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C-130H2 Ops Limits
| Question | |
|---|---|
| STARTING TIT: Max with enrich on (ground) | 100 C |
| STARTING TIT: Max without enrichment | 200 C |
| STARTING TIT: Max for air start | 200 C |
| STARTING TIT: Normal start limits | 750 – 830 C |
| STARTING TIT: TIT < 720 C: Do what? | write up, see MX |
| STARTING TIT: TIT 720 – 749 C: | write up, temp controlling check |
| STARTING TIT: TIT 830 – 850 C: | write up |
| STARTING TIT: TIT 850 – 965 C: | stop, write up, 1 retry |
| STARTING TIT: TIT >965 C: | stop, write, and see MX |
| STARTING TIT: Abnormal torch | stop, write, see MX |
| STARTING TIT: Engine start cycle (1 on, then) | 1 off, 5 off, 30 off |
| ENGINE TIT: Normal continuous range | 200 – 1010 C |
| ENGINE TIT: Takeoff range / time | 1067 - 1083 C / 5 min |
| ENGINE TIT: Takeoff reduced minimum | 970 C |
| ENGINE TIT: Military limit / time | 1049 C / 30 min |
| ENGINE TIT: Climb / max continuous | 1010 C |
| ENGINE TIT: Acceleration peak limits | >1083 C (5 secs)/1175 C max |
| ENGINE TIT: Crossover | 820 C +/- 20 C |
| ENGINE TIT: Normal Limiting | 1083 C |
| ENGINE TIT: Max downspeed TIT | 850 C |
| ENGINE TIT: # of thermocouples | 18 (2 elements each) |
| ENGINE TIT: thermocouple bad – range | 3.5 to 22 C degrees each |
| ENGINE RPM: Oil pressure / ignition by | 35% |
| ENGINE RPM: Normal Flight & Takeoff | 98 – 102% +/- 0.5% |
| ENGINE RPM: Norm flight idle (on ground) | 92.5 – 100.5% |
| ENGINE RPM: Normal ground idle | 94 - 102% |
| ENGINE RPM: Max reverse | 96 – 106% |
| ENGINE RPM: Low speed ground idle | 69 – 75.5% |
| ENGINE RPM: Ignition Relay on / off | 16% / 65% |
| ENGINE RPM: Feather on air start if no NTS by | 10% |
| ENGINE RPM: Air start light off norm/max | 30% / 40% max |
| ENGINE RPM: Speed sensitive valve actuate | 94% |
| ENGINE RPM: LSGI range | 9 - 30 deg |
| ENGINE TORQUE: Oil temp < 0 C | minimum |
| ENGINE TORQUE: Oil temp 0 to 40 C | 4,500 IN-LBS max |
| ENGINE TORQUE: Max allowable - takeoff | 19,600 IN-LBS (for 5 min) |
| ENGINE TORQUE: Max allowable in flight | 19,600 IN-LBS (30 min) |
| ENGINE TORQUE: Max continuous | 19,600 IN-LBS |
| ENGINE TORQUE: NTS operates at | -1,260 +/- 600 IN-LBS |
| ENGINE TORQUE: Torque to decouple | -6,000 IN-LBS |
| ENGINE TORQUE: Allowable Reverse Differential | 1,000 IN-LBS |
| THROTTLES: Temp Limiting Range | 0 - 65 degrees |
| THROTTLES: Temp Controlling Range | 0 - 65 degrees |
| THROTTLES: LSGI range | 9 - 30 degrees |
| AC ELECTRICAL: Frequency range | 380-420 cps |
| AC ELECTRICAL: Voltage range | 110-125 v |
| AC ELECTRICAL: Max AC load | 1.05 |
| AC ELECTRICAL: APU generator capacity | 40 kva |
| AC ELECTRICAL: APU generator load | 1.05 |
| AC ELECTRICAL: Gen caution (out) light illuminates | any phase below or equal to 95 for 4 seconds. |
| AC ELECTRICAL: Bus caution (off) light illuminates | average phase below 96v / any phase below 100v |
| AC ELECTRICAL: Generator capacity | 40 kva |
| DC ELECTRICAL: Voltage Range | 25-30v |
| DC ELECTRICAL: Max DC load | 1.03 |
| DC ELECTRICAL: DC power sources | Battery, 4TRs, Ext |
| DC ELECTRICAL: Battery voltage norm / min | 24v / 21v |
| DC ELECTRICAL: AC&EFC inverter power | ESSENTIAL DC |
| DC ELECTRICAL: Copilot inverter power | ISOLATED DC |
| PROP DE-ICE & ANTI-ICE: Timing cycle (De-Ice) | 15 sec on / 45 sec off |
| PROP DE-ICE & ANTI-ICE: Max Ground ops time (De-Ice) | 2 cycles (2 minutes) |
| PROP DE-ICE & ANTI-ICE: De-Icing amp load range | 65-90 Amps |
| PROP DE-ICE & ANTI-ICE: Anti-Ice amps | 20 Amps |
| WINDSHIELD ANTI-ICE: Cold Start Procedure | 5 seconds on, 10 seconds off, until -43 C |
| WINDSHIELD ANTI-ICE: Max OAT operations | 81 F (27 C) |
| WINDSHIELD ANTI-ICE: NESA temp / # of windows | 80-100 F / 9 |
| LEADING EDGE ANTI-ICE: Max ground ops time | 30 sec |
| LEADING EDGE ANTI-ICE: Normal operating range | 75-200 C |
| LEADING EDGE ANTI-ICE: Overheat range | >200 C |
| LEADING EDGE ANTI-ICE: Control valve open/close | 158-180 C |
| LEADING EDGE ANTI-ICE: Norm temp of anti-ice air | 350 C |
| LEADING EDGE ANTI-ICE: Check leading edge altitude / temp | >5000 ft MSL or < 20 C |
| FUEL DISTRIBUTION: Inboard / Outboard difference | 500 LBS - 1000 LBS |
| FUEL DISTRIBUTION: Symmetrical Tank difference | 1000 LBS |
| FUEL DISTRIBUTION: Wing to Wing difference | 1500 LBS |
| FUEL DISTRIBUTION: External Tank difference | 1000 LBS |
| FUEL DISTRIBUTION: Aux Tank difference | No factor |
| FUEL DISTRIBUTION: Max Effort Fuel Load | 6,200 LBS outboards, 23,500 LBS total in mains |
| FUEL SYSTEM PRESSURE: Main tank pump pressure | 15 – 24 psi |
| FUEL SYSTEM PRESSURE: Aux & ext tank pump pressure | 28 – 40 psi |
| FUEL SYSTEM PRESSURE: Low fuel press light on | 8.5 psi |
| FUEL SYSTEM PRESSURE: Aux & ext tank empty light | 23 psi |
| OXYGEN AND LIFE SUPPORT: O2 ports flight deck / total | 6 / 10 |
| OXYGEN AND LIFE SUPPORT: Fully serviced quantity | 25 liters |
| OXYGEN AND LIFE SUPPORT: Low light on | 2.5 liters on gage |
| OXYGEN AND LIFE SUPPORT: Press range (no flow) | 270-455 psi |
| OXYGEN AND LIFE SUPPORT: Press range (continuous) | 270-340 psi |
| OXYGEN AND LIFE SUPPORT: # of life rafts / capacity | 4 / 20 men |
| OXYGEN AND LIFE SUPPORT: Fire extinguishers | 4 |
| OXYGEN AND LIFE SUPPORT: Emergency lights illuminate | -2.5g’s or ESS DC off |
| OXYGEN AND LIFE SUPPORT: # of Emergency exit lights | 8 |
| OXYGEN AND LIFE SUPPORT: Portable oxygen bottles | 4 |
| ENGINE OIL PRESSURE: Max (start & warm-up) | 100 psi |
| ENGINE OIL PRESSURE: Normal range / allowable flux | 50-60 psi +/- 10 psi |
| ENGINE OIL PRESSURE: Minimum (LSGI) | <50 psi if normal at 100% |
| ENGINE OIL PRESSURE: After negative G, monitor engine for | 2 minutes |
| ENGINE OIL PRESSURE: After negative G, pressure should return within | 10 seconds (if not do ESP) |
| ENGINE OIL PRESSURE: After negative G, loss of oil when? | 30 to 90 seconds |
| GEARBOX OIL PRESSURE: Max (start & warm-up) | >250 psi |
| GEARBOX OIL PRESSURE: Normal range / allowable flux | 150-250 psi +/- 20 psi |
| GEARBOX OIL PRESSURE: Mission continuation | 130 psi |
| GEARBOX OIL PRESSURE: Minimum (LSGI) range | 50-250 psi |
| OIL TEMPERATURE: Max taxi & time | 85-100 C / 30 min |
| OIL TEMPERATURE: Max in-flight & time | 85-100 C / 5 min |
| OIL TEMPERATURE: Normal range | 60-85 C |
| OIL TEMPERATURE: Oil Cooler flaps maintain | 78-82 C |
| OIL TEMPERATURE: Minimum for takeoff | 40 C and increasing |
| OIL TEMPERATURE: Minimum (start & warm-up) | -40 C |
| OIL QUANTITY: Capacity range | 4 to 12 gal |
| OIL QUANTITY: Expansion space | 7.5 gal |
| OIL QUANTITY: Low light at | 4 gal |
| OIL QUANTITY: Allowable burn rate | 1 qt/hr (.25 gal/hr) |
| HYDRAULICS: Engine Pump Norm/Max | 2900-3200 / 3500psi |
| HYDRAULICS: Aux & Emergency Norm/ Max | 2900-3300 / 3500psi |
| HYDRAULICS: Shutdown if pressure over | 3900 psi |
| HYDRAULICS: RPM for indication | on speed |
| HYDRAULICS: RPM for norm press | 30 sec after on speed |
| HYDRAULICS: LSGI minimum press | 2550 psi |
| HYDRAULICS: Aileron boost pressure | 2050 psi |
| HYDRAULICS: Low press light on / off | 1000 psi / 1350 psi |
| HYDRAULICS: Suction boost light on | 20 psi |
| HYDRAULICS: Norm - 2 brake app left | 2900 - 3200 psi |
| HYDRAULICS: Norm – 1 brake app left | 2250 psi |
| HYDRAULICS: Emergency – 1 brake app left | 2900 psi |
| HYDRAULICS: Emergency accumulator preload | 1000 +/- 100 psi |
| HYDRAULICS: Utility/Boost/brake preload | 1500 +/- 100 psi |
| HYDRAULICS: Loss of sys press checklist | <2500 psi |
| HYDRAULICS: Do not shut off pump if | > 3450 |
| HYDRAULICS: Flaps 0-15: norm/caution | 1100-1400 / 1600 psi |
| HYDRAULICS: Flaps 15-100: norm/caution. | 2900- 3200/ 3500 psi |
| HYDRAULICS: Fluid quantity on board | 21 quarts (5 gal) |
| APU: Normal temp range | 260-650 C |
| APU: Max EGT | 650 C |
| APU: Normal RPM range | 95% - 105% |
| APU: Max RPM | 106% |
| APU: Stop switch | 110% |
| APU: Starter cycle | 1 min on, 4 min off |
| APU: Warm up | 1 minute for bleed air load |
| APU: Start and operate below | 20,000 MSL |
| APU: Door open ground / flight | 35 deg / 15 deg |
| APU: APU fuel burn | Approx 400 lbs/hr |
| PROPS: Prop brake disengage | 23% or starter app |
| PROPS: Pitchlock range | 25 - 55 deg |
| PROPS: Pitchlock RPM | 103% |
| PROPS: In pitchlock, maintain RPM | 96% - 98% |
| PROPS: To unlock pitchlock | Increase 2 deg |
| PROPS: Lo pitch stop blade angle | 23 deg |
| PROPS: Low pitch stop test | >200 in-lbs increase |
| PROPS: Prop oil quantity (total) | 26 quarts (6.5 gal) |
| PROPS: Prop oil sump capacity | 6.5 quarts in press side |
| PROPS: Prop low oil light on at | 2 quarts low in press side |
| PROPS: Torque to decouple | -6000 in-lbs |
| PROPS: Prop aux pump limit | 1 min on, 1 min off, not > 2 min in 30 min |
| PROPS: Static feather check time (R - F) | 25 sec |
| PROPS: Pull out if not pop out in | 6 sec |
| PROPS: Prop fail to feather, hold for | 30 sec |
| PROPS: NTS operates at | -1,260 +/- 600 in-lbs |
| PROPS: Blade angle in reverse | -6 to -8 degrees |
| BLEED AIR: Diffuser air temp/press | 600 F / 125 psi |
| BLEED AIR: Engine minimum out press (override) | 70 psi |
| BLEED AIR: Ground check for engine | 65–35 psi >= 16 sec |
| BLEED AIR: Ground check for APU | 30–15 psi >= 16 sec |
| BLEED AIR: Regulated output (Norm) | 40 - 50 psi |
| BLEED AIR: Regulators must be within | 3 psi of each other |
| PRESSURIZATION: Gauge range | -1.2 to 15.8” Hg |
| PRESSURIZATION: Safety valve open | < -0.76 & > 15.9” Hg |
| PRESSURIZATION: Controller nominal press | 15.16” Hg |
| PRESSURIZATION: Cockpit windshield cracked (1 or 2 panes) | 10” Hg max |
| PRESSURIZATION: Cargo windshield cracked (1 pane) | 10” Hg max |
| PRESSURIZATION: Cargo windshield cracked (2 panes) | 0” Hg max |
| PRESSURIZATION: Rate controller min / max rates | 30-200 / 1600-2900 |
| PRESSURIZATION: Crew door jettison pressure | < 3.1” Hg |
| PRESSURIZATION: Pressure to open pressure regulator valve | 12 psi |
| AIRSPEEDS AND ANGLES: Max airspeed (mach) | 0.64 mach |
| AIRSPEEDS AND ANGLES: T-storm penetration | 65 + power off stall, not to exceed 180 KIAS |
| AIRSPEEDS AND ANGLES: Windmill Taxi Start | 100 KIAS until 4000 feet / 40% |
| AIRSPEEDS AND ANGLES: Flaps 10 / 20 / 30 / 40 /50 | 220/210/200/190/180 |
| AIRSPEEDS AND ANGLES: Flaps 60/ 70 / 80 /90 /100 | 165/155/150/145/145 |
| AIRSPEEDS AND ANGLES: Door Only | 185 KIAS |
| AIRSPEEDS AND ANGLES: Ramp and Door | 150 KIAS |
| AIRSPEEDS AND ANGLES: Air deflector / troop door | 150 KIAS |
| AIRSPEEDS AND ANGLES: Lights | 250 KIAS |
| AIRSPEEDS AND ANGLES: Gear | 165 KIAS |
| AIRSPEEDS AND ANGLES: Wipers ineffective | 180 KIAS |
| AIRSPEEDS AND ANGLES: Troop door open / locked | 250 KIAS |
| AIRSPEEDS AND ANGLES: Crewdoor bailout | 150 KIAS |
| AIRSPEEDS AND ANGLES: Tire rotation (nose/main) | 139 KGS / 174 KGS |
| AIRSPEEDS AND ANGLES: Crosswind taxi norm/max | 30 KIAS / 60 KIAS |
| AIRSPEEDS AND ANGLES: Ditching | 10 + stall w/full flaps |
| AIRSPEEDS AND ANGLES: Max bank angle | 60 degrees |
| AIRSPEEDS AND ANGLES: Max bank angle w/flaps | 45 degrees |
| AIRSPEEDS AND ANGLES: Lowest vertical clearance | 5’ 9” (inboard prop) |
| AIRSPEEDS AND ANGLES: Max speed w/ 60 degrees nose wheel | 5 KIAS |
| AIRSPEEDS AND ANGLES: Max turn angle >=20 kgs | 20 degrees max |
| AIRSPEEDS AND ANGLES: Max speed/angle >= 155,000 lbs | 10 KIAS / 20 degrees |
| AIRSPEEDS AND ANGLES: Angle of flaps at full | 35 degrees |
| AIRSPEEDS AND ANGLES: Max reverse best at | 60 to 90 KIAS |
| AIRSPEEDS AND ANGLES: Hold / Instrument approach entry speed | 170 KIAS |
| AIRSPEEDS AND ANGLES: Inbound on approach speed | 150 KIAS |
| AIRSPEEDS AND ANGLES: Air Start with no NTS | 130 KIAS below 5000’ |
| AIRSPEEDS AND ANGLES: Recommend air start speed | 180 KIAS |
| AIRSPEEDS AND ANGLES: Airspeed for prop malfunction | 150 KTAS |
| AIRSPEEDS AND ANGLES: Elevator trim tab – electrical stop | 6 degrees down / 25 degrees up |
| AIRSPEEDS AND ANGLES: Elevator trim tab – mechanical stop | 8 degrees down / 27 degrees up |
| MISC: Temp for nacelle overheat | 300 F |
| MISC: Temp for turbine overheat | 700 F |
| MISC: # of nacelle/turbine overheat sensors | 7 nacelle / 4 turbine |
| MISC: Acceleration bleed valve open | below 94% RPM |
| MISC: Gear extension/retraction | 19 seconds or less |
| MISC: Preheat eng & APU below | -37 C |
| MISC: Cold WX Ops temperature | <= 0 C (32 F) |
| MISC: Hot WX Ops temperature | > 35 C (95 F) |
| MISC: Hot brake peak temperature time | 1 to 5 minutes |
| MISC: Peak hot temperature in wheel/tire | 20 to 30 min |
| MISC: Fusible plugs in tire melt | 390 F degrees |
| MISC: Cold WX Ops: LSGI until oil temp | 0 C degrees or more |
| MISC: Cold WX Ops: in ground idle until | 40 C degrees oil temp |
| MISC: Underfloor heat temp | 80 F |
| MISC: Start: prop rotation time | 5 sec max |
| MISC: Start: Starter Valve light on in | 5 seconds max (2-3 psi to open) |
| MISC: Start: Starter Valve light out in | 15 seconds after start release |
| MISC: Seat inertial reel locks at | 2 to 3 G’s |
| MISC: Pitot tubes for pilot / copilot | 1 & 3 / 2 & 4 |
Created by:
C130FE
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