EQC (C - 152) Flashcards
Engine manufacturer
Avco Lycoming
Propeller diameter and type
69 inches ; fixed pitch
Max. gross weight
1670 lbs / 759 kg
Max. baggage allowance
120 lbs / 24.6 kg
Standard empty weight (152 & 152 II)
152 = 1081 lbs
152 II = 1118 lbs
Fuel capacity (standard & extended)
standard = 26 gal
extended = 39 gal
Usable fuel (standard & extended)
standard = 24.5 gal
extended = 37.5 gal
Oil capacity
6 qts (sump)
Max. oil temperature
245 degrees F / 118 degrees C
Max. entry speed for chandelles, lazy eights, and steep turns
95 kts
White arc airspeed
35 - 85 kias
takeoff ground roll
725 ft
takeoff distance over 50 ft. obstacle
1340 ft
landing ground roll
475 ft
landing distance over 50 ft obstacle
1200 ft
Rate of climb @ sea level
715 fpm
alternator and battery voltage
alternator 28v
battery 24v
Engine failure during takeoff run procedures
- throttle IDLE
- brakes APPLY
- flaps RETRACT
- mixture IDLE CUT OFF
- Ignition OFF
- Master OFF
Engine failure immediately after takeoff procedures
- airspeed 60 KIAS
- mixture IDLE CUT OFF
- fuel s/o valve OFF
- ignition OFF
- flaps AS REQUIRED
- master OFF
Engine failure during flight procedures
- airspeed 60 KIAS
- carb heat ON
- primer IN & LOCKED
- fuel s/o valve ON
- Mixture RICH
- Ignition BOTH (or START if propeller is stopped)
Emergency landing without engine power procedures
- airspeed 60 KIAS
- mixture IDLE CUT OFF
- fuel s/o valve OFF
- ignition OFF
- flaps AS REQUIRED
- master OFF
- doors UNLATCH PRIOR TOUCHDOWN
- touchdown SLIGHTLY TAIL LOW
- brakes APPLY HEAVILY
Electrical fire in flight procedures
- master OFF
- all other switches (except ignition) OFF
- vents / cabin air / heat CLOSED
- fire extinguisher ACTIVATE
if fire out and electrical power is needed for flight:
- master ON
- circuit breakers CHECK (DO NOT RESET)
- radio / electrical switches - ON one at a time (except pitot heat)
- vents / cabin air / heat OPEN
1 lb = __ kg
- 454 kg
1 nm = __ km
1.852 km
Max. useful load
589 lbs (152)
552 lbs (152 II)
Tachometer normal operating range
1990 - 2550 rpm (green arc)
normal oil temperature range
100 - 245 degrees F (green arc)
normal oil pressure range
60 - 90 psi (green arc)
minimum oil pressure
25 psi (red line)
maximum oil pressure
100 psi (red line)
Flight load factor @ flaps up
+4.4 g
-1.76 g
Flight load factor @ flaps down
+3.5 g
Maximum demonstrated crosswind velocity
12 kts
Engine model number
O-235-L2C
Maximum engine power
110 BHP
Maximum engine speed
2550 rpm (red line)
Propeller manufacturer
McCauley Accessory Division
Center of gravity range
31 - 36.5 inches aft of datum (front face of firewall)
Approved fuel grades
- 100LL grade aviation fuel (blue)
- 100 grade aviation fuel (green)
Wing loading
10.5 lbs / sq. feet
Power loading
15.2 lbs / HP
Service ceiling
14,700 ft
Maximum speed @ sea level
110 kts
Maximum window open speed
143 KIAS