Specifications
Cardinal Specs
'68 177
'69 177A
'70-'74 177B
'75-'78 177B
1971 RG
1972-1978 RG
Interior Comparision
Other Cessnas
172 A
172 B
172 C
172 D-H
172 I Skyhawk
172 K Hawk XP
172 K-L Skyhawk
172 K-L
172 M Float
172 M Float 2
172 M Skyhawk
172 N Hawk 100
172 N-P Hawk 100
172 O Cutlass
172 P II Skyhawk
172 RG II Cutlass
182 A-D
182 E-H
182 J-M Skylane
182 N Skylane
182 P-Q
182 Q II
182
R 172 K Hawk XP
R182 RG II Skylane
R182 RG Turbo Skylane
T-182 Q II Turbo Skylane
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Cardinal 177B (1970 - 1974)
Aircraft Performance Specifications
This information is provided as a guide "at users risk" and is not intended for
flight planning purposes! Please consult the relevant Pilots Operating Handbook prior to flight.
177 B Cardinal
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Cessna® AIRCRAFT CORPORATION
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Serial numbers 17701371 through 17702123
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| General Information |
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1971 177B
Owned by the Flying Pigs Partnership
Pipestone, Minnesota.
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| Engine Make: |
Lycoming 180hp
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| Engine Model: |
O-360-A1F6 |
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| Propeller Type: |
McCauley® Constant Speed |
| Power (HP or Lbs Thrust): |
180 |
| Engine TBO: |
2000 |
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| S P E E D S |
|
MPH |
KTS |
KPH |
| Maximum Cruising Speed |
|
153 |
132 |
244 |
| Recommended Cruising Speed |
|
142 |
123 |
227 |
| Stalling Speed |
|
53 |
46 |
85 |
| F U E L C A P A C I T Y |
|
Lbs |
US Gals |
Litres |
| Standard Fuel |
|
330 |
50 |
189 |
| Long Range Version |
|
402 |
61 |
231 |
| W E I G H T S |
|
|
US Lbs |
Kilos |
| Gross Weight |
|
|
2500 |
1133 |
| Empty Weight |
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|
1485 |
673 |
| Max Useful Load |
|
|
1015 |
460 |
| Max Useful w/Full Fuel |
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|
685 |
310 |
| R A N G E
(No Reserve)
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|
SM |
NM |
KM |
Hrs |
| Max Range - Std Cruise (LR tanks) |
|
994 |
850 |
1574 |
6.8 |
| Max Range - Std Cruise (Std tanks) |
|
850 |
726 |
1344 |
5.7 |
| C E I L I N G S |
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Feet |
Meters |
| Max Service Ceiling |
|
14600 |
4449 |
| Max Engine Out Ceiling |
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0 |
0 |
| C L I M B R A T E S |
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Feet P/Min |
Meters P/Min |
| Max Climb, Sea Level, Gross Weight |
|
840 |
256 |
| Max Climb, Engine Out, Sea Level, Gross Weight |
|
0 |
0 |
| T A K E O F F & L A N D I N G D I S T A N C E S |
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Feet |
Meters |
| TakeOff Ground Roll, Sea Level, Gross Weight |
|
750 |
228 |
| TakeOff Over 50ft/15meter Obstacle, Sea Level, Gross Weight |
|
1400 |
426 |
| Landing Ground Roll, Sea Level, Gross Weight |
|
600 |
182 |
| Landing Over 50ft/15meter Obstacle, Sea Level, Gross Weight |
|
1220 |
371 |
| A I R C R A F T D I M E N S I O N S |
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Feet |
Meters |
| Cabin Width (at shoulder) |
|
4.0 (48 inches) |
1.2192 |
| Fuselage Length: 1970-71 (approx.) |
|
27 |
8.0 |
| Fuselage Length: 1972-74 (approx.) |
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27.3 |
8.32 |
| Fuselage: 1970-71 (usually tail section) Height (approx.) |
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8.7 |
2.65 |
| Fuselage: 1972-74 (usually tail section) Height (approx.) |
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9.2 |
2.45 |
| Total Wingspan (approx.) |
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35.6 |
10.85 |
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