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216 Cards in this Set
- Front
- Back
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High RAWS warning:
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380 +-20 FEET
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Low RAWS warning:
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170 +-10 FEET
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Minimum altitude for using AFCS:
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200 FEET
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Minimum recommended altitude for bailout
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3000 FEET
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Minimum altitude for two engine loiter
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1000 FEET
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APU automatic load monitoring altitude
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8000 FEET
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CABIN PRESS light illuminates
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10000 +-500 FEET
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Maximum altitude for starting APU in-flight
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20000 FEET
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Maximum altitude for using the APU for engine starts on deck
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6000 FEET
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Maximum altitude for flying with a cracked windscreen (middle layer)
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10000 FEET
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Maximum altitude before turning off landing lights
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10000 FEET
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Altitude for notifying crew to locate their O2
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FL250
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Maximum speed with flaps UP:
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VNE
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max airspeed maneuver
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275 kts
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Maximum speed with flaps at TAKEOFF/APPROACH
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190 KTS
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Maximum speed with flaps at LAND
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170 KTS
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Maximum speed with landing gear extended:
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300 KTS
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Maximum speed to extend landing gear (at 1.0 G):
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300 KTS
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Maximum speed to extend landing gear (greater than 1.0 G):
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190 KTS
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Maximum speed to retract landing gear
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190 KTS
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Maximum speed with landing lights extended
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260 KTS
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Maximum speed with overwing exit hatch open
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170 KTS
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Maximum speed with main cabin door open
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300 KTS
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Maximum speed with APU doors open
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225 KTS
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Maximum speed with IRDS turret extended:
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405 KTS
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Maximum speed with AIMS turret extended:
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405 KTS
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Maximum speed to extend or retract IRDS turret:
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375 KTS
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Maximum speed to extend or retract AIMS turret:
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350 KTS
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Speed range for dumping fuel:
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140 TO 300 KTS
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Speed range for in-flight restart
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170 TO 345 (MIN OF 210 IF RANGE CRITICAL)
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Maximum speed for retarding power levers into ground range:
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135 KTS
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Max speed for retarding power levers into ground range without electrical power:
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125 KTS
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Maximum speed with bomb bay doors open:
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VNE:
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Maximum speed with windshield heat inoperative:
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240 KTS BELOW 10000 FEET
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Normal speed range for NTS checks:
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180 +-10 KTS
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Maximum zero fuel weight (P-3C):
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80400LBS
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Maximum zero fuel weight (P-3C) with foam:
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82400 LBS
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Maximum normal landing weight:
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103880 LBS
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Max landing wt that does not require an immediate overweight landing inspection:
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114000 LBS
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Maximum recommended takeoff weight
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135000 LBS
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Maximum tank imbalances for tanks 1 & 4 for takeoff:
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1400 LBS
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Maximum tank imbalances for tanks 1 & 4 for in-flight and landing:
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4389 LBS
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Maximum tank imbalances for tanks 2 & 3 for takeoff:
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5025 LBS
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Maximum tank imbalances for tanks 2 & 3 for in-flight and landing:
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NO LIMIT
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Minimum fuel to obtain a dip in tanks 1 & 4 (in pounds):
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9500 LBS
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Minimum fuel to obtain a dip in tanks 2 & 3 (in pounds)
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5500 LBS
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APU fuel burn rate per hour with electrical power and ground air:
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300 PPH
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Flight station gages to hydrostatic tester difference limit:
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1200 LBS
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During an in-flight restart, light off should occur within:
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10 SEC
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During ground start, the time from rotation to LOW RPM should not exceed:
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60 SEC
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Flight station oxygen bottles endurance:
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3.5 HOURS AT 25000 FEET
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O2 walkaround bottle limit with little or no exertion:
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22 MIN
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O2 walkaround bottle limit with moderate exertion:
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5-10 MIN
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Engine oil cooler augmentation occurs within (after all parameters are met):
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8 SEC
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In-flight, maximum time allowed at zero or negative G’s:
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10 SEC
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After returning from zero or negative G’s, a feather shutdown is required if oil pressure fluctuations continue longer than:
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15 SEC
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Maximum time for landing lights on with no airflow:
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30 SEC
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Test cycle time for emp de-ice:
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44 SEC
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Normal cycle for emp de-ice:
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176 SEC
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Test cycle time for prop de-ice test:
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160 SEC
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Normal cycle for prop de-ice:
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160 SEC
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With a loss of power, the peanut gyro provides reliable information for:
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9 MIN
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Maximum time for OIL HOT light to be illuminated in the alpha range:
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5 MIN
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Maximum time for OIL HOT light to be illuminated in the beta range:
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30 MIN
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VRU limit depending on size and exertion level:
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12-60 MIN
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Stagnated start RPM reluctant to rise above:
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35-50%
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Digital SHP gauge will indicate actual engine SHP @
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43%
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Fuel flow initiation during start:
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16%
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During start, EDC press low light out between:
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16-65%
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During start, light off occurs between:
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16-33%
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During start, the fuel manifold drain valve is closed at:
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16%
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During start, the fuel manifold drain valve is held closed by fuel pressure above:
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65%
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Prop brake held released by RGB oil pressure above:
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21%
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PROP PUMP lights should be out during an in-flight restart by:
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55%
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Start button should pop out between:
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57-64%
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NORMAL RPM limits:
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96.3-99.1%
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LOW RPM limits:
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71.0-73.8%
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MAX REVERSE RPM limits:
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96.7-104.9%
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FLIGHT IDLE RPM limits:
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94.5-98.4%
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Fuel control maintains RPM above:
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97%
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Pitchlock regulator dumps at:
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103.5%
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Pitchlock reset resets RPM to:
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109%
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Fuel Topping Governor limits:
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104.2-106.7%
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APU on deck limits:
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98-102%
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APU in-flight limits:
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98-103%
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APU overspeed:
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106%
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LOW RPM:
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410-730C
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NORMAL RPM:
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445-645C
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Flight Idle:
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430-705C
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Maximum Reverse:
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580-790C
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Maximum Reverse:
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580-790C
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Maximum TIT for five seconds
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1175C
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Maximum TIT for five minutes:
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1077 +6-10C
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Maximum TIT for thirty minutes:
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1049C
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Maximum TIT for continuous operation:
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1010C
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Recommended climb TIT:
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950C
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Recommended cruise TIT:
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925C
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Maximum residual TIT for an in-flight restart (prior to F & I switch on):
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150C
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Maximum residual TIT for using PRIME (prior to F & I switch on):
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100C
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Maximum residual TIT for a ground start (prior to F & I switch on):
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200C
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Maximum TIT for hot start and continuing the start
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830C
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Maximum TIT for a hot start that requires a shutdown:
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850C
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Maximum TIT before a turbine inspection is required on a start:
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965C
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TIT overtemp light illuminates
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1080 +-2
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Maximum TIT allowed by the TD in temp controlling range:
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1077 +6-10C
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Amount of TIT rise during ground check of engine anti-ice system:
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CORRESPONDING
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Amount of TIT rise required during ground check of wing de-ice system:
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10C MIN
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Fuel heater strainer heats fuel to
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40-70F
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Zone 1 fire warning actuation temperature
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600F
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Zone 2 fire warning actuation temperature
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400F
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Zone 3 fire warning actuation temperature
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400F
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Normal engine oil temperature range for operation
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60-90C
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Normal engine oil temperature range for extremely cold weather operations:
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50-60C
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OIL HOT light illuminates:
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100C
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Transformer Rectifier overheat light illuminates:
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150C
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Leading Edge hot light illuminates:
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110C
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For takeoff, use engine anti-ice with visible moisture and temperatures below
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8C
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Loiter is not recommended with visible moisture and temp below:
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10C
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Loiter is not recommended with OAT below:
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0C
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MIL-L-23699 oil can be used down to:
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-40C
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MIL-L-7808 can be used down to:
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-54C
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-2 APU limits (continuous, peak 10 seconds, peak):
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688,710,715C
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-3 APU limits (continuous, peak):
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649,704C
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-10 APU limits (continuous, peak 10 seconds, peak)
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649,710,732C
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MAX REVERSE:
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0 *
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GROUND IDLE:
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9 *
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GROUND START:
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15 *
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NTS disabled below:
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24 *
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Pitchlock reset energized below:
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28 *
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Prop SYNC available above:
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32 *
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Oil cooler augmentation available below:
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32 *
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FLT IDLE:
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34 *
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Wheels warning below (with 153 knots):
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48 *
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Wheels warning below (with 142 knots):
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60 *
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FLT START:
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48 *
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Auto feather armed above:
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60 *
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TD switches to temp controlling above:
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66 *
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Beta follow up sets a minimum blade angle of 22.5 degrees at
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90 *
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Pitchlock cammed out below:
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17 *
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Pitchlock cammed out above:
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57*
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Pitchlock available between:
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17-57 *
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Low pitch stops sets minimum blade angle of:
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13 *
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Coordinator at MAX REVERSE:
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-13 *
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Coordinator at GROUND IDLE:
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-6 *
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Coordinator at GROUND START:
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0 *
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Coordinator at FLIGHT IDLE (beta range):
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11 *
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Coordinator at FLIGHT IDLE (alpha range):
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13 *
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Feather:
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86.65 *
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Pitchlock reset occurs when the power lever is below 28* and blade angle is above:
|
10 *
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Minimum air at 16%:
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25 PSI
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Oil pressure at 35%:
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RISING
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Oil pressure, RGB in LOW RPM:
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50-250 PSI
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Oil pressure, RGB in NORMAL RPM:
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130-250 PSI
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Oil pressure, power section in LOW RPM:
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50-60 PSI
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Oil pressure, power section in NORMAL RPM:
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50-60 PSI
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Max oil pressure, power section during start and warm-up:
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100 PSI
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OIL PRES light illuminates for RGB at:
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130 PSI
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OIL PRES light illuminates for power section at:
|
40 PSI
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Normal hydraulic pressure:
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2960-3200 PSI
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Minimum emergency brake pressure for flight
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1900 PSI
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Fuel boost pump lights illuminate (wing tank) at:
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2 PSI
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Fuel transfer pump lights illuminate at:
|
4 PSI
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Normal fuel boost pump pressure:
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15-30 PSI
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Minimum O2 for flight at 70 degrees F:
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1500 PSI
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A fully discharged brake accumulator statically reads:
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800 PSI +/- 25
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Fuel tank #5 pressure safe range (green section of indicator):
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0-7.0 PSI
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Fuel tank #5 pressure warning range (red section of indicator):
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+7 PSI
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Main and standby regulator valve maintains PSI higher than system demand by:
|
150 PSI
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Maximum oil pressure flux for RGB
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+-10 PSI
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Maximum oil pressure flux for power section
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+-5 PSI
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Maximum reverse SHP limits 1-4:
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1150+/- 150
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Maximum reverse SHP limits 2-3:
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1250 +/- 150
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Maximum SHP with oil temperature below 0 degrees C:
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MIN SHP
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Maximum SHP with oil temperature between 0 and 40 degrees C:
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1000 SHP
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Maximum SHP with oil temperature above 40 degrees C (no RGB flux):
|
MAX SHP
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Prop decouple range:
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-500 TO -1700 SHP
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NTS range for engines 1 and 4:
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-150 TO -500 SHP
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NTS range for engines 2 and 3:
|
-100 TO -500 SHP
|
|
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Minimum SHP for opening a bleed air valve during an NTS check
|
800 SHP
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Digital SHP gage red over torque light illuminates
|
@ 4600
|
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Maximum/Military/Normal rated SHP:
|
4600 SHP
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Flop over
|
5300 SHP
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Fuel tank capacity for tanks 1 and 4
|
1606 GAL
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Fuel tank capacity for tanks 2 and 3:
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1671 GAL
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Fuel tank capacity for tank 5:
|
1740 GAL
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Fuel tank capacity for tank 5A
|
906 GAL
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Prop de-ice current ranges for front spinners (ground test and flight):
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74-76 TO 100
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|
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Prop de-ice current ranges for cuffs (ground test and flight)
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48-51 TO 72
|
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Pro de-ice current ranges for aft spinners and islands (gnd test and flight):
|
58-63 TO 82
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|
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Applications a fully charged brake accumulator will give:
|
8
|
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Applications a fully charged emergency brake bottle will give:
|
3 FULL, 6 PARTIAL
|
|
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Hours a fully charged brake accumulator will hold the parking brakes for:
|
30
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Total capacity of #1 hydraulic system:
|
16.2 GAL
|
|
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Total capacity of #2 hydraulic system:
|
5.6 GAL
|
|
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Capacity of the #1 hydraulic system reservoir:
|
5.6 GAL
|
|
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Capacity of the #2 hydraulic system reservoir:
|
1.0 GAL
|
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Service level of the #1 hydraulic reservoir (in any configuration):
|
.8 GAL BELOW FULL
|
|
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Service level of the #2 hydraulic reservoir:
|
.75 GAL
|
|
|
Capacity of the bomb bay reservoir:
|
.75 GAL
|
|
|
Maximum wind velocity for opening the nose radome on deck:
|
20 KTS
|
|
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Output rating of the AC generators (volts, phase, frequency):
|
120 VAC, 3P, 400HZ
|
|
|
PMG rating (volts, phase, frequency):
|
39VAC, 1P, 600HZ
|
|
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Amount of air used for cooling and flame control in the engine (%):
|
75%
|
|
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Amount of air used for combustion in the engine (%):
|
25%
|
|
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Amount of dual element thermocouples on each engine:
|
18
|
|
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Max put capacity of the TD in temp controlling:
|
15%
|
|
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Max take capacity of the TD with RPM below 94%:
|
50%
|
|
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Max take capacity of the TD with RPM above 94%:
|
20%
|
|
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Bypass capacity of the TD:
|
20%
|
|
|
Isobaric range of operation (with AFC-341):
|
0-13.3 IN
|
|
|
Differential range of operation (with AFC-341):
|
13.3 TO 13.9 IN
|
|
|
Safety relief range of operation (with AFC-341):
|
13.9 TO 14.4 IN
|
|
|
Useable capacity of engine oil in the oil tank:
|
8.65 GAL
|
|
|
Unusable capacity of engine oil in the oil tank:
|
1.4
|
|
|
Foaming space:
|
5.7
|
|
|
Total capacity of engine oil tank:
|
15.75 GAL
|
