FRONT AND REAR COVER
INSIDE FRONT COVER, I
(SPECIFICATIONS SUPERCEDED, SEE SUPPLEMENT)
|
AA1B
SUPER YANKEE PERFORMANCE SPECIFICATIONS |
||
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GROSS WEIGHT: |
Take Off |
1685 lbs. |
|
|
Landing |
1600 lbs. |
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SPEED: |
Top Speed at Sea Level, 2700 RPM Maximum Continuous |
154 Mph |
|
|
Cruise, 75% Power at 6000 ft. |
152 Mph |
|
|
Cruise, 65% Power at 10,000 ft. |
151 Mph |
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RANGE: |
Cruise, 75% Power, 32 Gallons, No Reserve |
561 Stat. Miles |
|
|
Cruise, 65% Power, 32 Gallons, No Reserve |
614 Stat. Miles |
|
|
|
694 Stat. Miles |
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RATE OF CLIMB: |
At Sea Level |
1010 ft./min. |
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SERVICE CEILING |
|
14500 ft. |
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TAKE OFF: |
Ground Roll |
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|
|
Total Distance Over 50ft. Obstacle |
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|
LANDING: |
Ground Roll |
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|
|
Total Distance Over 50ft. Obstacle |
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|
WING LOADING |
|
16.7 lb./sq.-ft. |
|
POWER LOADING |
|
11.2 lb./hp. |
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BAGGAGE CAPACITY |
|
100 lb. |
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FUEL CAPACITY: |
TOTAL |
34 gal. |
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OIL CAPACITY: |
TOTAL |
8 qt. |
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PROPELLER |
Sensenich Fixed Pitch (Diameter x Pitch) |
72/62 |
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ENGINE |
Lycoming: 150 Hp at 2700 RPM |
O-320-xxx |
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NOTE: |
1. Range and endurance figures
do not include take off and climb allowance. |
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2. All performance figures
obtained with wheel fairings installed. |
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ISPECIFICATIONS SUPPLEMENT, NSIDE FRONT COVER
ii, iii
iv, 1-1
1-2, 1-3
1-4, 1-5 (FUEL SYSTEM SUPERCEDED, SEE
SUPPLEMENT)
1-6, 1-7
2-1, 2-2
2-3, 2-4
2-5, 3-1
3-2, 3-3
NOTE:
Short and
soft field take-offs in the AA1B Super Yankee are to be initiated with ½ Flaps
extended, when obstacles are cleared, retract the flaps and accelerate to the
desired climb speed.
3-4, 3-5
3-6, 3-7
3-8, 4-1
4-2, 4-3 (WEIGHT AND BALANCE LIMITS
SUPPERCEEDED, SEE SUPPLEMENTS)
4-4, 4-5 (WEIGHT AND BALANCE SUPPERCEEDED , SEE SUPPLEMENTS)
CURRENT
WEIGHT AND BALANCE AS OF APRIL 2016
|
|
Weight (Lbs.) |
Station (Inches) |
Moment Arm (Lb.-Inch) |
|
Basic Aircraft |
1152.9 |
73.8738 |
85169 |
|
Fuel |
|
82.3125 |
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|
Passengers |
|
92.3 |
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|
Baggage |
|
120 |
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|
|
|
|
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Total |
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================== |
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WEIGHT AND BALANCE
SUPPLEMENT
Blank, 5-1
5-2, 5-3 (SUPER YANKEE EXCEEDS
TAKE-OFF DATA IN FIGURE 8, PERFORMANCE DATA SUPERCEDED, SEE SUPPLEMENTS)
MAXIMUM RATE OF CLIMB
– 72 X 62 PROPELLER
Associated
Conditions:
|
Power |
Full
Throttle |
|
Flaps |
Up |
|
Mixture |
Lean
above 5000 Ft. for smooth operation. |
|
Weight (Lb.) |
Pressure Altitude (Ft.) |
Climb Speed IAS (MPH) |
Rate of Climb (Ft./Min.) |
|||
|
-20 Deg. C. (-4 Deg. F.) |
0 Deg. C. (32 Deg. F.) |
10 Deg. C. (50 Deg. F.) |
40 Deg. C. (104 Deg. F.) |
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|
1685 |
SL |
89.7 |
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|
1010 |
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2000 |
88.8 |
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|
833 |
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4000 |
87.9 |
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|
710 |
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6000 |
86.0 |
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|
532 |
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8000 |
85.1 |
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|
445 |
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10000 |
84.5 |
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|
376 |
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|
12000 |
84.0 |
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|
253 |
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CLIMB
PERFORMANCE SUPPLEMENT
5-4, 5-5 (CRUISE AND RANGE
PERFORMANCE SUPERCEDED, SEE SUPPLEMENTS)
Cruise Performance (72 x 62 Propeller)
Associated
Conditions:
|
Power |
Set to
Desired RPM |
|
Flaps |
Up |
|
Mixture |
Lean
below 75% rated power for best economy. |
|
RPM |
20 Deg. C. Below Std. Temp |
ISA Standard Temperature |
20 Deg. C. Above Std. Temp. |
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|
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
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|
Pressure Altitude 2000 Ft. |
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|
-9.0 Deg. C. (15.8 Deg. F.) |
11.0 Deg. C. (51.9 Deg. F.) |
31.0 Deg. C. (87.8 Deg. F.) |
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2700 |
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2600 |
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74 |
142 |
8.3 |
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2500 |
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68 |
134 |
7.7 |
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2400 |
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60 |
126 |
6.7 |
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2300 |
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55 |
121 |
6.2 |
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2200 |
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49 |
110 |
5.5 |
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2100 |
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RPM |
20 Deg. C. Below Std. Temp |
ISA Standard Temperature |
20 Deg. C. Above Std. Temp. |
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|
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
|
|
Pressure Altitude 4000 Ft. |
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|
-14.9 Deg. C. (5.2 Deg. F.) |
5.1 Deg. C. (41.2 Deg. F.) |
25.1 Deg. C. (77.2 Deg. F.) |
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2700 |
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|
84 |
154 |
9.5 |
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2600 |
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72 |
145 |
8.2 |
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2500 |
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65 |
138 |
7.4 |
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2400 |
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57 |
130 |
6.5 |
62 |
127 |
6.8 |
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2300 |
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53 |
124 |
6.0 |
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|
2200 |
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49 |
118 |
5.5 |
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2100 |
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43 |
107 |
4.8 |
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RPM |
20 Deg. C. Below Std. Temp |
ISA Standard Temperature |
20 Deg. C. Above Std. Temp. |
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|
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
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|
Pressure Altitude 6000 Ft. |
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|
-16.9 Deg. C. (1.6 Deg. F.) |
3.1 Deg. C. (37.6 Deg. F.) |
23.1 Deg. C. (73.6 Deg. F.) |
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2700 |
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2600 |
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2500 |
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2400 |
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63 |
136 |
7.1 |
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2300 |
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2200 |
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2100 |
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RPM |
20 Deg. C. Below Std. Temp |
ISA Standard Temperature |
20 Deg. C. Above Std. Temp. |
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|
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
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|
Pressure Altitude 8000 Ft. |
|||||||||
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|
-20.8 Deg. C. (-5.4 Deg. F.) |
-0.8 Deg. C. (30.5 Deg. F.) |
19.2 Deg. C. (66.6 Deg. F.) |
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|
2700 |
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2600 |
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2500 |
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2400 |
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2300 |
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2200 |
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2100 |
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RPM |
20 Deg. C. Below Std. Temp |
ISA Standard Temperature |
20 Deg. C. Above Std. Temp. |
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|
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
|
|
Pressure Altitude 10000 Ft. |
|||||||||
|
|
-24.8 Deg. C. (-12.6 Deg. F.) |
-8.8 Deg. C. (16.2 Deg. F.) |
11.2 Deg. C. (52.2 Deg. F.) |
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|
2700 |
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2600 |
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2500 |
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2400 |
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2300 |
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2200 |
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|
2100 |
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|
RPM |
20 Deg. C. Below Std. Temp |
ISA Standard Temperature |
20 Deg. C. Above Std. Temp. |
||||||
|
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
% BHP |
TAS MPH |
Fuel Flow (GPH) |
|
|
Pressure Altitude 12000 Ft. |
|||||||||
|
|
-28.8 Deg. C. (-19.8 Deg. F.) |
-8.8 Deg. C. (16.2 Deg. F.) |
11.2 Deg. C. (52.2 Deg. F.) |
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|
FT (2650) |
|
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|
59 |
149 |
6.5 |
|
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|
2600 |
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|
2500 |
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|
2400 |
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|
2300 |
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|
2200 |
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|
2100 |
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5-6, 5-7 (GLIDE RATIO IS 7.9:1)
Blank, 6-1
6-2, 6-3
6-4, 6-5
6-6, 7-1
7-2, 7-3
7-4, unnamed
