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100 Cards in this Set
- Front
- Back
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1
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1
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AIRSPEEDS
Indicator needles - max split |
max 6 knot split
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AIRSPEED
Turbulence penetration |
65 above power off stall, not to exceed 180 KIAS
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AIRSPEED
Flaps - 10% |
220
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AIRSPEED
Flaps - 20% |
210
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AIRSPEED
Flaps - 30% |
200
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AIRSPEED
Flaps - 40% |
190
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AIRSPEED
Flaps - 50% |
180
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AIRSPEED
Flaps - 60% |
165
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AIRSPEED
Flaps - 70% |
155
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AIRSPEED
Flaps - 80% |
150
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AIRSPEED
Flaps - 90% |
145
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AIRSPEED
Flaps - 100% |
145
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AIRSPEED
Landing gear extension/extended |
165
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AIRSPEED
Landing lights extension/extended |
250
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AIRSPEED
Ramp open |
150
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AIRSPEED
Cargo door open |
185
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AIRSPEED
Air deflector doors |
150
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AIRSPEED
Paratroop doors movement |
150
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AIRSPEED
Paratroop door open |
250
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AIRSPEED
Painted flight control surfaces |
250 unless stenciled
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AIRSPEED
Inop NESA |
185 below 10,000 ft
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AIRSPEED
Nose wheel max |
139
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AIRSPEED
Main wheels max |
174
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AIRSPEED
Landing gear doors removed |
200 - gear up or gear down
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AIRSPEED
Nose gear deflection degree/speed |
20*/20 knots
60*/5 knots |
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SPEED
Max taxi speed at >155,000 lbs |
10 knots
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AIRSPEED
Normal flap retraction speed |
20KIAS above takeoff speed
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AIRSPEED
Holding |
170 KIAS
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AIRSPEED
Approach entry |
170 KIAS
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AIRSPEED
Circling approach |
140 or approach speed whichever is greater
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AIRSPEED
3 or 4 engine approach |
70-60-50
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AIRSPEED
2 engine approach |
70-60-50
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PROPELLER RPM
10% |
Airstart NTS
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PROPELLER RPM
16% |
G-PIED on
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PROPELLER RPM
40% |
Airstart ignition
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PROPELLER RPM
60% |
Starter release
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PROPELLER RPM
65% |
PIED OFF
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PROPELLER RPM
96-98% |
Pitchlock ops
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PROPELLER RPM
103% |
Pitchlock
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PROPELLER RPM
103.5% |
Fuel topping
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HYDRAULIC SYSTEM
Normal pressure U/B |
2900-3200 psi
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HYDRAULIC SYSTEM
Max pressure U/B |
3500 psi
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HYDRAULIC SYSTEM
Normal pressure AUX |
2900-3300 psi
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HYDRAULIC SYSTEM
Max pressure AUX |
3500 psi
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HYDRAULIC SYSTEM
LSGI U/B |
2550
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HYDRAULIC SYSTEM
Normal brakes |
2900-3200 psi
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HYDRAULIC SYSTEM
Emergency brakes, normal pressure |
2900-3300 psi
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HYDRAULIC SYSTEM
Brakes max pressure |
3500 psi
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HYDRAULIC SYSTEM
One brake application remaining - normal |
2250 psi
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HYDRAULIC SYSTEM
One brake application remaining - emergency |
2900 psi
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HYDRAULIC SYSTEM
Aileron boost pressure |
2050 psi
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HYDRAULIC SYSTEM
Elevator boost pressure |
2900-3200 psi
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HYDRAULIC SYSTEM
Low rudder boost |
1100-1400 psi
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HYDRAULIC SYSTEM
Low boost caution |
1400-1600 psi
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HYDRAULIC SYSTEM
High rudder boost |
2900-3200 psi
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HYDRAULIC SYSTEM
high rudder boost max |
3500 psi
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HYDRAULIC SYSTEM
Low pressure light |
< 1000 psi
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HYDRAULIC SYSTEM
Suction boost light |
< 20 psi (11 AMPS --HOT--)
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HYDRAULIC SYSTEM
Do not turn switched off |
> 3500 psi
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HYDRAULIC SYSTEM
High pressure |
> 3900 psi
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HYDRAULIC SYSTEM
Loss of system pressure |
< 2500 psi
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HYDRAULIC SYSTEM
Engine start indication |
Indication by "on speed" full system pressure 30 sec after
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HYDRAULIC SYSTEM
Utility & Boost accumulator |
1500 +/- 100 psi
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HYDRAULIC SYSTEM
Normal brake accumulator |
1500 +/- 100 psi
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HYDRAULIC SYSTEM
Emergency brake accumulator |
1000 +/- 100 psi
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PRESSURIZATION
Normal range |
-1.2 to 15.8 in hg
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PRESSURIZATION
Before landing |
< 1.5 in ok to goto no pressure
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PRESSURIZATION
Takeoff, taxi, landing |
No pressure
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PRESSURIZATION
Safety valve opens |
- .76 to 15.9 in hg
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ANTI-ICING
Wing & empenange usage on ground |
No more than 30 sec
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ANTI-ICING
Leading edge temperature |
158*F - 180*F
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ANTI-ICING
Leading edge overtemp light |
215*F
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ANTI-ICING
Propeller usage on ground |
Two cycles on the ground
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ANTI-ICING
Cold start NESA -43*C |
5 sec on, 10 sec off
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ANTI-ICING
Blade, spinner, de-ice amps |
65-90 amps
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ANTI-ICING
Spinner anti-ice |
20 each for 65-90
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ANTI-ICING
Do not hold test switch for... |
more than 5 sec
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ANTI-ICING
Cold weather procedures |
0*C and below
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ANTI-ICING
Hot weather procedures |
35*C and above
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STARTER
Light must be on... |
within 5 sec
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STARTER
Light must go out... |
within 15 sec
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STARTER
Duty cycle |
1 min on, 1 min off
1 min on, 5 min off 1 min on, 30 min off |
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STARTER
Released at... |
60% RPM
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PROPELLER
Prop aux pump duty cycle |
1 min on, 1 min off
not to exceed 2 minutes in any 30 minutes. |
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PROPELLER
Allowable flux |
+/- 0.5 %, a total of 1%
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PROPELLER
Prop low oil light |
on at 2 quarts low in pressurized sump
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PROPELLER
Pressurized sump volume |
6.5 quarts
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PROPELLER
Total quantity |
26 quarts
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PERFORMANCE
Generators |
40-60 KVA
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PERFORMANCE
Brakes |
2030 PSI
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PERFORMANCE
Engines |
100% efficiency
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PERFORMANCE
Compute CFL |
> 30 degrees C
> 130,000 lbs 6000' RCR 12 or less |
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PERFORMANCE
Compute landing distance and landing ground roll |
< 5000' runway
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PERFORMANCE
VMCA1 in (normal bleed) |
subtract 2 kts
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PERFORMANCE
Vr |
Not greater than 139
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PERFORMANCE
Vrot |
5 kts less than...
the greater of Vmca1 (in) or V t/o |
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PERFORMANCE
Headwind |
50% for operational
100% for acceleration time check |
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PERFORMANCE
Tailwind |
150% always
100% for acceleration time check |
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PERFORMANCE
Gust |
Increase up to 10 kts
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