TPR_162D611621-2003A_01.pdf

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Part Number: Revision: Cage Code:

Title:

Release Date:

Work Authority:

Class: Type:

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.

TPR

_162D

6116212003A _01.pdf

D: Distribution authorized to Department of Defense and U.S.

DOD contractors only, for administrative and operational use.

Date of determination is 29 June 2007. Refer other requests for this document to OOALC/508 ACSS/SU, Hill AFB, UT,84056.

162D6116212003A 01 98747

FITTING TRUNNION, LANDING GEAR

30Mar2016

FA820207D0004

Part_Detail Make From

PART REPORT

APPLICATION

Revision:Part Number: CAGE Code:

Format:

Title:

Class: Type:

Release Date: Work Authority:

Opposite Type: Opposite Part:

Export Controlled: Proprietary: Security:

Distribution Statement:

Destruction Notice:

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.

162D6116212003A 01 98747

FITTING TRUNNION, LANDING GEAR

Part_Detail Make From

30Mar2016 FA820207D0004

N/A undefined MBD

YES DOD Controlled Unclassified

D: Distribution authorized to Department of Defense and U.S. DOD contractors only, for administrative and operational use. Date of determination is 29 June 2007. Refer other requests for this document to OOALC/508 ACSS/SU, Hill AFB, UT,84056.

For classified document, follow the procedures in DOD 5220.22M, Industrial Security Manual, Section 1119 or DOD 5200.1 R, Information Security Program Regulation, Chapter IX. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

The program's designated master product data management (PDM) system must be queried to determine the current application data (End Item, Unit(s), and Next Assembly) of this part.

TPR_162D6116212003A_01.pdf Page 2 of 7

APPROVAL

ASSEMBLY PARTS LIST OR MAKE FROM PART

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.

Function (Group/Role) Name Date

Design/Lead Rogers, David L 2016-03-04

Design/Lead Minks, Joshua D 2016-03-12

A/C Integration/Material & Processes Bolser, David R 2016-03-14

Manufacturing/Engineer Alexander, Jay H 2016-03-14

TO Publication/Lead Johnson, Paul E 2016-03-14

Design/Lead Minks, Joshua D 2016-03-16

Configuration Mgt/Release King, Robert E 2016-03-30

Data Generation/Engineer Chrisler, Matthew J 2016-03-28

Data Generation/Lead Chrisler, Matthew J 2016-03-28

Customer/Reviewer Rogers, George P 2016-03-16

Quantity Number Title Note

1 162D611621-5001 FORGING - LANDING GEAR TRUNION

FITTING

TPR_162D6116212003A_01.pdf Page 3 of 7

NOTES

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.

1. (GEN-01) An asterisk preceding a note number in the notes list refers either to a specific requirement in the MBD dataset identified by the note number enclosed in a triangle, or to a requirement in the parts list referenced by a note number in the notes column or in the procurement specification field, or per the "FLAGNOTE" attribute.

2. (CRIT-01) This is a Fatigue and Fracture Critical part, Class 1A, in accordance with

SM160M1000.

4. (MISC-01) Storage, handling and shipping shall be in accordance with Z-P801.

5. (NDT-02) Prior to shot peening, penetrant inspect per ASTM E1417. Pre-penetrant etch per P.S. 12050 or G-J301 to remove 0.0002 to 0.0005 inches from each surface prior to penetrant inspection. Relevant linear indications are unacceptable. Linear indications are those indications in which the length is more than three times the width. Evaluate all rounded penetrant indiations 0.016 inch diameter and larger under visible light and accept any rounded voids up to 0.005 inch diameter. Reject two or more voids in the range of

0.005 to 0.009 inch diameter which are located with 0.25 inch edge to edge or any single void with a diameter of 0.010 inch diamter or larger.

6. (NDT-19) Inspect ALL HOLES to quality level A2 in accordance with QATB M-40.

7. (MACH-19) Unless otherwise noted, maximum surface finish of ALL HOLES to be 63 micro-inches Ra per ASME B46.1 (1995).

8. (MACH-08) Prior to shot peening, unless otherwise noted, break all sharp edges .02 to .03 inches per P.S. 20024 or alternatively per G-F101.

9. (SP-13) Shot peen all surfaces, except holes, per AMS 2430 to provide 200% coverage, using an Almen intensity of .014A and a shot size of 280 to 460. Holes present in the part at the time of shot peening shall be suitably plugged/masked to prevent peening and damage of the holes.

10. (FIN-09) Sulfuric acid anodize per MIL-A-8625, Type II, Class 1.

11. (FIN-39) Unless otherwise noted, prime using MIL-PRF-23377, Type II, Class C. Apply per P.S. 13375 or alternatively per MIL-C-22751. Thickness shall be 0.0006 to 0.0009 inches.

*12. (FIN-25) Omit primer and topcoat from noted area(s).

13. (FIN-24) Unless otherwise noted, top coat using MIL-PRF-85285, Type I, Class H. Apply per Z-P401. Top coat shall be applied at a thickness of 0.0017 to 0.0023 inches. Color Number 16473 per FED-STD-595.

In conjunction with top coat application per Z-P401, the specified flash coat of primer, applied prior to application of the topcoat, shall be MIL-PRF-23377, Type II, Class C primer.

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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.

14. (ID-02) This part/assembly is interchangeable in accordance with MIL-I-8500D and is controlled through control media. The interchangeable features of this part/assembly are:

FEATURES ATTACHING TO MLG

AND WING ATTACH HOLES

Mark part/assembly using P.S. 16001 rubber stamp or stencil methods only or alternatively Z-R701, code RS or ST with the following: "INTERCHANGEABLE - DO NOT ALTER".

15. (ID-01) Identification marking per P.S. 16001, rubber stamp method only. Alternatively, parts may be identified per Z-R701, Code RS.

16. (GEN-15) DELETED

17. (MACH-05) Unless otherwise noted, kellering is allowable on all profile-toleranced surfaces not parallel or perpendicular to the feature's primary datum. Kellering is allowable on chamfered surfaces. All kellered surfaces are subject to a profile tolerance zone equal to

0.020 inch and oriented in the plane perpendicular to the direction of kellering.

18. (MACH-09) All corner radii intersecting plane surfaces shall blend smoothly from .02 to .12 corner radius.

19. (MACH-11) Unless otherwise specified, general surface mismatch shall not exceed .005 inches. Mismatch within 0.060 inches of the tangency of intersecting features (such as the intersection of a corner radius and the side of a stiffener) shall not exceed .010 inches, except that mismatch at intersections of equal height flanges and stiffeners shall not exceed .060 inches. The fillet radius associated with any surface mismatch shall be .09 inches minimum.

20. (MBD-12) Solid marker application of flag notes only (not datum target areas or feature control frames) shall have a surface profile tolerance all over of .060 regardless of feature size relative to datum A (primary), datum B (MMC {if applicable})(secondary), datum C (MMC {if applicable})(tertiary).

*21. (FIN-34) For noted area(s), omit general finishes (anodize, primer and topcoat) and instead conversion coat only per MIL-DTL-5541, Class 3.

*22. (FIN-32) For noted area(s) omit general finishes (anodize, primer, and topcoat) and instead brush chromate conversion coat per MIL-DTL-5541, Class 1A.

23. (019231) It is permissible to omit top coat and primer from surfaces identified as Datum A.

Additionally, it is permissible to omit top coat and primer from localized surfaces no larger than a circular region .75" in diameter as needed to facilitate fixturing.

24. (019418) It is permissible to omit the application of top coat as specified in Note 13 and instead apply at the 162D611621 next assembly level.

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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.

25. (MACH-23) Unless otherwise noted, the surface roughness average, Ra, of the as-machined part, shall not exceed 125 micro-inches per ASME B46.1 (2002).

700. (GDT-17) All dimensions, tolerances and datums per ASME Y14.5M (1994).

705. (GDT-02) The part shall be capable of being brought to the datum simulators by applying up to five pounds of force within any twelve-inch interval or an equivalent force within a smaller interval (e.g., half the allowed force at six-inch intervals, one quarter of the allowed force at three-inch intervals). Any number of allowed force units may be applied as long as the equivalent forces and intervals are maintained.

710. (GDT-03) Unless otherwise noted, tolerance for all features of constant thickness to be +/- .010.

740. (GDT-29) Unless otherwise noted, all part features are subject to a surface profile tolerance zone of .060 inch with respect to datum A (primary), datum B - F (secondary), and datum C (tertiary).

745. (004538) UNLESS OTHERWISE NOTED, TAPERED THICKNESS FEATURES THAT

DO NOT HAVE LOCATING FACES IDENTIFIED ARE SUBJECT TO A SURFACE

PROFILE TOLERANCE ZONE OF 0.060 INCH WITH REPECT TO DATUM A

(PRIMARY), DATUM B - F (MMC {IF APPLICABLE}) (SECONDARY), AND DATUM

C (MMC {IF APPLICABLE})(TERTIARY) ON ONE FACE WHILE THE OPPOSING

FACE SHALL MEET A .020 INCH SURFACE PROFILE TOLERANCE WITH

RESPECT TO THE FIRST FACE.

746. (004541) UNLESS OTHERWISE NOTED, ALL MACHINED FILLET RADII ARE

SUBJECT TO A PROFILE TOLERANCE ZONE EQUAL TO 0.020 AND ORIENTED IN

THE PLANE PERPENDICULAR TO THE RADIUS AXIS.

800. (GEN-06) All dimensions are in inches.

810. (GEN-02) Unless otherwise noted, dimensions, geometric definition requirements, and surface texture designations apply after the last operation prior to the application of chemical finishes, platings, paints, and/or coatings.

825. (GEN-09) Material substitution permissible per 162S900701.

900. (MBD-01) This part is a defined dataset per ASME Y14.41-2003 Model Only. This dataset containing the 3D representation of a part, its associated 3D geometry, 3D dimensions, 3D tolerances, and annotations along with its corresponding material and notes report specify the complete master definition.

905. (MBD-02) Annotation found in the MBD dataset may point to a solid entity that is not the master 3D geometry. These entities are called markers. The annotation is applicable to the area or volume of the master 3D representation geometry that contacts or intersects the marker (the marker may be fully embedded within the master geometry).

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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.

910. (MBD-03) Part is modeled in the as-fabricated condition. All features, including holes, must be fabricated as developed in the master model unless otherwise noted in the master model.

920. (MBD-05) Part shall be manufactured (programmed and fabricated) to the nominal definition. Nominal weight of the part is 22.97 lbs. This weight is reference only and includes an allowance for a slight mean shift (less than .001 inch) to the thickness's high side, possibility of cutter ramps, and paint.

925. (MBD-06) The location of all datums, datum target points, and all datum target areas shall be considered basic unless otherwise indicated.

930. (MBD-07) Datums A, B, and C are oriented to the local part axis system and intersect at the origin of the local part axis system.

935. (MBD-08) Unless otherwise noted, all features of the part are basic except holes with a diameter smaller than 1 inch.

940. (MBD-09) Loft (non-planar) surfaced 3D geometry shall be considered true offsets of each other unless otherwise noted on the 3D master geometry.

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A3DR_3DFrame: