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84 Cards in this Set
- Front
- Back
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Vmo |
236 |
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Vo |
158 (9921Lbs) 137 (7500Lbs) |
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Flaps 15 |
163 |
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Flaps 30 & 40 |
130 |
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Vlo |
177 |
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Vle |
236 |
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Vs |
91 |
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Vso |
64 |
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Best Glide |
114 (9921Lbs) |
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Vx |
110 |
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Vy |
120 |
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Landing Gear Emergency Extension |
110 |
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Max Demonstrated Crosswind Flaps 0 Flaps 15 Flaps 30 Flaps 40 |
Flaps 0 .............................................................30 Flaps 15 .......................................................... 25 Flaps 30 .......................................................... 20 Flaps 40 .......................................................... 15 |
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Ice on airframe limitations |
Climb speed/ Ice Mode/ Flaps 0...................... 130 Approach speed/ Flaps 15 .............................. 108 Approach speed/ Boot failure ........................ 134 Max flaps operative boots ...................... Flaps 15 Max flaps inoperative boots ..................... Flaps 0 |
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Max Ramp Weight |
9965Lbs |
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Max Takeoff Weight |
9921Lbs |
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Max Landing Weight |
9921Lbs |
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Max Zero Fuel Weight |
9039Lbs |
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Max Baggage Weight |
400Lbs |
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Wing Span |
53ft 3in |
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Aircraft Length |
47ft 3 in |
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Tail Height |
14ft |
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Max Operating Altitude |
FL 300 |
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Max number of PAX (Including Pilots) |
9 |
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Max Fuel Capacity |
406.8 Gal / 2,736 Lbs |
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Usable Fuel |
402 Gal / 2,703 Lbs |
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Max Fuel Imbalance |
178 Lbs / 3 LCD Segments |
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Fuel Low CAWS |
134 Lbs |
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Max Cabin Differential |
5.75 Psi (Yellow Arc) |
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Safety Valve Operation |
6.35 Psi |
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Cab Press CAWS |
6.5 Psi (Red Line) |
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Power Plant |
PT6A-67B |
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Min Oil Qty |
1 to 2 Qts below Max Hot/Cold |
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Max T/O ITT |
800C (5 Min) |
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Max Continuous ITT |
760C (750C TW Ops) |
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Max Transient ITT |
870C (20 Secs) |
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Max Start ITT |
1000C (20Secs) |
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Max Residual ITT for Start |
150C |
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Max T/O Torque |
44.3 PSI (5Min) |
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Max Continuous Torque |
36.9 Psi |
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Max Transient Torque |
61 Psi (20 Secs) |
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Min NG for Start |
13% |
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Max NG |
104% |
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Starter Limits |
1st Start Sequence .............................. 60 Secs OFF2nd Start Sequence ............................ 60 Secs OFF3rd Start Sequence ............................. 30 Mins OFF |
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Max Prop RPM |
1700 RPM |
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Overspeed Governor |
1802 RPM |
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Nf Governor |
1853 RPM |
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Min Prop RPM on the ground |
950 RPM |
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Autopilot Minimum Use Heights |
Normal Operations .................... Below 1000ft AGLILS Approaches ........................... Below 200ft AGL |
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Electrical System |
GEN 1 ........... 28V 300Amp (450Amp for 2 Mins)GEN 2 ........................................ 28V 115AmpBattery....................................... 24V 42 Amp/Hr EPS............................................. 24V 5 Amp/HrMin Volt for Batt Start .................... 24V GPU Output ...............500Amp min for all systemsGPU Output .............. 1000Amp min for start |
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TRIM RUNAWAY |
TRIM INTERRUPT Switch .............................. INTRCB of failed trim ............................................ PullTRIM INTERUPT Switch ................................ NORMIf main stabilizer trim has failed Pitch Trim .................. use ALTERNATE STAB TRIM |
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CAB PRESS CAWS |
Headset ............................................... REMOVEOxygen Mask ...................................... ONHeadset ............................................... BACK ON Aircraft MSN 321 and 401-500 Disconnect normal headset boom mic connector Connect oxygen mask microphone connectorAircraft MSN 501 and UP MASK/MIC Switch ............................... MASK |
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ECS CAWS |
Headset ............................................... REMOVE Oxygen Mask ...................................... ON Headset ............................................... BACK ON Aircraft MSN 321 and 401-500 Disconnect normal headset boom mic connector Connect oxygen mask microphone connector Aircraft MSN 501 and UP MASK/MIC Switch ............................... MASK |
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ENGINE FAILURE AFTER ROTATION |
Headset ............................................... REMOVE Oxygen Mask ...................................... ON Headset ............................................... BACK ON Aircraft MSN 321 and 401-500 Disconnect normal headset boom mic connector Connect oxygen mask microphone connector Aircraft MSN 501 and UP MASK/MIC Switch ............................... MASK |
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ENGINE FAILURE IN FLIGHT – PARTIAL POWER LOSS |
Indication => Uncommanded engine power reduction........................................ No Response to PCL movement PCL .......................................................... IDLEManual Override Lever ........................ Pull upwards and move slowly forward until engine responds, wait and let engine stabilized |
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ENG FIRE CAWS IN FLIGHT |
Engine Power ......................................................... Reduce to minimum acceptable according to flight situation ECS EMER Shut off ...................... PULL Headset ....................................... REMOVE Oxygen Mask .............................. ON Headset ....................................... BACK ON |
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EFIS FAILURE |
Indication ................... Display Unit goes blankEFIS CMPST Switch ............................... CMPST |
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AHRS FAILURE |
Indication => Attitude Fail and/or heading fail ON EFIS AHRS 1/AHRS 2 Switch .................... SWITCH AHRS |
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INVERTER FAILURE |
Indication ................. All 4 Display Units go blank RMIs FlagOverhead panel ..... Select alternate inverter |
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SIC Flight Restrictions Less than 50 hours or 25 hours and 10 TO/LDG |
No TO/LDG with PAX on board |
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SIC with less than 100 hours or 50 hours and 25 TO/LDG |
• Whenever there is an emergency, such as an engine failure, unless the Pilot-in-Command has specifically directed that the Second-in-Command fly the aircraft for reasons of operational safety. • Visibility is less than one mile. • The runway is wet or snow covered. • The cross-wind component is greater than 10 knots.• The runway winds are greater than 20 knots or the gust spread is greater than 10 knots. • The departure is made under conditions of ground icing, even if the aircraft has been deiced according to an approved program. • The takeoff is made using an alternate departure procedure due to combinations of high gross weight, altitude and temperature. • The landing is made at night, as defined in the FARs, to a runway that does not have at least 150 percent of the minimum calculated runway length, as required by 14 CFR. Thus, a required Part 135 runway length of 3,000 feet for normal operations, considering such things as wet-runway criteria, would require a minimum of 4,500 feet of available runway for night operations. |
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Crew Pairing PIC less than 200 hours SIC less than 100 hours |
• The Second-in-Command may not takeoff or land the aircraft and may not operate the controls at an altitude of less than 1,000 feet above the ground. • The flight should not depart when braking action is reported as poor or worse. • The flight should not depart if there is more than two inches of snow on the runway. • The flight should not depart when the cross-wind component is greater than 10 knots. • The flight should not depart when the runway winds are greater than 20 knots or the gust spread is greater than 10 knots. • The flight should not depart if the departure is made under conditions of ground icing, even if the aircraft has been deiced according to an approved program. • The crew should not make a landing at night to a runway that does not have at least 150 percent of the minimum calculated runway length, as required by 14 CFR. Thus, a required Part 135 runway length of3,000 for normal operations, considering such things as wet-runway criteria, would require a minimum of4,500 feet of available runway for night operations. |
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Alternate Min 135 |
1 hour before and 1 hour after ETA: Highest Of 2000 ft ceiling 1500 ft above lowest circling MDA 1500 ft above straight in if no circling published 3 SM |
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Suitable Alternate |
1 Navaid 400 ft AGL 1 SM 2 Navaid Two different RWY and Navaid 200ft AGL 1/2SM No LPV |
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Lower than Standard Take-Off Min |
Rwy STD Climb / Able to accomplish gradient |
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Take Off Alternate |
1 Hour distance no wind If Rwy is not the departure |
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Eligible On Demand |
2 Person Crew 1500 PIC 500 SIC |
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Severe Ice |
Build in unprotected areas Build in excess of removal capability |
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LAHSO |
Afm Landing distance +1000ft Runway |
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LAHSO not allowed when: |
More than 3KTS tailwind Wet Runway Windshear 20 minutes prior WX MIN 1500 ft 5SM with PAPI/VASI mins 1000ft 3SM |
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On Demand Max Duty Time |
1400 Annually 800 2 quarters 500 quarter 10 hours rest prior to duty |
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Commuter Duty Time |
1200 Annually 120 Monthly 34 week 8 hours flight time between rest 1 day off every 7 consecutive days |
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Company rest policy |
8 hours flight time 10 Rest 14 Duty |
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Operational Control |
Ability to initiate, delay, terminate or cancel a flight: President Director of OPS Chief Pilot Director of MX |
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Safety Valve opens |
Weight on wheels Ground Idle Dump Switch Max Cabin pressure difference 6.35 Negative Pressure |
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Ice Protection |
De Ice: Probe Heat Heated Lip Inertial separator Pusher Ice Mode |
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De Ice boots sequence |
Horizontal Stabilizer Main Wing lower inboard Main Wing upper inboard Main Wing lower outboard Main Wing upper outboard 8 seconds each - 40 seconds total |
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De Ice limitaton |
temperature below -40c and more than 40c |
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Prop De Ice |
ELECTRIC 28 VDC GEN1 BUS 1 >0 Standby 2 0 >= -16C |
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Pusher Ice Mode |
Activated when Prop DE ICE ON |
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Fuel System Description |
1.Fuelfed from main tank àcollector tank by Transfer Jet pump + flap valves2.Fuelfrom collector tank àcommon manifold–Normal= Delivery Jet pump–Start= electric boost pump3.Commonmanifold à Maintenance valve4.Maintenancevalve à Fuel Filter5.FuelFilter à Air separator6.Airseparator àFirewall shut-off valve7.Firewallshut-off valve àLow-pressure EDP8.Low-pressureEDP à Oil-Fuel Heat Exchanger–Excessfuel under pressure returned to tanks using motive flow9.Oil-FuelHeat Exchanger àHigh-Pressure EDP à FCU |
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Fuel Max Imbalance |
3 LCD |
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Fuel Boost Pump On |
2 LCD Difference |
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Fuel System |
Transfer Pump Flap Valve / Delivery Jet maintenance shutoff Filter Vapor separator Low pressure switch Firewall Shutoff Low pressure pump Motive flow line Oil Heat exchange High Pressure Pump Filter FCU - Return Line |
