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EC-130H
EC-130H Limitations
| Term | Definition |
|---|---|
| MAX TIT FOR ENRICHMENT START | 100 C |
| MAX TIT FOR NORMAL START | 200 C |
| TIT DURING NORMAL START | 750-830 C |
| STARTING TIT <720C | MX ACTION REQUIRED |
| STARTING TIT 720-750C | 781 / TEMP CONTROLLING CHECK |
| STARTING TIT 830-850C | 781 |
| STARTING TIT 850-965C | STOP START / 718 / 1 RESTART |
| STARTING TIT EXCEEDS 965C | STOP START / 718 / MX |
| ABNORMAL TORCH DURING START | 781 / MX INSPECTION |
| TAKEOFF POWER ENGINE TIT | 1067 - 1083 C |
| TAKEOFF POWER MAX DURATION | 5 MINUTES |
| REDUCED POWER ENGINE TIT | 970 C |
| MILITARY POWER ENGINE TIT | 1049 C |
| MILITARY POWER MAX DURATION | 30 MINUTES |
| CLIMB / CONTINUOUS ENGINE TIT | 1010 C |
| CROSSOVER ENGINE TIT | 800-840 C |
| NORMAL LIMITING ENGINE TIT | 1083 C |
| MAX DOWNSPEED ENGINE TIT | 850 C |
| >1083 FOR 5 SECONDS OR >1175 MOMENTARILY | REDUCE POWER / 781 / OVERTEMP INSPECTION |
| TERMOCOUPLE MALF ENGINE TIT INDICATION | 3.5 - 22 C |
| MAX RPM FOR LIGHTOFF | 35% |
| MAX RPM FOR NO OIL PRESSURE | 35% |
| RPM FOR LOW SPEED GROUND IDLE | 69 - 75.5% |
| RPM FOR NORMAL GROUND IDLE | 94 - 102% |
| RPM FOR REVERSE | 96 - 106% |
| RPM IN FLIGHT IDLE (LOW PITCH STOP ENGAGED) | 92.5 - 100.5% |
| NORMAL RPM (NORMAL AND MECH GOV) | 98 - 102% |
| RPM ALLOWABLE FLUX | +/- 0.5% FOR TOTAL OF 1% |
| STARTER DISENGAGE RPM | 60% |
| PROP BREAK DISENGAGE RPM | 23% |
| PITCHLOCK RPM | 103% |
| FUEL TOPPING RPM | 103.5% |
| REINDEX CORRECTS APPROX RPM | 2-5% |
| MAX RPM FOR AIRSTART LIGHTOFF | 30 NORMAL / 40 MUST |
| OIL TEMP <0 TORQUE | MIN TORQUE |
| OIL TEMP 0-40C TORQUE | 4,500 IN-LBS MAX |
| MAX ALLOWABLE TORQUE | 19,600 IN-LBS |
| NTS ACTION TORQUE | -1,260 +/- 600 IN-LBS |
| ALLOWABLE REVERSE TORQUE DIFFERENCE | <1,000 IN-LBS BETWEEN SYMMETRICALS |
| DECOUPLES TORQUE | -6,000 IN-LBS |
| MIN TORQUE FOR PROP CHECK | 8,000 IN-LBS |
| MIN TORQUE FOR REINDEX | 8,000 IN-LBS |
| MAX TORQUE FOR PROP CHECK W/>10KT WIND OFFSET >30 DEGREES | 7,000 IN-LBS |
| MAX ENGINE OIL PRESSURE START/WARMUP | 100 PSI |
| NORMAL ENGINE OIL PRESSURE | 50-60 PSI |
| MINIMUM ENGINE OIL PRESSURE AT LSGI | <50 PSI OKAY IF WITHIN LIMITS AT 100% RPM/OIL TEMP NORMAL |
| ENGINE OIL PRESSURE ALLOWABLE FLUX | +/- 10 PSI |
| MAX GEARBOX OIL PRESSURE START/WARMUP | >250 PSI |
| NORMAL GEARBOX OIL PRESSURE | 150 - 250 PSI |
| MINIMUM GEARBOX OIL PRESSURE FOR MISSION ACCOMPLISHMENT | 130 PSI |
| MINIMUM GEARBOX OIL PRESSURE AT LSGI | <150 PSI OKAY IF WITHIN LIMITS AT 100% RPM/OIL TEMP NORMAL |
| GEARBOX OIL PRESSURE ALLOWABLE FLUX | +/- 20 PSI |
| NORMAL OIL QUANTITY | 4 - 12 GALLONS |
| OIL QUANTITY LOW LEVEL LIGHT | 4 GALLONS |
| OIL ALLOWABLE BURN RATE | 0.25 GAL/HR |
| OIL TEMP MAX ON GROUND (30 MINS) | 85 - 100 C |
| OIL TEMP MAX INFLIGHT (5 MINS) | 85 - 100 C |
| NORMAL OIL TEMP | 60 - 85 C |
| OIL TEMP MIN FOR START | -40 C |
| OIL TEMP MIN FOR TAKEOFF | 40 C AND INCREASING |
| OIL COOLER TRIES TO MAINTAIN | 80 C |
| DC VOLTAGE RANGE | 25 - 30 V |
| MAX DC LOAD | 1.03 |
| BATTERY VOLTAGE MINIMUM | 18 - 21 V |
| BATTERY VOLTAGE NORMAL | 24 V |
| DC POWER LIGHT | CORRECT POLARITY |
| 90 KVA GENERATOR FREQ RANGE | 380 - 420 HZ |
| AC VOLTAGE RANGE 90 KVA | 110 - 120 V |
| MAX AC LOAD | 1.0 |
| ATM GENERATOR CAPACITY | 20 / 30 KVA |
| ATM VOLTAGE | 110 - 125 V |
| ATM FREQUENCY | 380 - 420 HZ |
| ATM LOAD W/ COOLING AIR | 1.0 |
| ATM LOAD W/O COOLING AIR OR >40 C | 0.66 |
| CP INVERTER POWER/RATE ISO DC | 250 VA |
| AC EI&FC POWER/RATE ESS DC | 2500 VA |
| EXT AC POWER LIGHT | CORRECT PHASE |
| #1 SPECIAL SYSTEMS BUS POWER | #1 ENGINE GENERATOR |
| #2 SPECIAL SYSTEMS BUS POWER | #2 ENGINE GENERATOR |
| #3 SPECIAL SYSTEMS BUS POWER | #3 ENGINE GENERATOR |
| #4 SPECIAL SYSTEMS BUS POWER | #4 ENGINE GENERATOR |
| INBOARD / OUTBOARD FUEL DIFFERENTIAL | 500 - 1000 LBS |
| SYMMETRICAL FUEL DIFFERENTIAL | 1000 LBS |
| WING TO WING FUEL DIFFERENTIAL | 1500 LBS |
| EXTERNAL TANK FUEL DIFFERENTIAL | 1000 LBS |
| AUX TANK DIFFERENTIAL | 1 FULL 1 EMPTY |
| MAIN TANK BOOST PUMP PRESSURE | 15 - 24 PSI |
| AUX / EXT TANK BOOST PUMP PRESSURE | 28 - 40 PSI |
| LOW PRESSURE LIGHT ILLUMINATES | 8.5 PSI |
| TANK EMPTY LIGHT ILLUMINATES | 23 PSI |
| OUTBOARDS FUEL REMAINING AFTER DUMP | 2100 LBS |
| INBOARDS FUEL REMAINING AFTER DUMP | 1800 LBS |
| A/R SURGE CONTROL VALVE REGULATES PRESSURE | 45 - 60 PSI |
| A/R PRESSURE DISCONNECT SWITCH PRESSURE | 85 PSI |
| SPEAR POD MAX OUTBOARD FUEL ON GROUND (2 ANSWERS) | 6900 LBS GEN 2 / 6800 LBS GEN 3 |
| SPEAR POD MAX INBOARD FUEL ON GROUND | 7600 LBS |
| SPEAR POD MAX IN MAIN TANKS | 29,000 LBS |
| SPEAR POD MAX OUTBOARD FUEL INFLIGHT | 8300 LBS |
| SPEAR POD MAX INBOARD FUEL INFLIGHT | 7600 LBS |
| SPEAR POD INBOARD / OUTBOARD FUEL DIFFERENTIAL INFLIGHT (3 ANSWERS) | 400 - 800 GEN2 / 500 - 900 GEN3 / 500 - 1000 FOR MAX TANKER LOAD |
| SPEAR POD MAX OUTBOARD FUEL FOR LANDING | 6900 LBS |
| SPEAR POD MAX INBOARD FUEL FOR LANDING | 7600 LBS |
| PROP DE-ICING LOAD MIN/MAX | 65 - 90 AMPS |
| PROP DE-ICING TIMING CYCLE | 15 SEC ON / 45 SEC OFF |
| PROP DE-ICING MAX GROUND OPERATION | 2 CYCLES |
| PROP ANTI-ICE AMPERAGE | 20 AMPS / PROP |
| NORMAL HYDRAULIC PRESSURE | 2900 - 3200 PSI |
| MAX ALLOWABLE HYDRAULIC PRESSURE | 3500 PSI |
| MIN HYDRAULIC PRESSURE AT LSGI | 2550 PSI |
| MAX RPM FOR HYDRAULIC PRESSURE INDICATION | ON SPEED |
| MAX RPM FOR NORMAL HYDRAULIC PRESSURE INDICATION | ON SPEED + 30 SECONDS |
| AILERON PRESSURE | 2050 PSI |
| HYDRAULIC SYSTEM PRESSURE RELIEF OPENS AT | 3450 PSI |
| HYDRAULIC SYSTEM PRESSURE RELIEF FULL FLOW AT | 3850 PSI |
| ESP IF HYDRAULIC PRESSURE EXCEEDS | 3900 PSI |
| HYDRAULIC LOW PRESSURE LIGHT ILLUMINATES | 1000 PSI |
| SUCTION BOOST PUMP LIGHT ILLUMINATES | 20 PSI |
| MINIMUM PRESSURE W/ FAILED SUCTION BOOST PUMP | 2500 PSI |
| AUX SYSTEM NORMAL PRESSURE | 2900 - 3300 PSI |
| AUX SYSTEM MAX PRESSURE | 3500 PSI |
| MAX HANDPUMP PRESSURE | 4100 PSI |
| UTILITY PRELOAD PRESSURE | 1500 +/- 100 PSI |
| BOOSTER PRELOAD PRESSURE | 1500 +/- 100 PSI |
| AUX PRELOAD PRESSURE | 300 PSI |
| NORMAL BRAKES HYDRAULIC ACCUMULATOR PRESSURE | 1500 +/- 100 PSI |
| EMERGENCY BRAKES HYDRAULIC ACCUMULATOR PRESSURE | 1000 +/- 100 PSI |
| UTILITY RESERVOIR / SYSTEM QUANTITY | 3.2 GAL / 13.1 GAL |
| BOOSTER RESERVOIR / SYSTEM QUANTITY | 2.0 / 9.2 GAL |
| AUX RESERVOIR / SYSTEM QUANTITY TYPE 1 | 3.4 / 6.6 GAL |
| AUX RESERVOIR QUANTITY TYPE 2 | 6.22 GAL |
| NORMAL BRAKE PRESSURE | 2900 - 3200 PSI |
| MAX ALLOWABLE NORMAL BRAKE PRESSURE | 3500 PSI |
| 2 NORMAL BRAKE APPLICATIONS REMAIN | 2900 PSI |
| 1 NORMAL BRAKE APPLICATION REMAINS | 2250 PSI |
| EMERGENCY BRAKE PRESSURE NORMAL PRESSURE | 2900 - 3300 PSI |
| EMERGENCY BRAKE PRESSURE MAX PRESSURE | 3500 PSI |
| 1 EMERGENCY BRAKE APPLICATION REMAINS | 2900 PSI |
| NORMAL 0 - 15% FLAPS RUDDER BOOST PRESSURE | 1100 - 1400 PSI |
| CAUTION 0 - 15% FLAPS RUDDER BOOST PRESSURE | 1400 - 1600 PSI |
| MAX 0 - 15% FLAPS RUDDER BOOST PRESSURE | 1600 PSI |
| NORMAL 15 - 100% FLAPS RUDDER BOOST PRESSURE | 2900 - 3200 PSI |
| MAX 15 - 100% FLAPS RUDDER BOOST PRESSURE | 3500 PSI |
| OXYGEN SYSTEM FULL QUANTITY | 25 L |
| OXYGEN SYSTEM MIN QUANTITY FOR USE | 2.5 L |
| OXYGEN SYSTEM OPERATING PRESSURE NO FLOW | 270 - 455 PSI |
| OXYGEN SYSTEM OPERATING PRESSURE CONTINUOUS FLOW | 270 - 340 PSI |
| OXYGEN SYSTEM LOW QUANTITY LIGHT ILLUMINATES | 2.5 L |
| GTC NORMAL RPM | 95 - 105% |
| GTC OVERSPEED RPM | 110% |
| GTC START LIGHT RPM | 35% |
| GTC ON SPEED LIGHT RPM | 95% |
| GTC FUEL & IGNITION CIRCUITS ENERGIZED | OIL PRESSURE REACHES 3 PSI |
| GTC STARTER DUTY CYCLE | 1 MIN ON / 4 MINS OFF |
| GTC WARM UP >0C | 1 MIN |
| GTC WARM UP <0C | 4 MIN |
| LEADING EDGE ANTI-ICE MAX GROUND OPERATION | 30 SEC |
| LEADING EDGE ANTI-ICE GAUGE INOP RANGE | 0 - 75 F |
| LEADING EDGE ANTI ICE-GAUGE NORMAL RANGE | 70 - 200 F |
| LEADING EDGE ANTI-ICE GAUGE OVERHEAD RANGE | >200 F |
| LEADING EDGE ANTI-ICE CONTROL VALVE OPENS/CLOSES | 158 / 180 F |
| LEADING EDGE ANTI-ICE MIXED AIR TEMP | 350 F |
| NESA MAX OAT GROUND OPS | 81 F / 27 C |
| NESA COLD START PROCEDURE | -43 C, 5 SEC ON/ 10 SEC OFF |
| GTC MIN BLEED AIR PRESSURE | 35 PSI |
| GTC BLEED DOWN CHECK | 30 - 15 PSI IN >8.5 SEC |
| ENGINE BLEED AIR MIN PRESSURE FOR CHECK | 70 PSI |
| ENGINE BLEED AIR CHECK | 65 - 35 PSI IN >10 SEC |
| DIFFUSER AIR PSI / TEMP | 125 PSI AT 600 F |
| FLIGHT DECK A/C EFFECT ON PSI GUAGE | PSI GUAGE READS 6 PSI LOW |
| PRESSURIZATION GAUGE RANGE | -1.2 - 15.8 IN HG |
| SAFETY VALVE OPENS | -0.76 - 15.9 IN HG |
| MAX DIFFERENTIAL PRESSURE | 15.16 IN HG |
| 1 PANE WINDSCREEN CRACKED CABIN PRESSURE | <10 IN HG |
| 1 PANE CARGO COMP CRACKED | <10 IN HG |
| 2 PANE CARGO COMP CRACKED | 0 IN HG |
| PRESSURIZATION RATE CONTROLLER MIN | 30 - 200 |
| PRESSURIZATION RATE CONTROLLER MID | 900 |
| PRESSURIZATION RATE CONTROLLER MAX | 1600 - 2900 |
| CREWDOOR JETTISON PRESSURIZATION LIMIT | 3.1 IN HG |
| TIME TO GAIN CONTROL OF OUTFLOW VALVE FROM AUTO TO MANUAL | 40 SEC |
| MAX TAXI WEIGHT | 155,000 |
| MAX TAKEOFF WEIGHT | 155,000 |
| EWP TAKEOFF WEIGHT | 175,000 |
| RECOMMENDED LANDING WEIGHT | 130,000 |
| EWP LANDING WEIGHT | 155,000 |
| CROSSWIND TAXI | 30 KNOTS / 90 DEGREES |
| MAX CROSSWIND TAXI | 60 KNOTS / 90 DEGREES |
| TURN LIMIT >155K OR AT 20 KNOTS | 20 DEGREES |
| T-STORM PENETRATION AIRSPEED | POWER OFF STALL SPEED +65 KNOTS NOT TO EXCEED 180 KNOTS |
| WINDMILL TAXI START AIRSPEED | 100 KIAS UNTIL 4K RUNWAY REMAINING |
| 10% FLAPS MAX AIRSPEED | 220 KNOTS |
| 20% FLAPS MAX AIRSPEED | 210 KNOTS |
| 50% FLAPS MAX AIRSPEED | 180 KNOTS |
| 100% FLAPS MAX AIRSPEED | 145 KNOTS |
| CARGO RAMP & DOOR OPEN MAX AIRSPEED | 150 KNOTS |
| CARGO DOOR OPEN MAX AIRSPEED | 185 KNOTS |
| PARATROOP DOOR UNLOCKED MAX AIRSPEED | 150 KNOTS |
| PARATROOP DOOR OPEN & LOCKED MAX AIRSPEED | 250 KNOTS |
| AIR DEFLECTOR DOORS MAX AIRPSEED | 150 KNOTS |
| LANDING GEAR AND LIGHTS MAX AIRSPEED | 165 KNOTS |
| PAINTED SURFACES (NOT STENCILED) MAX AIRSPEED | 250 KNOTS |
| AIR START AIRSPEED | 180 KNOTS |
| AIR START AIRSPEED W/ NO NTS | 130 KNOTS |
| BAILOUT CREW ENTRANCE DOOR AIRSPEED | 150 KNOTS |
| MAX NOSE TIRE ROTATION GROUND SPEED | 139 KNOTS |
| MAX MAIN TIRE ROTATION GROUND SPEED | 174 KNOTS |
| MAX BANK ANGLE 0% FLAPS | 60 DEGREES |
| MAX BANK ANGLE W/ FLAPS | 45 DEGREES |
| TEMP LIMITING (THROTTLE TRAVEL) | 0 - 65 DEGREES |
| TEMP CONTROLLING (THROTTLE TRAVEL) | 65 - 90 DEGREES |
| LOW SPEED GROUND IDLE RANGE (THROTTLE TRAVEL) | 9 - 30 DEGREES |
| PITCHLOCK RANGE (PROP DEGREES) | 25 - 55 DEGREES |
| WITH PITCHLOCKED PROP, MAINTAIN RPM | 96 - 98% RPM |
| TO UNLOCK PITCHLOCK | INCREASE BLADE ANGLE 2 DEGREES |
| FEATHER BLADE ANGLE | 92.5 DEGREES |
| REVERSE BLADE ANGLE | -6 TO -8 DEGREES |
| COLD WEATHER OPS TEMP | 0 C / 32 F |
| HOT WEATHER OPS TEMP | 35 C |
| BATTERY BUS ITEMS | 1. FIRE EXT 2. ALARM BELL 3. JUMP LIGHTS 4. ISOL DC BUS OFF IND 5. DC VOLT METER 6. EMERG DEPRES 7. EMERG EXIT LIGHT EXT 8. AC EXT POWER SW SOL 9. EMERGENCY LOCATOR TRANSMITTOR 10. (AVP) ESIS SEC POWER 11. (AVP) SSAC REL CONTROL |
| ENGINE SHUTDOWN CONDITIONS | 1 ENG FIRE 2 TURBINE O/H 3 NACELLE O/H 4 UNCONTROL PWR 5 CERTAIN PROP MALFS 6 UNCONTROL RISE IN TIT 7 UNCONTROL DROP IN OIL PRESS 8 UNCONTROL RISE IN OIL TEMP 9 UNUSUAL VIBRATION/ROUGHNESS 10 THROTTLE CNTRL CABLE FAIL 11 EXCESSIVE VIS FLUID LEAK |
| FIRE HANDLE PULLED | 1 SHUTOFF VLV/ENG FUEL CONT CLS 2 ENG OIL SHUTOFF VLV CLS 3 FIREWALL FUEL SHUTOFF VLV CLS 4 FIREWALL HYD SHUTOFF VLVS CLS 5 ENG BLEED AIR VALVE CLOSED 6 START CONTROL CIRCUITS DEENERGIZED 7 PROP FEATHERED 8 FIRE EXT VALVES POSITIONED 9 AGENT ARMED |
| PROP AUX PUMP LIMITS | 1 MIN ON / 1 MIN OFF : NOT TO EXCEED 2 OPERATIONS IN ANY 30 MIN PERIOD |
| PROP STATIC FEATHER CHECK LIMITS | TIME REVERSE TO FEATHER 25 SEC : MIN OIL TEMP 20 C |
| TURBINE OVERHEAT TEST | NO MORE THAN 30 SEC ON. DO NOT TEST AGAIN FOR 1 MIN |
| TURBINE OVERHEAT DETECTORS | 4 AT 700 F |
| NACELLE OVERHEAT DETECTORS | 7 AT 300 F |
| ENGINE STARTER DUTY CYCLE | 1 ON / 1 OFF / 1 ON / 5 OFF / 1 ON / 30 OFF |
| NEGATIVE G CONDITION | MONITOR FOR 2 MINS. IF OIL PRESSURE IS LOST & NOT BACK IN 10 SECONDS, ESP |
| AIRCRAFT FIRE EXT BOTTLE PRESSURE | 600 - 640 PSI AT 70 F |
| NORMAL BRAKE COOLING TIME FOR ABORTED TAKEOFF OR FLAPS UP LANDING ABOVE 130K | 65 MINS |
| NORMAL BRAKE COOLING TIME WHEN BRAKES ARE CHECKED DURING GROUND ROLL | 10 MINS. OMITTED IF RUNWAY AVAILABLE EXCEEDS CFL BY 300 FEET |
| FUSIBLE PLUGS | 3 IN EACH WHEEL ASSEMBLY SET AT 390 F |
| PEAK TEMPS OCCUR IN BRAKE ASSEMBLY | 1 - 5 MINS |
| PEAK TEMPS OCCUR IN WHEEL ASSEMBLY | 20 - 30 MINS |
| DO NOT TOW OR TAXI A/C AFTER MAX BRAKE APPLICATIONS | 15 MINS |
| MAX G'S SYMMETRICAL MANEUVER | -1 TO 3.0 G |
| MAX G'S UNSYMMETRICAL MANEUVER | 0 - 2.33 G |
| DIGITAL FUEL QUANTITY INDICATOR MALFUNCTIONS THAT REQUIRE C/B TO BE PULLED | INOPERATIVE, E6, E8, E9 |
| HOT BRAKE DISTANCE | CLEAR FOR 300 FEET. W/ FLARES, CLEAR FOR 600 FEET |
| LOW PITCH STOP CHECK SHOULD GET TORQUE INCREASE | >200 IN LBS OF TORQUE INCREASE |
Created by:
tuffkix
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