BE-350 Flashcards
Max takeoff weight
15,000 lbs
Maximum ramp weight
15,100 lbs
Max landing weight
15,000 lbs
Max zero fuel weight
12,500 lbs
Prohibited maneuvers
Acrobatic maneuvers, including spins
Flaps up G limits
3.1 Positive, 1.24 negative
Flaps down G limits
2.0 positive, 0 negative
Maximum part 91 occupancy
15 passengers
What is the restriction on aft-facing seats on takeoff and landing
The seatback and headrest of each occupied aft-facing seats must be in the full upright position.
Max operating altitude
35,000 ft
Max operating alt with yaw damper inoperative
5000 ft
The yaw damp works. When does it need to be engaged by?
5000 ft
Max altitude with either standby fuel pump inoperative
Flight is prohibited (sorry)
Max altitude with no cross feed capability
20,000 ft
Max operating air temp limits from sea level to 25,000 ft PA
ISA + 37 C
Max operating air temp limits from above 25,000 ft PA
ISA + 31 C
Minimum operating air temp limit
-53.9 C
Maximum cabin pressure differential
6.6 psi
Maneuvering speed
184 KIAS
Approach flaps extension speed
202 KIAS
Full flaps extension speed
158 KIAS
Max Landing gear extension speed
184 KIAS
Max Landing gear retraction speed
166 KIAS
Max landing gear speed with gear fully extended
184 KIAS
Min control speed (Vmca) flaps up
94 KIAS
Min control speed (Vmca) flaps approach
93 KIAS
Max operating speed (SL to 21,000 ft)
263 KIAS
Max operating speed (21,000 to 35,000 ft)
263-194 / .58M
Max ITT for start
1000 C for 5 seconds maximum
Normal oil pressure for start
0-200 psi
Normal oil temp for start
-40 C minimum
Max ITT for idle
750 C for 5 seconds max
Idle N1
62% (min)
Idle prop RPM
1050 (min)
Idle oil pressure
60 psi (min)
Idle oil pressure
-40 to 110 C
Torque (takeoff and max continuous)*
100
*inadvertent excursions up to 102% is time limited to 7 minutes.
Max ITT (takeoff, max continuous, and max cruise)
820 C
Max N1 (takeoff max continuous, cruise climb, max cruise, and transient)
104%
Max prop RPM (takeoff, max continuous, cruise climb, max cruise)*
1700 RPM
*Excursions up to 1735 are limited up to 7 minutes
Oil pressure range (all phases except for start, idle, and max reverse)*
0 to 110 psi
*fluctuations +/- 10psi are acceptable
Max transient torque*
156%
*time limited to 20 seconds
Max cruise climb ITT
785 C
Max reverse ITT
760 C
Max transient ITT*
850
*time limited to 20 seconds
Max reverse prop RPM
1650
Max transient prop RPM*
1870
*time limited to 20 seconds
Max transient oil pressure
200 psi
Max reverse oil temp
0-99 C
When the prop RPM is below 1000psi, what is torque limited to?
62% N1
Oil pressure under 90 PSI is ________. Under emergency conditions, to complete a flight, a lower oil px of __ psi is permissible at power not exceeding __% torque.
Undesirable; 60psi, 62% N1
Min oil temp of __C recommended for few heater option at takeoff power.
55 C
Oil tank capacity per engine
Approx 14 quarts
Oil that can be drained per engine
Approx 11 quarts
What is the propeller type? 5 things
Constant-speed, Full feathering, Reversing Counter-weighted Hydraulically-actuated
Propeller RPM transient
1870 RPM for 20 seconds max
What does sustained prop order speed faster than 1700 RPM indicate?
Failure of the primary governor.
Flight with a failed primary governor can continue as long as…
Prop over speeds do no exceed 1768 RPM and torque doesn’t exceed 96% N1. Sustained prop over speeds fastere than 1768 RPM are not approved.
When must prop autofeather be armed?
For takeoff, climb, and approach.
Emergency exits must be unlocked prior to _______.
Takeoff
Do not _____ power levers in flight.
Lift
Can the aircraft be towed with the control locks installed?
No
Do not tow the aircraft if one or more ____ ___ _____ are deflated.
Landing gear struts.
Fuel quantity yellow arc
0-265 lbs
Pneumatic pressure green arc range
12 to 20 psi
Vacuum gauge (normal from 35K to 15K ft)
2.8 to 4.3 inches HG
Vacuum gauge wide green arc (normal from 15K to Sea Level)
4,3 to 5.9 inches HG
Prop device ammeter normal range
26 to 32 amps
Max weight in baggage compartment
550 lbs
Max demonstrated crosswind
20 knots
Max tailwind component for takeoff and landing
10 knots
The MFD must be operational prior to _______.
Engine start
Minimum autopilot engage height after takeoff is ___
400 AGL
Minimum autopilot use height during cruise
1000 ft AGL
Minimum autopilot use height during approach
79 ft AGL
Minimum autopilot use height during steep approach
160 ft AGL
Yaw damper must not be used for ___________
Take off and landing
The terrain awareness and display must be inhibited by selecting _____ ______ when within __ NM of takeoff, approach, or landing at an airport not contained in the EGPWS airport database.
TERR INHIBIT; 15 NM
The area within the scan arc and within __ ft of the BE-350 operating weather radar can be dangerous. Do not operate in any moded other than STBY or TEST when a person in that range.
2 ft
External power unit voltage output.
28 to 28.4 VDC
External power unit amperage output
300 amps continuous
External power unit amp surge capability
1000 amp surge
Max generator load (sea level to 34000 ft)
100%
Max generator load (above 34,000 ft)
95%
62-70% N1 (Ground operations) max generator load
75%
70 to 100% N1 (Ground operations) max generator load
100%
Starter Limitation- standard start cycle
30 secs ON, 5 mins OFF
30 secs ON, 5 mins OFF
30 secs ON, 30 mins OFF
What phases of flights must the rudder boost be on for?
All phases of flight
When using recommended engine fuels, __ standby pump(s) is required for takeoff, but in such a case, cross feed of fuel _____ (will/will not) be available from the side of the inoperative standby fuel pump.
1 standby pump; will not
When is cross feed permitted?
Only when one engine is inoperative.
When is crossfeed capability for flight above 20,000 ft required?
When operating on emergency fuels.
In what order must you fuel up the gas tanks?
Mains full and then the auxiliary tanks
Lathing with low fuel pressure is limited to __ hours before overhaul of the __________ is required.
10; engine driven fuel pump
Maximum allowable fuel imbalance
300 lbs
Total usable fuel quantity
3611 lbs
Each main fuel tank capacity
1273 lbs
Each aux tank capacity
533 lbs
When should left and right anti-ice be on?
When in ambient temperatures of +5 C or below when flight free of visible moisture cannot be assured
Min temp for de-ice boots
-40 C
Do not operate the brake de-ice above what temp?
15 C
The cabin shall not be pressurized during what phases of flight?
Takeoff and landing
When should you not operate the electric heat (hint: it’s not a temp limit)
When the pedestal floor outlet is blocked or the cockpit door is closed.
Landing gear cycle limits
1 up and 1 down cycle is limited to 1 every 5 minutes for a total of 6 cycles, followed by a 15 minute cool-down period
L/R OIL PRES LO annunciator
Indicates engine oil pressure is below 60 psi. Oil pressure between 60-90 is undesirable; tolerate only to the completion of the flight. Do not exceed 62% torque.
L/R CHIP DETECT light
Indicates possible metal contamination in the forward gear reduction case oil supply
L/R IGNITION ON light
Indicates the start switch is on and that the auto ignition system is armed and engine torque is below 17%
L/R PROP PITCH light
Designated prop is below the flight idle stop
PROP GND SOL
Indicates that the prop ground idle stop solenoid has failed. One or both props won’t decrease to ground idle upon touchdown resulting in an increase in drag and possible yawing
L/R AUTOFEATHER light
Indicates that the designated autofeather is armed and power levers are above approx 90% N1
L/R GEN light
Designated generator is offline
L/R GEN TIE OPEN
Indicates that the designated bus is isolated from the center bus
MAN TIES CLOSE light
Indicates generator bus ties have been manually closed
BAT TIE OPEN light
Indicates that the battery is isolated from the gen buses
L/R FUEL PRESS LOW light
Indicates that fuel pressure is below approx 10 psi
L/R NO FUEL XFR light
Indicates motive flow pressure is lost while fuel remains in the aux tank on the same side.
FUEL CROSSFEED light
Indicates that the CROSSFEED valve is in the selected position
L/R FUEL QTY
Illumination indicates that the designated side has less than 30 minutes of fuel remaining at max continuous power
Illumination of a light in the gear handle means 1 of 5 things:
- Landing gear in transit
- One or more gear not down and locked
- One or more gear not fully retracted
- Gear up but power back below 84-86% N1
- Gear up but flaps extended beyond approach
LDG/TAXI LIGHT annunciator on
Means that the gear is up but the taxi lights are still on
CABIN ALTITUDE light
Indicates that cabin altitude exceeds 10,000 ft
CABIN ALT HI (warning)
Indicates that cabin pressure altitude exceeds 12,000 ft
CABIN DIFF HI (warning)
Indicates cabin differentiate exceeds 6.9 psi
L/R BLEED FAIL warning light
Indicates melted or failed plastic bleed air failure warning line. They may also momentarily illuminate during simultaneous wing boot and brake de-ice operation at low N1 speed
DUCT OVERTEMP caution
Floor distribution air duct has reached 300 F
