AERO COMMANDER 520

STANDARD DATA: Seats 6-7. Gross wt. 5,400. Empty wt. 3,800. Fuel capacity 150. Engines two 260-hp Lycomings. PERFORMANCE: Top mph 211. Cruise mph 196. Stall mph 57. Initial climb rate 1,800. Ceiling 24,400. Range 850. Takeoff distance (50′) 950. By 1951, Ted Smith was general manager of the Aero Commander company and the Model 520 more »

AERO COMMANDER 560

STANDARD DATA: Seats 5-7. Gross wt. 7,000. Empty wt. 4,690. Fuel capacity 223. Engines two 350-hp Lycomings. PERFORMANCE: Top mph 288. Cruise mph 230. Stall mph 73. Initial climb rate 1,587. Range 1,705. Ceiling 21,900. Takeoff distance (50′) 1,350. Landing distance (50′) 1,375. STANDARD DATA: Seats 5-7. Gross wt. 6,500. Empty wt. 4,300. Fuel capacity more »

AERO COMMANDER L 3805

STANDARD DATA: Seats 6-7. Gross wt. 4,600. Empty wt. 2,800. Fuel capacity 100. Engines two 190-hp Lycomings. PERFORMANCE: Top mph 181. Cruise mph 165. Stall mph 57. Initial climb rate 1,450. Ceiling 24,400. Range 850. Takeoff run 780. Landing roll 849. The Aero Design and Engineering Corp., the predecessor of the Aero Commander Company, was more »

BEECH MODEL 18

STANDARD DATA: (D18S) Seats: 5-7; Gross weight: 8,750 lbs.; Empty weight: 5,770 lbs.; Fuel capacity: 206-286 gals.; Engines: two 450 hp Pratt & Whitney Wasp Juniors. PERFORMANCE: Top speed: 230 mph; Cruise speed: 211 mph; Stall: 77 mph; Initial climb rate: 1,190 fpm; Range: 985 nm; Ceiling: 20,500 ft.; Takeoff distance, 50 ft.: 1,760 ft.; more »

BEECHCRAFT 1900

STANDARD DATA: 1900D Seats 19+2. Gross wt. 17,120. Empty wt 10,650. Engines two 1,280-shp Pratt & Whitney PT6A-67D turboprops. Fuel 665. PERFORMANCE: Max Cruise 288 kts. Initial climb rate 1,910. Ceiling 25,000. Range 1,498 nm. Takeoff 3,813′. Landing 2,790′. After Raytheon acquired Beechcraft, the company looked for a re-entry into the regional aircraft market. The more »

BEECHCRAFT KING AIR 200/300/350

Beech Super King Air Beech Super King Air 350 STANDARD DATA: (A200) Seats: 6-13; Gross weight: 12,500 lbs.; Empty weight: 7,437 lbs.; Fuel capacity: 544 gals.; Engine: two 850 shp Pratt & Whitney reverse-flow free turbines. PERFORMANCE: Top speed: 333 mph; Cruise speed: 328 mph; Stall: 86 mph; Initial climb rate: 2,450 fpm; Ceiling: 33,880+ more »

BEECHCRAFT KING AIR 90 SERIES

Beechcraft King Air E90 STANDARD DATA: (E90) Seats 6-10. Gross wt. 10,100. Empty wt. 6,052. Fuel capacity 474. Engines two 550-shp Pratt & Whitney reverse-flow free turbines. PERFORMANCE: Cruise mph 287. Stall mph 89. Initial climb rate 1,870. Ceiling 27,620. Range 1,507. Takeoff distance (50′) 2,024. Landing distance (50′) 2,110. STANDARD DATA: (F90) Seats 7-10. more »

CAMAIR TWIN NAVION

STANDARD DATA: Seats 4. Gross wt. 4,500. Empty wt. 3,000. Fuel capacity 188-200. Engines two 300 hp fuel-injected Continentals. PERFORMANCE: Top mph 215. Cruise mph 200. Stall mph 60. Initial climb rate 2,000. Ceiling 22,000. Range 900. Takeoff run 400. Landing roll 600. The Camair flew for the first time in 1953 and was designed more »

CESSNA 310

STANDARD DATA: (310R) Seats 4-6. Gross wt. 5,500. Empty wt. 3,358. Fuel capacity 102-207. Engines two 285-hp fuel-injected Continentals. PERFORMANCE: Top mph 238. Cruise mph 224. Stall mph 81. Initial climb rate 1,662. Ceiling 19,750. Range 568-1,303. Takeoff distance (50) 1,700. Landing distance (50) 1,790. STANDARD DATA: (T310R) Seats 4-6. Gross wt. 5,500. Empty wt. more »

Cessna 340

  Cessna 340 Used Price: $290,000 Engine make/model: Cont. TSIO-520-NB [email protected]: 310 to 20,000 ft. Horsepower for takeoff: 310 TBO hrs.: 1400 Fuel Type: 100/100LL Propeller type: McCauley CS/76 in. Landing Gear type: Tri./Retr. Max ramp weight (lbs.): 6025 Gross weight (lbs.): 5990 Max landing weight (lbs.): 5990 Zero fuel weight (lbs.): 5630 Empty weight, more »

CESSNA 401/402

STANDARD DATA: (402 C Businessliner) Seats 6- 10. Gross wt. 6,885. Empty wt. 4,069. Fuel capacity 213. Engines two 325-hp turbocharged Continentals. PERFORMANCE: Top mph 266. Cruise mph 224. Stall mph 78. Initial climb rate 1,450. Ceiling 26,900. Range 461–1,101. Takeoff distance (50′) 2,195. Landing distance (50′) 2,485. STANDARD DATA: (401) Seats 6-8. Gross wt. more »

CESSNA 411/414 CHANCELLOR

STANDARD DATA: (Chancellor) Seats 8. Gross wt. 6,750. Empty wt. 4,357. Fuel capacity 213. Engines two 310-hp turbocharged Continentals. PERFORMANCE: Top mph 275. Cruise mph 258. Stall mph 83. Initial climb rate 1,580. Ceiling 31,350. Range 600-1,507. Takeoff distance (50′) 2,595. Landing distance (50′) 2,393. STANDARD DATA: (411) Seats 6-8. Gross wt. 6,500. Empty wt. more »

CESSNA CORSAIR

STANDARD DATA: Seats 6-8. Gross wt. 8,200. Empty wt. 4,846. Fuel capacity 367. Engines two 450-shp Pratt & Whitney turbines. PERFORMANCE: Top mph 304. Initial climb rate 1,888. Ceiling 34,000. Range 1,621. Cessna’s second entry into the propjet market came in 1980 with the introduction of the Corsair. Its seating for up to eight and more »

CHAMPION LANCER

STANDARD DATA: Seats 2. Gross wt. 2,450. Empty wt. 1,790. Fuel capacity 60. Engines two 100-hp Continentals. PERFORMANCE: Top mph 130. Cruise mph 120. Stall mph 62. Initial climb rate 642. Range 510. Ceiling 12,900. Takeoff run 500. The Champion Lancer was (during its production run) the least expensive twin produced in this country. Champion’s more »

CONVAIR 240/340/440

Convair CV-240 Convair 540 Convair 580 STANDARD DATA: (240) Seats 44. Gross wt. 41,790. Empty wt. 27,682. Fuel capacity 1,550. Engines two 2,100-hp Pratt & Whitney Twin-row Wasps. PERFORMANCE: Top mph 347. Cruise mph 291. Landing mph 88. Initial climb rate 1,520. Ceiling 30,000. Range 1,800. Takeoff distance (50′) 2,760. Landing distance (50′) 3,970. STANDARD more »

DE HAVILLAND CANADA DASH 7-8

STANDARD DATA: Dash 7 Seats 52. Gross wt. 43,500. Empty wt. 25,800. Fuel capacity 1,480. Engines four 1,120 shp Pratt & Whitney Aircraft of Canada turboprops. PERFORMANCE: Top mph 271. Cruise mph 265. Initial climb rate 1,270 fpm. Ceiling 23,600. Takeoff run 5,700. Landing roll 3,040. Range 810-1,300. Dash 8 Q400 Dash 8 Q200 STANDARD more »

DOUGLAS DC-3

STANDARD DATA: Seats 28-30. Gross wt. 25,200. Empty wt. 16,865. Fuel capacity 411. Engines two 1,200-hp Pratt & Whitney Twin-Wasps. PERFORMANCE: Top mph 230. Cruise mph 207. Stall mph 67. Initial climb rate 1,130. Range 2,125. Ceiling 23,200. The DC-2 was developed from the DC-1. The DC-2 first flew in 1934, and production continued until more »

DOUGLAS DC-4/C-54

STANDARD DATA: Seats 42. Gross wt. 65,000. Empty wt. 35,000. Fuel capacity 2,100. Engines four 1,000-hp Pratt & Whitney Twin-Wasps. PERFORMANCE: Top mph 285. Cruise mph 222. Stall mph 80. Initial climb rate 1,200. Range 3,500. Ceiling 25,000. The DC-4 design was the product of a group effort involving the technical departments of five of more »

DOUGLAS DC-6/DC-7

STANDARD DATA: (DC-6) Seats 64-92. Gross wt. 106,000. Empty wt. 49,767. Fuel capacity 3,992-5,512. Engines four 2,500-hp Pratt & Whitney Double Wasps. PERFORMANCE: Top mph 360. Cruise mph 307. Landing mph 93. Initial climb rate 1,120. Range 3,860. Takeoff distance (50′) 4,500. Landing distance (50′) 3,010. STANDARD DATA: (DC-7) Seats 62-99. Gross wt. 143,000. Empty more »

EVANGEL 4500 STOL

STANDARD DATA: Seats: 9; Gross weight: 5,500 lbs.; Empty weight: 3,530 lbs.; Fuel capacity: 111 gals.; Engines: two 300 hp Lycomings. PERFORMANCE: Top speed: 230 mph; Cruise speed: 182 mph; Stall speed: 67 mph; Initial climb rate: 1,500 fpm; Range: 637 nm; Service ceiling: 21,030 ft.; Takeoff distance (50 ft.): 1,125 ft.; Landing distance (50 more »

FAIRCHILD HILLER FH-227 (FOKKER)

STANDARD DATA (FH-227): Seats: 44-52; Gross weight: 43,500 lbs.; Empty weight: 22,923 lbs.; Fuel capacity: 1,364 lbs.; Engines: two 2,300 shp Rolls-Royce Dart turboprops. PERFORMANCE: Top speed: 294 mph; Top cruise: 270 mph; Stall speed: 87 mph; Initial climb rate: 1,560 fpm; Range: 1,655 nm; Service ceiling: 28,000 ft.; Takeoff run: 3,950 ft.; Landing roll: more »

FORD TRI-MOTOR

STANDARD DATA: Seats: 15; Gross weight: 13,250 lbs.; Empty weight: 7,800 lbs.; Engines: three 425 hp Pratt & Whitneys. PERFORMANCE: Top speed: 140 mph; Cruise speed: 115 mph; Landing speed: 60 mph; Range: 500 nm; Service ceiling: 20,000 ft. The “Tin Goose” is perhaps the most important aircraft in U.S. airline history. The original Stout more »

GAF NOMAD

STANDARD DATA: (N22B) Seats 13. Gross wt. 8,500. Empty wt. 4,613. Fuel capacity 269-363. Engines two 420 shp Allison turboprops. PERFORMANCE: Cruise mph 193. Stall mph 75. Initial climb rate 1,460. Ceiling 21,000. Range 840. Takeoff (50′) 1,180. Landing (50′) 1,110. Takeoff run (STOL) 600. Landing run (STOL) 250. STANDARD DATA: (N24A) Seats 17. Gross more »

GRUMMAN GOOSE/WIDGEON

STANDARD DATA: (Goose) Seats 4-6. Gross wt. 8,000. Empty wt. 5,425. Fuel capacity 220. Engines two 400 hp Pratt & Whitney Wasp Juniors. PERFORMANCE: Top mph 201. Cruise mph 191. Initial climb rate 1,100. Range 640. Ceiling 21,000. STANDARD DATA: (Widgeon) Seats 4-5. Gross wt. 4,525. Empty wt. 3,240. Fuel capacity 108. Engines two 200 more »

MARTIN 202

  STANDARD DATA: Martin 202 Seats 40. Gross wt. 39,900. Empty wt. 26,930. Engines two 2,100-hp Pratt & Whitney. PERFORMANCE: Top mph 311. Cruise mph 286. Stall mph 76. Initial climb rate 2,200. Range 635. Ceiling 33,000. Takeoff distance (50′) 1,565. Landing distance (50′) 1,720. STANDARD DATA: Martin 404 Seats 52. Gross wt. 44,900. Engines more »