N NAKASHMA PROPELLER CO., LTD. Head Office & Works/688-1,Jodo-Kitagata,Okayama,Japan Phone: (086 )279-5111 Fax phone: (086 )279-5466 DATE 10th Dec.,2001 MESSRS. SHN KURUSHMA DOCKYARD CO.,LTD. NSPECTON REPORT FOR PROPELLER HULL NO./NAME 5138 CLASSF CATON N K PROPELLER DATA DAMETER 5,850 mm PTCH (O.7R) 4,069.3 mm EXP. AREA 14.7831 nf NO.OF BLADES 4 TURNNG DRECTON RGHT HANDED MATERAL KABC3 WORK NO. 100487 CHARGE NO. 01284 MASS 15,900 kg DRAWNG NO. M32-220-00 NAKASHMA PROPELLER CO.,LTD. QUALTY CONTROL DEPT.
MATERAL TEST REPORT CUSTOMER :SHN KURUSHMA DOCKYARD CO. LTD. H NAKASHMA PROPELLER CO.,LTD. SHP NO. :5138 WORK NO. :100487 688-1 JODO KTAGATA OKAYAMA JAPAN DRAWNG NO. :M32-220-00 MTRL. SPEC. :K A B C 3 ARTCLE Highly Skewed Propeller Date of Test: 10.12.2001 SZE HARD- MPACT SZE OF Testing Machine NO. Term of TENSLE TEST OF T. P. NESS TEST TEST PECE Tensile: D.= 14 mm T-84 @ 17 Validity DENTlF- (DESGNED) T-67856 O.2% 2002 CATON P.S.ltllllrl!tik. ACTUAL T.S. EL. HB Charpy G.L. = 70 mm 1-1260 March, NO. PC. NO. Area i<ij/ll<nrri LOAD % kgf-m/cm - 2 N/mrrf N/mrrf in mm min. min. min. CH.NO. 245 590 16 Particulars: 01284 K-284 153.9 268.0 687.1 21. 1 Type 4 BLADES SOLD KEYLESS Pouring Date;, Diameter 5850 mm 12. 1 1.2001 Pitch (0.7R) 4069.3 mm Exp area 14.7831 SO.M Stamping Date; 27.11.2001 W:;:t (as fin ish e d ) 15,900 kg CHEMCAL COMPOSTON (%) Mass (as cast) 17,660 kg Cu Zn Mn Fe A Sn N i Pb Statical balancing test good 77.0- MAX. 0.5-2.0-7.0- MAX. 3.0- MAX. Finish nspection'.... good CH.NO. 82.0 1. 0 4.0 6.0 11. 0 O. 1 6.0 0.0. DATE; 10.12.2001 01284 81.35 O. 19 0.82 4.21 9.37 0.02 4.02 0.02 Witnessed by We hereby certify that the material described herein has been made and tested in accordance with /r UMJ the Nippon Ka j Kyokal Surveyor to Nippon K a j i Kyokai rule in the contract. Manager of Quality Control Sec.
NSPECTON REPORT J * /) :(, SHu or NAME ---'AA --+------+----"-------" &t )(.:t SHN!<U!<u)H'" JJ / b g CUSTOMER DOCkYARD CO" /.,100 DESCRPTON PRO PE LJ 'E/< 00 M " M DRAWNG Hu fv1 32.... 1.1-0... 00 MATERAL SPEC. {(A8C; t-------t----------+---------""----- --------- jtf. A V -1f. J1 n l'spocton - V" l'specton DATE. 0 - DeC - 0 POSTOO OF PTCH MEASUMEN' note; * n-pitch measurement, the point of / O from G.L. in the Drawing is to be 0. * Position of" pitch measurffnent are indicated as a base of 0. TRALNG EDGE 25"D LEADNG EDGE - 0.6R 0.5R SCALE = NOO NAKASHMA PROPELLER CO.L TD-
(SNO. 5138) o. 3 R DESGNED PTCH 4217.8 mm UNT: Dm POS ANGLE FROM DESGNED HEGHT FROM ACTUAL HEGHT TON THE CENTER LNE THE CENTER LNE No.A No.B No.C No.D 1 35 404.8 405.0 404.5 405.0 404.5 2 10 110.1 110.0 110.5 110.0 110.5 TOTAL OF HEGHT 515.0 515.0 515.0 515.0 514.9 0.1 0.1 0.1 0.1 TOLERANCE (%) +2.25 0.02 0.02 0.02 0.02 o. 4 R DESGNED PTCH 4202.1 mm POS ANGLE FROM DESGNED HEGHT FROM ACTUAL HEGHT TON THE CENTER 11 NE THE CENTER LNE No.A No.B No.C No.D 1 30 346.8 347.0 347.0 347.0 347.0 2 15 165.5 165.0 165.0 165.0 165.5 TOTAL OF HEGHT 512.0 512.0 512.0 512.5 512.3-0.3-0.3-0.3 0.2 TOLERANCE (%) +2.25-0.06-0.06-0.06 0.04 o. 5 R DESGNED PTCH 4172.8 mm POS ANGLE FROM DESGNED HEGHT FROM ACTUAL HEGHT TON THE CENTER LNE THE CENTER LNE No.A No.B No.C No.D 1 25 287.8 288.0 288.0 287.5 288.0 2 15 166.5 166.5 166.5 166.5 166.5 TOTAL OF HEGHT 454.5 454.5 454.0 454.5 454.3 0.2 0.2-0.3 0.2 TOLERANCE (%) +1.5 0.04 0.04-0.07 0.04 o. 6 R DESGNED PTCH 4129.5 mm POS ANGLE FROM DESGNED HEGHT FROM ACTUAL HEGHT TON THE CENTER LNE THE CENTER LNE No.A No.B No.C No.D 1 20 228.6 228.5 228.5 228.0 228.5 2 15 167.6 167.5 167.5 167.5 167.5 TOTAL OF HEGHT 396.0 396.0 395.5 396.0 396.2-0.2-0.2-0.7-0.2 TOLERANCE (%) + 1.5-0.05-0.05-0.18-0.05
o. 7 R DESGNED PTCH 4069.3 mm POS ANGLE FROM DESGNED HEGHT FROM ACTUAL HEGHT TON THE CENTER LNE THE CENTER LNE No.A No.B No.C No.D 1 15 168.6 168.5 168.5 168.0 168.0 2 15 168.0 168.0 168.5 168.0 168.5 TOTAL OF HEGHT 336.5 337.0 336.0 336.5 336.6-0.1 0.4-0.6-0.1 TOLERANCE (%) +1.5-0.03 0.12-0.18-0.03 o. 8 R DESGNED PTCH 3989.1 mm POS ANGLE FROM DESGNED HEGHT FROM ACTUAL HEGHT TON THE CENTER LNE THE CENTER LNE No.A No.B No.C No.D 1 10 109.9 110.0 109.5 110.0 110.0 2 15 166.6 166.0 166.5 166.5 166.5 TOTAL OF HEGHT 276.0 276.0 276.5 276.5 276.5-0.5-0.5 0.0 0.0 TOLERANCE (%) +1.5-0.18-0.18 0.00 0.00 o. 9 R DESGNED PTCH 3888.5 mm POS ANGLE FROM DESGNED HEGHT FROM ACTUAL HEGHT TON THE CENTER LNE THE CENTER LNE No.A No.B No.C No.D 1 15 160.9 160.5 161. 0 161. 0 160.5 TOTAL OF HEGHT 160.5 161. 0 161. 0 160.5 160.9-0.4 0.1 0.1-0.4 TOLERANCE (%) +1.5-0.25 0.06 0.06-0.25 PTCH DEVATON N % TORE LANCE No.A No.B No.C No.D MEAN PTCH (%) PER BLADE +1.0-0.07-0.01-0.06-0.03 MEAN PTCH (%) FOR PROP. +0.75-0.04 (%)
BLADE WDTH SNO.5138 RADUS 0.3 R 0.4 R 0.5 R 0.6 R 0.7 R 0.8 R 0.9 R 0.925 t 0.95 R 0.975 DESGNED n434.0 1654.0 1811.0 1870.0 1807.0 1607.0 1207.0 1 865.0 / TOLERANCE ±29.3 ±29.3 ±29.3 ±29.3 ±29.3 ±29.3 ±29.3 ± 1 ± 29.3 ± / ci A 0.0 + 1. a 0.0 0.0 0.0 0.0 0.0 L + 1. a / z w Q <r;...:j co B + 1.0 + 1.0 + 1.0 0.0 + 1. a 0.0 +1.0 1 + 1.0 / C +1.0 0.0 + 1.0 + 1.0 0.0 +1.0 + 1. a 1 0.0 / D 0.0 0.0 0.0 t 1.0 + 1.0 + 1.0 + 1. 01/ O. Oil RAKE TOLERANCE + 58. 5 mm BLADE No. A B C D Ej REMARKS RAKE vs6"d POSTON OF BLADE CENTER LNE (126.7) +0.3 + 1.3 +2.8 + 5.3 V / O.3RO.9R O.3R () DETAL OF RAKE 1 """= CD O.3R O.6R @ O.9R 309 <1-.5 z.,s. "1 4J6./ -1-- f-po- DES GN A a/2,s 330,0 <739..r V 1 V B 3/6,D 33'1-..5- <1.<1.4, D ---- c ;j/c,o ;;o 4<1</-...t- O.3R (),bp1. O.9R TP D ;)/,o '?. "" 4<Z'() RADUS TOLERANCE + 8.7 mm BLADE No. A B C D E/ REMARKS DESGNED 2925 2925 2925 2925 / ACTUAL 0 0 0 01 MEDAN LNE OF BLADES TOLERANCE ± 1.0 BLADE No. A"LB B"'C CAD D "A EL REMARKS DESGNED 90 90 90 90 /0 ACTUAL 0 0 0 ov NAKASHMA PROPELLER CO.,L TD.
BLADE THCKNESS SNO.5138 RADUS 0.3 R 0.4 R 0.5 R POSTON( X/322.6 537.8 896.31075.5 397.0 661.61058.61257.0 307.9 769.71186.21394.5 DESGNED Yn83.8 200.0 171.2 133.2 152.0 165.9 142.2 110.7 107.0 135.2 115.9 90.5 TOLERANCE + 5.0-3.0 + 4.1-2.4 + 3.3-2.0 d A +0.2 0.0 +0.8 +0.3 +0.5 +0.6 +0.3 +0.3 +0.5 +0.8 +0.1 +0.5 z w B +0.7 +0.5 +0.3 +0.3 +0.5 +0.1 +0.3 +0.8 +0.5 +0.3 +0.6 +1.0 Q c +0.2 0.0 +0.8 +0.8 0.0 +0.1 +0.8 +0.8 0.0 +0.3 +0.6 +0.5 -<...:1 0 +0.7 0.0 +0.3 +0.8 0.0 +0.6 +0.8 +0.3 0.0 +0.8 +0.1 + 1.0 m RADUS 0.6 R 0.7 R 0.8 R POSTON )504.9 841.51252.91458.6 343.3 858.31237.81427.5 482.1 803.51124.91285.6 DESGNED Yv.) 99.1 108.3 93.1 72.9 66.5 83.9 72.4 56.9 56.2 61.4 53.5 42.3 TOLERANCE + 2.7-1.6 + 2.5-1. 5 + 2.5-1. 5 d A +0.4 +0.2 +0.9 +0.1 0.0 +0.1 +0.6 +0.6 +0.3 +0.1 0.0 +0.7 z B +0.4 +0.7 +0.4 +0.6 0.0 +0.1 +0.1 +0.6 +0.8 + 0.1 +0.5 +0.2 w Q c +0.9 +0.2 +0.9 +0.6 +0.5 +0.6 +0.6 +0.1 +0.3 +0.6 +0.5 +0.7 -<...:1 0 +0.9 +0.7 +0.4 +0.1 +0.5 +0.6 +0.1 +0.1 +0.8 to.6 0.0 +0.2 m RADUS 0.9 R 0.925 R L 0.95 R POSTON )()241. 2 603.0 844.2 964.8 A 259.2 432.0 604.8 691.2 DESGNED '{) 32. 5 40.4 36.0 29.1 /" 27.8 30.2 27.6 22.7 TOLERANCE + 2.5-1. 5 + /' - + 2.5-1. 5 d A +0.5 +0.6 +0.5 +0.9 /' +0.2 +0.3 +0.9 +0.8 z B w +0.5 +0.1 +0.5 +0.4 /' +0.2 +0.3 +0.9 +0.3 Q C 0.0 +0.6 0.0 +0.4 /' +0.7 +0.8 +0.4 +0.8 -<...:1 0 0.0 +0.1 0.0 +0.9 V +0.7 +0.8 +0.4 +0.3 m RADUS 0.975 R / o2.t- / POSTON,..y cts8, / X DESGNED /" 217.8- / TOLERANCE + /- )ln. 217,8- /< d A // /' 220.0 z B w / 2/'j',D // Q C... V ;2/7',0./ -<...:1 0 /'.2/8.D /' /" m E // ---- NAKASHMA PROPELLER CO.,L TD.
RECORD OF BALANCNG TEST S'.NCJ.&-13 2- ) f /,si). mm 67ft mm NORMAL DEVATON DEVATON WHEN ATTACHED THE UNBALANCE WEGHT 60D 9 AT,LJ "B LADE TP. 60D 3 =1 t: 6,?M -/.f8,.... {) J c.! {i l.a 13.. ('... " '0 li <'-! '{) 7f)LfJdrNC.. ACTUAL UNBALANCE WEGHT /. /S-"")l.1j--& 0'=$/. 1 ( l -DRAWl NG ) vffx, 3. 0 tc.--.---- RECORDNG PUTE STAY.ua F.L FL Nt.. K ASH' MAP 0 PEL L ERe O. L TO.
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