Statements (73)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:aircraft_operated |
gptkb:DHC-4_Caribou
high-wing. fixed-wing aircraft. good short takeoff and landing capabilities. 8.1 m. STOL (Short Takeoff and Landing) aircraft 24.8 m. 8,000 kg empty. 80 kg/m². twin-engine turboprop. used for cargo and personnel transport. versatile transport. |
| gptkbp:armament |
gptkb:none
|
| gptkbp:climb_rate |
5.5 m/s.
|
| gptkbp:combat_role |
cargo transport
|
| gptkbp:crew |
2
required for military operations. |
| gptkbp:design |
De Havilland Canada design team
military and civilian transport. |
| gptkbp:engine |
2
1,200 hp Pratt & Whitney Canada. |
| gptkbp:engine_type |
turboprop
P T6 A-67 R. |
| gptkbp:features |
high-wing configuration
|
| gptkbp:financial_performance |
good low-speed stability.
|
| gptkbp:first_flight |
gptkb:1965
still in service with some operators. |
| gptkbp:flaps |
slotted flaps.
|
| gptkbp:fuel_capacity |
3,000 L
|
| gptkbp:height |
8.1 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
DHC-5 N
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
24.8 m
|
| gptkbp:manufacturer |
gptkb:De_Havilland_Canada
|
| gptkbp:material |
aluminum.
|
| gptkbp:max_speed |
300 km/h
|
| gptkbp:max_takeoff_weight |
900 m
1,200 m 11,340 kg |
| gptkbp:military_technology |
DHC-5 N-1.
DHC-5 N-2. |
| gptkbp:modifications |
various for different roles.
|
| gptkbp:nickname |
gptkb:dog_breed
|
| gptkbp:notable_event |
none reported
|
| gptkbp:operational_history |
used in various roles by military and civilian operators.
|
| gptkbp:operational_range |
1,500 km with maximum payload.
|
| gptkbp:power_consumption |
9.2 kg/hp.
|
| gptkbp:primary_user |
gptkb:military_officer
gptkb:Canadian_Forces |
| gptkbp:produced_by |
approximately 200 units
|
| gptkbp:production_years |
1965-1988
|
| gptkbp:propulsion |
variable-pitch propellers.
|
| gptkbp:range |
1,500 km
|
| gptkbp:retirement_year |
1988 from Canadian Forces.
|
| gptkbp:role |
gptkb:aircraft
|
| gptkbp:seating_capacity |
gptkb:32
4,500 kg large rear ramp. capable of operating in rough airstrips. |
| gptkbp:service_ceiling |
7,620 m
|
| gptkbp:services |
1965 with Canadian Forces.
|
| gptkbp:speed |
250 km/h.
|
| gptkbp:successor |
gptkb:none
|
| gptkbp:surface |
elevators, ailerons, rudder.
|
| gptkbp:tail_type |
T-tail.
|
| gptkbp:variant |
gptkb:DHC-5_Buffalo
|
| gptkbp:wing_area |
100 m²
|
| gptkbp:wingspan |
30.5 m
30.5 m. |
| gptkbp:bfsParent |
gptkb:DHC-5_Buffalo
|
| gptkbp:bfsLayer |
5
|