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235 Cards in this Set
- Front
- Back
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AIRSPEEDS: Indicator needles |
Max 6 KT Split |
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AIRSPEEDS: Turbulence |
65 above power-off stall not to exceed 180 |
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AIRSPEEDS: FLAPS 10% |
220 |
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AIRSPEEDS: FLAPS 20% |
210
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AIRSPEEDS: FLAPS 30% |
200
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AIRSPEEDS: FLAPS 40% |
190
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AIRSPEEDS: FLAPS 50% |
180
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AIRSPEEDS: FLAPS 60% |
165
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AIRSPEEDS: FLAPS 70% |
155
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AIRSPEEDS: FLAPS 80% |
150
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AIRSPEEDS: FLAPS 90% |
145
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AIRSPEEDS: FLAPS 100% |
145 |
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AIRSPEEDS: Landing gear |
165 |
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AIRSPEEDS: Landing lights |
250 |
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AIRSPEEDS: Ramp open |
150 |
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AIRSPEEDS: Only cargo door open |
185 |
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AIRSPEEDS: Air deflectors |
150
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AIRSPEEDS: Paratroop doors move |
150 |
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AIRSPEEDS: Paratroop doors open |
250 |
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AIRSPEEDS: Painted flight controls |
250 unless stencled |
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AIRSPEEDS: Inoperative NESA |
185 below 10,000' |
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AIRSPEEDS: Nose wheels |
139 |
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AIRSPEEDS: Main wheels |
174 |
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AIRSPEEDS: Landing gear with doors removed |
200, gear up or down |
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AIRSPEEDS: Nose gear deflection |
20 deg/20 knots 60 deg/5 knots |
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AIRSPEEDS: Max taxi >155,000 lb |
10 knots |
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AIRSPEEDS: Normal flap retract |
20 KIAS above take-off speed |
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AIRSPEEDS: Holding |
170 |
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AIRSPEEDS: Approach entry |
170 |
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AIRSPEEDS: Circling approach |
>140 or Vapp |
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AIRSPEEDS: 3 or 4 engine approach |
70-60-50 |
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AIRSPEEDS: 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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PROPELLER RPM: Allowable flux |
+- 0.5 for a total 1%
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PROPELLER: Prop aux pump |
1 min on, 1 min off (not exceed 2 min in any 30 min period) |
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PROPELLER: Prop low oil light |
2 quarts low in |
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HYDRAULIC SYSTEM PSI: Normal pressure U/B |
2900-3200 |
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HYDRAULIC SYSTEM PSI: Max pressure U/B |
3500 |
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HYDRAULIC SYSTEM PSI: Normal pressure AUX |
2900-3300 |
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HYDRAULIC SYSTEM PSI: Max pressure AUX |
3500 |
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HYDRAULIC SYSTEM PSI: LSGI U/B |
2550 |
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HYDRAULIC SYSTEM PSI: Normal brakes gage |
2900-3200 |
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HYDRAULIC SYSTEM PSI: Emergency brakes gage |
2900-3300 |
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HYDRAULIC SYSTEM PSI: Brakes gages MAX |
3500 |
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HYDRAULIC SYSTEM PSI: Normal brake failure 1 brake application remaining |
2250 |
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HYDRAULIC SYSTEM PSI: Emergency brake failure 1 brake application remaining |
2900 |
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HYDRAULIC SYSTEM PSI: Aileron boost |
2050 |
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HYDRAULIC SYSTEM PSI: Elevator boost |
2900-3200 |
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HYDRAULIC SYSTEM PSI: Low rudder boost |
1100-1400 |
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HYDRAULIC SYSTEM PSI: Low boost caution |
1400-1600 |
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HYDRAULIC SYSTEM PSI: High rudder boost |
2900-3200 |
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HYDRAULIC SYSTEM PSI: High boost max |
3500 |
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HYDRAULIC SYSTEM PSI: Low pressure light |
<1000 PSI |
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HYDRAULIC SYSTEM PSI: Suction boost light |
<20 PSI 11 AMPS (hot) |
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HYDRAULIC SYSTEM PSI: Do not turn off switches |
>3500 PSI |
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HYDRAULIC SYSTEM PSI: High pressure |
>3900 PSI |
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HYDRAULIC SYSTEM PSI: Loss of system pressure procedure |
<2500 PSI |
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HYDRAULIC SYSTEM PSI: Engine start hyd. (Pull yoke off stops for accurate reading) |
Indication by on speed, full pressure 30 seconds after |
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HYDRAULIC SYSTEM PSI: Utility accumulator |
1500 +- 100 PSI |
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HYDRAULIC SYSTEM PSI: Booster accumulator |
1500 +- 100 PSI |
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HYDRAULIC SYSTEM PSI: Normal brake accumulator |
1500 +- 100 PSI |
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HYDRAULIC SYSTEM PSI: 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: Do not force CABIN ALT knob |
Above 10,000' or below -1,000' |
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PRESSURIZATION: Before landing |
<1.5 inches OK to go no pressure |
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PRESSURIZATION: Takeoff, Taxi, Landing |
No pressure |
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PRESSURIZATION: Safety valve opens |
-0.76 to 15.9 in. HG |
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PRESSURIZATION: Crew door no jettison |
Above 3 inches pressure |
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ANTI-ICING: Wing and empennage |
No more than 30 sec on ground |
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ANTI-ICING: Leading edge temp |
158 deg. F - 180 deg. F |
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ANTI-ICING: Overtemp light |
215 deg. F |
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ANTI-ICING: Propeller |
Two cycles on ground |
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ANTI-ICING: Cold start NESA-43 deg. 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 |
More than 5 sec |
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ANTI-ICING: Between tests |
5 minutes |
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ANTI-ICING: Cold weather procedures |
0 deg. C and below |
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ANTI-ICING: Hot weather procedures |
35 deg. C and above |
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STARTER: Light must be on |
Within 5 seconds |
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STARTER: Light must go out |
Within 15 seconds |
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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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PERFORMANCE: Generators |
40-60 kVA |
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PERFORMANCE: Brakers |
2030 PSI |
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PERFORMANCE: Engines |
100% efficiency |
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PERFORMANCE: Serialization |
H = 1500 Series,1716+below, 1790 HR = 1717+up |
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PERFORMANCE: Calculate CFL |
+30 deg, 130K lbs, 6000', RCR 12 or less |
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PERFORMANCE: Do landing distance, ground roll |
<6000' runway |
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PERFORMANCE: Vmca1in (normal bleed) |
subtract 2 knots |
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PERFORMANCE: Vr |
Not greater than 139 |
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PERFORMANCE: Vrot |
5 knots < greater of Vmca1in or VTO |
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PERFORMANCE: Headwind |
50% 100% for accel check |
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PERFORMANCE: Tailwind + gust increment |
150% 100% for accel check |
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PERFORMANCE: Gust |
Increase up to 10 knots |
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PERFORMANCE: Crosswind + gust increment |
35 knots max |
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PERFORMANCE - RCR: No brakes |
2 |
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PERFORMANCE - RCR: Icy/poor braking |
5 |
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PERFORMANCE - RCR: Wet/fair braking |
12 |
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PERFORMANCE - RCR: Wet/grooved/no glare |
20 |
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PERFORMANCE - RCR: Dry/good braking |
23 |
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PERFORMANCE - RSC: Tenths of an inch |
1 inch = RSC of 10 |
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PERFORMANCE - RCR: Dry loose snow that drifts in 10 knots |
1/3 actual depth up to 3 inches |
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PERFORMANCE - RCR: Both RCR/RSC present |
RSC precedence |
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PERFORMANCE - RCR: CO approval |
RSC of over 1 |
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ENGINE TORQUE IN/LBS: Max torque |
19,600 |
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ENGINE TORQUE IN/LBS: Oil temp < 0 deg |
Minimum |
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ENGINE TORQUE IN/LBS: Oil temp 0 deg to 40 deg |
4,500 max |
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ENGINE TORQUE IN/LBS: Oil temp > 40 deg |
Up to 19,600 |
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ENGINE TORQUE IN/LBS: NTS |
-1260 +- 600 |
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ENGINE TORQUE IN/LBS: Decouple |
-6000 |
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ENGINE TORQUE IN/LBS: Reverse |
No more than 1000 between symmetrical |
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RPM %: Ignition by |
35% |
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RPM %: Oil pressure by |
35% |
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RPM %: LSGI |
69-75.5%
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RPM %: Ground idle |
94-102% |
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RPM %: Reverse |
96-106% |
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RPM %: Flight idle |
92.5-100.5% |
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RPM %: Above flight idle |
98-102% |
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STARTING TIT DEG C: Max prior w/enrich |
<100 deg |
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STARTING TIT DEG C: Max prior to start |
<200 deg |
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STARTING TIT DEG C: Record, temp cont. check |
721 deg - 750 deg |
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STARTING TIT DEG C: Normal start range |
751 deg - 830 deg |
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STARTING TIT DEG C: Record |
830 deg - 850 deg |
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STARTING TIT DEG C: Stop, one restart |
850 deg - 965 deg |
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STARTING TIT DEG C: Maintenance required |
<720 deg or >965 deg or abnormal torch |
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ENGINE TIT DEG C: Normal range |
200 deg - 1010 deg |
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ENGINE TIT DEG C: Take-off 5 minutes max |
1067 deg - 1083 deg |
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ENGINE TIT DEG C: Military 30 minutes max |
1049 deg |
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ENGINE TIT DEG C: Max continuous/climb |
1010 deg |
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ENGINE TIT DEG C: Recommended climb |
970 deg |
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ENGINE TIT DEG C: Recommended cruise |
932 deg |
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ENGINE TIT DEG C - POWER ACCELERATION PEAK: Exceeds 1083 for more than 5 seconds or 1175 momentarily |
Reduce, record, inspect before next flight |
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ENGINE TIT DEG C - POWER ACCELERATION PEAK: Crossover |
800 deg - 840 deg |
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ENGINE TIT DEG C - POWER ACCELERATION PEAK: Max downshift |
850 deg |
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ENGINE TIT DEG C - POWER ACCELERATION PEAK: Landing in "locked" TD |
Within 5000' of field |
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ENGINE TIT DEG C - POWER ACCELERATION PEAK: After landing LSGI |
2 minutes |
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ENGINE TIT DEG C - POWER ACCELERATION PEAK: Ground stop speed |
Max 40 knotes in NSGI
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FIRE EXTINGUISHING PRESSURE: Limit based on temp |
Chart page 1-32 |
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FIRE AND OVERHEAT DEG F: Nacelle |
On at 300 deg F |
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FIRE AND OVERHEAT DEG F: Turbine |
On at 700 deg F |
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FIRE AND OVERHEAT DEG F: Lights |
ESS DC |
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FIRE AND OVERHEAT DEG F: Agent and valved |
Battery bus |
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FIRE AND OVERHEAT DEG F: Turbine overheat test |
30 sec on, 1 min off |
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ENGINE OIL TEMP DEG C: Normal |
4-12 gallons |
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ENGINE OIL TEMP DEG C: Tank capacity |
19.5 gallons |
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ENGINE OIL TEMP DEG C: Low light |
<4 gallons |
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ENGINE OIL TEMP DEG C: Normal temp |
60 deg - 86 deg |
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ENGINE OIL TEMP DEG C: Min start oil temp |
-40 deg |
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ENGINE OIL TEMP DEG C: Start, warmup |
Up to +40 |
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ENGINE OIL TEMP DEG C: Flight |
85-100 deg for 5 minutes |
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ENGINE OIL TEMP DEG C: Ground |
85-100 deg for 30 minutes
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ENGINE OIL PRESSURE: Normal |
50-60 psi |
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ENGINE OIL PRESSURE: Max during start and warmup |
100 |
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ENGINE OIL PRESSURE: LSGI |
Can be as low as 50 psi |
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ENGINE OIL PRESSURE: Fluctuation |
+-10 psi 20 psi excursion |
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GEARBOX OIL PRESSURE: Normal range |
150-250 psi |
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GEARBOX OIL PRESSURE: Start and warmup |
Can exceed 250 |
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GEARBOX OIL PRESSURE: Fluctuation |
+-20 psi 40 psi excursion |
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GEARBOX OIL PRESSURE: LSGI |
50 psi |
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AC ELECTRICAL: Engine gen rating |
40 kVA |
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AC ELECTRICAL: APU gen rating |
40 kVA |
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AC ELECTRICAL: ATM gen rating |
20 kVA, 30 kVA w/air |
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AC ELECTRICAL: Voltage |
110-125 |
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AC ELECTRICAL: Frequency |
380-420 |
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AC ELECTRICAL: ENG/APU gen load |
0-1.05 |
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AC ELECTRICAL: ATM gen load |
1.0 with cooling air 0.66 w/o air or temp > 40 |
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DC ELECTRICAL: Voltage |
25-30 volts |
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DC ELECTRICAL: Load |
0-1.03% of max load |
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DC ELECTRICAL: Battery voltage |
24 volts |
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DC ELECTRICAL: Min battery voltage |
23 volts for NiCad |
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DC ELECTRICAL: CP inverter |
250 volt/amps |
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DC ELECTRICAL: AC inst inverter |
2500 volt/amps |
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APU: Exhaust gas temp |
260 deg C - 650 deg C |
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APU: RPM |
95-105% 106% max |
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APU: #2 fuel < 2000 pounds |
Fuel boost pump on |
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APU: Altitudes |
-1000 to 20,000 |
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APU: Airspeed |
<200 KIAS |
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APU: APU door |
15 deg air, 35 deg ground |
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APU: Starter duty cycle |
1 min on, 4 min off |
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APU: APU start light out |
35% |
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APU: Start to onspeed |
35 seconds |
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APU: Overspeed |
110% |
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APU: Bleed air switch on |
95% |
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APU: Cold weather warmup |
4 minutes |
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APU: Warmup/cooldown |
1 minutes |
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APU: Door shuts |
<20 psi oil, 18% RPM |
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OXYGEN: Normal usable range |
200-1800 psi |
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OXYGEN: May be used to |
0 psi empty |
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OXYGEN: Min for normal use |
50 psi |
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WEIGHT LBS: Taxi max normal |
155,000 |
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WEIGHT LBS: Taxi max EWP |
175,000 |
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WEIGHT LBS: Take-off max normal |
155,000 |
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WEIGHT LBS: Take-off EWP |
175,000 |
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WEIGHT LBS: Normal landing |
130,000/up to 540 FPM |
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WEIGHT LBS: Landing max normal |
155,000/up to 300 FPM |
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WEIGHT LBS: Landing EWP |
175,000/300 FPM |
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WEIGHT LBS: Fuel in #1, 4 tanks |
>6,600 lbs/up to 300 FPM |
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BLEED AIR: APU minimum |
35 psi |
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BLEED AIR: APU bleed air check |
30-15 psi not less than 16 seconds |
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BLEED AIR: Engine check |
After 70 psi then 65-35 not less than 16 seconds |
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BLEED AIR: Negative rotation |
Reduce psi to 45 |
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BLEED AIR: Regulators |
All within 3 psi |
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BLEED AIR: Regulating at |
Approx. 50 psi |
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BLEED AIR: Overheat |
215 deg F |
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FUEL SYSTEM: Main tank press |
15-24 psi |
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FUEL SYSTEM: Aux tank press |
28-40 psi |
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FUEL SYSTEM: Ext tank press |
28-40 psi |
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FUEL SYSTEM: Dump pump |
28-40 psi |
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FUEL SYSTEM: Eng low press |
<8.5 psi |
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FUEL SYSTEM: Aux tank empty |
<23 psi |
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FUEL SYSTEM: Ext tank empty |
<23 psi |
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FUEL SYSTEM: All fuel valves |
ESS DC |
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FUEL SYSTEM: All dump pumps |
MAIN AC |
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FUEL SYSTEM: Main boost pumps |
LEMR |
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FUEL SYSTEM: Indicators |
AC INST C/B |
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FUEL SYSTEM: Symmetric tanks |
No more than 1000 lb difference |
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FUEL SYSTEM: Between wings |
No more than 1500 lb |
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FUEL SYSTEM: Outboard to inboard tanks |
500-1000 pounds more |
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FUEL SYSTEM: Emergency fuel |
50 hours max |
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FUEL SYSTEM: Gages accurate |
3 deg roll, 0 deg pitch |
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Reasons to Stop Start |
1. Any Reason 2. No START VALVE OPEN light in 5s 3. No RPM in 5s 4. No Ignition by 35% RPM 5. No Oil Pressure by 35% RPM 6. Negative Parallel by 65% RPM 7. No hydraulic pressure by On-Speed 8. No full hydraulic pressure by 30s after On-Speed (as low as 2550 in LSGI) 9. Start sequence takes more than 1 min (70s HIGH + HOT) 10. Negative De-enrichment 11. Peak TIT > 850 deg C 12. Peak TIT < 720 deg C |
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G-PIED |
16% - ON G - Geneva Lock - Open P - Parallel valve - Open (Parallel operation) I - Igniters - Energized E - Enrichment - Open momentarily (if selected) D - Drip Valve - Energized closed |
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PIED |
65% - OFF P - Parallel valve - Closed (Series operation) I - Igniters - De-energized E - Enrichment - De-energized (normally de-energized by 50 PSI switch) D - Drip Valve - De-energized (held closed by fuel pressure) |
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Reduction Gear Assemblies |
G - Generator H - Eng. Driven Hyd Pump O - Oil Pumps S - Starter T - Tach Gen |
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Engine Accessories |
O - Oil Pump F - Fuel Control F - Fuel Pump S - Speed Sensing Control S - Speed Sensing Valve |
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Operation of Fuel Control affected by: |
Throttle Position Compressor Inlet Air Temperature (CIT) Engine Speed (RPM) Compressor Inlet Air Pressure (CIP) |
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TIT Limits: Ground start Enrichment start Inflight start Stop start - maintenance Record - temp controlling check Normal start range Record and continue Stop start Inspection required Max continuous Military (30 min) Maximum (5 min) More than 5 sec - inspect Momentary - inspect Normal operations - climb Normal operations - cruise |
200 C 100 C 200 C <= 720 C 721-750 C 750-830 C 830-850 C > 850 C > 965 C 1010 C 1049 C 1067-1083 C 1083 C 1175 C 970 C 932 C |
