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57 Cards in this Set
- Front
- Back
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91.155 |
Condition Lever Fuel Cutoff
Engine Start Switch Starter only for remainder of starter limit Engine Start Switch Off Do Not Attempt Another Start |
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No Light-off |
Condition Lever Fuel Cutoff Engine Start Switch Off Follow Engine Clearing Procedures |
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Engine Clearing procedures |
Condition Lever Confirm Fuel Cutoff Starter Let cool for 1 minute after previous start attempt Engine Start Switch Starter Motor for 40 seconds Engine Start Switch Off Starter Let cool for 1 minute before attempting another start sequence |
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Engine fire in flight |
Condition Lever Fuel Cutoff Propeller Lever Feather Firewall Shutoff Valve Close Engine Securing Checklist Complete |
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Engine fire on ground |
Condition Lever Fuel Cutoff Firewall Shutoff Valve Close Engine Fire on the Ground Checklist Complete |
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Engine Failure during ground roll |
Power Levers Ground Fine Brakes As Required to achieve stopping performance If Insufficient Runway Remains for Stopping: Condition Levers Fuel Cutoff Firewall Shutoff Valve Close Gang Bar Down / Off Boost Pumps Off |
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Engine Failure in flight |
Power Max Continuous Power Set Airspeed Maintain 108 kts or greater Gear Retracted Flaps Retracted Inoperative Engine Identified Inoperative Engine Verified Inoperative Engine Propeller Feathered Engine Securing Checklist Complete Identification and Verification should be gained from evaluating the engine gauges |
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Engine Failure on A published portion if the instrument approach |
Power Increase to maintain desired airspeed Course Maintain Gear Considered Flaps Considered Inoperative Engine Identified Inoperative Engine Verified Inoperative Engine Propeller Feathered Single Engine Landing Checklist Complete |
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Emergency engine shutdown |
Condition Lever Fuel Cutoff Propeller Lever Feather Firewall Shut-Off Valve Closed Emergency Engine Shutdown Checklist Complete |
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Emergency descent |
Power Levers Idle Propeller Levers High RPM Flaps Approach <184 kts Gear Down Airspeed 182 knots maximum |
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Unscheduled elevator trim |
Pitch Control Maintain with elevator Elevator Trim Switch Off Manual Trim Re-trim as required |
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High diff pressure |
Anytime Differential Pressure goes into the Red Arc: Cabin Altitude Controller Select Higher Cabin Altitude Setting If Condition Persists: Bleed Air Valve Closed Cabin Pressure (after cabin has depressurized) Dump Bleed Air Valve Open |
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Smoke in the cockpit |
Crew Oxygen System Confirm On Crew Don Masks Microphone Switch Set to Mask Smoke in the Cockpit Checklist Complete |
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Loss of pressurization |
Crew Oxygen System Confirm On Crew Don Masks Microphone Switch Set to Mask Loss of Pressurization Checklist Complete |
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Va, Vturb |
163, 161 |
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Vx and vy |
101, 112 |
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Landing final approach/balked landing speed |
101 |
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Vmc, blue line |
80, 108 |
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Minimum battery voltage, |
23 regular, 20 external power,1000 amps momentarily, 300 continuous 28-.4 |
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Voltmeter readings on test |
Tpl fed- 16.5-28.0 L and R gen- 27.5-29.0 Ctr- 23 min
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Yellow fuel quantity |
0-265 |
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Yellow fuel quantity |
0-265 |
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Describe propeller |
Two full-feathering, constant-speed, reversing, four-bladed |
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Max OAT |
Isa+37 |
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SERVE |
Supportive, Ethical, Resourceful, Vigilant about Safety, Empathetic |
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Crew Briefings, RATAL |
Risk, Altitudes, Terrain, Approach, Limitations |
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Rotation, 50 FT |
97, 104. VX is 101 Vy is 112 |
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Cruise climb speeds |
0-10=150 10-20=130 20-25=120 25-30=110 |
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Vsse |
97 |
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Landing gear speeds |
182, 163 |
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Landing Gear cycles |
1 full cycles every three minutes, total of 10 then 15 min cooldown |
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Flight load limits, Gs |
3.2 positive, 1.33 negative Flaps= 2.00 positive, 0.00 Negative |
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Cg limits |
152 aft at 10,100 150.6 at 9600 Ref datum is 83.5 inches from nose jack point MAC edge is 135.9 and Length is 75.9 |
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Pneumatic pressure arc |
12-20/20 |
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Gyro suction |
0-15000= 4.3-5.9 15000-35000=2.8-4.3 |
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Approved oils |
7.5 and 5 centistoke turbine oils |
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Boost pumps takeoff |
Are required to be operational |
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Propeller speed limits |
Max 2420 for five seconds, anything over 2200 is a primary gov failure, anything over 2288 is both primary and overspeed governor failure (1976 for -135) |
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Stall speeds |
78 full flaps idle power, 88 flaps up idle power |
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Oil temp for takeoff |
Recommended 55 for fuel-heating during takeoff, 74-80 is normal range |
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Oil temp for takeoff |
Recommended 55 for fuel-heating during takeoff, 74-80 is normal range |
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Oil pressure |
80-100 is normal, up to 200 on cold starts, 40-80 is reduced power to complete flight, below 40 is too low. |
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Minimum prop rpm |
1000/1100 |
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Oil capacity |
14 quarts, 12.5 refill capacity, operating range add 4--full |
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Wing loading/power loading |
34.4lbs/ft2, 9.2lbs/shp |
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Generator limits |
0-50=59% 50-80=61% 80to85=70% |
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Starter limits |
3 cycles 40 on 60 off then 30 minutes |
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Approved fuels |
Jet A,A-1,B, some military grades, 80 red,100Ll Blue, 100 green. |
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Avgas limits |
150 hours tbo, 8000 ft pressure altitude if boost pumps inop, must have crossfeed capability above 8000. |
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Fuel system quantities |
384 total useable, 192 each side, 131 wing, 61 nacelle. X6.7 |
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Fuel system quantities |
384 total useable, 192 each side, 131 wing, 61 nacelle. X6.7 |
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Max occupancy |
13 including crew |
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Broken windshields |
Require a placard found in the POH. Cabin pressure btwn 2.0-4.6 for front and depressurized for side. |
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Dimensions |
35ft 6 inches long which is the same as the turning radius 14ft 3 inches Height 27 inch entry width Wingspan 50ft 3in inches |
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Best glide, VXSE |
125 best glide, 100vxse |
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Strut inflation |
3 inches |
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Max taxi speed |
15 knots |
