FUEL GAUGES Do not take off if: Fuel gauges indicate _____ Less than _____

FUEL GAUGES In the yellow arc or \< 265 lbs each main tank.

LIMITATIONS Flashcards by Tim Lankford

MANEUVERING SPEED VA

(12,500 lbs.)

MANEUVERING SPEED VA

(12,500 lbs.)

181 KIAS

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MAXIMUM FLAP SPEEDS

Approach (40%) …… ____

Full Down (100%)….. ____

MAXIMUM FLAP SPEEDS

Approach (40%) .…. 200 KIAS

Full Down (100%) … 157 KIAS

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MAX LANDING GEAR OPERATING SPEED

(VLO/VLE)

EXTENSION …………… ____

RETRACTION …………. ____

EXTENDED …………….. ____

MAX LANDING GEAR OPERATING SPEED

(VLO/VLE)

EXTENSION ……………181 KIAS

RETRACTION …….……163 KIAS

EXTENDED ……………..181 KIAS

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MAXIMUM OPERATING SPEED

VMO ……………… ____

MMO ……………… ____

MAXIMUM OPERATING SPEED

VMO ………………. 259 KIAS

MMO ……………… 0.52 Mach

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Maximum Range Glide

135 KIAS

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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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Air Minimum Control Speed (VMCA)

86 KIAS

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Emergency Descent Airspeed

Emergency Descent

181 KIAS

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

115 KIAS

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

(BLUE LINE)

121 KIAS

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One-Engine-Inoperative Enroute Climb

121 KIAS

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CABIN PRESSURIZATION LIMIT

Max Cabin Press Differential …____

CABIN PRESSURIZATION LIMIT

Max Cabin Press Diff …… 6.6 psi

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EXTERNAL POWER LIMITS

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

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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GENERATOR LIMITS

Maximum sustained generator load is limited as follows:

Sea Level - FL310…. ____

> FL310 ………..………. ____

Ground Ops …………. ____

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:

Sea Level FL310 ….. 100%

> FL310 ……………..……88%

Ground Ops …………. 85%

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AUXILIARY FUEL

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

AUXILIARY FUEL

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

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EMERGENCY ENGINE FUELS

Comm Aviation Grades….. ____

Military Aviation Grades…. ____

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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FUEL GAUGES

Do not take off if:

Fuel gauges indicate _____
Less than _____

FUEL GAUGES

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

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.

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.

FUEL IMBALANCE

Max Structural…… _______

Autopilot …………… _______

FUEL IMBALANCE

Max Structural … 1,000 LBS

Autopilot …………. 300 lbs

FUEL CROSS-FEED

Cross-feeding of fuel is permitted:

one engine is inoperative

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.

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.

FUEL LIMITS

APPROVED ENGINE FUELS

Commercial Grades……… ____

Military Grades……………… ____

FUEL LIMITS

APPROVED ENGINE FUELS

Commercial Grades

Jet A / Jet A-1 / Jet B

Military Grades

JP-4 / JP-5 / JP-8

FUEL MANAGEMENT USABLE FUEL (Gallons x 6.7 = Pounds)

Total Usable Fuel …………… ____

Each Main Fuel Tank ……… ____

Each Auxiliary Tank ………… ____

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)

ICING LIMITATIONS

Ice Vanes Extended …………____

Ice Vanes Retracted …………____

Manual Override System…..____

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.

**ICING LIMITATIONS** ## Footnote Min Temp Operation of Deicing Boots ..\_\_\_\_ Min Airspeed Icing Flight ..........…....… \_\_\_\_ Flaps extended in icing conditions ..... \_\_\_\_

**ICING LIMITATIONS** ## Footnote Min Operation of Deicing Boots .. –40°C Min Airspeed Icing Flight ......…... 140 kts Prohibited except for approach and landings

LANDING GEAR CYCLE LIMITS

Landing gear cycles (1 up —1 down) ## Footnote Limited to: 1 every ................ 5 minutes Total ..................... 6 cycles Followed by: ...... 15-minute cool-down

**MAXIMUM OBSERVED ITT (°C)** ## Footnote STARTING................................... \_\_\_\_ TRANSIENT.................................. \_\_\_\_ TAKEOFF / MAX CONT............. \_\_\_\_ CRUISE CLIMB / (NORMAL) .... \_\_\_\_ MAXIMUM REVERSE................. \_\_\_\_

**MAXIMUM OBSERVED ITT (°C)** ## Footnote Starting ................................. 1,000°C (5 SECS) Transient ..........................…. 850°C Takeoff and Max Cont...…... 800°C Climb / (Normal) Cruise ….. 770°C Maximum Reverse .........…. 750°C

**MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS** ## Footnote Normal Operation ................... \_\_\_\_ Yaw Damp System INOP ...... \_\_\_\_

**MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS** ## Footnote Normal Operation ....... 35,000 feet Y/D INOP .. No limit - Strakes installed

**MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS** ## Footnote Sea Level - FL250 ...... \_\_\_\_ Above FL250 ............... \_\_\_\_

**MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS** ## Footnote Sea Level - FL250 ...... ISA + 37°C Above FL250 .............. ISA + 31°C

**MAX WEIGHT – BAGGAGE COMPARTMENT** ## Footnote Equipped With Fold-Up Seats ........... \_\_\_\_ Not Equipped With Fold-Up Seats ... \_\_\_\_

**MAX WEIGHT – BAGGAGE COMPARTMENT** ## Footnote Equipped With Fold-Up Seats .......... 510 lbs Not Equipped With Fold-Up Seats .. 550 lbs

**OIL PRESSURE LIMITATIONS**

**OIL PRESSURE LIMITATIONS** ## Footnote 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

**OIL TEMPERATURE** ## Footnote Starting ................................. \_\_\_\_ Takeoff / Max Cont ............ \_\_\_\_ Climb / (Normal) Cruise .... \_\_\_\_ Transient .........................….. \_\_\_\_

**OIL TEMPERATURE** ## Footnote 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)

**POWER LEVERS**

**POWER LEVERS** ## Footnote 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.)

**PROPELLER ROTATIONAL SPEED LIMITS** ## Footnote Reverse .................................. ____ rpm All Other Conditions ............. ____ rpm Transients \< 5 Seconds ....... ____ rpm

**PROPELLER ROTATIONAL SPEED LIMITS** ## Footnote Reverse ....................................... 1,900 rpm All Other Conditions ................. 2,000 rpm Transients \< 5 Seconds ........... 2,200 rpm

**PROPELLER ROTATIONAL OVERSPEED LIMITS** ## Footnote \>\_\_\_\_ 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.

**PROPELLER ROTATIONAL OVERSPEED LIMITS** ## Footnote \>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.

**PROPELLER RPM (N2)** ## Footnote Takeoff and Maximum Continuous .... \_\_\_\_ Transient ................................................... \_\_\_\_

**PROPELLER RPM (N2)** ## Footnote Takeoff / Max Continuous .... 2000 Transient ................................. 2200 (5 SECS)

**RPM (% N1)** ## Footnote Takeoff / Max Cont …... \_\_\_\_ Transient ......................... \_\_\_\_

**RPM (% N1)** ## Footnote Takeoff / Max Cont .... 101.5% Transient ..................... 102.6% [10 SECS]

**SEATS** ## Footnote AFT-FACING SEATS

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.

STARTER LIMITS

40 seconds ON 60 seconds OFF 40 seconds ON 60 seconds OFF 40 seconds ON 30 minutes OFF

**TORQUE (FT-LBS)** ## Footnote TAKEOFF / MAX CONT... \_\_\_\_ TRANSIENT.......................... \_\_\_\_

**TORQUE (FT-LBS)** ## Footnote TAKEOFF / MAX CONT .... 2,230 TRANSIENT ....................... 2,750 (5 SECS)

WEIGHT LIMITS ## Footnote Maximum Ramp Weight ........... \_\_\_\_ Maximum Takeoff Weight......... \_\_\_\_ Maximum Landing Weight ....... \_\_\_\_ Maximum Zero Fuel Weight..... \_\_\_\_

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

**WIDE WHITE ARC**

**WIDE WHITE ARC** 75 - 99 Stall speed (VSO) Max weight Full flaps Idle power