Citabria 7ECA Flashcards

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1
Q

Engine Make/Model

Foreword, POH ii

A

Lycoming O-235-C1

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2
Q

Rated Horsepower (HP & RPM)

Operating Limitations, POH 1-2

A

115 HP | 2,800 RPM

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3
Q

Tachometer Range

Operating Limitations, POH 1-2

A

1,800-2,800 RPM

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4
Q

Cylinder Head Temperature Range

Operating Limitations, POH 1-2

A

90-500 ℉

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5
Q

Oil Temperature Range

Operating Limitations, POH 1-2

A

100-245 ℉

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6
Q

Oil Pressure Range

Operating Limitations, POH 1-2

A

Caution | 25-60 PSI
Normal | 60-100 PSI

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7
Q

Engine Fire at Start

Emergency Procedures, POH 2-2

A
Starter    | Continue On
Mixture    | Idle Cut-off
Throttle   | Full
-- - If Fire Persists - --
Mixture    | Idle Cut-off
Fuel Valve | Off
Ignition   | Off
Electrical | Off
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8
Q

Engine Fire in Flight

Emergency Procedures, POH 2-2

A
Mixture    | Idle Cut-off
Fuel Valve | Off
Ignition   | Off
Electrical | Off
Cabin Heat | Off
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9
Q

Electrical Fire

Emergency Procedures, POH 2-3

A
Electrical          | Off
Ignition            | On
Air Vents & Window  | Open
-- - If Fire Persists - --
=> Emergency Landing
-- - If Fire Stopped - --
Master              | On
Electrical Req.     | One-by-One
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10
Q

Alternator/Electrical Failure

Emergency Procedures, POH 2-3

A
-- - Ammeter Discharge - --
Master              | Cycle
-- - If Discharge Continues - --
Electrical Not-Req. | Off
=> Lost Comms
=> Safety Landing
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11
Q

Engine Failure on Take-Off

Emergency Procedures, POH 2-4

A
-- - If Enough Runway - --
Throttle   | Idle
-- - Tail Down - --
Brakes     | Max
-- - If Airborne - --
Elevator   | Pitch Down
Airspeed   | 65 MPH
-- - If Enough Altitude - --
Fuel Valve | On
Mixture    | Rich
Carb. Heat | On
Magnetos   | On

Trun back only above 700 FT AGL

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12
Q

Engine Restart

Emergency Procedures, POH 2-4

A
Airspeed   | 65 MPH
Ignition   | On
Mixture    | Full Rich
Fuel Valve | On
Carb. Heat | On
Primer     | Locked
-- - If No Restart - --
Adjust Any of the Above
=> Emergency Landing

Engage starter if propeller is stopped

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13
Q

Rough Engine

Emergency Procedures, POH 2-5

A
-- - RPM Decrease - --
Carb. Heat | On
Throttle   | Full
-- - RPM Decrease -> Increase - --

Keep carb. heat on as long as suspected icing conditions exist

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14
Q

Partial Power Loss

Emergency Procedures, POH 2-5

A
=> Engine Restart
=> Emergency Landing
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15
Q

High Oil Temperature

Emergency Procedures, POH 2-5

A
* Loss of Oil
* Overheating
* Failed Oil Cooler by-pass Valve
-> Low Oil Pressure
Throttle | Reduce
Airspeed | Cruise
Mixture  | Full Rich
=> Safety Landing
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16
Q

Low Oil Pressure

Emergency Procedures, POH 2-5

A
* Failed Oil Pressure Relief Valve
* Failed Oil Pump
* Loss of Oil
* Clogged Oil Line
* High Oil Temperature
* Failed gauge
=> Safety Landing
17
Q

Safety Landing

Emergency Procedures, POH 2-5

A
* Higher/Closer Pattern
* Within Gliding Distance
=> Before Landing C/L
Airspeed | 60-65 MPH
Throttle | Idle

If slipping, lower wing into the wind

18
Q

Emergency Landing

Emergency Procedures, POH 2-6

A
Airspeed   | 60-65 MPH
Trim       | Set
Mixture    | Idle Cut-off
Fuel Valve | Off
Master     | On
Emergnecy  | 121.5 | 7700
* 1,000 FT Over Ldg. Point
* 500 FT Downwind & Abeam
Electrical | Off
Airspeed   | 60-65 MPH

Three point touch-down
Remove & activate ELT

19
Q

Ditching

Emergency Procedures, POH 2-6

A
=> Emergency Landing
Door | Jettison
* Land into Wind
* Parallel to Swells on Calm Wind
* Contact Water Nose High
* Do Not Stall
20
Q

Severe Turbulence

Emergency Procedures, POH 2-7

A
Airspeed Max | 120 MPH
Airspeed Rec | 80 MPH
* Level Fligh Attitude
21
Q

Stall

Emergency Procedures, POH 2-7

A
* Aerodynamic Buffet
Ailerons | Neutral
Rudder   | Lateral Control
-- - Recovery - --
Elevator | Lower Nose
Throttle | Full
Rudder   | Lateral Control
22
Q

Spin

Emergency Procedures, POH 2-7

A

~~~
Throttle | Idle
Rudder | Full Opposite
Elevator | Slightly Forward
Neutral
Ailerons | Neutral
* Rotation Stops in 1/2-1 Turns
Rudder | Neutral
Elevator | Smooth Level
```

No full/abrupt elevator control movements

23
Q

Overstress

Emergency Procedures, POH 2-8

A
Airspeed Rec. | 60-70 MPH

No large control movements
No additional Gs

24
Q

Crosswind Take-Off

Normal Operating Procedures, POH 3-7

A
Ailerons | Into Wind
Elevator | Tail High
* Prevent Drifting
* Prevent Premature Take-Off
25
Q

Airspeeds

IAS in MPH at max gross weight

A
Vs     | 51 MPH
Rotate | 55-60 MPH
Vx     | 58 MPH
Glide  | 65 MPH
Vy     | 69 MPH
DMMS   | 72 MPH
Climb  | 75-80 MPH
Va     | 120 MPH
Vno    | 120 MPH
Vne    | 162 MPH
26
Q

Leaning

Airplane POH 3-8, Engine POH 3-4

A

Full Rich Take-off, Max continous, Climb & cruise over 75%
High elevation, Above 5,000 FT
Take-off & Climb -> Adjust for smooth operation
Lean at any altitude below 75% max power
Lean to engine roughness -> Enrich to smooth

Always enrich mixture before increasing power

27
Q

Descent Cooling

Normal Operating Procedures, POH 3-9

A
  • Maintain CHT in green
  • Avoid windmilling
28
Q

Landing with Gusty Winds

Normal Operating Procedures, POH 3-10

A
  • Increase airspeed by 5 MPH
  • Wheel landing
29
Q

Landing on Soft Fields

Normal Operating Procedures, POH 3-8

A

Three Point Landing

30
Q

Max Take-off Weight

Operating Limitations, POH 1-3

A

1650 LBS

31
Q

Fuel Capacity

Aircraft and Systems Description, POH 6-2, Servicing, POH 7-2

A
Max  | 36 GAL / 18 GAL Each
Usable | 35 GAL / 17.5 GAL Each
32
Q

Oil Capacity

Aircraft and Systems Description, POH 6-2

A

6 QTS

33
Q

Engine Oil System

Aircraft and Systems Description, POH 6-5

A

Oil Pressure and Temperature
* Controlled by engine driven pump
* Gauges with direct reading (no electrical)

34
Q

Electrical System

Aircraft and Systems Description, POH 6-8

A
  • 12V system
  • 60A engine driven alternator
  • 14+/-.5V by regulator
  • Battery discharge at low RPM
  • Cycle master to reset overvoltage relay
35
Q

Fuel System

Aircraft and Systems Description, POH 6-10

A
  • Correct fuel indication in level flight
  • Non-vented caps
  • Unsecured caps -> fuel leak
36
Q

Take-Off Performance

CAA Sup. 1, Page 5

A
  • Reduce 5% for each 5 KTS headwind
  • Increase 12% for each 2 KTS tailwind
    (max 5 KTS tailwind)
  • Increase ground roll 15% on grass
37
Q

Landing Performance

CAA Sup. 1, Page 5

A
  • Reduce 5% for each 5 KTS headwind
  • Increase 12% for each 2 KTS tailwind
    (max 5 KTS tailwind)
  • Increase ground roll 30% on grass
38
Q

Carburetor Heat

Engine POH 3-5

A

Take-Off Carb Heat Off (carb. ice very remote at wide open throttle)
Climb Throttle 80% or above, Carb Heat Off.
If Carb Heat On -> Over-Rich -> Lean to smooth op.
Cruise Carb Heat On when dump, cloudy, foggy or hazy regardless of OAT
Landing Carb Head On if icing is suspected
RPM Drop Carb Heat On and Throttle Full