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1. light business jet (max to weight= 5670 kg, 12500lbs)

1.1. Embraer Phenom 100 (EMB-500) (pg 41)-light business jet-up to 8 passenger

-Wing span: 12.29 m (40 ft 4 in)-Length overall: 12.8 m (42 ft 0 in)-max TO weight: 4750kg (10472 lb)-basic operating weight (incl pilot): 3235kg (7132lb)-max fuel weight: 1272 kg(2804 lbs)-max landing weight: 4430 kg (9766lb)-max power loading: 315 kg/kN (3.09 lb/lb st)-max level speed: 390 kts (722 km/h)-max operating altitude 12495 m (41000ft)-TO run: 953m (3125 ft)

Range with four passenger :-with VFR reserves 1320 n miles (2444 km)-with NBAA IFR reserves, 100 n miles alternate: 1178 n miles( 2181

km)Power Plant: Two Pratt & Whitney turbofans, each rated at 7.54 kN (1695lb st)Fuel in wing tanks: combined capacity 1580 litres.

1.2. Embraer Legacy 450 (pg 43)-light business jet-up to 7 or 9 passenger

-Wing span: 20.25 m (60 ft 5+1/4 in)-Length overall: 19.15 m (62 ft 0 in)-max payload weight: 1270 kg (2800 lb)-max fuel weight: 726 kg(1600 lbs)-max landing weight: 4430 kg (9766lb)-max operating Mach NO. 0.83-max cruising speed M0.82-Econom. cruising speed M 0.78-max certified altitude: 13715 m (45000ft)-Balanced field length: 1220 m (4000 ft)-landing run 701m (2300 ft)Range, NBAA IFR reserves, 200 n miles (370 km) alternate:

-with four lassengers at long range cruising speed : 2300 nmiles(4259km)

-with eight passengers at M0.78: 2200 n miles (4074 km)Power Plant: Two Honeywell HTF7500E turbofans.

1.3. Beechcraft 390 Premier IA (pg 682)-light business jet-up to 6 passenger-Wing span: 13.56 m (44 ft 6 in)

-Length overall: 14.02 m (46 ft 0 in)-empty weight: 8350 lb



-max TO weight 5670 kg (12500 lb)-max fuel weight 1665 kg (3670 lb)-max landing weight: 5262 kg (11600 lb)-max power loading: 277 kg/kN-max wing loading 247.1 kg/m^2

-max operating speed: SL to FL270: 320 kt (593 km/h)above FL270: M 0.8

-max cruising speed at FL330: 451 kt (835 km/h)-long range cruising speed at FL410: 369 kt (683 km/h)-max c ertified altitude: 12500 m (41000 ft)-service ceiling, OEI: 8534 m (28000 ft)-TO field length: 1156 m(3795 ft)-landing distance: 966 m (3170 ft)-landing from 15 m (50 ft):- Range, max cruising speed, 100 n mile alternate:

- with 657 kg payload : 787 n miles (1457 km)-with max fuel and 168 kg payload: 1360 n miles (2518 km)- with four passengers: 1131 n miles (2094 km)

-Ferry range: 1502 n miles (2781 km)Power Plant: Two Williams turbofans, each rated at 10.23 KN.Fuel total capacity 2096.2 litres of which 2073.6 litres usable.

1.4. Cessna 510 Citation Mustang (pg 753)-light business jet-up to 4 passenger-Wing span: 13.03 m (42 ft 9 in)

-Length overall: 12.37 m (40 ft 7 in)-empty weight: 5350 lb-max TO weight 3921 kg (8645 lb)-max fuel weight 1170 kg (2580 lb)-max landing weight: 3629 kg (8000 lb)-max power loading: 302 kg/kN-max wing loading 201 kg/m^2-max operating speed: 250 kt (463 km/h)-max operating speed, Mach: 0.63-cruising speed at FL350: 340 kt (630 km/h)-long range cruising speed

-max c ertified altitude: 12500 m (41000 ft)-TO balanced field length: 948 m(3110 ft)-landing run:729m (2390 ft)-landing from 15 m (50 ft):- Range, 100 n mile alternate: 1150 n miles (2129 km)-Ferry range:Power Plant: Two Pratt&Whitney turbofans, each rated at 6.49 KN.Fuel total capacity 1458 litres.

1.5. Cessna 525 Citation CJ1 (754)-light business jet



-up to 5 passenger-Wing span: 14.2 m (46 ft 7 in)-Length overall: 12.98 m (42 ft 7 in)-empty weight: 6820 lb-max TO weight 4853 kg (10700 lb)

-max fuel weight 1460 kg (3220 lb)-max landing weight: 4491 kg (9900 lb)-max power loading: 278 kg/kN-max wing loading 217.7 kg/m^2-max operating speed SL to FL305: 263 kt (487 km/h)-max operating speed,above FL305, Mach: 0.71-max cruising speed at FL310: 389 kt (720 km/h)-max c ertified altitude: 12500 m (41000 ft)-TO field length: 789 m (2590 ft)-landing run:729m (2390 ft)-landing from 15 m (50 ft):- Range, 100 n mile alternate: 1300 n miles (2590 km)Power Plant: Two Williams turbofans, each rated at 8.74 KN.Fuel total capacity 1818 litres.

1.6. Spectrum S-40 Freedom (pg 935)-light business jet-up to 9 passenger-Wing span: 13.21 m (43 ft 4 in)-Length overall: 16.46 m (54 ft 0 in)-max TO weight 4332 kg (9550 lb)

-max fuel weight 1633 kg (3600 lb)-max landing weight: 3924 kg (8650 lb)-max payload : 1089 kg (2400 lb)-max power loading: 238 kg/kN-max cruising speed at: 440 kt (815 km/h)-service ceiling : 13715 m (45000 ft)-service ceiling, OEI: 11125 m (36500 ft)-landing run: 914 m (3000 ft)-landing from 15 m (50 ft):-landing run: 914 m (3000 ft)-Max range, 100 n mile alternate, pilot and four passengers : 2030 n miles

(3759 km)-Ferry range: 2250 n miles (4167 km)Power Plant: Two GE Honda turbofans, each rated at 9.32 KN.

2. turboprop transport (Max TO = 8618 kg ,19000 lb)

2.1. HAI Y-12F Aircar (pg 121)



-twin-turboprop light transport-up to 19 passenger-Wing span: 19.89 m (65 ft 3 in)-Length overall: 16.47 m (54 ft 0 in)-max TO weight 8400 kg (18518 lb)

-max fuel weight 2500KG (5511 LB)-max payload 3000 kg( 6614 lb)-max power loading 5.12 kg/kW-max cruising speed : 232 kt(430km/h)-long range cruising speed : 202kt (375 km/h)-service ceiling : more than 7000 m (22960ft)-service ceiling, OEI: 4000m (13120 ft)-TO run: 575 m(1885 ft)-landing run: 630m (2070 ft)- Range, 200 n mile( 108 km), alternate and 45 min reserves:

-with max payload 831 n miles (1540 km)-witn max fuel: 1042 n miles (1930 km)

Power Plant: Two 820 kW Pratt & Whitney turboprops, driving a five blademetal propeller.

2.2. AI L 410UVP-E(pg 155)-twin-turboprop transport-up to 19 passenger-Wing span: 19.98 m (65 ft 6+1/2 in)-Length overall: 14.425 m (47 ft 3+3/4 in)-empty weight: 3960-4020 kg (8730-8863 lb)

-max TO weight 6600 kg (14550 lb)-max usable fuel weight 1300 kg (2866 lb)-max landing weight 6400 kg (14110 lb)-max payload 1710 kg(3770 lb)-max power loading 5.90 kg/kW-max wing loading 189kg/m^2-max operating speed: 185 kt (343km/h) EAS-max cruising speed at FL138: 210 kt (388km/h)-econ. cruising speed at FL138: 197 kt (365 km/h)-max rate of climb at SL :396 m/min (1300 ft/min)-rate of climb at SL, OEI: 100 m/min (328 ft/min)

-service ceiling : 6460 m (21200 ft)-service ceiling, OEI: 2900 m (9525 ft)-TO run: 455 m(1495ft)-landing run: 309 m (1015 ft)- Range, at FL 138, max cruising speed, 45 min reserves:

-with max payload: 362 n miles (670 km)-with max fuel: 711 n miles (1317 km)

Power Plant: Two 559 kW turboprops, each driving an five blade, constantspeed, reversible –pitch metal propeller (with feathering).

2.3. Reims F406 Caravan II (pg 217)-twin-turboprop transport-up to 12 passenger



-Wing span: 11 m (36 ft 1 in)-Length overall: 7.24 m (23 ft 9 in)- empty weight: 2283 kg (4890 lb)-max TO weight 4245 kg (9360 lb)-max fuel weight 1444 kg (3138 lb)

-max landing weight 4245 kg (9360 lb)-max payload 2219 kg (4892 lb)-max power loading 5.99 kg/kW-max wing loading 190.3 kg/m^2-max operating speed: 229 kt (424 km/h) IAS-max cruising speed: 246 kt (455 km/h)-econ. cruising speed: 200 kt (370 km/h)-max rate of climb at SL: 544 m/min (1850 ft/min)-rate of climb at SL, OEI: 121 m/min (397 ft/min)-max c ertified altitude: 9145 m (30000 ft)-service ceiling, OEI: 4935 m (16200 ft)-TO run: 526 m(1495ft)-landing from 15 m (50 ft): 674 m ( 2215 ft)- Range, with max fuel at max cruising speed, 45 min reserves: 1153 nmiles ( 2135 km)Power Plant: Two turboprops,each 373kW, each driving three-blade,reversible –pitch and automatic feathered metal propeller.Fuel in two wing tanks, combind capacity 1823 litres of which 1798 litresusable.Oil capacity 17.2 litres.

2.4. Skydesign Skylander SK-105 (pg 221)-twin-turboprop tranport-up to 19 passenger-Wing span: 21.6m (70 ft 10+1/2 in)-Length overall: 14.78m (48 ft 6 in)-empty weight: 4500 kg (9921 lb)-max TO weight 8390 kg (18496 lb)-max fuel weight 2585 kg (5699 lb)-max landing weight 8390 kg (18496 lb)-max payload 3400 kg(7496 lb)-max power loading 5.12 kg/kW

-max wing loading 195.5 kg/m^2-max level speed at FL100: 212 kt (393km/h)-max cruising speed at FL100: 180 kt (207 km/h)-econ. cruising speed at FL100: 150 kt (278 km/h)-max rate of climb at SL: 655 m/min (2149 ft/min)-TO run: 655 m(2740 ft)-landing run: 755 m (2477 ft)- Range, 100 n mile alternate : 597 n miles (1106 km)Power Plant: Two Pratt&Whitney Cancada PT6A-65B turboprops, each820kW, driving Hartzel five blade, metal propeller.Fuel contained in two integral wing tanks, combined capacity of 3230litres.



2.5. CSIR Saras (pg 268)-twin-turboprop tranport-up to 18 passenger-Wing span: 14.7 m (48 ft 2+3/4 in)-Length overall: 15.02 m (49 ft 3+1/4 in)

-empty weight: 4166 kg (9074 lb)-max TO weight 6100 kg (13448 lb)-max fuel weight 1326 kg (2923 lb)-max landing weight 6100 kg (13448 lb)-max payload 1232 kg (2716 lb)-max power loading 4.81 kg/kW-max wing loading 237.4 kg/m^2-max level speed at FL250: 297 kt (550 km/h)-econ. cruising speed at FL125: 243 kt (450 km/h)-max rate of climb at SL: 700 m/min (2297 ft/min)-rate of climb at SL, OEI: 130 m/min (427 ft/min)-service ceiling : 11000 m (36090 ft)-service ceiling, OEI: 6000 m(19680 ft)-TO run: 700 m(2300 ft)-TO field length: 1000 m (3.280 ft)-landing run: 850 m (2790 ft)-landing field lenth: 1200 m (3937 ft)- Range, IFR reserves:

-with 8 passengers 756 n miles (1400 km)-with 14 passengers 216 n miles (400 km)-self ferry: 1038 n miles (1924 km)

Power Plant: Two 634 kW Pratt&Whitney Cancada PT6A-66 turboprops or895 kW Pratt&Whitney PT6A-67s turboprops.Fuel contained in two integral wing tanks, combined capacity of 1608 litresof which 1595 litres are usable.

2.6. PZL Mielec M28 05 Skytruck (pg 458)-twin-turboprop transport-up to 19 passenger-Wing span: 22.065 m (72 ft 4+3/4 in)-Length overall: 13.10 m (42 ft 11+3/4 in)-empty weight: 4398 kg (9696 lb)

-max TO weight 7500 kg (16534 lb)-max fuel weight 1766 kg (3893 lb)-max landing weight 7500 kg (16534 lb)-max payload 2300 kg (5070 lb)-max power loading 4.57 kg/kW-max wing loading 188.8 kg/m^2-max operating speed: 191 kt (355 km/h)-econ. cruising speed at FL984: 146 kt (270 km/h)-max rate of climb at SL: 660 m/min (2165 ft/min)-service ceiling : 7620 m (25000 ft)-service ceiling, OEI: 3750 m (12300 ft)-TO run: 255 m(835 ft)-landing run: 260 m (855 ft)



-landing from 15 m (50 ft): 560 m (1835)- Range at FL984, 45 min reserves:

-with max payload 432 n miles (800 km)-with max fuel 809 n miles (1500 km)-self ferry: 1038 n miles (1924 km)

Power Plant: Two 820 kW Pratt&Whitney Canada PT6A-65B turbopropseach driving a Hartzel five-blade, fully fethering propeller with revesepitch.. Two main fuel tanks in outer wings, each 660 litres; two auxiliary tanks inwing-centre section, each of 189 litres; two auxiliary tanks in uoter wings,each 189 litres; total wing fuel 2278 litres.Oil capacity 16 litres per engine.

2.7. BNG BN2B-20 Islander (pg 623)-light utility twin-turboprop transport-up to 10 passenger-Wing span: 14.94 m (49 ft 0 in)-Length overall: 10.86 m (35 ft 7+3/4 in)-empty weight: 1925 kg (4244 lb)-max TO weight 2993 kg (6600 lb)-max fuel weight standard 354 kg (780 lb); with optional tanks in wing tips:585 kg (1290 kg)-max landing weight 2933 kg (6600 lb)-max payload with max optional fuel 484 kg (1066 lb)-max power loading 6.7 kg/kW-max wing loading 99.2 kg/m^2

-max level speed at SL: 151 kt (280km/h)-max cruising speed at 75% power at FL 70: 142 kt (264 km/h)-cruising speed at 67%power at FL90: 137kt (254 km/h)-max rate of climb at SL: 344 m/min (1130 ft/min)-absolute ceiling: 6005 m (19700 ft)-service ceiling : 3445 m (11300 ft)-service ceiling, OEI: 1525 m (5000 ft)-TO run at SL: 215 m(705 ft)- Range, 45 min reserves:

-standard fuel: 693 n miles (1183 km)-with optional tanks: 1075 n miles ( 1990 km)

Power Plant: Two Textrom Lycoming 224 kW flat –six engines, each drivinga Hartzel two-blade constant-speed feathering metal propeller.total fuel capacity 518 ltires. Usable fuel 492 litres. Total oil capacity 22.75 litres.

2.8. Beechcraft King Air 350 (pg 679)-utility turboprop twin.-up to 8 passenger-Wing span: 17.65 m (57 ft 11in)-Length overall: 14.22 m (46 ft 8 in)empty weight: 3883 kg (8560 lb)-max TO weight 6804 kg (15000 lb)-max fuel weight: 1638 kg (3611 lb)



-max landing weight: 6804 kg (15000 lb)-max power loading: 4.35 kg/kW;-max wing loading: 236.2 kg/m^2-max level speed min weight: 315 kt (584 km/h)-max cruising speed, at FL240: 310 kt (574 km/h)

-long range cruising speed at FL330: 237 kt (439 km/h)-service ceiling: 10670 m (35000 ft)-service ceiling, OEI: 6555 m (21500 ft)-max rate of climb at SL: 832 m/min (2731 ft/min)-rate of climb at SL, OEI: 168 m/min (552 ft/min)-TO balanced field length: 1006 m (21500 ft)-landing distance: 821 m (2695 ft)-Range, IFR reserves, 100 n mile (185 km) alternate:

-long-range cruise: -with max payload 947 n miles (1753 km)-with max fuel: 1598 n miles (2959 km)-with four passengers: 1725 n miles (3194 km)

-high-speed cruise: -with four passenger: 1470 n miles (2722 km)-Range ferry: 1814 n miles (3359 km)Power Plant: two 783 kW Pratt&Whitney Canada turboprops, each drivinga Hartzel four-blade constant speed fully feathering reversible pitch metalpropeller. Total fuel capacity of 2040 litres.

2.9. DHC6 SRS 300 (pg 21)-max TO weight 5670 kg (12500 lb)-max landing weight: 5579kg (12300 lb)

-Wing span: 19.81 m (65 ft 0 in)-Length overall: 15.77 m (51 ft 9 in)-max payload: 2313 kg (5100 lb)-max cruising speed, at FL100: 202 m/h (324 km/h)-service ceiling: 8400m (27700 ft)-service ceiling, OEI: 2530 m (11600 ft)-rate of climb at SL: 439 m/min (1440 ft/min)-rate of climb at SL, OEI: 300 m/min (910 ft/min)-TO run: 250 m (820 ft)-TO to 15 m: 402 m (1320 ft)-landing from 15 m :320 m (1050 ft)

-landing run: 171 m (650 ft)-Range at max cruising speed, 3250 lb payload: 680 miles (1100 km)Power Plant: two 579 SHP Pratt&Whitney Canada turboprops, each drivinga Hartzel three-blade fully feathering metal propeller. Total fuel capacity of 1432 litresOil capcacity: 8.7 litres per engine.

2.10. LET L-410 (pg27)-twin turboprop light transport-12 – 17 pass-Wing span: 17.1 m (56 ft 1+1/2 in)-Length overall: 13.71 m (44 ft 11/1/2 in)- empty weight: 2803 kg (6189 lb)



-max TO weight 5100 kg (11243 lb)-max landing weight: 5100kg (11243 lb)-max payload: 1920 kg (4233 lb)-max cruising speed, at FL100: 233 m/h (375 km/h)-service ceiling: 7770m (25500 ft)

-service ceiling, OEI: 3220 m (10575 ft)-rate of climb at SL: 486 m/min (1594 ft/min)-rate of climb at SL, OEI: 156 m/min (512 ft/min)-TO run: 205 m (675 ft)-TO to 15 m: 360 m (1180 ft)-landing from 15 m :590 m (1310 ft)-landing run: 180 m (590 ft)-Range max fuel : 745 miles (1200 km)-Range with 3085 lb (1400 kg) payload: 470 miles (760 km)Power Plant: two 700 SHP M 601 turboprops, each driving a three-bladefully feathering reversible pitch metal propeller. Total fuel capacity of 1120 litres

2.11. Dassault MD 320 Hirondelle (Swallow)(pg 49)-twin turboprop utility transport-up to10 pass-Wing span: 14.55 m (47 ft 8+3/4 in)-Length fuselage: 12.25 m (40 ft 2+1/4 in)- empty weight: 3350 kg (7386 lb)-max TO weight 5400 kg (11905 lb)-max landing weight:

-max payload: 860 kg (1896 lb)-max cruising speed: 320 m/h (520 km/h)-service ceiling: 9400m (30850 ft)-service ceiling, OEI: 5000 m (16400 ft)-rate of climb at SL:-rate of climb at SL, OEI:-TO run:-TO to 15 m: 750 m (2460 ft)-landing from 15 m: 650 m (2135 ft)-landing run:-Range with 45 min reserves: at 450 km/h: 1926 miles (3100km )

-Range with 45 min reserves at 500 km/h: 1243 miles (2000 km)Power Plant: two 920 SHP turboprops, each driving a three-blade fullyfeathering reversible pitch metal propeller.-Total fuel capacity of 1750 litres

2.12. Dornier DO 8 D1 Skyservant (pg 90)-twin engine STOL transport and utility-up to 12-13 passenger-Wing span: 15.5 m (50 ft 10+1/4 in)-Length overall: 12 m (39 ft 4+1/2 in)- empty weight: 2166 kg (4775 lb)-max TO weight 3650 kg (8050 lb)-max landing weight: 3650 kg (8050 lb)



-max payload:-max wing loading: 127.5 kg/m^2 ( 26.11 lb/sq ft)-max power loading: 4.8 kg/hp (11.6 lb/hp)-max cruising speed (75 % power) at FL100 : 178 m/h (286 km/h)-econ cruising speed( 50% power) at FL100: 143m/h (230km/h)

-service ceiling: 7400m (24300 ft)-service ceiling, OEI: 2750m (9000 ft)-rate of climb at SL: 360m/min (1180ft/min)-rate of climb at SL, OEI:-TO run:-STOL TO to 15 m: 347 m (1140 ft)-FAA 23 TO to 15 m :518 m (1700 ft)-STOL landing from 15 m: 372 m (1220 ft)-FAA 23 landing run: 597 m (1960 ft)-Range with max fuel at FL 100, 50% power, no reserves :1125 miles(1810 km )Power Plant: two 380 HP six-cilinder horizontally oposed air cooledengines,, each driving a three-blade constant speed metal propeller.

2.13. Handley Page HP 137 Jetsream(pg 202))-twin turboprop light transport-4-18 passenger-Wing span: 15.85 m (52 ft 0 in)-Length overall: 14.37m (47 ft 1+1/2 in)-empty weight(with 2 crew): 3833 kg (8450 lb)-max TO weight: 5670 kg (12500 lb)

-max payload: 1510 kg (3330 lb)-max fuel weight:-max landing weight: 5670 kg (12500 lb)-max power loading: 3.33 kg/shp;-max wing loading: 226 kg/m^2perf at AUW -= 12000 lb(5442 kg)-max cruising speed: 306 m/h (493 km/h)-econ cruising speedat FL300: 250m/h (403km/h)-service ceiling: 9140m (30000 ft)-service ceiling, OEI:-rate of climb at SL: 640m/min (2100 ft/min)

-rate of climb at SL, OEI:-TO run: 593 m/min (1771 ft/min)-T O to 15 m: 759 m (2490 ft)-landing from 15 m: 710 m (2300 ft)-landing run: 425 m (1395 ft)-Range with max fuel, reserves for 45 min: 1900 miles (3085 km )-Range with max payload, reserves for 45 min: 240 miles (386 km)Power Plant: two 850 HP turboprop engines, each driving a three-bladeconstant speed metal propeller.Fuel capacity: 1727 litres.

2.14. Beechcraft 99 airliner (pg 256)-twin-turboprop light passenger, freight or executive transport



-up to 17 passengers-Wing span: 14 m (45 ft 10+1/2 in)-Length overall: 13.58 m (44 ft 6+3/4 in)-empty weight: 2621 kg (5780 lb)-max TO weight 4717 kg (10400 lb)

-max fuel weight:-max landing weight:-max power loading:-max wing loading:perf at max TO weight-max cruising speed,at FL100: 254 m/h (409 km/h)-normal cruising speed,at FL120: 252 m/h (406 km/h)-service ceiling: 7210 m (23650 ft)-service ceiling, OEI: 2470 m (8100 ft)-rate of climb at SL:-rate of climb at SL, OEI:-TO run: 549 m (1800 ft)-TO to 15 m:-landing from 15 m: 677 m (2220 ft)-landing run:-range max, 45 min reserves,16 passenger ahn 218 kg baggage: 375miles (603 km)Power Plant: two 550 shp turboprop engine, three blade fully fathering,reversible pitch constant speed propeller.Fuel capacity of 1415 litres.

2.15. Beechcraft king air 100 (pag 257) (pressurized)- twin-turboprop light passenger, freight or executive transport-up to 15 passengers-Wing span: 13.98 m (45 ft 10+1/2 in)-Length overall: 12.17 m (39 ft 11+1/4 in)-empty weight: 2905 kg (6405 lb)-max TO weight 4808 kg (10600 lb)perf at max TO weight-cruising speed,high cruise power: at FL210: 274 m/h (441 km/h)

at FL160: 282 m/h (454 km/h)-at FL120: 287 m/h (462 km/h)

-cruising speed, low cruise power:-at FL210: 260 m/h (418 km/h)-at FL160: 269 m/h (433 km/h)-at FL120: 273 m/h (439 km/h)

-service ceiling: 7895 m (25900 ft)-service ceiling, OEI: 3595 m (11800 ft)-rate of climb at SL: 671m/min (2200 ft/min)-rate of climb at SL, OEI: 185m/min (608 ft/min)-TO run: 503 m (1650 ft)-TO to 15 m: 610 m (2000 ft)-landing from 15 m: 386 m (1265 ft)-landing run: 241 m (790 ft)- range at high cruise power, 45 min reserves:



-at FL210: 1067 miles (1717 km)-at FL160: 931 miles (1498 km)-at FL120: 829 miles (1334 km/h)

-range at low cruise power, 45 min reserves:-at FL210: 1150 miles (1850 km)

-at FL160: 996 miles (1602 km)-at FL120: 890 miles (1430 km/h)

Power Plant: two 680 shp turboprop engine, three blade fully fathering,reversible pitch constant speed propeller.Fuel capacity of 1415 litres.

2.16. Swearingen Merlin II A (pag 444)-twin turboprop transport-8- 10 passengers-Wing span: 13.98 m (45 ft 10+1/2 in)-Length overall: 12.22 m (40 ft 1+1/4 in)-empty weight: 2926 kg ( 6450lb)-max TO weight 4536 kg (10000 lb)-max fuel weight:-max landing weight: 42218 kg (9300 lb)-max power loading: 3.41 kg/shp;-max wing loading: 174 kg/m^2perf at max TO weight- cruising speed, at FL150: 295 m/h (475 km/h)-max speedflaps and gear down: 158 m/h (254 km/h)-econ cruising speed,

-service ceiling: 9110 m (29900 ft)-service ceiling, OEI: 3810 m (12500 ft)-rate of climb at SL: 783 m/min (2570 ft/min)-rate of climb at SL, OEI: 213 m/min (700 ft/min)-TO to 15 m: 792 m (2600 ft)-landing from 15 m : 670 m (2200 ft)-max range at 272 m/h (439 km/h), FL275, 45 min reserves: 1785 miles(2872 km)Power Plant: two 665 shp turboprop engines, three blade fully fathering,reversible pitch constant speed propeller.Standard fuel capacity of 1461 litres.

3. turboprop light transport ( max 5670 km, 12500 lb)

3.1. Evector EV-55 Outback (pg 167)-twin-turboprop tranport-up to 9 passenger-Wing span: 16.10 m (52 ft 9+3/4 in)-Length overall: 14.35 m (47 ft 1 in)-empty weight: 2626 kg (5789 lb)-max TO weight 4600 kg (10141 lb)

-max usable fuel weight-max landing weight 4600 kg (10141 lb)



-max payload 1824 kg (4021 lb)-max power loading 5.76 kg/kW-max level speed at FL100: 220 kt (408 km/h)-TO to 15 m : 510 m (1675 ft)-landing from 15 m : 309 m (1675 ft)

- Range, 30 min reserves: 1210 n miles ( 2240 km)Power Plant: Two 400 kW Pratt & Whitney Pt^A-21 turboprops, driving afour blade, constantspeed, fully-feathering propellers.

3.2. Wolfsberg corvus 1 (pg 182)-twin-turboprop tranport-up to 8 passenger-Wing span: 16.5 m (54 ft 1+1.2 in)-Length overall: 11.3 m (37 ft 1 in)-empty weight: 1950 kg (4299 lb)-max TO weight 3100 kg (6834 lb)-max fuel weight: 475 kg (1047 lb)-max landing weight 3100 kg (6834 lb)-max power loading 6.71 kg/kW-max wing loading 104.7 kg/m^2-max level speed: 148 kt (274 km/h)-max cruising speed at 75% power:133 kt (246km/h)-econ. cruising speed: 120kt (222 km/h)-max rate of climb at SL: 335 m/min (1100 ft/min)-service ceiling : 5000 m (16400 ft)-service ceiling, OEI: 1860m (6100 ft)

-TO run: 145 m (475 ft)-TO to 15 m: 330 m (1085 ft)Power Plant: Two 231.2 kW Teledyne Continental flat six engines, drivingtwo-blade constant-speed propellers.Fuel combined in two integral tanks in outer wings, combined 660 litres of which 640 litres usable.

3.3. Daher-Socata TBM 850 ( pg 222)-business turboprop-up to 5 passenger-Wing span: 12.68 m (41 ft 7+1/4 in)

-Length overall: 10.645 m (34 ft 11 in)-empty weight: 2081 kg (4588 lb)-max TO weight 3354 kg (7394 lb)-max fuel weight: 888 kg (1957 lb)-max landing weight 3186 kg (7024 lb)-max payload: 605 kg (1333 lb)-max power loading: TO: 5.72 kg/kW; cuise: 5.29 kg/kW-max wing loading 186.3 kg/m^2-max cruising speed at FL260: 320 kt (593km/h)-econ. cruising speed at FL310: 252 kt (467 km/h)-max rate of climb at SL: 752 m/min (2380 ft/min)-max certified altitude: 9450 m (31000 ft)-TO to 15 m: 866 m (2845 ft)



-landing from 15 m : 741 m (2435 ft)- Range, 45 min reserves:with max fuel:

-econ cruise: 1584 n miles (2933 km)-max cruise: 1409 n miles (2609 km)

Power Plant: one 1361 kWPratt&Whitney Canada PT6A-66D turboprop, flat

rated at 634 kW,driving a four -blade constant-speed, fully feathering,reversible pitch metal propeller.Fuel combined in two integral tanks in each wing, combined 1142 litres of which 1100 litres usable.Oil capacity 12 litres.

3.4. Extra EA-500 (pg 234)-business turboprop-up to 5 passenger-Wing span: 11.68 m (38 ft 3+3/4 in)-Length overall: 10.13 m (33 ft 2+3/4 in)-empty weight: 1445 kg (3186 lb)-max TO weight 2130 kg (4695 lb)-max fuel weight: 553 kg (1220 lb)-max landing weight 2000 kg (4409 lb)-max power loading: 6.35 kg/kW;-max wing loading: 149.4 kg/m^2-cruising speed at mid-cruise weight:

-90% power at FL120: 226 kt (419 km/h)-75% power at FL250: 200 kt (370 km/h)-40% power at FL250: 173kt (320 km/h)

-max rate of climb at SL: 407 m/min (1335 ft/min)-max certified altitude: 7620m (25000 ft)-TO run: 381 m (1250 ft)-TO to 15 m: 625 m (2050 ft)-landing from 15 m : 625 m (2050 ft)-landing run: 280 m (917 ft)- Range with reserves:

- 204 kg (450 lb) useful load: 1600 n miles (2963 km)- 363 kg (800 lb) useful load: 1000 n miles (1852 km)-454 kg (1000 lb) useful load: 700 n miles (1269 km)-max cruise: 1409 n miles (2609 km)

Power Plant: one 336 kW Rolls-Royce turboprop, driving a five-bladeconstant-speed, reversible pitch composite propeller.Fuel combined in two integral tanks in each wing, 680 litres of which 652litres usable.

3.5. Piaggio P 180 Avanti( pg 401)-business TWIN- turboprop-up to 9 passenger-Wing span: 14.035 m (46 ft 0 in)-Length overall: 14.41 m (47 ft 3+1/2 in)-empty weight: 3538 kg (7800 lb)-max TO weight 5488 kg (12100 lb)-max fuel weight: 1271 kg (2802 lb)



-max landing weight 5216 kg (11500 lb)-max payload 907 kg (2000 lb)-max power loading: 4.33 kg/kW;-max wing loading: 343.1 kg/m^2-max level speed at FL310: 398 kt (737 km/h)

- at FL280 402 kt (744 km/h)-cruising speed at max cruise power:

-FL300: 390 kt (722 km/h)-FL350: 374 kt (693 km/h)-FL390: 349 Kt (646 km/h)

-max rate of climb at SL: 899 m/min (2950 ft/min)-max certified altitude: 12500 m (41000 ft)-service ceiling: 12040 m (39500 ft)-service ceiling, OEI: 7391 m (24250 ft)-rate of climb at SL : 899 m/min (2850 ft/min)-rate of climb at SL, OEI : 204m/min ( 670 ft/min)-TO run: 867 m (2850 ft)-TO to 15 m, SL at max TO weight: 986 m (3235 ft)-landing from 15 m at max landing weight: 1067 m (3500 ft)-landing run: 872 m (2860 ft)- Range at max range power: 1793 n miles (3320km)-max range

-at max range power: 1507 n miles (2791 km)-at max cruise power: 1456 n miles (2696 km)

Power Plant: two 1216 kW Pratt&Whitney Canada PT6A-66Bturboprops,flat rated at 634 kW driving a Hartzel five-blade aluminium

constant speed fully feathering reversible-pitch pusher propeller.Fuel in two fuselage tanks and two wing tanks. Total fuel capacity 1597litres of which 1583 are usable.

3.5. Vulcanair AP 68TP A-Viator( pg 409)-utility turboprop twin-up to 9 (10) passenger-Wing span: 12 m (39 ft 4+1/2 in)-Length overall: 11.27 m (36 ft 11+1/2 in)-empty weight: 1680 kg (3704 lb)-max TO weight 3000 kg (6614 lb)

-max fuel weight: 675 kg (1488 lb)-max landing weight 2850 kg (6283 lb)-max payload 870 kg (1918 lb)-max power loading: 6.13 kg/kW;-max wing loading: 153.2 kg/m^2-max level speed at SL: 200 kt (370 km/h)-max cruising speed at FL120: 220 kt (407 km/h)-service ceiling: 7925 m (26000 ft)-service ceiling, OEI: 3475 m (11400 ft)-max rate of climb at SL: 472 m/min (1550 ft/min)-rate of climb at SL, OEI: 82 m/min (270 ft/min)-TO run: 400 m (1315 ft)-TO to 15 m: 620 m (2035 ft)



-landing from 15 m: 700 m (2300 ft)-landing run: 320 m (1050 ft)- Range with max fuel,cruising speed, at FL120: 850 n miles (1574 km)Power Plant: two Rolls Royce turboprops each flat rated at 245 kW drivinga Hartzel three-blade constant speed reversible-pitch pusher propeller.

Two interconnected fuel tanks in each wing and a 38 litre tank in eachengine nacelle, giving a total usable capacity of 480 litres.

3.6. Myasishchev M-1011T Sokol (pg 525)-light utility turboprop twin-up to 7 passenger-Wing span: 13 m (42 ft 8 in)-Length overall: 9.975 m (32 ft 8+3/4 in)-empty weight: 2190 kg (4828 lb)-max TO weight 3270 kg (7209 lb)-max fuel weight: 450 kg (922 lb)-max landing weight 3160 kg (6966 lb)-max payload 870 kg (1918 lb)-max power loading: 5.84 kg/kW;-max wing loading: 191.7 kg/m^2-max cruising speed: 210 kt (390 km/h)-cruising altitude: 7600 m (24940 ft)-TO run: 460 m (1315 ft)-landing run: 390 m (1280 ft)- Range with max fuel,45 min reserves: 594 n miles (1100 km)-Range ferry: 701 n miles (1300 km)

Power Plant: one 559 kW Walter M601 turboprop driving Avia Hamilton fiveblades propeller.

3.7. Facl Kestrel (pg 629)-business turboprop-up to 6 passenger-Wing span: 13.11 m (43 ft 0 in)-Length overall: 11.4 m (37 ft 4*4/3 in)-empty weight: 2115 kg (4663 lb)-max TO weight 3628 kg (8000 lb)-max fuel weight: 771 kg (1700 lb)

-max power loading: 4.87 kg/kW;-max cruising speed at FL 280: 352 kt (652 km/h)-econ. cruising speed: 214 kt (396 km/h)-service ceiling: 9450 m (31000 ft)-max rate of climb at SL: more then 1219 m/min (4000 ft/min)-Range with max fuel: 1618 n miles (2966 km)-Range ferry: 1914 n miles (3544 km)Power Plant: one Pratt&Whitney turboprop, flat rated at 746 kW, four bladeHartzel reversible pitch prpeller.Fuel capacity of 965 litres.

3.8. Beechcraft Bonanza 36 (pg 673)-utility transport



-up to 6 passenger-Wing span: 10.21 m (33 ft 6 in)-Length overall: 8.38 m (27 ft 6 in)-empty weight: 1148 kg (2700 lb)-max TO weight 1655 kg (3650 lb)

-max fuel weight: 201 kg (444 lb)-max power loading: 7.4 kg/kW;-max wing loading: 98.5 kg/m^2-max level speed min weight: 184 kt (340 km/h)-max cruising speed, mid cruise weight at FL100: 171 kt (317 km/h)-normal cruise speed at FL100:163 kt (302 km/h)-long range cruising speed at FL100: 80 kt (148 km/h)-service ceiling: 5640 m (18500 ft)-max rate of climb at SL: 375 m/min (1230 ft/min)-TO run: 583 m (1913 ft)-landing from 15 m : 442 m (1450 ft)-landing run: 290m (950 ft)- Range with 2 passengers at FL100: 751 n miles( 1390 km)-Range, normal cruising speed at FL 100: 775 n miles (1435 km)- Range, long range cruising speed at FL100: 916 n miles (1696 km)Power Plant: one 224 kW Teledyne Continental flat-six engine ,three bladeHartzel constant speed metal propeller.Fuel capacity of 303 litres of which 280 litres usable.

3.9. Piper PA-34-220T Seneca V (pg 889)-utility twin

-up to 6 passenger-Wing span: 10.8 m (35 ft 5 in)-Length overall: 7.52 m (24 ft 8+1/4 in)-empty weight: 1539 kg (3393 lb)-max TO weight 2154 kg (4750 lb)-max fuel weight: 348 kg (444 lb)-max landing weight: 2047 kg (4513 lb)-max power loading: 6.57 kg/kW;-max wing loading: 111.1 kg/m^2-max level speed: 218 kt (404 km/h)-cruising speed,max cruise power at FL100: 182 kt (337 km/h)

-cruising speed normal cruise power at FL100: 176 kt (326 km/h)-long range cruising speed at FL100:-max certified altitude: 7620 m (25000 ft)-service ceiling, OEI: 5030 m (16500 ft)-max rate of climb at SL: 446 m/min (1462 ft/min)-rate of climb at SL, OEI: 76 m/min (250ft/min)-TO run: 349 m (1145 ft)-TO to 15 m: 521 m (1710 ft)-landing from 15 m : 665 m (2180 ft)-landing run: 427 m (1400 ft)-Range at long range cruise power,with 45 min reserves:

-at FL100: 812 n miles (1503 km)-at FL150: 828 n miles (1533 km)



-at FL185: 819 n miles (1516 km)Power Plant: one 146 kW Teledyne Continental TSIO and one 164 kW Teledyne Continental LTSIO flat-six turbocharded counter rotatingengine ,two blade Hartzel fully fathering. propeller.Fuel capacity of 485 litres of which 462 litres usable.

Oil capcity 7.5 litres.

3.10. Mitsubishi MU-2 (pg 143)-twint turboprop utility transport- 6-12 passenger-Wing span: 11.95 m (39 ft 2 in)-Length overall: 12.03 m (39 ft 5+3/4 in)

- empty weight: 2915 kg (6426 lb)-max TO weight 4700 kg (10361lb)-max fuel weight:-max landing weight: 4470 kg (9854 lb)-max power loading: 3.3 kg/hp;-max wing loading: 284 kg/m^2perf at AUW= 4160 kg (9170lb)-max cruising speed,at FL100: 326 m/h (326 km/h)-econ cruising speed FL200: 300 m/h (482 km/h)-service ceiling: 8230 m (27000 ft)-service ceiling, OEI: 3540 m (11600 ft)-rate of climb at SL: 792 m/min (2600 ft/min)-rate of climb at SL, OEI:

-TO run:-TO to 15 m: 510 m (1675 ft)-landing from 15 m : 450 m (1475 ft)-landing run:-max range tanks full at FL230: 1550 miles (2500 km)Power Plant: 2* 705 shp turboprop engine ,three blade fully fathering,reversible pitch constant speed propeller.Fuel capacity of 1388 litres.

3.11. Beechcraft H18 (pg 247)-twin engined light transport

-7-9 passenger-Wing span: 15.14 m (49 ft 8 in)-Length overall: 10.7 m (35 ft 2+1/2 in)-empty weight: 2651 kg (5845 lb)-max TO weight 4490 kg (9900 lb)-max fuel weight:-max landing weight: 4310 kg (9500 lb)-max power loading: 5 kg/hp;-max wing loading: 134.2 kg/m^2perf at max TO weight-max cruising speed(66.7% power),at FL50: 209 m/h (336 km/h)

-at FL100: 220 m/h (354 km/h)-econ cruising speed, 44.5 power at FL50: 178 m/h (286 km/h)



at FL100: 185 m/h (298km/h)-service ceiling: 6520 m (21400 ft)-service ceiling, OEI: 2865 m (9400 ft)-rate of climb at SL: 427 m/min (1400 ft/min)-rate of climb at SL, OEI: 80m/min (260ft/min)

-TO run:-TO to 15 m: 631 m (2072 ft)-landing from 15 m : 564 m (1850 ft)-landing run:-max range , 44.5 % fuel at FL100, 45 min reserves: 1530 miles (2460km)Power Plant: two 450 shp radial air-cooled engine ,three blade fullyfathering, reversible pitch constant speed propeller.Fuel capacity of 750 litres+ aux tanks 1205 litres.OIL cap: 53 litres.

3.12. Beechcraft Queen air A65 (pg 253)-business and utility aircraft-up to 7 passengers-Wing span: 13.98 m (45 ft 4 in)10+1/2-Length overall: 10.82 m (35 ft 6 in)-empty weight: 2249 kg (4960 lb)-max TO weight 3493 kg (7700 lb)-max fuel weight:-max landing weight: 3343 kg (7350 lb)-max power loading: 5.45 kg/hp;

-max wing loading: 135.7 kg/m^2perf at max TO weight-max cruising speed(70% power),at FL150: 214 m/h (344 km/h)-econ cruising speed, 45 power at FL150: 171 m/h (275 km/h)-service ceiling: 9540 m (31300 ft)-service ceiling, OEI: 4725 m (15500 ft)-rate of climb at SL: 396 m/min (1300 ft/min)-rate of climb at SL, OEI: 75m/min (245 ft/min)-TO run: 360m (1180 ft)-TO to 15 m: 475 m (1560 ft)-landing from 15 m : 533 m (1750 ft)

-landing run: 405 m(1330 ft)-range +aux fuel at economy cruising speed, 45 min reserves: 1660miles (2670 km)Power Plant: two 340 shp isx cilinder horizontally opposed air-cooledsupercharged engine, three blade fully fathering, reversible pitch constantspeed propeller.Fuel capacity of 1000 litres.OIL cap: 30 litres.

3.13. Beechcraft Queen air B80 (pg 254)-business aircraft, commuter airliner and utility aircraft-6-7 passengers-Wing span: 15.32 m (50 ft 3 in)



-Length overall: 10.82 m (35 ft 6 in)-empty weight: 2286 kg (5040 lb)-max TO weight 3992 kg (8800 lb)-max fuel weight:-max landing weight: 3992 kg (8800 lb)

-max power loading: 5.53 kg/hp;-max wing loading: 146 kg/m^2perf at max TO weight-max cruising speed(70% power),at FL150: 220 m/h (360 km/h)-econ cruising speed, 45 power at FL150: 183 m/h (294 km/h)-service ceiling: 8168 m (26800 ft)-service ceiling, OEI: 3596 m (11800 ft)-rate of climb at SL: 388 m/min (1275 ft/min)-rate of climb at SL, OEI: 80 m/min (265 ft/min)-TO run: 418 m (1372 ft)-TO to 15 m: 594 m (1800 ft)-landing from 15 m : 704 m (2311 ft)-landing run: 408 m(1340 ft)-range max, 45 min reserves: 1560 miles (2510 km)Power Plant: two 380 shp six cilinder horizontally opposed air-cooledsupercharged engine, three blade fully fathering, reversible pitch constantspeed propeller.Fuel capacity of 809 litres.OIL cap: 30 litres.

3.14. Cessna model 401 (pg 305)

-executive transport-6-8 passengers-Wing span: 12.5 m (39 ft 10+1/4 in)-Length overall: 10.29 m (33 ft 9 in)-empty weight: 1663 kg (3668 lb)-max TO weight 2858 kg (6300 lb)-max fuel weight:-max landing weight: 2818 kg (6200 lb)-max power loading: 10.5 kg/hp;-max wing loading: 157.2 kg/m^2perf at max TO weight

-max cruising speed (75% power), at FL100: 216 m/h (347 km/h)-max cruising speed (75% power), at FL200: 236 m/h (380 km/h)-econ cruising speed, at FL250: 215 m/h (346 km/h)-service ceiling: 7980 m (26180 ft)-service ceiling, OEI: 3565 m (11700 ft)-rate of climb at SL: 491 m/min (1610 ft/min)-rate of climb at SL, OEI: 78 m/min (255 ft/min)-TO run: 517 m (1695 ft)-TO to 15 m: 677 m (2220 ft)-landing from 15 m : 538 m (1765 ft)-landing run: 777 m(237 ft)-range at max cruising speed, FL200: 694 miles (1117 km)-range at econ cruising speed at FL250: 808 miles (1300 km)



Power Plant: two 300 shp six cilinder horizontally opposed air-cooledsupercharged engine, three blade fully fathering, reversible pitch constantspeed propeller.Standard fuel capacity of 378.5 litres.OIL cap: 22.75 litres.

OIL cap: 22.75 litres.

MIL-F-8785CLevels of flying qualities:-level 1: Flying qualities clerly adequate for the mision Flight Phase-level 2: Flying qualities adequate to accomplish the mission Flight Phase,but some increaze in pilot workload or degradation in missioneffectiveness, or both, exists.-level 3: Flying qualities such that the airplane can be controled safely, butpilot workload is excessive or mission effectiveness is inadequate, or both.

Short period damping ratio limits.

FlightPhase

Category A andCategory C

Category B

Minimum Maximum Minimum Maximum

Level 1 0.35 1.3 0.3 2Level 2 0.25 2 0.2 2Level 3 0.15* - 0.15* -*May be reduced at altitude above 20000 feet if aproved by the procuringactivity

Phugoid damping Requirements

Flying Quality DampingLevel 1 0.04

Level 2 0

Level 3 sec

Dutch Roll Undamped Natural Frequency and Damping RatioRequirementsLevel Flight

PhaseCategory

Class Min

1 ABC



2 All3 All

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