Form: AIF 8001 AIRBUS Ry INDUSTRIE Point Shall Be Flat And Chamfered. See Procurement Specification For Details ® Tri-wing® recess Per NAS4000 see Table 1 £7 {Ar.) 24 prita ep" (code D) When Specified By Part No. Csk Optional. UNJF-3A Threads Per MIL-S-8879 Except For curved Bage optional Reduction Of Thread Major Dia Per "TD" Head marking shall be depressed .010 max. (0,25) and arranged as follows:~ First Sector - Mark with basic number ("ABS" Optional). Second Sector - Mark with Manufacturer's symbol (symbol location optional in any sector), grip dash number and "D", when applicable. "D" identifies bolt with drilled shank. Third Sector - Mark with recess dash number, encircled. Recess number should be approximately 25¢ larger than other numerals in head marking. TABLE 1 DIMENSIONS. Dimensions are given in inch (mm) unless otherwise stated. : D Dia. © Before Coating : After Coating : Recess wax. Number ) Max. Min. Max. + Min. 7245: 5607: 5601: 5615: .5605:NAS4000— (29,06) + (26,59)_+ (6,32) + (14, 242) : (14,227) : (14,262) = (14,237) 111. Gasoge? e276! 1.16: 4275: 6232: 622 76241 +6230: NAS4O00~| : 2(32,41) + (29,69)_+ (7,09) + (15,829) : (15,814) : (15,850) = (15,624) 112 T.531: 1.406: .334: 7482: 7471 777490: . 7480: NASAOOO=: 2 7500°26, (38,89) + (35,71)_: (8,48) : (19,004) : (18,989 19,025) : (18,999) :13 : TABLE 1 CONTINUED ON PAGE 02 aerwmc © rg a RectsTERED TRADEMARK OF THE PHILLIPS SCREW COMPANY + Page + les. /Rev. ‘Approved Title AIRBUSINOUSTAIE | orn, 100° aD, TaI-HING© recess, . CLOSE TOLERANCE, GAL-4V TYTANIUM ALLOY, CWA TONG THREAD ABS0113 Pam 02 ot _04 Published and distributed by: AIRBUS-INDUSTRIE. Copyright 1978 AIRBUS-INDUSTRIE 31700 BLAGNAC FRANCEAiR BUS inousTRIE wW TABLE 1 DIMENSIONS. (CONTINUED) :Dia.: H Gauge :W Gauge Dia.: © Mo: bia); Rad. | Protrusion(c) : +-0002 £.010: +#,010: | BTol —: (40,005) __:_Max. + (#0,25): (40,25): | 1,006: 034: 218: 141 0,064): _ (25,466) + same s Tia 0,069): (28,250) = 70031: 1.3438 (0,079): (34,133) _: (1,118) + (6,40) (0,86) _:(5,54)_:(3,58)_+ (0,76): (0,38) 249s. 14 (6,32)_: (3,58) 72522 «141 (3,58) TABLE 1 DIMENSIONS. (CONTINUED) ¥() 21g) PROCUREMENT SPECIFICATION: NAS4O04 EXCEPT FOR PROTECTIVE TREATMENT AND LUBRICATION (c), (@), ETC.: SEB NOTES ON PAGE 03. oayea (2) 10/84 (3) 09/85 Page 02 Published and distributed by: AIRBUS INDUSTRIE Copyright 1078 AIRBUSINDUSTRIE 31700 BLAGNAG FRANCE Form: AIF 8002Form: AIF 8003, AIRBUS Sy INDUSTRIE Material: G6AL-4V Titanium Alloy per AMS4928 or ANS4967. Heat Treat: 160 to 180 KSI (1100 to 1240 N/nm?) Ultimate Tensile. 95 KSI (655 N/m?) Min. Ultimate Shear. Finish: Bolts to be coated with Aluminium (IVD) to MIL-C-83488 Type II Class 3 to be identified with Blue Dye on thread end of bolt plus chamfer. Grip" dimension equals grip dash number times .0625 (1,588). "Length" equals "Grip" plus "I (See page 02). Example of Part Number e.g. for a .625 (15,88) dia. bolt with undrilled shank and 1625 (15,88) grip the part number is:~ ABSO113.-10 10 Basic Part Number. __Grip Dash No. (in .0625 (1,588) increments) :_Dia, Dash No, (in .0625 (1,588) increments) Replace dash "-" after basic part number with " for bolt with drilled shank. | e.g. For a .750 (19,05) dia. bolt with a drilled shank and .750 (19,05) grip the part number is:- ABSO113D «120-12. Basic Part Number Grip Dash No. (in .0625 (1,588) increments) Bolt with drilled shank_; NOTES __Dia. Dash No. (in .0625 (1,588) increments) a. ‘Grip! of bolt shall be measured from the top of bolt head to the end of the full cylindrical portion of the shank. b. Dimensions A, A’ and B are included for engineering reference only and are not to be used for Inspection. Values A, At and B are calculated limits resulting from tolerances on W, H, B and Head Angle. c. Dimensions for H gauge protrusion shall be inspected per NASS27. a. Cotter pin hole centre line : within .010 (0,25) and normal within 2° of bolt centre line. e. surface texture + on shank, conical surface of head, thread flanks and thread oot 3Y/"(Oy8 wicrons); other suriaces 1Q5/ (3,2 microns) f£. Concentricity : Conical surface of head to shank diameter within .003 (0,076) TIR. "p" dia. to thread pitch dia. within "Y" TIR. Shank straightness : within "2" TIR per inch (25,4 mm) of length. ABS0113 [ime eae tome Qos id Published and distributed by: AIRBUS-INDUSTRIE Copyright 1978 AIRBUS-INDUSTRIE 31700 BLAGNAC FRANCEALRBUS 4) INDUSTRIE wWw RESTRICTED USAGE : FOR REPAIR WORK ONLY 0156 (0,396) and .0312 (0,792) OVERSIZE SHANK FOR REPLACEMENT OF BOLTS SHOWN ON PAGE O1. Head Marking: Same as shown on page 01 Plus identification for oversize, as applicable, to be included in second sector. Identify .0156 (0,396) oversize by "x". Identify .0312 (0,792) oversize by " See pages 01 thru 03 for dimensions not shown. Head height dimensions (B Max.) are reduced with oversize shanks. Reduction is: .0065 (0,165) for .0156 (0,396) Oversize Bolts 0130 (0,330) for .0312 (0,792) Oversize Bolts. Major diameter of threads may conform to "TD" on page 02 or to MIL-S~8879. TABLE II OVERSIZE PART NUMBERS AND DIMENSIONS: : Basic Part No. iNominal :D Diameter .0156 (0,396) Oversize Shank: Thread aise Before Coating 0156 (0,396) 7500-16 7788 : 2(19,797)_: (19,782) * Grip Dash Number in .0625 (1,588) increments. 734 Grip Length_: Revision: (1) 09/85 Published and distributed by: AIRBUS-INDUSTRIE 31700 BLAGNAC FRANCE For material, finish and procurement information, see page 03. Examples of part number 4.0156 (0,396) oversize = ABSO113-10-*#x 10312 (0,792) oversize = ABS0113-10-**Y After Coating Oversize Max. Min. : Max. _: Min. ABSO113-9-**K :.5605-16: — .5763 +5757 + 5771 = 5 2 (24,623)_: (14,658) :ABSOII5: :-6250-18 6382 6396 (16,210): (16,246) :RBSOLI3-12-**%:, 7500-16: . 7638 +1632: 1646: 7636 + (19,400): (19,385) (19,421) + (19,395)_+ 'D Diameter .0312 (0,792) Oversize Shank? ~5625-18: .5919 75913 + .5927 ¢ . 5017 2(15,034) + (25,019) _:(15,055)_ (15,029) 6250-18: 6544 6538 76552: 6542 (16,622) _: (16,607) _+ (16,642) _+ (16,617) + 7802 2 (10,817) +7792 (29,792): ABS0113 Page 04 Copyright 1978 AIRBUS INDUSTRIE Form: AIF 8002