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1026 FLIGH T International, 28 June 1962T A B L E 3 : T U R B O P R O P S

Des ignatManufacturer

Allison 2505 0 1 - D 1 3B S G n o m e P . 1 2 0 0Proteus 765C P & W A P T 6 A - 6G ELycomingL T C 4 G - 3Napier E land 504R-R Dart 3D a r t 6Dart 7 /2

Dart 10 /1Dart 12Tyne 11Tyne 12Tyne 20T y n e 2 2Tyne 32R o v e r T P / 9 0Turb . As tazou 2Bas tan 4Oredon 2T u r m o 3 D 2T u r m o 3 D 3Turmo 6

onMil i tary

Y T 6 3T 5 6 - 1 AT 5 6 - 1 0 WM k 2 5 5Y T 7 4T 6 4 - 8T 5 3 - 7T 5 5

Mk 101M k 2 1 , 2 2

Engineconfiguration6a + l c, 2ct, 2pt14a, 4t14a, 4t14a, 4t10a, 2ct, lpt1 2 a + l c , 2 c t , 2 p t3a + l c , l e t , l p t14a, 2ct, 2pt5a + l c , l e t , l p t7a + l c , l e t , 2pt10a, 3t2c, 2t2c , 2 t2c , 3 t2c , 3t2c, 3t6a, 9a, It, 3t6a, 9a, It, 3t6a, 9a, It, 3t6a, 9a, It, 3t6a, 9a, It, 3tl c , Itl a + l c , 3tla + l c , 3 tl a + l c , 3 tl a + l c , 2 ct , lp tl a + l c , 2 c t , 2 p t2a + l c , 2ct , 2pt

Length(in)

145.2145.1145.179 .3100.66 211 35 8 . 462 .295 .59 5989899 .4999 .49108.7108 .7108.735 .4468 .474 .46 07 276

D i a m .(to)2727 .527 .517 *40.1192 4 t2 324 .7636 '38383838384 3 . 24 3 . 243 .219.9182 214.434 .4434 .44

Weight0 b )

1,7501,64559 52 ,9002 7 05 4079 51,8201,0261,1061,227

1,3771,3782 ,2752 ,1772 ,2032 0 027 1468*2 0 266 166 188 1

AirflowOb/sec)

32.532 .512.34 6524 .510.733.520 .520 .523 .5

272746 .546 .546 .51.885.569. 82. 51313

Press .

9 .259.258. 17. 3612.66 75. 45. 45. 66.356.3513.513.513.52. 865. 565. 55. 5

Maximum powers.b.p.; c.h.p.; r.p.m.2 5 0 ;3 ,460 ; 3 ,740 ; 13 ,8203 ,460 ; 3 ,740 ; 13 ,820; 4 ,585 ; 13 ,8201,150; 1 ,200; 26,2603 , 9 1 5 ; 4 , 4 4 5 ; 1 1 , 7 0 0

5 5 0 ; 578; 37 ,500; 2 ,850; 15,5901 ,100 ; 1 ,150 ; 26 ,0002 ,445 ; 2 ,535 ; 18 ,7503 ,230 ; 3 ,500 ; 12 ,5001,345; 1 ,480; 14,5001,535; 1 ,670; 14,5001 ,910 ; 2 ,100 ; 15 ,0002 ,750 ; 3 ,030 ; 15 ,000; 3 ,245; 15,0004 ,850 ; 5 ,325 ; 15 ,2505 ,095 ; 5 ,505 ; 15 ,2505,440; 5 ,855; 15,2506 , 6 2 5 ; 7 , 0 7 5 ; 1 5 , 2 5 07 ,870 ; 8 ,400 ; 15 ,250118; 118 ; 47 ,000530; 562 ; 43 ,500917; 986 ; 33 ,500196; 207 ; 59 ,0001,285; 1 ,335; 22,4601,450; ; 33,5001 ,800 ; ; 32 ,000

Typical cruise powerFeet; knots ; c .h .p . ; s.f.c.6 ,000 ; 200 ; 206 ; 0 .7325 ,000 ; 360 ; 1 ,905 ; 0.4670 ; 0 ; 8 0 5 : 0 . 7 2 825 ,000 ; 340 ; 2 ,675 ; 0 .5010 ; 0 ; 4 9 5 ; 0 . 6 820 ,000 ; 370 ; 1 ,522 ; 0.493.20 ,000 ; 261 ; 1 ,660 ; 0 .5620 ,000 ; 300 ; 955 ; 0 .6520 ,000 ; 300 ; 985 ; 0.63420 ,000 ; 300 ; 1 ,315 ; 0.57320 ,000 ; 300 ; 1 ,615 ; 0.55620 ,000 ; 300 ; 1 ,612 ; 0.55525 ,000 ; 370 ; 3 ,195 ; 0.3842 5 , 0 0 0 ; 3 7 0 ; 3 , 2 2 0 ; 0.38825 ,000 ; 320 ;0; any; 100; 1 .3620 ,000 ; 270 ; 398 ; 0.4929 ,900 ; 350 ; 795 ; 0 .580; 0 ; 855 ; 0.737

T B O(hr)

2 ,2002 ,40080 04 ,0003 ,5003,000.2 ,0001,000

Main applications

_ElectraC-130A HerculesP 3 V - 1Britannia 320A O - 1C L - 6 6V . 7 0 0V . 7 0 0 DV . 8 1 0 , A W . 6 5 0 , F . 2 7 , 7 4 8Hera ld , Gul fs treamY S - 1 1H P . 1 2 4 , 7 4 8 M FV a n g u a r dC L - 4 4 , Y u k o n , B e l f a s tBr .1150 , Transa l lPotez 840 , Marquis , PorterSup. Broussard , Spira leBr.941 , 942Spirale IIIBr.943

* Height 31.55in; t height 46in; tcowled powerplant: free-turbine speed.

T A B L E 4 : T U R B O S H A F T S

Des ignat ionManufacturer Mi l i tary

AiResearch 331Al l i son 250 -CB M W 6 0 1 2Boeing 520 -6B S G n o m e H . 1 2 0 0Coupled GnomeH . 1 2 0 0Nimbus 750C P & W A P T 6 B - 9Continenta l 217 -5AD B P T L 6Fia t 4301 .000GE CT58-100-1

L y c o m i ng L T C 1 B - 1L T C 1L T C 4Napier Gazel leP & W A J F T D 1 2Turb . Artous te 2 CArtouste 3BT u r m o 3 C 3

T 6 3 - 5Y T 6 0Mk 101M k l l OMk 100Y T 7 4T 7 2 - 2

T58-8BT 6 4 - 2T 6 4 - 6T 5 3 - 1 AT 5 3 - 9T 5 5 - 5M k l 6 2

Eng ineconfiguration2c ,3 t6a + l c , 2ct , 2ptl c , I t1c , l e t , lp t10a , 2ct , lp t2 X G n o m e2 a + l c , 2 c t , l p t3a + l c , l e t , l p tl a + l c , 2c t , l p t4a + l c , 2ct , lp tl c , l e t , l p t10a, 2ct, l pt10a, 2ct, lpt14a, 2ct, 2pt14a , 2ct , 2ptS a + l c , l e t , l p t5 a + l c , l e t , l p t7 a + l c , l c t , 2 p t11a, 2ct. l pt9a, 2ct, 2ptl c , 2 tla + l c , 3 tl a + l c , 2 c t , 2 p t

Length(in)40 .538 .524 .557.354.87861 .65942 .487 0595555918347 .6147 .6145 .467 0 *56.457 .666 .5

D i a m .(in) Weight(lb)18.5415.81525 .5174120.11919.3820 .32 2 . 41616252 42 32324.7633.521.920 .420 .425.8

Airflow(lb/sec)19914 710 032 532 8

1,04339 024 521 04 4 038 630 429 58 6471 34 8 448 557 09 2 087 025 328 741 4

4 .395. 312.3

24 .611510.412.412.424 .524 .510.710.716.5

9. 513

Press ,ratio

6.258. 18.16. 5648. 38. 312.612.666< u6. 53 .885. 25. 5

M a x . p o w e rs.h.p.; r.p.m.;minutes time500; 39 ,000 ;2 5 0 ; 4 8 , 7 5 0 ;8 9 ; 4 5 , 0 0 0 ;5 5 0 ;1 ,250 ; 26 ,750 ; 2 |

1 ,000 ; 35 ,300 ; 5550; 37 ,500 ;5 0 0 ; 42 ,500 ; 51 ,050 ; 18 ,600 ;6 9 0 ; 25 ,0001 ,050 ; 26 ,260 ; 51 ,250 ; 26 ,260 ; 52 ,810 ; 13 ,600 ; 102 , 8 5 0 ; 1 3 , 6 0 0 ;860; 25 ,240 ;1 , 1 0 0 : 2 6 , 0 0 0 ;2 ,200 ; 14 ,550 ;1 ,575 ; 19 ,900 ;4 , 0 5 0 ;500; 34 ,000 ;c o n t550; 34 ,000 ;c o n t1 , 5 0 0 ; 3 3 , 5 0 0 ;

Outputr.p.m.6,0006,0203-8,0006,00019,5002 ,9152 , 1 5 06,2305,9766,000

19,50019,5005,20013,6006,6806 ,61014,5502 ,5009,0006,0006,0005,700

Rated or lhr powerFeet; knots ; s .h .p . ; s.f.c.; r.p.m.

0 ; 0 ; 1 9 1 ; 0 . 7 7 ; 4 6 , 1 0 00; 0 ; 500 ; 0 .67 ;10 ,000 ; 100 ; 950 ; 0 .602 ; 25 ,9205 ,000 ; 0 ; 770 ; 0.7050 ; 0 ; 4 8 5 ; 0 . 6 9 ;6 ,000 ; 0 ; 265 ; 0 .78 ; 41 ,0000; 0 ; 760 ; 0 .70 ;10 ,000 ; 0 ; 785 ; 0 .63 ; 25 ,92020 ,000 ; 0 ; 680 ; 0 .585 ; 25 ,92015 ,000 ; 100 ; 1 ,720 ; 0 .494 ; 13 ,60015 ,000 ; 100 ; 1 ,750 ; 0 .485 ; 13 ,600

0; 0 ; 1 ,330 ; 0 .695 ; 19 ,3000; 0 ; 3 ,200 ;0 ; 0 ; 345 ; 1 .02 ; 32 ,0003 ,280 ; 0 ; 405 ; 0 .81 ;

Main applications

LOH hel icoptersSa i lp lanesAgust as , W'w ind, 107Wessex 2 and 4S c o u t , W a s p , S R . N 2Hi l ler Ten99 , Piasecki

107, S-61L. S-62H R B - 1 , H U 2 K , H S S - 2X C - 1 4 2H U - 1 , H^3BH U - 1 DH C - 1 BWessex 31S-64A l o u e t t e 2Alouette 3Super Frelon

1 Along engine axis; engine is installed diagonally.

T A B L E 5 1 P I S T O N E N G I N E S

Des ignat ionAgusta GA.40G A . 7 0 VA . 1 4 0 VAlv is Leonides 531A r d e m 4 C 0 2Continenta l A65O 2 0 0 AO 3 0 0 AI O 4 7 0 DFrankl in 2A-1104 A - 2 2 56 A G S - 3 3 5L y c o m i n g I O 3 6 0T V 0 4 3 5 - A 1 AG O 4 8 0 - B 1 A 6I O 5 4 0I G S O 5 4 0 - B 1 A

V O 5 4 0 - C 1 AM - 3 3 2M - 3 3 7Mete or Al fa 4Alfa 5P o t e z 4 D - 3 44E-206E-00

Configuration0 20 4 , vert0 4 , vertR 9 , g , s0 40 40 40 60 6 , i n j0 20 406 , inj , g , turb0 4 , in j0 6 , vert , turb0 6 . B0 6 , in j0 6 , in j , g, s0 6 , v er tI 4 LI6L, s (opt . )R 8R 8I 4 L . S0 40 6

Dimens ions ( inches )Length24.118.52 2 . 8 354 .430 .42 8 . 5 339 .7543 .3123 .730 .54132.8134 .7339 .8438 .6248 .534 .734 3 . 455 .54 5 . 2 734 .2546 .830.737.3

Width30 .921 .2631 .494 1 . 531.531 .5631 .533 .5630.731 .531 .633 .3733 ,5833 .1234 .2534 .2534 .716.718.423 .42 3 . 420 .530.130.6

Height17.7118.52 7 . 1 741 .520 .323 .182 3 . 2 519.7522 .725.121 .2522 .4736.512 8 . 0 219.620 .2924 .5823 .924 .72 3 . 423 .427 .623 .922 .7

W e i g h t0 b )123.46176 .4255 .886 013 317 019 026 84 2 613 022 84 1 029 14 6 84 3 24 375 3 24 3 92 2 531 33 202 6 84 0 82 0 727 5

B o r e(to)3 .9373 .6224.514. 83.0313 .8754 .06254 .062554 .54. 54 .55.1254 .8755.1255 .1255.1255 .1254 .134 .134 . 1 3 34 .1334.9214 .334 .33

Stroke(to)3 .743. 43 .494. 82 .523 .6253 .8753 .87543. 53. 53. 54 .3753.8753.8754 .3754 .3754 .3754 .534 .533.0713.0714 . 7 2 43 .5433 .543

Capaci ty( c u i n )91 .1140.3222 .937 8372 .6217 120 130 147 111 222 533 536 043 54 8 054 054 0

5 4 0242 .78364 .25329 .52329 .523 572 0931 3

F u e lgrade80 /8780 /8791100 /130807380 /878 0 / 8 7100 /115100/13080 /87100 /1309 1 / 9 6100 /13080 /87100 /130100 /130

100 /1307 27 2100 /13080 /87100 /130

M a x i m u mpowerh.p.; r.p.m.4 1 ; 2 ,7008 2 ; 3 ,300139; 3 ,200650; 3 ,20030 .7 ;3 ,0006 5 ; 2 ,300100; 2 ,7501 4 5 ; 2 , 7 0 0260; 2 ,6256 0 ; 3 ,000125; 2 ,800260; 3 .200*180; 2 ,7002 6 0 ; 3 , 2 0 0 t270; 3 ,4002 9 0 ; 2 ,575380; 3 ,400

305; 3 ,200140; 2 ,700210; 2 ,750220; 2 ,800320; 4 ,000260; 2 ,550105; 2 ,7501 5 3 ; 2 ,700

Typical cruise powerFt; h.p; r.p.m.; gal/hr0 ; 20 ; 2 ,000 ; 1 .450 ; 64 ; 3 ,000 ; 4 .655 ,000 ; 107 ; 3 ,000 ;10 ,250 ; 360 ; 2 ,600 ; 250; 43 ; 2 ,000 ; 3 .10 ; 6 5 ; 2 , 5 0 0 ;0 ; 1 0 3 ; 2 , 4 0 0 ;5 ,000 ; 188 ; 2 ,300 ;0 ; 0 ; 60 ; 3 ,000 ;0 ; 0 ; 125 ; 2 ,800 ;15 ,000 ; 0 ; 230 ; 3 ,200 ;7 ,500 ; 135 ; 2 ,450 ;6 ,000 ; 195 ; 2 ,750 ;6 , 0 0 0 : 2 2 0 : 2 , 3 5 0 :13 ,000 ; 270 ; 2 ,750 ;9 , 5 0 0 ; 2 4 0 ; 3 , 2 0 0 ;1 ,000 ; 95 ; 2 ,400 ; 5 .615 ,000 ; 140 ; 2 ,400 ;0; 200 ; 2 ,400 ;0 ; 75 ; 2 ,450 ;0 ; 107 ; 2 ,400 ;

Main applications

Agu sta A 103BA g u s t a A 1 0 4Scott i sh Av ia t ion Twin Pioneer 3R o l l a s o n T u r b u l e n tCessna 150 , EmeraudeSuper Ra l lye , Beag le 117 & 218Cessna 310 Mousqueta ire , Travel Air , Aireda leBel l , Agus tasD o 2 7A e r o C o m m a n d e r 5 0 0 BA e r o C o m m a n d e r 6 8 0 FHi l lersA e r o 1 4 5 , M e t a - S o k o lM o r a v a L . 2 0 0 ATargets and dronesN o r d 3 2 0 2 , 3 4 0 01051 Ambassadeur"""

At up to 10,000ft; t At up to 13,000ft.