Oral Review Flashcards
Lost Comm Procedure (FAR 91.185)
If VFR, remain VFR, squawk 7600, land as soon as practical.
If IFR, squawk 7600 and fly:
Route (first that applies)
- Assigned
- Vectored
- Expected
- Filed
Altitude (whichever is highest until descent is required for landing):
- Minimum IFR Altitude
- Expected
- Assigned
To maintain IFR currency, a pilot must have made….
6 approaches and demonstrated proper holding procedures as well as radial and bearing tracking in the last 6 months.
An alternate is not required if the weather is….
is forecast at least as a 2000’ ceiling and vis of at least 3 miles from 1 hour before and after your ETA.
VA 3800 lbs
135 KIAS Maneuvering speed @ 3800 lbs
VA 2700 lbs
112 KIAS Maneuvering speed @ 2700 lbs
VNE
202 KIAS Red Line Never Exceed Speed
VNO
169 KIAS Top of Green Arc
VLE
140 KIAS Max speed with gear extended
VLO Down
140 KIAS Max gear extension
VLO Up
109 KIAS Max gear retraction
VFE
111 KIAS Top of White Arc Max Flap Extension
VYSE
88 KIAS Blue Line Best Rate of Climb Single Engine
VY
88 KIAS Best Rate of Climb
VSSE
82 KIAS Safe speed for intentional engine failure
VXSE
82 KIAS Best Angle of Climb Single Engine
VX
82 KIAS Best Angle of Climb
VR
75 KIAS Rotation
VS
57 KIAS Bottom of Green Arc Stall Speed Clean
VMC
56 KIAS Red Line MCA
VSO
55 KIAS Bottom of White Arc
BEFORE LAND CHECKLIST
Gear 3 GREEN Fuel Selector ON FLAPS 25 (VFE 111 KIAS) Mixtures FORWARD Props FORWARD Fuel Pumps ON
CRUISE CHECKLIST
POWER Set 22"/2300RPM Engine Instruments CHECK COWL FLAPS AS REQUIRED L FUEL PUMP OFF/CK PRESSURE R FUEL PUMP OFF/CK PRESSURE LANDING LIGHT OFF MIXTURES LEAN AS REQUIRED
AFTER TAKEOFF CHECKLIST
POWER 24"/2500RPM FLAPS/GEAR UP CHECK COWL FLAPS AS REQUIRED 88 (Blue Line) VY UNTIL 500' AGL 110 KIAS passing 500' 1000' REDUCE POWER TO 24"/2500 RPM
MMULTI-G-BREST
Max Power + Max Gross Weight - Un favorable CG + Landing Gear Up + Takeoff Configuration + Inoperative Engine Windmilling + Ground Effect + Bank into Operative Engine (5 degrees) - Rudder Pressure <150lbs - Exceptional Pilot Skills Standard Day + Twenty Degree Recovery
Useable Fuel
108 Gal
Critical engine
None
Propeller Feather is not possible when?
Engine RPM below 950
Landing gear is held up by…..
hydraulic pressure
squat switch is on the….
Left main gear
What does an “ALT” light indicate?
inoperative alternator
The vacuum pump is located on?
Both left and right engines
Inboard stall vane provides stall indication when…..
flaps are 25 or 40
Loss of engine causes how much climb performance?
80% because of prop drag
The gear horn will sound under what conditions?
Gear selector up position on the ground
manifold below 14”
flaps at second or third notch
Max Demonstrated X Wind Component?
17 Knots
Describe the Engines
Lycoming 0-360 180HP
air cooled
normally aspirated
direct drive
Describe the Electrical system
14 volt
12 volt battery 35 AMP
2 70 AMP Alternators
overvolt shut off at 17 volts
Describe the propeller system
Hartzell two blade controllable pitch constant speed full feather oil pressure regulates pitch forward = low pitch (high RPM) back = high pitch (low RPM) feathered nitrogen charged cylinder and springs move prop back no feather below 950 RPM
Weight X Arm =
Moment
Total Moment / Total Weight =
CG
Moment =
Weight X Arm
CG =
Total Moment / Total Weight
Max Ramp Weight - Zero Fuel Weight =
Usable Fuel Weight
Fuel Weight / 6 =
Fuel Gallons
Usable Fuel Weight =
Max Ramp Weight - Zero Fuel Weight
Oil Weight =
7.5 Lbs/Gal
Fuel Weight =
6 Lbs/Gal
Unusable Fuel =
2 gals (12 Lbs)
Max hold speed
< 6000 200 KTS
> 6000 < 14000 230 KTS
>14000 265 KTS
Hold leg time
< 14000 1 min
> 14000 1.5 min
How is approach category calculated and what are they?
1.3 VSO A = 0-90 kts B = 91 - 120 kts C = 121 - 140 kts D = 141 - 165 kts E = above 165 kts
Calculate VDP using DISTANCE
HAT/300 = Distance in NM from appraoch end of the runway
Calculate VDP using TIME
HAT/10 = Time in SECONDS to subtract from the time from FAF to MAP depicted on the chart.
Aircraft inspections: A-AVIATES
ADs - All ADs must be complied with Annual Inspection - 12 calendar months VOR check - 30 days for IFR Inspection - 100 hours if for hire Altimeter - 24 calendar months Transponder - every 24 calendar months ELT - 12 calendar months, 1/2 batt, 1 hr use Static Pitot System - 24 calendar months
Aircraft Docs ARROWE
Airworthiness Cert Registration Cert Radio License Operating Limitations (POH) Weight and Balance Equipement list
IFR Take Off mins
2 engines or less = 1 sm vis
+ 2 engines = 1/2 sm vis
Alternate Mins
Precision approach - 600/2
Non Precision approach - 800/2
No IAP - mins allow for VFR approach
Only GPS - can not use as ALT (unless WAAS)
Alternate required when….
1 hour before and after ETA weather is forecast less than 2000/s of if airport is VFR only
MMULTI-G-BREST
Max Power + Max Gross Weight - Un favorable CG + Landing Gear Up + Takeoff Configuration + Inoperative Engine Windmilling + Ground Effect + Bank into Operative Engine (5 degrees) - Rudder Pressure <150lbs - Exceptional Pilot Skills Standard Day + Twenty Degree Recovery
Useable Fuel
108 Gal
Critical engine
None
Propeller Feather is not possible when?
Engine RPM below 950
Landing gear is held up by…..
hydraulic pressure
squat switch is on the….
Left main gear
What does an “ALT” light indicate?
inoperative alternator
The vacuum pump is located on?
Both left and right engines
Inboard stall vane provides stall indication when…..
flaps are 25 or 40
Loss of engine causes how much climb performance?
80% because of prop drag
The gear horn will sound under what conditions?
Gear selector up position on the ground
manifold below 14”
flaps at second or third notch
Max Demonstrated X Wind Component?
17 Knots
Describe the Engines
Lycoming 0-360 180HP
air cooled
normally aspirated
direct drive
Describe the Electrical system
14 volt
12 volt battery 35 AMP
2 70 AMP Alternators
overvolt shut off at 17 volts
Describe the propeller system
Hartzell two blade controllable pitch constant speed full feather oil pressure regulates pitch forward = low pitch (high RPM) back = high pitch (low RPM) feathered nitrogen charged cylinder and springs move prop back no feather below 950 RPM
Weight X Arm =
Moment
Total Moment / Total Weight =
CG
Moment =
Weight X Arm
CG =
Total Moment / Total Weight
Max Ramp Weight - Zero Fuel Weight =
Usable Fuel Weight
Fuel Weight / 6 =
Fuel Gallons
Usable Fuel Weight =
Max Ramp Weight - Zero Fuel Weight
Oil Weight =
7.5 Lbs/Gal
Fuel Weight =
6 Lbs/Gal
Unusable Fuel =
2 gals (12 Lbs)
Max hold speed
< 6000 200 KTS
> 6000 < 14000 230 KTS
>14000 265 KTS
Hold leg time
< 14000 1 min
> 14000 1.5 min
How is approach category calculated and what are they?
1.3 VSO A = 0-90 kts B = 91 - 120 kts C = 121 - 140 kts D = 141 - 165 kts E = above 165 kts
Calculate VDP using DISTANCE
HAT/300 = Distance in NM from appraoch end of the runway
Calculate VDP using TIME
HAT/10 = Time in SECONDS to subtract from the time from FAF to MAP depicted on the chart.
Aircraft inspections: A-AVIATES
ADs - All ADs must be complied with Annual Inspection - 12 calendar months VOR check - 30 days for IFR Inspection - 100 hours if for hire Altimeter - 24 calendar months Transponder - every 24 calendar months ELT - 12 calendar months, 1/2 batt, 1 hr use Static Pitot System - 24 calendar months
Aircraft Docs ARROWE
Airworthiness Cert Registration Cert Radio License Operating Limitations (POH) Weight and Balance Equipement list
IFR Take Off mins
2 engines or less = 1 sm vis
+ 2 engines = 1/2 sm vis
Alternate Mins
Precision approach - 600/2
Non Precision approach - 800/2
No IAP - mins allow for VFR approach
Only GPS - can not use as ALT (unless WAAS)
Alternate required when….
1 hour before and after ETA weather is forecast less than 2000/s of if airport is VFR only
At least one of the following visual references required for decent from MDA….
- Approach lighting system
- Threshold
- Threshold Markings
- Threshold Lights
- Runway end identifier lights (REIL)
- Visual approach slope indicator (VASI)
- Touchdown zone or markings
- Touchdown zone lights
- Runway or Runway markings
- Runway lights
