|
Model TSC-1A3 Teal III was a 180 hp development of the 150
hp TSC-1A2 Teal II. The engine pylon and engine cowling was
refined to look more streamlined.
|
GENERAL
|
|
|
Manufacturer |
Teal
Aircraft Corporation |
|
Address |
St.
Augustine, Florida, USA |
|
Model |
TSC-1A3
Teal III |
|
Seats |
2 at +71",
1 at +96" |
|
Approved Type Certificate No. |
A15EA |
|
Approved |
Not
approved |
|
Category |
2PCAmM |
|
Applicable Serial Numbers |
(22) |
|
Fuel Capacity (total)
- Standard 2 x 23 US gal wing tanks
- With optional 24.5 US gal hull tank |
46 US gal (40.6 US gal usable)
70.5 US gal (64.6 gal usable) |
|
|
DIMENSIONS
|
|
|
Length
(Max) |
23 ft 7 in |
|
Height (Max Land) |
9 ft 5 in |
|
Cabin Width (interior) |
x ft x in |
|
Cabin Height (interior) |
x ft x in |
|
Cabin Length (interior) |
x
ft x in |
|
Baggage Compartment (volume) |
x cu ft |
|
Draft Loaded |
x ft x in |
|
|
|
LANDING GEAR
|
|
|
Main Gear |
Spring steel struts |
|
Tread |
8 ft 3 in |
|
Base |
x ft x in |
|
Landing Gear Travel |
? in |
|
Main Wheels |
6.00 x 6 |
|
Inflate to |
20 psi |
|
Brakes |
x |
|
Tail Wheel |
Scott Model 3200, 6.00 x 2.50 |
|
Inflate to |
35 psi |
|
|
|
WINGS
|
|
|
Wing Airfoil Section |
NACA
4415 |
|
Span |
31 ft 11 in |
|
Chord |
5 ft 0 in |
|
Aspect Ratio |
6.50 |
|
Incidence |
4º |
|
Dehedral |
4º |
|
Total Area |
157 sq ft |
|
Aileron Total Area |
10 sq ft |
| |
Flap Airfoil
Section |
NACA
6321 |
| |
Flap Length |
116
in |
| |
Flap Chord |
13
in |
|
Flap Total Area |
20.9
sq ft |
|
|
|
EMPENNAGE
|
|
|
Hor. Stabilizer Incidence |
-5 º |
|
Tailplane Span |
8 ft 0 in |
|
Tailplane Chord |
42 in |
| |
Hor. Stabilizer
Airfoil Section |
NACA
0010 |
|
Hor. Stabilizer Area |
15.4 sq ft |
|
Elevator Area |
12.6 sq ft |
| |
Fin Airfoil
Section |
NACA
0010 |
|
Fin Area |
10.1 sq ft |
|
Dorsal Fin Area |
1.9 sq ft |
|
Rudder Area |
6.8 sq ft |
|
|
|
WEIGHTS
|
|
|
Gross - Land |
2
300
lbs |
|
Gross - Water |
2
300 lbs |
|
Empty |
1
450 lbs |
|
Max. Baggage (at +96") |
230 lbs |
|
Max. Wing Loading |
14.6 lbs/sq ft |
|
Max. Power Loading |
12.8 lbs/hp |
|
|
|
SURFACE MOVEMENTS
|
|
|
Rudder |
±
28° |
|
Ailerons |
up
+30°, down -20° |
|
Elevators |
up
+21°, down -17° |
|
Elevator Tab |
up
+16°, down -30° |
|
Rudder Tab |
± 30° |
|
Water Rudder |
±
28° |
|
Flaps |
-15° |
|
|
|
ENGINE
|
|
|
Manufacturer |
AVCO Lycoming |
|
Address |
Williamsport, PA, USA |
|
Model |
O-360-A1H6 |
|
Approved Type Certificate No. |
E-286 |
|
Weight (dry) |
298
lbs |
|
Number of Cylinders |
4 |
|
Rated Power |
180 hp |
|
Rated Speed |
? rpm |
|
Overspeed |
? rpm |
|
Maximum speed (ground) |
? rpm |
|
Reverse Propeller Speed |
N/A |
|
Crankshaft Rotation |
Clockwise |
|
Propeller Shaft Rotation |
Clockwise |
|
Propeller to Crankshaft Ratio |
1:1 |
|
Propeller Shaft Spline Size |
SAE
AS-127 Type 2 Mod. |
|
Cylinder Head Temperature |
Max. 500° F |
|
Fuel Grade |
100/100LL |
|
Fuel Consumption
(75% pwr) |
10.1
gal/hr |
| |
Miles Per Gallon |
75%
pwr 12.8 SM
55% pwr 13.1 SM |
|
Fuel Pressure |
Min. 0.5 psi, max. 8 psi |
|
Compression Ratio |
8.50:1 |
|
Piston Displacement |
361
cu in |
|
Bore |
5.125
cu in |
|
Stroke |
4.375
cu in |
|
Fuel Pump (Auxiliary) |
Bendix # 478630, 12
V |
|
Carburetor |
PAC
HA-6 |
|
Ignition |
Slick4230;
4202 Dual Magnetos |
|
Magneto Breaker Point Gap |
? |
|
Distributor Point Gap |
? |
|
Maximum Drop on Magneto or Distributor |
? RPM |
|
Ignition Timing |
25 deg BTC |
|
Firing Order |
1-x-x-x |
|
Spark Plugs |
Champion EM42E or
eqv. |
|
Spark Plug Gap |
.016" to
.022" |
|
Valve Clearance |
(lifter
bled down, cold) .?" |
|
Starter |
? Volt, x |
|
Alternator |
12 Volt x 40 Ampere |
|
Battery |
Exide AC-78/M, 37
Ampere hours |
|
Oil Temp (Max) |
245° F (above 60° F ambient
air)
210° F (below 10° F ambient air)
|
|
Oil Temp (Normal) |
100 - 180° F (ground)
160 - 180° F (in flight) |
|
Oil Pressure (Start/Warmup) |
max.
115 psi |
|
Oil Pressure (Normal) |
55
- 95 psi |
|
Oil Pressure (Idle Min) |
25 psi |
|
Oil Capacity |
8 US qts
(6 qts usable) |
|
Oil Specifications (Above 40º F) |
SAE 40 |
|
Oil Specifications (Below 20º F) |
SAE 20 |
|
Max Time Between Oil Changes |
? hrs |
|
|
|
PROPELLER
|
|
|
Model (Standard) |
Hartzell HC-C2YL-1B/7663-3 C/S |
|
Blades |
2 x metal |
|
Diameter |
72 in |
|
Pitch |
+12º (low) to +27.5º (high) |
|
Governor |
Hartzell F-2-6-A |
|
|
|
PERFORMANCE
|
|
|
Max Structural Cruise Speed (Vno) |
97
mph / 84 kts |
|
Design Maneuvering Speed (Va) |
97
mph / 84 kts |
|
Never Exceed Speed (Vne) |
123
mph / 107 kts |
|
Max Flaps Extended Speed (Vfe) |
90
mph / 78 kts |
|
Max Gear Extended Speed (Vle) |
123
mph / 107 kts |
|
Max Ldg. Gear Operation (Vlo) |
100
mph / 87 kts |
| |
Max side windows
open |
110
mph / 96 kts |
|
Cruise Speed (Vc) |
@ 75% pwr
@ 7 500 ft: 123 mph / 107 kts
@ 55% pwr @ 7 500 ft: 112 mph / 98 kts |
|
Best Range Speed
(Vbr) |
? |
|
Best Endurance Speed
(Vbe) |
? |
|
Best Climb Angle Speed
(Vx) |
? |
|
Best Rate of Climb Speed
(Vy) |
70 mph
/ 61 kts |
|
Rate of Climb (Sea Level) |
810
ft/min @ 2 300 lbs |
|
Approach Speed (Vref) |
70 mph
/ 61 kts |
|
Best Power-Off Glide Speed
(Vbg) |
75 mph
/ 65 kts |
|
Minimum Descent Speed
(Vmd) |
? |
|
Stalling Speed
(Vs0)
- @ flaps -15° and gear down |
52
mph / 45 kts |
| |
1.3 Vs0 |
67
mph / 59 kts |
|
Stalling Speed (Vs1) |
58
mph |
| |
Crosswind
Operating Limit |
15
mph land, 20 mph water |
|
Service Ceiling |
14
000 ft |
|
Range at Cruising
- std. fuel 46 US gal + 45 min reserve |
75%
+ reserve 400 SM / 348 NM
65% + reserve 410 SM / 356 NM
55% + reserve 417 NM / 363 NM |
|
Take-off Run - Land |
? ft
@ 2 300 lbs |
|
Take-off Run - Water |
? ft
@ 2 300 lbs |
| |
Take-off Distance - Land
(to 50 ft AGL) |
1
135 ft @ 2 300 lbs |
| |
Take-off Distance - Water
(to 50 ft AGL) |
1
255 ft @ 2 300 lbs |
| |
Landing Distance
- Land (from 50 ft AGL) |
650
ft @ 2 300 lbs |
| |
Landing Distance
- Water (from 50 ft AGL) |
? ft @ 2
300 lbs |
|
Landing Run - Land |
? ft @ 2
300 lbs |
|
Landing Run - Water |
?
ft @ 2 300 lbs |
|
|
|
