310 QUIZ Flashcards
What model, type and horsepower are the engines on the 310?
Model–IO520MB
Type–Fuel injected, direct drive, aircooled, horizontally opposed, 6 cylinder, 520 cubic inch
Horsepower–285 hp @ 2700 rpm
What is the height, width, and length of 310?
H - 11 feet / W - 37 feet / L - 32 feet
What is the normal prop tip ground clearance?
Less than 1 foot
What type of props are on the 310?
Constant speed, full feathering, non reversing, hydraulically actuated.
What type of fuel does our 310 use?
100 AV FUEL (green) 100 LowLead (blue)
Max weight capacity of nose baggage compartment?
350 pounds
Max ramp weight?
5725 pounds
Max Take off weight?
5680 pounds
Max landing weight?
5400 pounds
What is the max luggage weight for the aft baggage (station 126)?
160 pounds
What is the total fuel capacity of our 310, how many tanks and their respective quantities?
183 gallons total
5 tanks – (2) Main/Tip tanks=50 gallons each, (2) Aux tanks=31.5 gallons each, (1) Nacel tank=20 gallons
What is the total Oil Capacity of each engine?
13 quarts (1 quart for the oil fliter)
What is the minimum oil capacity to operate?
9 quarts
What is the Vmc airspeed for the 310?
Vmc-80
What is Vy (blueline) airspeed for the 310?
Vy 106 kts
What is the Vne (never exceed) airspeed for the 310?
Vne - 223 kts
What is the Vr (rotate) airspeed for the 310?
Vr - 92 kts
What is Vbg (best glide-dual engine failure) airspeed for the 310?
Vbg - 111 kts
What is the normal operating range for the Tachometer?
2100 -2500 (green arc)
What is the normal operating range for the manifold pressure gauge?
15.0 - 24.5 inches of Hg (green arc)
What is the Max Oil Pressure?
100 PSI
What is the Max Oil Temp?
240 Degrees (red line)
What is the Max Cylinder Head Temp?
460 Degrees F (red line)
What is the minimum Fuel Flow?
2.5 PSI
How many emergency exits, and where are they located?
2 - Entry door and left pilot side window
What is the fuel capacity of the left AUX tank?
31.5 gallons
Which tanks MUST be selected during take off and landing?
MAINS/TIPS
What are the emergency procedures for Engine Failure before takeoff?
A) Throttles – Close immediately
B) Brakes or Land and brakes
What are the Emergency Procedures for Engine Failure after takeoff?
A) Mixture, Props, Throttles - full forward
B) Gear up
C) identify INOP Engine
D) For Inop Engine (throttles/mixture closed, prop feather)
What is an important flight consideration when flying on 1 engine?
Establish 5 degree bank into OP engine, no more than 10 degrees bank into INOP engine during any turn
What are the Emergency Procedures for both engines failing in cruise?
Wings flaps up, landing gear up, Props to feather…minimum airspeed…111 kts
What are the emergency procedures for ground fire on the ground?
If possible move aircraft off the fire, brake, both throttles closed, both mixtures idle cutoff, batteries off, mags off, GET OUT.
What are the emergency procedures for engine fire inflight?
1) AUX fuel pumps off B) Secure Engine with fire I. THROTTLES CLOSED II. MIXTURE CUT OFF III. PROP FEATHER IV. FUEL SELECTOR OFF
What are the emergency procedures for inflight cabin fire?
A) Electrical load reduced/minimized
B) Attempt to isolate the source of fire/smoke
C) Wemacs open
D) cabin Air Controls Open all vents (close if increased air flow make smoke worse)
What are emergency procedures for emergency descent?
A) Throttles - idle, Props - Full Forward, Mixtures - adjust as needed
B) Wing flaps UP
C) Landing gear UP
D) Moderate bank initiated
What are the emergency procedures for a Spin?
A) Throttles closed
B) Ailerons neutralized
C) Rudder full opposite direction of spin
D) Yoke push forward until spin stops - neutralize rudder once soin stops
E) Yoke pull back to recover from the dive
A Main tire blows out during takeoff (above Vr), on climb out, what should a pilot NOT DO?
Retract the gear
What memorization items are there on the Landing Gear will not extend?
NONE - refer to the AFM - Chapter 3-29 and follow check list
FYI–Announce PAN-PAN-PAN to controlers to troubleshoot. If gear extension continues to fail without solution, declare an emergency before landing
What is the Max Demo Crosswind Velocity
19 kts
When using external power source (EPU), DO NOT turn on these switches until EDU is removed to avoid damage?
The batteries and alternators
During prop feathering checks at run up, do not allow the RPMs to fall below ______ RPMs?
1000 RPMs
What are the max and min allowable suction ranges on the instrument?
4.75 - 5.25 inches Hg
What is lift off speed?
92 kts
What is the cruise climb settings for the 310?
2500 RPM and 24.5 inches Hg
With an obstacle ahead requiring steep climb angle, what speed with flaps up gear up should the aircraft be flown?
Vx - 85 kts sea level
89 kts at 15000 feel
Make sure the aircraft does not exceed _______ pounds before attempting to land?
5400 pounds
The Pitot Heat switch should be turned “ON” at least ______ minutes before entering potential icing conditions?
5 minutes inflight
2 minutes on the ground
What is the empty weight of the 310?
3876 pounds
How often must our 310 be weighed?
Every 3 years or after addition or removal of equipment
What is the zero-fuel weight of the 310?
4900 pounds
What are described as the flight controls on the 310?
Ailerons, elevator, rudder, and trim systems
The ailerons trim is located on which side?
Left
What type of system are the ailerons and elevator?
Push pull rod attached to bell crank
How are the wing flaps powered?
Electric
Can the landing gear be retracted on the ground?
No - a squat switch is located on the left landing gear shock strut…when aircraft weight is on switch it cuts power to landing gear retraction
If the landing gear emergency hand-crank is not stowed in its clip, what condition will prevail?
The gear will not operate normally electrically.
How many detents (selections) can the 310 fuel selectors provide, and what are they?
4 – main, aux, cross feed, no fuel (off)
How are the brakes powered?
Hydraulics
What type of electrical system does the 310 have?
28 volt, negative ground, DC system. a 24 volt battery, (2) 100 amp alternators
“Low Voltage”light illuminates when the airplane bus voltage falls below ______ volts?
25 volts
What setting should be selected on an external power source (EDU) before using it on the 310?
28 volts
When the Pitot Heat Switch is turned “ON”, what items are heated?
Pitot tube, Stall warning vane, & optional wing locker fuel vents
How will a failed vacuum pump be alarmed/signaled to the pilot?
A red button will pop out on the suction gauge
At what point will a stall warning horn sound?
5 to 10 kts above the stall
Where is the gas fired heater located in the 310?
Nose compartment
What type of props are on the 310?
All-metal, 3 bladed, constant speed, full feathering, single acting, governor regulated
What inspections are required on our 310?
100 hour and annual
What items are to be displayed in the aircraft at all times?
Airworthiness Cert, Aircraft Registeration, Radio License
What items are to he carried at all times?
W&B, Equipment List, POH/AFM, Pilot check list
How and in what order do the de-ice boots system work?
Manual switch activated, tail boots activated for 6 seconds first, then the wing boots activated for 6 seconds, then the switch springs back to off
When should Deice Boots be activated?
When ice accumulates between 1/4 to 1/2 inch
When should the heated windshield be activated?
On the ground–for brief electrical test
Inflight–before entering visible moisture with O.A.T. below 40F
Is our 310 Certified for Flight into Known Icing?
Yes
What equipment is required to be Certified for Known Ice?
Wing boots (inboard and outboard) and Rudder/Elevator Deice Boots, Windshield Heat, Dual 100 amp alternator, Heated Pitot Tube, Stall Warning Heat, Prop Heat
Read chapter 7 of POH before
TEST DAY.
310 and 414