|
GENERAL
|
| Manufacturer |
Trident Aircraft
Ltd. |
| Address |
Sidney, British
Columbia, Canada |
| Model |
TR-1 Trigull |
| Seats |
4 + 2 |
| Approved Type
Certificate No. |
Canadian DOT Type
Approval A119
US ATC No: A19EA |
| Issue Date |
1976-10-28 (Canada)
1976-12-16 (USA) |
| Type Certifcate Holder |
1987-05-20
Viking Air Ltd.
#9 - 9600 Canora Road
Sidney, British Columbia
Canada V8L 4R1 |
| |
|
|
DIMENSIONS
|
|
Length
(Wheels down) |
29 ft 4 in |
| Height (Max Land) |
12 ft 6 in |
| Cabin Width (interior) |
3 ft 11 in |
| Cabin Height
(interior) |
4 ft 2.2 in |
| Cabin Length
(interior) |
8
ft 0.8 in |
| Baggage Compartment
(volume) |
12.9 cu ft |
| |
|
|
LANDING GEAR
|
| Main Gear |
Tricycle, hydraulic
retraction.
Oleo-pneumatic shock-absorbers. |
| Track |
12 ft 0 in |
| Base |
12 ft 1 in |
| Main Wheels |
7.00-6 |
| Inflate to |
35 psi |
| Brakes |
Cleveland hydraulic
disc |
| Nose Wheel |
6.00-6 |
| Inflate to |
35 psi |
| |
|
|
WINGS
|
| Airfoil Section |
NACA
23015R-4 (modified) |
| Span |
wing floats up: 41
ft 9 in
wing floats down: 38 ft 10 in |
| Chord |
6 ft 0 in |
| Aspect Ratio |
wing floats
up: 7.11
wing floats down: 6.55 |
| Incidence |
2° 15' deg |
| Dihedral |
2° |
| Total Area |
wing floats up:
245.2 sq ft
wing floats down: 230.2 sq.ft |
| Aileron Total Area |
9.6 sq ft |
| Flap Total Area |
44.2 sq ft |
| |
|
|
EMPENNAGE
|
| Tailplane Area |
29.6 sq ft |
| Elevator Span |
15 ft 5 in |
| Elevator Total Area |
26.3 sq ft |
| Fin Area |
31.3 sq ft |
| Rudder Area |
9.8 sq ft |
| |
|
| |
|
|
WEIGHTS
|
| Gross - Normal |
3800
lbs |
| Gross - Turbo |
3950 lbs |
| Empty |
2500 lbs |
| |
|
|
SURFACE
MOVEMENTS
|
| Rudder |
± 30 ° |
| Ailerons |
± 20 ° |
| Elevators |
± 28 ° |
| Elevator Tabs |
± 25 ° |
| Water Rudder |
± 30 ° |
| Flaps |
Down 30 ° |
| |
|
|
ENGINE
|
| Models |
(1) Teledyne
Continental Tiara 6-320
(2) Lycoming IO-540-M1A5D
(3) Lycoming TIO-540-J2BD
|
| Rated Power |
(1) 320 hp @ 4400
rpm
(2) 300 hp
(3) 340 hp |
| Power Loading |
12.67
lbs/hp(2) |
| Propeller to
Crankshaft Ratio |
0.5:1 (1) |
| Fuel Grade |
100/130 minimum
grade aviation |
| Fuel Consumption
(Cruise 75%) |
16 US gal/hr (1) |
| Fuel Pressure |
2 to 9 psi |
| Compression Ratio |
?:1 |
| Piston Displacement |
? cu in |
| Bore |
? cu in |
| Stroke |
? cu in |
| Fuel Capacity |
100 US gal |
| Oil Capacity |
(2) 12 qts |
| |
|
|
PROPELLER
|
| Model (Standard) |
Hartzell c/s |
| Blades |
3 reversible |
| Diameter |
84 in |
| Model (Reversible
Option) |
Hartzell HC12x20-2 |
| Blades |
2
x L8427 wooden |
| Diameter |
84 in |
| Pitch |
+18 deg to -12 deg
(reverse) |
| |
|
|
PERFORMANCE
|
| Max Structural Cruise
Speed (Vno) |
178 mph TIAS |
| Max Maneuvering Speed
(Va) |
? mph TIAS |
| Never Exceed Speed
(Vne) |
211 mph TIAS |
| Max Flaps Extended
Speed (Vfe) |
? mph TIAS |
| Max Gear Extended
Speed (Vle) |
? mph |
| Cruise Speed (Vc)
@ 75% pwr |
? mph |
| Best Range Speed
(Vbr) |
? |
| Best Endurance Speed
(Vbe) |
? |
| Approach Speed
(Vref) |
? mph IAS |
| Best Power-Off Glide
Speed (Vbg) |
? |
| Minimum Descent Speed
(Vmd) |
? |
| Stalling Speed (Vs0)
- Gear/Flaps Down |
? mph IAS |
| Stalling Speed (Vs1)
- Gear/Flaps Up |
? mph IAS |
| Best Climb Angle Speed
(Vx) |
? |
| Best Rate of Climb
Speed (Vy) |
? mph IAS |
| Rate of Climb (Sea
Level) |
? ft/min |
| Service Ceiling |
18 000 ft |
| Range at Cruising (71
US gal) |
520 miles |
| Take-off Distance -
Land |
800 ft |
| Take-off Distance -
Water |
1000 ft |
| Take-off Time - Water |
25 secs |
| Landing Run - Land |
400 ft |
| Landing Run - Water |
700 ft |
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