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Bad Points Schweizer - older design - needs more maintenance, 100 hour check often turns up needed repairs Adams says 'cannot give a definite answer, each has its good points. This is a list of my personal likes + dislikes for each model'. SAFETY Schweizer Helicopters A Name You Trust The long-established history of safety is a hallmark of Schweizer helicopters. As the most trusted light helicopter for training and missions, pilots appreciate the confidence the Schweizer 269A-D series, now S300™, S300CBi™, and S333, delivers. The S300™ series has the finest safety record of any FAA Read More.
QUALITY. PERFORMANCE. SAFETY
Schweizer Helicopters A Name You Trust
The long-established history of safety is a hallmark of Schweizer helicopters. As the most trusted light helicopter for training and missions, pilots appreciate the confidence the Schweizer 269A-D series, now S300™, S300CBi™, and S333, delivers. The S300™ series has the finest safety record of any FAA certified, piston-powered helicopters which is substantiated by the National Transportation Safety Board (NTSB) accident statistics.
New Production of 300™ Series Schweizer Helicopters Civilization 6 full crack.
There are two manuals pertaining to the 2-33 Schweizer Glider: a. Aircraft Operating Instructions (AOI) produced by DND; and b. The SGS 2-33 Sailplane Flight-Erection-Maintenance Manual produced by K & L Soaring LLC. The SGS 2-33 Sailplane Flight-Erection-Maintenance Manual produced by K & L. Schweizer 269 Helicopter Maintenance Manual. $15.05 shipping. 206-062-200-121 269A Schweizer Quad Plate. Or Best Offer. FAST 'N FREE. 269A9299 MODIFIED - Lower Pulley Shaft Wrench, Schweizer 300, Hughes 269, TH-55. $99.00 +$7.95 shipping. Make Offer - 269A9299 MODIFIED - Lower Pulley Shaft Wrench, Schweizer 300.
Schweizer proudly supports all existing ships and is pleased to introduce the production of the S300™, S300CBi™, and S333™.
Excellent Safety Record ● Stable Handling Characteristics ● Rugged Reliable Component Design
Specifications
SCHWEIZER 300C™
Performance | |
Standard day, sea level, maximum gross weight unless otherwise noted | |
Maximum speed (VNE) | 95kts. 176km/hr |
Maximum cruise speed (vh) | 86 kts. 159km/hr |
Hover ceiling, In-Ground-Effect (1700 lb) | 10,800 ft. / 3,292 m |
Hover ceiling, Out-of-Ground-Effect (1700 lb) | 8,600 ft. / 2,621 m |
Range (long range cruise* speed @ 4,000 feet) (no reserve) | • 32.5 gallon • 64.0 gallon |
Weights | |
Maximum takeoff gross weight | 2,050 lb. / 930kg |
Empty weight, standard configuration | 1,100 lb. / 499 kg |
Useful load | 950 lb. / 431 kg |
Dimensions | |
Fuselage length | 22.19 ft. / 930 kg |
Fuselage width | 4.25 ft. / 1.30 m |
Fuselage height | 7.17 ft. / 2.18 m |
Overall length (rotors turning) | 30.83 ft. / 9.40 m |
Overall height (to top of tail rotor | 8.72 ft. / 2.65 m |
Width (canopy) | 4.25 ft. / 1.30 m |
Main rotor Diameter | 26.83 ft. / 8.18 m |
Main landing gear tread (fullycompressed) | 6.54 ft. / 1.99 m |
Accommodations | |
Normal cabin seating (training) | 2 passengers |
Maximum certified cabin seating (utility) | 3 passengers |
Cabin length | 4.75 ft. / 1.45 m |
Cabin width | 4.92 ft. / 1.50 m |
Powerplant | |
Type | Textron Lycoming HIO–360–D1A |
Powerplant ratings (per engine, standard day, sea level) | - Takeoff (5-minute) 190 shp / 141 kw - Maximum continuous 190shp /141 kw |
Fuel Capacity | |
Standard fuel capacity | 32.5 US gal - 123.03 |
Extended range capacity | 64.0 US gal - 242.27 |
Specifications
SCHWEIZER 300CBi™
Performance | |
Standard day, sea level, maximum gross weight unless otherwise noted | |
Maximum speed (VNE) | 94kts. 174km/hr |
Maximum cruise speed (vh) | 80kts. 148km/hr |
Hover ceiling, In-Ground-Effect (1700 lb.) | 7,000 ft / 2,133 m |
Hover ceiling, Out-of-Ground-Effect (1700 lb.) | 4,800 ft. / 1,463 m |
Range (long range cruise* speed @ 4,000 feet) (no reserve) | • 32.5 gallon • 64.0 gallon |
Weights | |
Maximum takeoff gross weight | 1,750 lb. / 794kg |
Empty weight, standard configuration | 1,102 lb. / 500 kg |
Useful load | 648 lb. / 294 kg |
Dimensions | |
Fuselage length | 22.19 ft. / 930 kg |
Fuselage width | 4.25 ft. / 1.30 m |
Fuselage height | 7.17 ft. / 2.18 m |
Overall length (rotors turning) | 30.83 ft. / 9.40 m |
Overall height (to top of tail rotor) | 8.72 ft. / 2.65 m |
Width (canopy) | 4.25 ft. / 1.30 m |
Main rotor Diameter | 26.83 ft. / 8.18 m |
Main landing gear tread (fully compressed) | 6.54 ft. / 1.99 m |
Accommodations | |
Normal cabin seating (training) | 2 passengers |
Maximum certified cabin seating (utility) | 3 passengers |
Cabin length | 4.75 ft. / 1.45 m |
Cabin width | 4.92 ft. / 1.50 m |
Powerplant | |
Type | Textron Lycoming HIO–360-G1A |
Powerplant ratings (per engine, standard day, sea level) | -Takeoff (5-minute) 180 shp / 134 kw -Maximum continuous 180shp / 134 kw |
Fuel Capacity | |
Standard fuel capacity | 32.5 US gal / 123.03 |
Extended range capacity | 64.0 US gal / 242.27 |
S333™ Light Turbine-Powered Multi Mission
Featuring Rugged Design, Outstanding Performance, and Low Operating Costs
Schweizer 300 Maintenance Manual Online
Ideal applications include:
- Utility Applications
- Military Training
- Law Enforcement
Interested in test flying and purchasing a new model Schweizer?
Schweizer 300 Price
Please contact the authorized service center nearest to you or call 817.405.2100 today.
The initial contract was awarded by the Army Materiel Command in St. Louis, Missouri and was for an initial batch of 20 TH-55As at a total contract cost of $517,500 ($25,875 each), with the first group to be delivered by December, 1964. The contract also contained an option for the purchase of 215 more TH-55As in fiscal year 1965 for $5,563,125. The TH-55A was purchased to replace and supplement the OH-13 and the OH-23 in the primary training role at at the U.S. Army Primary Helicopter School at Fort Wolters. Both the OH-13 and OH-23 were used in Vietnam, and attrition and age eventually reduced the numbers available for training. New production of the TH-55A expanded its role and eventually it became the pre-eminent training helicopter with the U.S. Army eventually purchasing 792 . When Fort Wolters closed in 1973 the TH-55A continued to train new student pilots at Fort Rucker until 1988.
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The only variant used by the U.S. Army was the TH-55A which was powered by a Lycoming HIO-360-BIA of 180 hp. Refined versions of the original Model 269A design evolved into the Model 300 and were produced for the civilian market, as well as the military forces of other nations. Hughes Helicopters was purchased by McDonnell Douglas Helicopters in 1983, and production was transferred to Schweizer Aircraft Corporation. In 1986 Schweizer purchased the entire Model 300 program. By late 1999 nearly 3,500 Hughes/Schweizer 300's of all models had been sold - making it one of the most successful helicopters ever produced.
Schweizer 300 Maintenance Manual Pdf
Specifications: | Performance: | |
Diameter of main rotor | Max level speed at S/L | 86 mph |
Diameter of tail rotor | Max cruising speed at S/L | 75 mph |
Length overall, rotors fore and aft | Max rate of climb at S/L | 1,450 ft min |
Width, rotors for and aft | Vertical rate of climb | 740 ft min |
Height | Service Ceiling | 15,200 ft |
Skid Track | Hovering ceiling in ground effect | 9,500 ft |
Weight empty | Hovering ceiling out of ground effect | 5,800 ft |
Max normal T-O | Range | 200 miles |