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Flying > C150 PERFS > Flashcards

C150 PERFS Flashcards

1
Q

C150 cruise speed at 7000’, 75% power

A

106 KIAS

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2
Q

C150 ROC at sea level

A

670 FPM

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3
Q

C150 service ceiling

A

14000’

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4
Q

C150 takeoff perfs

A

Ground roll 225 meters

Total distance over 50’ obstacle 422 meters

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5
Q

C150 Landing perfs

A

Ground roll 136 meters

Total distance over 50’obstacle 330 meters

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6
Q

C150 Stall speeds CAS

A

Flaps up, power off : 48 kts

Flaps down, power off : 42 kts

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7
Q

C150 total fuel capacity

A

Standard tanks 26 gallons = 98 liters,
total usable = 85 liters
Long range tanks 38 gallons = 143 liters
total usable = 132 liters

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8
Q

C150 max speed at sea level

A

109 KIAS

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9
Q

C150 Vx

A

Best angle, sea level through 10 000 ‘ : 56 KIAS

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10
Q

C150 Vy

A

Best rate : sea level : 68 KIAS ; 10 000’ : 62 KIAS.

nb : best rate near the ground = 60 KIAS.

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11
Q

C150 Vne

A

141 KIAS

Never exceed speed

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12
Q

C150 Vno

A

107 KIAS
Maximum structural Cruising speed. Do not exceed this speed except in smooth air and with caution. Vno is the upper end of green arc.

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13
Q

C150 Va

A

97 KIAS at MTOW (1600 lbs)

Manoeuvring speed : Do not make full or abrupt control movements above this speed.

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14
Q

C150 Vfe

A

85 KIAS

Do not exceed this speed with flaps down.

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15
Q

C150 PANEL

A

CLIMB TO 2.500 ft QNH
ON DOWNWIND, ABEAM SIERRA 4 : prendre un repère (hangar,…)
ABOVE SIERRA 4 : CARBU HOT + IDLE
CORRECT ATTITUDE -> 70 Knots -> TRIM
-> TURN IMMEDIATELY TO DOWNWIND, ADJUNSTING LENGHT OF DOWNWIND AND BASE ACCORDING TO WIND.
ANGLE DOWNWIND -> BASE : 90° or 2x45°
ANGLE BASE -> FINAL : 90° or 2x45°, !!! PAS D’ANGLE AIGU !!!
FLAPS : AT DISCRETION
LAND AT SIERRA 4
!!! TAKE INTO ACCOUNT THE WIND !!!

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16
Q

White arc.

A

Full flap operating range. Lower limit is Vso in landing configuration ; Upper limit is Vfe.

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17
Q

C150 Vso

A

Stalling speed or the minimum steady flight speed at wich the airplane is controlable in the landing configuration at the most forward center of gravity.

18
Q

Green arc

A

Normal operating range : Lower limit is maximum weight Vs at most forward CG without flaps. Upper limit is maximum cruising speed (Vno)

19
Q

Yellow arc

A

Operations must be conducted with caution and only in smooth air. Vno is the lower limit of yellow arc, and Vne is the upper limit.

20
Q

Red line

A

Vne.

21
Q

C150 Maneuver speed limit

A

95 KIAS

22
Q

C150 Flight Load Factors

A

Flaps Up + 4.4/-1.76 g

Flaps Down + 3.5 g

23
Q

C150 Emergencies speeds

A 
Emergency descent 143 KIAS
Best glide 60 KIAS
Approach engine inoperative 
       Flaps Up 65 KIAS
       Flaps Down 55 KIAS
24
Q

C150 GO AROUND

A

1) NOSE UP ATTITUDE
2) FULL POWER
3) FLAPS 10°
When 65 KIAS and positive vario
4) FLAPS UP

25
Q

C150 AFTER T/O CL

A

Landing Lights ……………………………………………. OFF
Flaps …………………………………………………………… UP

26
Q

C150 DESCENT AND APPROACH CL

A

Fuel Quantities…………………………………… CHECKED
Fuel Valve ……………………………………………………. ON
Mixture ……………………………………………………… RICH
Carburetor Heater ………………………………………..____
Flight instruments – Altimeters ……………………….____
Crew Briefing ………………………………… COMPLETED

27
Q

ENGINE FAILURE OVER RWY

A

1) ATTITUDE DOWN 70 KIAS

2) FULL FLAPS

28
Q

CHAT CL

A

C is for COCKPIT CLEAR
H is for HEIGHT (2000’ AGL minimum)
A is for AREA (not populated)
T is for TRAFFIC

29
Q

C150 SLOW FLIGHT without FLAPS

A

1) CARBU HEATER HOT
2) CHAT CL
3) POWER 1700 RPM
4) ALTITUDE HOLD
5) WHEN 63 KIAS, POWER 2000-2100 RPM TO HOLD 60 KIAS.
6) TRIM THE ACFT

30
Q

C150 SLOW FLIGHT with FLAPS

A

1) CARBU HEATER HOT
2) CHAT CL
3) FLAPS 10°
4) POWER 1700 RPM
5) ALTITUDE HOLD
6) WHEN 58 KIAS, POWER 2100 RPM TO HOLD 55 KIAS.
6) TRIM THE ACFT

31
Q

SPIRAL DIVE RECOVERY

A

1) IDLE and CARBU HOT
2) WINGS LEVEL
3) ATTITUDE : NOSE ON HORIZON
4) FULL POWER TO CLIMB @ 70 KIAS.

32
Q

C150 FORCED LANDING

A

FLY-FIND-FIX

1) FLY 70 KIAS, TRIM
2) FIND AIRFIELD (obstacles, surface, wind…)
3) FIX
1. PRIME : LOCKED
2. MAGNETOS : BOTH, or left or right.
3. CARBU : HOT
4. MIXTURE : RICH
5. FUEL VALVE : ON

4) SAFETY ACTIONS
1. MAYDAY CALL
2. DE-LOCK DOORS
3. BRIEF PAX
4. CHECK BELTS FASTEN
5. MAGNETOS OFF, MIXTURE CUT, FUEL VALVE OFF.
6. LEAVE BATT ON.
7. BEFORE TOUCHING : MASTER OFF

33
Q

C150 MTOW

A

1600 lbs = 727 kg.

34
Q

C150 battery voltage

A

12 V.

35
Q

C150 alt. voltage.

A

14V.

36
Q

C150 fuel system

A

2 tanks in the wings, feeding by gravity, no fuel pump,

Consumption 20L/h, 10% security = 22L/h.

37
Q

C150 vacuum driven instruments :

A

ATTITUDE INDICATOR and DIRECTIONAL GYRO.

38
Q

C150 gyroscopic instruments :

A

DG, AI and turn and bank indicator. NB turn and bank is electricaly driven and remains operative in case of vacuum pump failure.

39
Q

C150 Landing w/o elevator control procedure.

A

Trim for horizontal flight at 55 KIAS and with flaps 20°
Maintain the trim setting
Control glide angle with power only
At flare out, trim to full nose up position.
Close throttle at touchdown.

40
Q

C150 Alternator check :

A

During runup (1700 RPM) if the circuit is loaded with use of flaps motor for exemple, the ammeter must remain within a needle width of its initial position.

41
Q

C150 Stall warning

A

Occurs 5 to 10 knots before the actual stall speed is reached.

42
Q

Dead cut check

A

If magneto check fail, try to kill the engine with ignition switch, not mixture. If the engine keeps on running, at least one magneto is not grounded ! Place board to warn about “live propeller” !

Flying (4 decks)

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