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FENIX B-200 > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

MANEUVERING SPEED VA

(12,500 lbs.)

A

MANEUVERING SPEED VA

(12,500 lbs.)

181 KIAS

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2
Q

MAXIMUM FLAP SPEEDS

Approach (40%) …… ____

Full Down (100%)….. ____

A

MAXIMUM FLAP SPEEDS

Approach (40%) .…. 200 KIAS

Full Down (100%) … 157 KIAS

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3
Q

MAX LANDING GEAR OPERATING SPEED

(VLO/VLE)

EXTENSION …………… ____

RETRACTION …………. ____

EXTENDED …………….. ____

A

MAX LANDING GEAR OPERATING SPEED

(VLO/VLE)

EXTENSION ……………181 KIAS

RETRACTION …….……163 KIAS

EXTENDED ……………..181 KIAS

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4
Q

MAXIMUM OPERATING SPEED

VMO ……………… ____

MMO ……………… ____

A

MAXIMUM OPERATING SPEED

VMO ………………. 259 KIAS

MMO ……………… 0.52 Mach

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5
Q

Maximum Range Glide

A

Maximum Range Glide

135 KIAS

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6
Q

NARROW WHITE ARC

A

NARROW WHITE ARC

99 to 157

Lower limit - Stall speed (VS) at max weight flaps up / idle power.

Upper limit - Max speed permissible flaps extended beyond Approach (40%).

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7
Q

Air Minimum Control Speed (VMCA)

A

Air Minimum Control Speed (VMCA)

86 KIAS

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8
Q

Emergency Descent Airspeed

A

Emergency Descent

181 KIAS

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9
Q

One-Engine-Inoperative Best Angle-of-Climb (VXSE)

A

115 KIAS

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10
Q

One-Engine-Inop Best Rate-of-Climb (VYSE)

(BLUE LINE)

A

121 KIAS

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11
Q

One-Engine-Inoperative Enroute Climb

A

One-Engine-Inoperative Enroute Climb

121 KIAS

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12
Q

CABIN PRESSURIZATION LIMIT

Max Cabin Press Differential …____

A

CABIN PRESSURIZATION LIMIT

Max Cabin Press Diff …… 6.6 psi

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13
Q

EXTERNAL POWER LIMITS

Set to _____ volts Capable of generating a minimum of ____ amps momentarily and ____ amps continuously.

A

EXTERNAL POWER LIMITS

Set to 28.0–28.4 volts Capable of generating a minimum of 1000 amps momentarily and 300 amps continuously

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14
Q

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:

Sea Level - FL310…. ____

> FL310 ………..………. ____

Ground Ops …………. ____

A

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:

Sea Level FL310 ….. 100%

> FL310 ……………..……88%

Ground Ops …………. 85%

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15
Q

AUXILIARY FUEL

Do not put any fuel into the ____ tanks unless the ____ tanks are full.

A

AUXILIARY FUEL

Do not put any fuel into the auxiliary tanks unless the main tanks are full

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16
Q

EMERGENCY ENGINE FUELS

Comm Aviation Grades….. ____

Military Aviation Grades…. ____

A

EMERGENCY ENGINE FUELS

COMMERCIAL

  • 80, 80/87 (Red)
  • 91/98 • 100/130 (Green)
  • 100LL Blue - In some countries colored green and designated “100L.”

MILITARY

  • 115/145 Purple
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17
Q

FUEL GAUGES

Do not take off if:

  • Fuel gauges indicate _____
  • Less than _____
A

FUEL GAUGES

  • In the yellow arc or
  • < 265 lbs each main tank.
18
Q

FUEL

OPERATING WITH LOW FUEL PRESSSURE

Operation of either engine with its corresponding fuel pressure annunciator (L / R FUEL PRESS) (ILLUM) limited to ______ before overhaul or replacement of the engine-driven fuel pump.

NOTE: Wind-milling time need not be charged against this time limit.

A

FUEL

Operation of either engine with its corresponding fuel pressure annunciator (L / R FUEL PRESS) illuminated limited to 10 hours before overhaul or replacement of the engine-driven fuel pump.

NOTE: Wind-milling time need not be charged against this time limit.

19
Q

FUEL IMBALANCE

Max Structural…… _______

Autopilot …………… _______

A

FUEL IMBALANCE

Max Structural … 1,000 LBS

Autopilot …………. 300 lbs

20
Q

FUEL CROSS-FEED

Cross-feeding of fuel is permitted:

A

one engine is inoperative

21
Q

EMERGENCY ENGINE FUELS

Limitations on the Aviation Gasoline:

__ hours between engine overhauls.

__ or below if either STBY pump INOP.

X-feed required for climbs above ___.

Operation above ____ prohibited.

A

AIRSPEEDS

  • 150 hours between engine overhauls.
  • FL200 or below if either STBY pump INOP.
  • X-feed capability required for climbs above FL200.
  • Above FL310 is prohibited.
22
Q

FUEL LIMITS

APPROVED ENGINE FUELS

Commercial Grades……… ____

Military Grades……………… ____

A

FUEL LIMITS

APPROVED ENGINE FUELS

Commercial Grades

Jet A / Jet A-1 / Jet B

Military Grades

JP-4 / JP-5 / JP-8

23
Q

FUEL MANAGEMENT USABLE FUEL (Gallons x 6.7 = Pounds)

Total Usable Fuel …………… ____

Each Main Fuel Tank ……… ____

Each Auxiliary Tank ………… ____

A

FUEL MANAGEMENT USABLE FUEL (Gallons x 6.7 = Pounds)

Total Usable Fuel …….. 3645 lbs (544 gal)

Each Main Fuel Tank … 1,293 lbs (193 gal)

Each Auxiliary Tank …… 529 lbs (79 gal)

24
Q

ICING LIMITATIONS

Ice Vanes Extended …………____

Ice Vanes Retracted …………____

Manual Override System…..____

A

ICING LIMITATIONS

EXT - =< +5°C

RET - All Takeoff / Flight > +15°C.

ICE VANE EMERG MANUAL EXT - Once activated do not operate electrically until override assembly has been properly reset on ground.

NOTE: Even after the manual extension handle has been pushed back in, the manual override system is still engaged.

25
Q

ICING LIMITATIONS

Min Temp Operation of Deicing Boots ..____

Min Airspeed Icing Flight ……….…….… ____

Flaps extended in icing conditions ….. ____

A

ICING LIMITATIONS

Min Operation of Deicing Boots .. –40°C

Min Airspeed Icing Flight ………… 140 kts

Prohibited except for approach and landings

26
Q

LANDING GEAR CYCLE LIMITS

A

Landing gear cycles (1 up —1 down)

Limited to:

1 every ……………. 5 minutes

Total ………………… 6 cycles

Followed by: …… 15-minute cool-down

27
Q

MAXIMUM OBSERVED ITT (°C)

STARTING…………………………….. ____

TRANSIENT……………………………. ____

TAKEOFF / MAX CONT…………. ____

CRUISE CLIMB / (NORMAL) …. ____

MAXIMUM REVERSE…………….. ____

A

MAXIMUM OBSERVED ITT (°C)

Starting …………………………… 1,000°C (5 SECS)

Transient ……………………..…. 850°C

Takeoff and Max Cont……… 800°C

Climb / (Normal) Cruise ….. 770°C

Maximum Reverse …………. 750°C

28
Q

MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS

Normal Operation ………………. ____

Yaw Damp System INOP …… ____

A

MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS

Normal Operation ……. 35,000 feet

Y/D INOP .. No limit - Strakes installed

29
Q

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS

Sea Level - FL250 …… ____

Above FL250 …………… ____

A

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS

Sea Level - FL250 …… ISA + 37°C

Above FL250 ………….. ISA + 31°C

30
Q

MAX WEIGHT – BAGGAGE COMPARTMENT

Equipped With Fold-Up Seats ……….. ____

Not Equipped With Fold-Up Seats … ____

A

MAX WEIGHT – BAGGAGE COMPARTMENT

Equipped With Fold-Up Seats ………. 510 lbs

Not Equipped With Fold-Up Seats .. 550 lbs

31
Q

OIL PRESSURE LIMITATIONS

A

OIL PRESSURE LIMITATIONS

60-85 psi - < 1100 ft-lb torque.

< 60 psi - Engine shut down, or land at the nearest suitable airport

NOTE: Minimum power +/- 10 psi fluctuations are acceptable

32
Q

OIL TEMPERATURE

Starting …………………………… ____

Takeoff / Max Cont ………… ____

Climb / (Normal) Cruise …. ____

Transient …………………….….. ____

A

OIL TEMPERATURE

Starting ………………….. –40°C (Min)

Takeoff / Max Cont …. 0°– 99°C

(Min +55°C recommended for fuel heater operation at T/O power)

Climb / Cruise …………. 0°– 99°C

Transient. …………………. 0°– 104°C

(Values > 99°C limited to 10 minutes)

33
Q

POWER LEVERS

A

POWER LEVERS

Do not lift power levers in flight.

(Lifting the power levers in flight, or moving the power levers in flight below the flight idle position, could result in a nose-down pitch and a descent rate leading to aircraft damage and injury to personnel.)

34
Q

PROPELLER ROTATIONAL SPEED LIMITS

Reverse ……………………………. ____ rpm

All Other Conditions …………. ____ rpm

Transients < 5 Seconds ……. ____ rpm

A

PROPELLER ROTATIONAL SPEED LIMITS

Reverse ………………………………… 1,900 rpm

All Other Conditions …………….. 2,000 rpm

Transients < 5 Seconds ……….. 2,200 rpm

35
Q

PROPELLER ROTATIONAL OVERSPEED LIMITS

>____ RPM - Failure of the primary governor.

____ RPM Torque limited to 1,800 ft-lbs.

>____ RPM Unapproved.

[Indicates failure of both primary and secondary governor.]

____ RPM (5 Secs) - Max propeller overspeed limit.

A

PROPELLER ROTATIONAL OVERSPEED LIMITS

>2000 RPM - Failure of the primary governor.

2000-2080 RPM - Torque limited to 1,800 foot-lbs.

>2080 RPM - Unapproved.

[Indicates failure of both primary and secondary governor.]

2200 RPM (5 Secs) - Max overspeed limit.

36
Q

PROPELLER RPM (N2)

Takeoff and Maximum Continuous …. ____

Transient …………………………………………… ____

A

PROPELLER RPM (N2)

Takeoff / Max Continuous …. 2000

Transient …………………………… 2200 (5 SECS)

37
Q

RPM (% N1)

Takeoff / Max Cont …… ____

Transient ……………………. ____

A

RPM (% N1)

Takeoff / Max Cont …. 101.5%

Transient ………………… 102.6% [10 SECS]

38
Q

SEATS

AFT-FACING SEATS

A

SEATS

  • Must be placarded on the leg cross member.
  • If occupied, seatback must be in the upright position for takeoff / landing.
  • The headrest should be positioned properly.
39
Q

STARTER LIMITS

A

40 seconds ON 60 seconds OFF

40 seconds ON 60 seconds OFF

40 seconds ON 30 minutes OFF

40
Q

TORQUE (FT-LBS)

TAKEOFF / MAX CONT… ____

TRANSIENT…………………….. ____

A

TORQUE (FT-LBS)

TAKEOFF / MAX CONT …. 2,230

TRANSIENT ………………….. 2,750 (5 SECS)

41
Q

WEIGHT LIMITS

Maximum Ramp Weight ……….. ____

Maximum Takeoff Weight……… ____

Maximum Landing Weight ……. ____

Maximum Zero Fuel Weight….. ____

A

Maximum Ramp Weight …….. 12,590 pounds

Maximum Takeoff Weight ….. 12,500 pounds

Maximum Landing Weight …. 12,500 pounds

Maximum Zero Fuel Weight . 11,000 pounds

42
Q

WIDE WHITE ARC

A

WIDE WHITE ARC

75 - 99

Stall speed (VSO)

Max weight

Full flaps

Idle power

FENIX B-200 (5 decks)

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