Attachement_A_(CSI).pdf

REV: ENGINEERING DATA REQUIREMENTS

(ATTACHMENT “A”)

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

THE FOLLOWING INSTRUCTIONS ARE FURNISHED FOR THE MANUFACTURE OF:

ORIFICE SUPPORT TUBE ASSEMBLY - KC135

PART NUMBER:

458-56182-1

NATIONAL STOCK NUMBER:

1620-01-150-0027

PREPARED BY:

Jeff Naylor

OFFICE:

417 SCMS/GUEA

DATE:

2 October 2015

HILL AFB FORM 462

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

SUPERSEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.

2.0 417 SCMS/GUEA 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.

3.0 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 MANUAL, SPECIFICATIONS, AND STANDARDS AND FULLY

UNDERSTAND THE REQUIREMENTS NECESSARY TO MANUFACTURE LANDING GEAR COMPONENTS. ANY

QUESTIONS CAN BE FORWARDED TO 417 SCMS/GUEA.

4.0 THIS COMPONENT/ASSEMBLY IS A CRITICAL SAFTEY ITEM (CSI). THE CRITICAL SAFTEY PROCESSES (CSP)

ARE AS FOLLOWS:

CSP MATERIAL

CSP HEAT TREATMENT

CSP MAGNETIC PARTICLE INSPECTION

CSP FLUORESCENT PENETRANT INSPECTION

CSP THREADS

CSP GLASS BEAD PEEN

CSP ULTRASONIC INSPECTION

CSP ANODIZE

CSP FORGING

5.0 MAJOR ASSEMBLY: DRAWING 458-56182-1 MAIN LANDING GEAR SHOCK STRUT ORIFICE SUPPORT TUBE

ASSEMBLY

5.1 SUBCOMPONENTS/SUBASSEMBLIES: 458-56161-1, 458-56187-1, 60-6551-1, ANS, BACN1OBY-55

5.2 MARKING AND IDENTIFICATION SHALL BE PER MIL-STD-130. BOTH PART NUMBER AND SERIAL

NUMBER SHALL BE MARKED ON THE PART IN THE LOCATION SHOWN ON THE DRAWING. THE

SERIAL NUMBER SHALL 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 SERIAL NUMBER SHALL APPEAR AS “SN 9874701040001”. THE HEIGHT OF EACH

ALPHANUMERIC CHARACTER SHALL BE A MAXIMUM OF .125 INCHES.

5.3 DIMENSION AND TOLERANCE USE ASME Y14.5 IN LIEU OF ANSI 14.5.

5.4 SURFACE ROUGHNESS USE ASME B46.1 IN LIEU OF ANSI B46.1 AND BACD2097.

6.0 DRAWING: 458-56161 ORIFICE SUPPORT TUBE MAIN LANDING GEAR

6.1 MATERIAL: 7175 ALUMINUM ALLOY HAND FORGING PER SAE AMS 4149 IN LIEU OF AMS 4109 AND D3-

6002.

OFFICE:

417 SCMS/GUEA

6.2 HEAT TREAT TO T74 PER SAE AMS 2772.

6.3 DIMENSION AND TOLERANCE USE ASME Y14.5 IN LIEU OF ANSI 14.5.

6.4 SURFACE ROUGHNESS USE ASME B46.1 IN LIEU OF ANSI B46.1 AND BACD2097.

6.5 THREADS PER SAE AS 8879 IN LIEU OF MIL-S-8879.

6.6 FLUORESCENT PENETRANT INSPECTION PER ASTM E 1417, TYPE I, METHOD B, C, OR D, LEVEL 3 OR 4

IN LIEU OF BAC 5423. 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 INSPECTION SHALL BE CERTIFIED TO LEVEL II WITH THE INSPECTION PROCEDURE

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

6.7 ULTRASONIC INSPECT PER SAE AMS STD 2154 CLASS A IN LIEU OF BAC 5439.

6.8 GLASS BEAD PEEN PER SAE AMS 2430 IN LIEU OF BAC 5951.

6.9 ANODIZE PER MIL-A-8625 TYPE II, CLASS 1 IN LIEU OF F-2.959 AND F-12.101.

6.10 APPLY PRIMER TO THREADS PER THE FOLLOWING IN LIEU OF 458-56002:

A. APPLY A LIBERAL AMOUNT OF EPOXY WATERBORNE PRIMER PER MIL-PRF-85582, TYPE I,

CLASS 2 OR EPOXY POLYAMIDE PRIMER PER MIL-PRF-23377, TYPE I BY SCRUBBING FOR A

FEW SECONDS WITH CHEESE CLOTH OR EQUIVALENT. THE ENTIRE SURFACE MUST BE

COVERED.

B. BEFORE PRIMER DRIES, GENTLY REMOVE EXCESS WET PRIMER WITH CHEESE CLOTH OR

EQUIVALENT AND LET DRY.

7.0 DRAWING: 60-6551 OLEO ASSEMBLY PISTON ROD RING

7.1 DIMENSION AND TOLERANCE USE ASME Y14.5 IN LIEU OF ANSI 14.5.

7.2 SURFACE ROUGHNESS USE ASME B46.1 IN LIEU OF ANSI B46.1 AND BACD2097.

7.3 MAGNETIC PARTICLE INSPECTION PER ASTM E 1444 IN LIEU OF MIL-I-6868. 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 THE AIA/NAS-410.

7.4 TAG PART PER MIL-STD-130 IN LIEU OF D18462.

OFFICE:

417 SCMS/GUEA

7.5 FORM STRAIGHTEN AND FIT METAL PARTS USING BEST AIRCRAFT INDUSTRY STANDARDS IN LIEU

OF BAC 5300.

7.6 MATERIAL: CAST IRON PER SAE AMS 7310 IN LIEU OF AMS 7310.

7.7 NO FINISH IN LIEU OF F 1.10.

7.8 NO MATERIAL SUBSTITUTION IN LIEU OF BAC 5005.

SUBASSEMBLY: 458-56187-1 ORIFICE PLATE ASSEMBLY

SUBCOMPONENTS: 458-56187-2, 30-3111

8.0 DRAWING: 30-3111 ORIFICE OLEO ASSEMBLY INSERT

8.1 TAG PART PER MIL-STD-130 IN LIEU OF D18462.

8.2 DIMENSION AND TOLERANCE USE ASME Y14.5 IN LIEU OF ANSI 14.5.

8.3 SURFACE ROUGHNESS USE ASME B46.1 IN LIEU OF ANSI B46.1 AND BACD2097.

8.4 MAGNETIC PARTICLE INSPECTION PER ASTM E 1444 IN LIEU OF MIL-I-6868. 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 THE AIA/NAS-410.

8.5 NO FINISH REQUIRED IN LIEU OF F-1.10.

8.6 MATERIAL: 4140 STEEL PER SAE AMS-6349 OR SAE AMS-6382 IN LIEU OF MIL-S-5626 OR D18462.

8.7 NOT REQUIRED: BACD 2097, BAC 5601, BAC5682, BAC 5004, DWG 2-5000, BAC 5300, BAC 5005, BAC 5009.

9.0 DRAWING: 458-56187-2 ORIFICE PLATE ASSEMBLY

9.1 DIMENSION AND TOLERANCE USE ASME Y14.5 IN LIEU OF ANSI 14.5.

9.2 SURFACE ROUGHNESS USE ASME B46.1 IN LIEU OF ANSI B46.1 AND BACD2097.

9.3 CLEAR FINISH PER BAC 5710 TYPE 41 NOT REQUIRED.

9.4 APPLY NO FINISH EXCEPT TEMPORARY COATING FOR PROTECTION DURING HANDLING, STORAGE

AND TRANSPORTATION PER MIL-C-81309.

9.5 FLUORESCENT PENETRANT INSPECTION PER ASTM E 1417, TYPE I, METHOD B, C, OR D, LEVEL 3 OR 4

IN LIEU OF (CONTRACTOR SPECIFICATION). THE FOLLOWING ACCEPTANCE/REJECTION CRITERIA

OFFICE:

417 SCMS/GUEA

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 INSPECTION SHALL BE CERTIFIED TO LEVEL

II WITH THE INSPECTION PROCEDURE DEVELOPED BY A LEVEL III AS SPECIFIED IN AIA/NAS-410

9.6 BREAK SHARP EDGES PER INDUSTRY STANDARDS IN LIEU OF BAC 5300.

9.7 THREADS PER SAE AS 8879 IN LIEU OF MIL-S-8879.

9.8 FORGING MADE FROM DRAWING 458-56185-1.

10.0 DRAWING: 458-56185-1

10.1 DIMENSION AND TOLERANCE USE ASME Y14.5 IN LIEU OF ANSI 14.5.

10.2 SURFACE ROUGHNESS USE ASME B46.1 IN LIEU OF ANSI B46.1 AND BACD2097.

10.3 THE FORGING SHALL BE PROCURED FROM SOURCES APPROVED BY 417 SCMS/GUEB, USING THE

ORIGINAL CERTIFIED FORGING PROCEDURES AND DIES/TOOLING OR EQUIVALENT (E.G.,

REFURBISHED/RESUNK BY APPROVED FORGING SOURCE).

A. PRIOR TO CONTRACT AWARD, THE DETAILED PART BIDDER SHALL PROVIDE VERFICATION

(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.

B. 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.

1. FORGING DRAWING: 458-56185-1

2. DIE #: 3632-1

3. LOCATION OF FORGING DIES: GENERAL DYNAMICS OTS, 1200 N Glenbrook Ave, Garland

TX 75040

4. PHONE: 972-494-7860

5. CAGE: 3LCX2

C. IF THE FORGING SOURCE IS LISTED AS UNKNOWN OR THE CONTRACTOR WISHES TO

DEVELOP ADDITIONAL SOURCES,THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN

WRITINGOF 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 417 SCMS/GUEA 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

OFFICE:

417 SCMS/GUEA

GOVERNMENT HAS UNLIMITED USE RIGHT OF THE DIES AND FORWARD A COPY OF THIS

LETTER TO THE GOVERNMENT CONTRACTING OFFICER.

10.4 MATERIAL: 7175 ALUMINUM PER SAE AMS-A-22771 IN LIEU OF BMS 7-214.

10.5 HEAT TREAT TO T74 PER SAE AMS 2772 IN LIEU OF BMS7-124.

10.6 APPLY NO FINISH EXCEPT TEMPORARY COATING FOR PROTECTION DURING HANDLING, STORAGE

AND TRANSPORTATION PER MIL-C-81309.

10.7 FORM STRAIGHTEN AND FIT METAL PARTS USING BEST AIRCRAFT INDUSTRY STANDARDS IN LIEU

OF BAC 5300.

10.8 ULTRASONIC INSPECT PER SAE AMS STD 2154 CLASS A IN LIEU OF BAC 5439.