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UH-1 H Weight and Balance.pdf (328 kb) Download

UH-1 H Performance Planning Manual.pdf
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UH-1 Utility Helicopter Specifications

Max load	4000 pounds
Max weight	9500 pounds
Max ceiling height	12600 ft	Oxygen compulsory over 10 000 ft
Max range	276 nm
Max cruising speed	111 knots
Endurance	2 - 2.5 hours
Length overall	57 ft 9.5 in
Fuselage length	41 ft 11 in
Rotors operating	57 ft 1 in
Rotors static	57 ft 1 in
Main rotor diameter	48 ft	Two-blade semi-rigid bonded all-metal
Tail rotor diameter	8 ft 6 in	Two-blade rigid delta hinge bonded all-metal
Height	14 ft 6 in
Thread	8 ft 6.5 in
Span, max lateral	9 ft, 4 in
Engines	Turboshaft Lycoming T53 L-13 B
Engine output	1400 shp
Errors and omissions exempted

OH-58 Kiowa Specifications
Light Utility Helicopter

Crew	1
Passengers	4
Propulsion	1 Turbo shaft engine
Engine model	Allison 250-C20
Engine power	294 kw	394 shp
Speed	222 km/h	120 kts
Service ceiling	6.400 m	21.000 ft
Range	450 km	243 nm
Empty weight	840 kg	1.852 lbs
Max take-off weight	1.520 kg	3.351 lbs
Rotor blades (main/tail)	2/2	2/2
Main rotor diameter	10,16 m	33,3 ft
Tail rotor diameter	1,65 m	5,4 ft
Rotor disc area	81,1 m	872 ft
Length (fuselage)	9,81 m	32,2 ft
Length	11,82 m	38,8 ft
Height	2,91 m	9,6 ft
Total production	ca. 2200
Developed from	Bell 206
ICAO code	B06
Data for (version)	Bell OH-58B Kiowa
Remarks	Military variant of JetRanger
Errors and omissions exempted

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