORGING HOUSE IN WRITING, AT THE SAME TIME THE ORDER FOR THE DIES IS

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 10 of 19

PLACED, THAT THE GOVERNMENT HAS UNLIMITED USE RIGHTS OF THE DIES AND FORWARD A COPY OF THIS

LETTER TO THE GOVERNMENT CONTRACTING OFFICER.

91.4. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE

FORGING DRAWING AND SAE AMS-F-7190 FOR STEEL FORGINGS AND SAE AMS-A-22771 FOR ALUMINUM FORGINGS. THE DETAILED PART CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE FORGING SOURCE AND RETAIN IN THEIR RECORDS FOR NO LESS THAN 10 YEARS. LANDING GEAR ENGINEERING

RESERVES THE RIGHT TO REVIEW THIS DOCUMENTATION AS NEEDED.

92. OPTIONAL (IN LIEU OF FORGING): MACHINE FROM 4140 STEEL BAR PER SAE AMS 6349 OR SAE AMS 6382.

93. TOOLING POINTS PER ASME Y14.5 IN LIEU OF BAC5405.

94. IN LIEU OF FINISH CODE F-1.20: CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870 TYPE II

CLASS 2.

95. DRAWING: 63-1428 (DUST SEAL)

96. DRAWING: 63-1427 (-1 SEAL RETAINER)

97. MATERIAL: USE SAE 8630 STEEL PER SAE AMS 6280.

98. ALTERNATE MATERIAL USE SAE-AMS 6350, SAE-AMS 6351, SAE-AMS 6345 STEEL SHEET IN LIEU OF QQ-S-685.

99. HEAT-TREAT STEEL PER SAE AMS-H-6875 (95-120 KSI) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875.

100. IN LIEU OF FINISH CODE F-1.20: CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870 TYPE II

CLASS 2.

101. DRAWING: 63-1580 (ROLLER)

102. MATERIAL: USE AMS SAE 6447, SAE AMS 6444 OR SAE AMS 6440 STEEL INLIEU OF 52100 STEEL PER MIL-S-7420.

103. PER F-1.10, D2-5000: APPLY NO FINISH EXCEPT TEMPORARY PROTECTION MAY BE APPLIED FOR HANDLING, TRANSPORTATION AND STORAGE MAY BE APPLIED PER MIL-PRF-16173 CLASS II GRADE 3 OR MIL-C-11796 CLASS 3.

104. HEAT-TREAT STEEL PER SAE AMS-H-6875 TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875 AND BAC5601.

105. DRAWING: 63-1953 (WASHER-LOCK ACTUATOR ROD)

106. PER F-1.10, D2-5000: APPLY NO FINISH.

107. DRAWING: 65-27514 (-4 UPPER LINK ASSY)

108. MARKING AND UNIQUE IDENTIFICATION (UID) TO MEET DRAWING REQUIREMENTS PER MIL-STD-130 AND THE

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 11 of 19

108.1. TESA TAPE LABEL APPLIED DIRECTLY TO PART AND HRI ETCHED DIRECTLY ON PART: UNIQUE

READABLE INFORMATION (HRI) AND MACHINE-READABLE INFORMATION (MRI) MARKINGS. QUALITY AND TECHNICAL REQUIREMENTS FOR BOTH THE MRI AND HRI SHALL BE IN ACCORDANCE WITH SAE AS9132. THE METHOD OF MARKING FOR THE HRI SHALL BE LIMITED TO ELECTRO-CHEMICAL ETCHING, DOT PEEN, VIBRO PEEN, OR MICRO-MILL. THE DEPTH OF EACH MARK SHALL BE FROM .003 - .005 INCHES. THE HRI MARK SHALL INCLUDE BOTH THE PART NUMBER AND THE SERIAL NUMBER. THE SERIAL NUMBER WILL BE LIMITED TO 16 ALPHANUMERIC CHARACTERS INCLUDING THE VENDOR CAGE (FSCM) OF THE CONTRACTOR NAMED ON THE CONTRACT, DATE OF MANUFACTURE IN THE FORMAT MMYY, AND A UNIQUE 4-DIGIT NUMBER STARTING WITH 0001 IN NUMERICAL ORDER OF MANUFACTURE. THE HRI SHALL APPEAR AS “SN 9874701040001”. THE HEIGHT OF EACH ALPHANUMERIC CHARACTER IN THE HRI SHALL BE A MAXIMUM OF .125 INCHES. THE METHOD OF MARKING FOR THE MRI SHALL BE IN ACCORDANCE WITH DRAWING 200827953-11A. APPLY TWO TOPCOATS POLYURETHANE OVER LABEL PER MIL-PRF-85285, TYPE I, CLEAR PER FED-STD-595.THE LOCATION OF THE UID SHALL BE IN ACCORDANCE WITH EO 13C0145-H. TESA TAPE LABEL SHALL ONLY BE PLACED ON THE TOP COAT

OF THE PAINTED COMPONENTS.

109. (-2 COVER): MATERIAL: 6061-T6 ALUMINUM ALLOY EXTRUSION PER AMS-QQ-A-200/8 IN LIEU OF QQ-A-200/8.

98.1 IN LIEU OF FINISH CODE F-2.20: CHROMIC ACID ANODIZE PER MIL-A-8625 TYPE I OR IC (PREFERRED), CLASS 1.

110. DRAWING: 6-68043 (-1 SIDE PLATE SEAL)

111. MATERIAL: USE MIL-I-24768 IN LIEU OF MIL-P-15035.

112. DRAWING: 65-27513 (-3 UPPER LINK) CRITICAL SAFETY ITEM

113. PART HAS BEEN DETERMINED TO BE A SAFETY CRITICAL ITEM. REFERENCE EO 05A2078 FOR CSI CHARACTERISTICS.

114. HEAT-TREAT STEEL PER SAE AMS-H-6875 (200-240 KSI) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875.

(BAC5617)

115. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT

WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

866 IN LIEU OF BAC5032.

116. ON STEEL PARTS HEAT-TREATED TO 180 KSI UTS OR ABOVE, CHROMIUM PLATE PER MIL-STD-1501, TYPE II CLASS 2

TO MEET DRAWING REQUIREMENTS IN LIEU OF FINISH CODE F-1.843.

117. THE MAXIMUM ALLOWABLE DELAY FOR THE 4-HOUR BAKE BETWEEN CHROMIUM PLATE AND CADMIUM PLATE

OPERATIONS AS REFERENCED IN MIL-STD-1501 SHALL BE 4 HOURS.

118. HOLE PREPARATION, MACHINING, AND GRINDING PER BEST AIRCRAFT INDUSTRY PRACTICES/STANDARDS AND

THE FOLLOWING IN LIEU OF BAC5440 TYPE I:

118.1. MACHINE, DE-BUR AND BLEND METALS TO MEET DRAWING REQUIREMENTS PER BEST AIRCRAFT INDUSTRY

PRACTICES.

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 12 of 19

118.2. DRILLING, REAMING AND HONING TO MEET DRAWING SPECIFICATIONS USING BEST AIRCRAFT INDUSTRY

119. IN LIEU OF FINISH CODE F-1.181 (F-1.308): CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870

TYPE II CLASS 2. BAKE 12 HOURS MINIMUM AT 375 ± 25F AFTER PLATE.

120. DRAWING: 65-2861 (-4 UPPER LINK) FORGING

121. USE 4330M STEEL MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6411 OR SAE AMS 6427 IN LIEU OF

AMS6427. (BMS7-27, BMS7-28)

122. FORGE STEEL PER SAE AMS-F-7190 TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-F-7190.

122.1. THE CONTRACTOR MAY PROCURE FORGINGS FROM SOURCES PRE-APPROVED BY LANDING GEAR ENGINEERING PER PARAGRAPH (A), OR MAY ELECT TO DEVELOP SOURCES PER PARAGRAPH (B).

123. IF FORGINGS ARE PROCURED FROM TOOLING APPROVED BY OO-ALC LANDING GEAR ENGINEERING, ORIGINAL

CERTIFIED FORGING PROCEDURES AND DIES/TOOLING OR EQUIVALENT (E.G., REFURBISHED/RESUNK BY APPROVED FORGING SOURCE AND HAVING THE SAME DIE NUMBER DESIGNATION) SHALL BE USED. NEW TOOLING AT AN EXISTING SOURCE WILL BE QUALIFIED PER PARAGRAPH (B). PRIOR TO CONTRACT AWARD, THE DETAILED PART BIDDER SHALL PROVIDE VERIFICATION (E.G., FORGING QUOTE) TO THE GOVERNMENT THAT THE CERTIFIED DIES AND PROCEDURES ARE AVAILABLE FOR THEIR USE IN THE EVENT THEY ARE THE SUCCESSFUL BIDDER.

123.1. FORGING DRAWING: (65-2861)

123.2. DIE #: UNKNOWN

123.3. LOCATION OF FORGING DIES: UNKNOWN

123.4. PHONE:

123.5. CAGE CODE:

124. IF THE FORGING SOURCE IS LISTED AS UNKNOWN OR THE CONTRACTOR WISHES TO DEVELOP ADDITIONAL

GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE PRIOR TO CONTRACT AWARD. THE CONTRACTOR SHALL NOT PROCEED TO OBTAIN NEW DIES WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT-PROCURING AGENCY (SEE OO-ALC LANDING GEAR ENGINEERING FORGING SQS FOR FURTHER INFORMATION ON FORGING TOOLING QUALIFICATION REQUIREMENTS). THE GOVERNMENT SHALL HAVE UNLIMITED USE OF THE DIES DEVELOPED UNDER THIS CONTRACT. THE CONTRACTOR SHALL INFORM THE FORGING HOUSE IN WRITING, AT THE SAME TIME THE ORDER FOR THE DIES IS PLACED, THAT THE GOVERNMENT HAS UNLIMITED USE RIGHTS OF THE DIES AND FORWARD A COPY OF THIS LETTER TO THE

GOVERNMENT CONTRACTING OFFICER.

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 13 of 19

124.1. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE

FORGINGS. THE DETAILED PART CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE

125. HEAT-TREAT STEEL PER SAE AMS-H-6875 (220-240 KSI ) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875.

(BAC5617)

126. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT

WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

127. CADMIUM PLATE PER MIL-STD-870, TYPE II, CLASS 2 IN LIEU OF BAC5718.

128. DRAWING: 65-4828 (-19 LOWER LINK)

129. MARKING AND UNIQUE IDENTIFICATION (UID) TO MEET DRAWING REQUIREMENTS PER MIL-STD-130 AND THE

129.1. TESA TAPE LABEL APPLIED DIRECTLY TO PART AND HRI ETCHED DIRECTLY ON PART: UNIQUE

READABLE INFORMATION (HRI) AND MACHINE-READABLE INFORMATION (MRI) MARKINGS. QUALITY AND TECHNICAL REQUIREMENTS FOR BOTH THE MRI AND HRI SHALL BE IN ACCORDANCE WITH SAE AS9132. THE METHOD OF MARKING FOR THE HRI SHALL BE LIMITED TO ELECTRO-CHEMICAL ETCHING, DOT PEEN, VIBRO PEEN, OR MICRO-MILL. THE DEPTH OF EACH MARK SHALL BE FROM .003 - .005 INCHES. THE HRI MARK SHALL INCLUDE BOTH THE PART NUMBER AND THE SERIAL NUMBER. THE SERIAL NUMBER WILL BE LIMITED TO 16 ALPHANUMERIC CHARACTERS INCLUDING THE VENDOR CAGE (FSCM) OF THE CONTRACTOR NAMED ON THE CONTRACT, DATE OF MANUFACTURE IN THE FORMAT MMYY, AND A UNIQUE 4-DIGIT NUMBER STARTING WITH 0001 IN NUMERICAL ORDER OF MANUFACTURE. THE HRI SHALL APPEAR AS “SN 9874701040001”. THE HEIGHT OF EACH ALPHANUMERIC CHARACTER IN THE HRI SHALL BE A MAXIMUM OF .125 INCHES. THE METHOD OF MARKING FOR THE MRI SHALL BE IN ACCORDANCE WITH DRAWING 200827953-11A. APPLY TWO TOPCOATS POLYURETHANE OVER LABEL PER MIL-PRF-85285, TYPE I, CLEAR PER FED-STD-595.THE LOCATION OF THE UID SHALL BE IN ACCORDANCE WITH EO 12C0100-H. TESA TAPE LABEL SHALL ONLY BE PLACED ON THE TOP COAT

OF THE PAINTED COMPONENTS.

130. -11 (SIDE PLATE ASSY.

131. F-12.42: INSTALL ANTI-FRICTION AND FRICTION BEARING WITH A THIN FILM OF MIL-PRF-23827.

132. -12 (SIDE PLATE ASSY

133. F-12.42: INSTALL ANTI-FRICTION AND FRICTION BEARING WITH A THIN FILM OF MIL-PRF-23827.

134. DRAWING: 65-4827 (-4 LOWER LINK)

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 14 of 19

135. 65-4827-1 FORGING IS NO LONGER AVAILABLE, OPTIONAL TO MACHINE FROM MATERIAL PER NOTE 136 OR MAKE

FROM 65-18749-5.

136. MATERIAL USE 4330M STEEL PER SAE AMS 6411 OR SAE AMS 6427 IN LIEU OF MIL-S-8699.

137. HEAT-TREAT STEEL PER SAE AMS-H-6875 (220-240 KSI) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-6875.

(BAC5617)

138. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT

WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

866 IN LIEU OF BAC5032.

139. HOLE PREPARATION, MACHINING, AND GRINDING PER BEST AIRCRAFT INDUSTRY PRACTICES/STANDARDS AND

THE FOLLOWING IN LIEU OF BAC5440 TYPE I:

139.1. MACHINE, DE-BUR AND BLEND METALS TO MEET DRAWING REQUIREMENTS PER BEST AIRCRAFT INDUSTRY

PRACTICES.

139.2. DRILLING, REAMING AND HONING TO MEET DRAWING SPECIFICATIONS USING BEST AIRCRAFT INDUSTRY

140. IN LIEU OF FINISH CODE F-1.181 (F-1.308): CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870

TYPE II CLASS 2. BAKE 12 HOURS MINIMUM AT 375 ± 25F AFTER PLATE.

141. DRAWING: 69-70401 (-1 BRACKET-NLG, LOCK ALIGNMENT STRIPES)

142. MATERIAL 4130 STEEL ALLOY PER SAE AMS 6345, SAE AMS 6350 OR SAE AMS 6351 TO MEET DRAWING

REQUIREMENTS IN LIEU OF MIL-S-18729.

143. HEAT-TREAT STEEL PER SAE AMS-H-6875 (125-145 KSI) TO MEET DRAWING REQUIREMENTS IN LIEU OF BAC5617.

144. CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER SAE AMS-QQ-P-416 TYPE II CLASS 2 IN LIEU OF FINISH

CODE F-16.02.

145. DRAWING: 65-1382 (-7 & -8 SIDE PLATE)

146. MARKING AND UNIQUE IDENTIFICATION (UID) TO MEET DRAWING REQUIREMENTS PER MIL-STD-130 AND THE

146.1. TESA TAPE LABEL APPLIED DIRECTLY TO PART AND HRI ETCHED DIRECTLY ON PART: UNIQUE

READABLE INFORMATION (HRI) AND MACHINE-READABLE INFORMATION (MRI) MARKINGS. QUALITY AND TECHNICAL REQUIREMENTS FOR BOTH THE MRI AND HRI SHALL BE IN ACCORDANCE WITH SAE AS9132. THE METHOD OF MARKING FOR THE HRI SHALL BE LIMITED TO ELECTRO-CHEMICAL ETCHING, DOT PEEN, VIBRO

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 15 of 19

PEEN, OR MICRO-MILL. THE DEPTH OF EACH MARK SHALL BE FROM .003 - .005 INCHES. THE HRI MARK SHALL INCLUDE BOTH THE PART NUMBER AND THE SERIAL NUMBER. THE SERIAL NUMBER WILL BE LIMITED TO 16 ALPHANUMERIC CHARACTERS INCLUDING THE VENDOR CAGE (FSCM) OF THE CONTRACTOR NAMED ON THE CONTRACT, DATE OF MANUFACTURE IN THE FORMAT MMYY, AND A UNIQUE 4-DIGIT NUMBER STARTING WITH 0001 IN NUMERICAL ORDER OF MANUFACTURE. THE HRI SHALL APPEAR AS “SN 9874701040001”. THE HEIGHT OF EACH ALPHANUMERIC CHARACTER IN THE HRI SHALL BE A MAXIMUM OF .125 INCHES. THE METHOD OF MARKING FOR THE MRI SHALL BE IN ACCORDANCE WITH DRAWING 200827953-03A. APPLY TWO TOPCOATS POLYURETHANE OVER LABEL PER MIL-PRF-85285, TYPE I, CLEAR PER FED-STD-595.THE LOCATION OF THE UID SHALL BE IDENTIFIED ON EO 09A2998. TESA TAPE LABEL SHALL ONLY BE PLACED ON THE TOP COAT OF THE

PAINTED COMPONENTS.

147. (CSI) USE 4330M STEEL MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6411 OR SAE AMS 6427 IN LIEU

OF AMS 6411 OR MIL-S-8699.

148. (CSI) FORGE STEEL PER SAE AMS-F-7190 TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-F-7190.

148.1. THE CONTRACTOR MAY PROCURE FORGINGS FROM SOURCES PRE-APPROVED BY LANDING GEAR

149. IF FORGINGS ARE PROCURED FROM TOOLING APPROVED BY OO-ALC LANDING GEAR ENGINEERING, ORIGINAL

CERTIFIED FORGING PROCEDURES AND DIES/TOOLING OR EQUIVALENT (E.G., REFURBISHED/RESUNK BY APPROVED FORGING SOURCE AND HAVING THE SAME DIE NUMBER DESIGNATION) SHALL BE USED. NEW TOOLING AT AN EXISTING SOURCE WILL BE QUALIFIED PER PARAGRAPH (B). PRIOR TO CONTRACT AWARD, THE DETAILED PART

. 1. FORGING DRAWING: 65-1382-4

2. CONTROL OF FORGING PROCESS: W. PAT CROW, INC

3. DIE #: 5087

4. LOCATION OF FORGING DIES:

W. PAT CROW, INC

200 LUXTON STR.

FT. WORTH, TX 76104-1720

5. PHONE: (817) 536-2861

6. CAGE: 97490

7. POC: SHELLIE SULLIVAN

150. IF THE FORGING SOURCE IS LISTED AS UNKNOWN OR THE CONTRACTOR WISHES TO DEVELOP ADDITIONAL

SOURCES OR NEW TOOLING AT AN EXISTING FORGING SOURCE, THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE PRIOR TO CONTRACT AWARD. THE CONTRACTOR SHALL NOT PROCEED TO OBTAIN NEW DIES WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT-PROCURING AGENCY (SEE OO-ALC LANDING GEAR ENGINEERING FORGING SQS FOR FURTHER INFORMATION ON FORGING TOOLING QUALIFICATION REQUIREMENTS). THE GOVERNMENT SHALL HAVE UNLIMITED USE OF THE DIES DEVELOPED UNDER THIS CONTRACT. THE CONTRACTOR SHALL INFORM THE FORGING HOUSE IN WRITING, AT THE SAME TIME THE ORDER FOR THE DIES IS PLACED, THAT

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 16 of 19

150.1. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE

FORGINGS. THE DETAILED PART CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE

151. TOOLING POINTS PER ASME Y14.5 IN LIEU OF BAC5405.

152. (CSI) HEAT-TREAT STEEL PER SAE AMS-H-6875 (220-240 KSI ) TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-H-

6875. (BAC5617)

153. (CSI) ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT

TREAT WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE PERFORMED WITHOUT A WAIVER FROM OO-ALC LANDING GEAR ENGINEERING. GRINDING WILL BE PER MIL-

STD-866.

154. (CSI) ON STEEL PARTS HEAT-TREATED TO 180 KSI UTS OR ABOVE, CHROMIUM PLATE PER MIL-STD-1501, TYPE II

CLASS 2.

155. THE MAXIMUM ALLOWABLE DELAY FOR THE 4-HOUR BAKE BETWEEN CHROMIUM PLATE AND CADMIUM PLATE

OPERATIONS AS REFERENCED IN MIL-STD-1501 SHALL BE 4 HOURS.

156. (CSI) CADMIUM PLATE PER MIL-STD-870, TYPE II, CLASS 2 IN LIEU OF F-1.181, (D2-5000)

157. DRAWING: 6-68012(-1 BEARING)

158. USE ALUMINUM-NICKEL-BRONZE MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 4640 IN LIEU OF

AMS 4640.

159. IN LIEU OF FINISH CODE 4.10: NO FINISH REQUIRED.

160. DRAWING: 66-17942 (-1 PLUG)

161. AN814-6DL HAS BEEN SUPERCEDED BY SAE AS 5169.

162. IN LIEU OF FINISH CODE F-2.940: CHEMICAL TREAT TO MEET THE REQUIREMENTS OF MIL-DTL-5541 CLASS 1A, USING MANUAL TECHNIQUES ONLY.

163. DRAWING: 69-58643 (-1 PIN ASSY.)

164. USE 4340 STEEL MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6415 OR SAE AMS 6484 IN LIEU OF MIL-

S-5000.

165. HEAT-TREAT STEEL PER SAE AMS-H-6875 (180-200 KSI) TO MEET DRAWING REQUIREMENTS IN LIEU OF BAC5617.

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 17 of 19

166. ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT TREAT WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE

167. IN LIEU OF FINISH CODE F-1.901 SILVER PLATE PER ASTM B 700 (BAC5715).

168. IN LIEU OF FINISH CODE F-1.181 (F-1.308): CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870

TYPE II CLASS 2. BAKE 12 HOURS MINIMUM AT 375 ± 25F AFTER PLATE.

169. DRAWING: 69-61471 (-1 BEARING.)

170. USE ALUMINUM-NICKEL-BRONZE MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 4640 IN LIEU OF

AMS 4640.

171. IN LIEU OF FINISH CODE 4.10: APPLY NO FINISH.

172. DRAWING: 69-68032 (-1 BOLT)

173. MACHINING, GRINDING AND HOLE PREPARATION AFTER HEAT TREATMENT TO MEET DRAWING REQUIREMENTS

SHALL BE PER BAC5440. GRINDING PER MIL-STD-866 IN LIEU OF BAC5440.

174. DRAWING: BACB30NE 3D10 (BOLT)

174.1. (BOEING PART STANDARD)

175. DRAWING: 9-55622 (-4 ARM ASSY.) -2 FORGING

176. (CSI) FORGE STEEL PER SAE AMS-F-7190 TO MEET DRAWING REQUIREMENTS IN LIEU OF MIL-F-7190.

176.1. THE CONTRACTOR MAY PROCURE FORGINGS FROM SOURCES PRE-APPROVED BY LANDING GEAR

177. IF FORGINGS ARE PROCURED FROM TOOLING APPROVED BY OO-ALC LANDING GEAR ENGINEERING, ORIGINAL

CERTIFIED FORGING PROCEDURES AND DIES/TOOLING OR EQUIVALENT (E.G., REFURBISHED/RESUNK BY APPROVED FORGING SOURCE AND HAVING THE SAME DIE NUMBER DESIGNATION) SHALL BE USED. NEW TOOLING AT AN EXISTING SOURCE WILL BE QUALIFIED PER PARAGRAPH (B). PRIOR TO CONTRACT AWARD, THE DETAILED PART

177.1.1.1. FORGING DRAWING: 9-55622

CONTROL OF FORGING PROCESS: USAF

DIE #: 9556222

LOCATION OF DIES: W. PAT CROW FORGINGS

200 LUXTON STREET

PO BOX 1720

FT. WORTH TX 76101-1720

PHONE: 817-536-2861

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 18 of 19

CAGE: 94790

177.1.1.2. FORGING DRAWING: 9-55622

CONTROL OF FORGING PROCESS: USAF

DIE #: 8109

LOCATION OF DIES: KROPP FORGE

5301 W. ROOSEVELT RD

CICERO IL 60804

PHONE: 708-652-6691

CAGE: IY4W9

178. IF THE FORGING SOURCE IS LISTED AS UNKNOWN OR THE CONTRACTOR WISHES TO DEVELOP ADDITIONAL

GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE PRIOR TO CONTRACT AWARD. THE CONTRACTOR SHALL NOT PROCEED TO OBTAIN NEW DIES WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT-PROCURING AGENCY (SEE OO-ALC LANDING GEAR ENGINEERING FORGING SQS FOR FURTHER INFORMATION ON FORGING TOOLING QUALIFICATION REQUIREMENTS). THE GOVERNMENT SHALL HAVE UNLIMITED USE OF THE DIES DEVELOPED UNDER THIS CONTRACT. THE CONTRACTOR SHALL INFORM THE FORGING HOUSE IN WRITING, AT THE SAME TIME THE ORDER FOR THE DIES IS PLACED, THAT

178.1. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE

FORGINGS. THE DETAILED PART CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE

179. (CSI) USE 4340 STEEL MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6415 OR SAE AMS 6484 IN LIEU OF

MIL-S-5000 OR USE 4140 STEEL ALLOY MATERIAL TO MEET DRAWING REQUIREMENTS PER SAE AMS 6349 OR SAE AMS

6382 IN LIEU OF MIL-S-5626

180. (CSI) HEAT-TREAT STEEL PER SAE AMS-H-6875 (180-200 KSI ) TO MEET DRAWING REQUIREMENTS IN LIEU OF

BAC5617.

181. (CSI) ON STEEL PARTS HEAT TREATED 180 KSI AND ABOVE, ANY SURFACES GROUND/MACHINED AFTER HEAT

TREAT WILL BE INSPECTED FOR BURNS PER MIL-STD-867. NO MORE THAN THREE SUCCESSIVE INSPECTIONS SHALL BE PERFORMED WITHOUT A WAIVER FROM OO-ALC LANDING GEAR ENGINEERING. GRINDING WILL BE PER MIL-

STD-866.

182. (CSI) ON STEEL PARTS HEAT-TREATED TO 180 KSI UTS OR ABOVE, CHROMIUM PLATE PER MIL-STD-1501, TYPE II

CLASS 2 IN LIEU OF F-15.04.

183. THE MAXIMUM ALLOWABLE DELAY FOR THE 4-HOUR BAKE BETWEEN CHROMIUM PLATE AND CADMIUM PLATE

OPERATIONS AS REFERENCED IN MIL-STD-1501 SHALL BE 4 HOURS.

184. (CSI) IN LIEU OF F-15.24: CADMIUM PLATE TO MEET DRAWING REQUIREMENTS PER MIL-STD-870 TYPE II CLASS 2.

OFFICE SYMBOL:

417 SCMS/GUEA

DATE:

HILL AFB FORM 462 Page 19 of 19

185. THE FOLLOWING DOCUMENTS ARE NOT REQUIRED FOR MANUFACTURE AND WILL NOT BE PROVIDED:

185.1. BAC: 5004, 5005, 5009, 5018, 5047, 5049, 5300, 5307, 5424, 5440, 5482, 5601, 5602, 5617, 5718 AND 5730

185.2. BACD: 2041, 2074, 2097

185.3. DOCUMENT: D2-5000, D6-1276, D6-19736, D6-5000, D8-45000,

406 SCMS/GULAA-Hill October 1, 2015

Statement Of Work (SOW) for Packaging & Preservation

ASSIST Documents for Specifications Listed in the GSA Index of Federal Specifications, Standards and Commercial Item Descriptions The contractor shall use the public ASSIST Quick Search website to access specification, standards, data item descriptions documents listed in this contract solicitation:

http://quicksearch.dla.mil

PRESERVATION, PACKAGING & MARKING REQUIREMENTS

The contractor shall develop, implement and maintain the preservation, packaging and packing of all items to be delivered under the terms of this contract. Packaging procedures will be established in accordance with AFMCI 24- 201, specifically Paragraph 3.7 and MIL-STD-2073-1, Standard Practice for Military Packaging (current revision);

Packaging requirements are identified in the AFMC Form 158, Packaging Requirements submitted by the responsible packaging specialist. All “markings and labeling” of shipments shall conform to MIL-STD 129, DoD Standard Practice, Military Marking for Shipment and Storage (current revision)

INTERNATIONAL STANDARDS FOR PHYTOSANITARY MEASURES (ISPM NO. 15)

REQUIREMENTS

The contractor shall use the wood packaging material regulation for international trade which describes phytosanitary (including treatments) that have been approved for wood packaging material and provides for the approval of new or revised treatments. Use the latest revision of (ISPM No. 15), and the following statement complies with the United Nations-implemented restrictions on wood packaging material (WPM). “This requirement is specifically concerned with invasive species such as 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 worldwide shipments (direct vendor deliveries, Air Logistics complex (ALC), Container Consolidation Points (CCP), Aerial Ports, Water Ports, or other DoD installations.):

ELECTROSTATIC MATERIAL (When Applicable) The Contractor shall apply provisions of MIL-STD-1686 (current revision) when identifying all solid state devices and modules containing diodes, translators, integrated circuits and/or other microelectronic components sensitive to electrostatic forces. All such items shall be packaged IAW MIL_STD 2073-1 using electrostatic free barrier materials and shall clearly bear “Electrostatic Sensitive Device” labels IAW MIL-STD 129, Department of Defense Standard Practice Military Marking for Shipment and Storage.

REUSABLE CONTAINERS

The contractor shall safeguard all received reusable shipping containers that meet the requirements of the AFMC Form 158 and are suitable for return shipment of serviceable assets. The contractor shall dispose of and replace unserviceable containers with new containers that meet requirements of the AFMC Form 158. Contact the Administering Contracting Office (ACO) for disposition and replacement when Long Life Reusable Containers (LLRC) are received in an unserviceable condition.

SOW for Packaging & Preservation Standards (Cont.) October 1, 2015

REPORTING DISCREPANCIES

The contractor shall use Web Supply Discrepancy Report (WebSDR) to submit/reply to an Supply Discrepancy Report (SDR), when improperly packed assets are received/shipped in other than the contracted packaging requirements (coded data or Special Packaging Instructions (SPI) drawings) from Department of Defense (DoD) components/ or contractor activities.

The contractor shall request for a WebSDR account via the following URL:

https://www.transactionservices.dla.mil/daashome

(See Defense Logistics Management (DLM) 4000.25-M, Volume 2, Supply Standard and Procedures, Chapter 17, Supply Discrepancy Reporting, http://www2.dla.mil/j-6/dlmso/elibrary/manuals/dlm/dlm_pubs.asp ).

Exceptions when no damage has occurred are as follows:

- Items packaged before the current SPI date.

- An alternate pack may be used, provided the prime Air Force Sustainment Complex, Packaging office at the Air Logistics Complex (ALC) approves and issues a waiver, deviation number, which would be annotated on the exterior container on the lower right hand portion of the identification side of the container.

- In accordance with Technical Order (T.O.) 00-85B-3, How to Package Air Force Spares, the contractor may substitute the next larger size fast pack, of the type I or type II to ship transportation priorities 1 and 2 shipments as long as there is no decrease in any of the container dimensions without the requirement of a waiver deviation. T.O.

00-85-3, can be access via the website: http://www.tinker.af.mil/shared/media/document/AFD-061220-059.pdf

HAZARDOUS MATERIALS (When Applicable) The contractor shall ensure Hazardous shipments comply with International Civil Aviation Organization (ICAO), U.S.

Code of Federal Regulations (CFR) Title 49, International Air Transport Association (IATA) Dangerous Goods Regulation, International Maritime Dangerous Goods Code (IMDG, Annex 1), and AFMAN24-204_IP, Preparing Hazardous Materials for Military Air Shipments. Packaging shall meet “DOT specification or a United Nation (UN) specification ” manufactured in accordance with 49 CFR, Part 178 and the final packages assembled IAW 49 CFR, Parts 100-185 as applicable. A Competent Authority Approval (CAA) shall be acquired from the responsible Associate Administrator or other designated Department official to perform a function requiring prior consent under the Hazardous Material Regulation (HMR). Packages(s) shall be marked IAW MIL-STD-129, DoD Standard Practice, and Military Marking for Shipment and Storage. If a symbol is used to represent the manufacturer or the approval agency certifying compliance with 49 CFR 178, subparts L and M, the symbol must be registered with the U.S. Department of Transportation. A copy of the Contractor’s Test Report and signed certification that the package configuration meets both CFR and UN requirements shall be made available to the procuring contract office, as required, prior to acceptance or shipment of any portion of the product IAW Contract Data Requirements List (CDRL) (Reference AFMC Form 158). Safety Data Sheets (SDS) are required for known hazardous items and applicable items shown in FED-STD-313, Tables I and II. The SDS shall have any applicable identification number, such as National Stock Number or Special Item Number. A copy of the SDS shall be mailed or e-mailed no later than “FIVE” days prior to contractual delivery of items:

AFMC AFMC

406 SCMS/GULAA AFLCMC/LZSA

Attn: Wendy Monson Attn: Tonita Davis/DSN 785-7901 Packaging Specialist PHS&T POC E-mail: wendy.monson@us.af.mil E-mail: Tonita.davis@us.af.mil

DSN: 777-1457

https://www.transactionservices.dla.mil/daashome http://www2.dla.mil/j-6/dlmso/elibrary/manuals/dlm/dlm_pubs.asp http://www.tinker.af.mil/shared/media/document/AFD-061220-059.pdf mailto:Tonita.davis@us.af.mil

SOW for Packaging & Preservation (Cont) October 1, 2015

APPLICABLE GOVERNMENT PACKAGING DOCUMENTS

NOTE: “UTILIZE THE MOST RECENT POLICY”

AFI 24-203, Preparation and Movement of Air Force Cargo

AFMAN 24-204_IP, Preparing Hazardous Materials for Military Air Shipments

AFMCI 24-201, AFMC Packaging and Materials, Handling Policies and Procedures

DLMS 4000.25-M, Defense Logistics Management Systems (DLMS), Volume 2, Supply Standards and Procedures, Chapter…