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C-130E Limitations Last update 11 July 2007

This document provides the limitations and operating parameters for the C-130E aircraft. It covers topics such as temperature limits, engine TIT, engine torque, prop de-icing, windshield anti-ice, oil quantity, AC electric, and DC electric.

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C-130E Limitations Last update 11 July 2007

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  1. C-130E Limitations Last update 11 July 2007

  2. TABLE OF CONTENTS Click a category to jump to that slide, or spacebar to advance through every slide.

  3. STARTING TIT Click to return to Table Of Contents 100 °C 200 °C 830 °C Stop Start / 781 / Inspect 781 / MX required 781 / Temp Control Check Normal Start Limits 781 / Continue Start Stop Start / 781 / Retry Stop Start / 781 / Overtemp Inspec Max for enrichment………………………………. Max Normal Start………………….……………… Max During Start………..………………………… What do you do if? Abnormal Torch…………………………………... 720 °C or less……………………………………... 720 °C to 750 °C …………………….................... 750 °C to 830 °C………………………………….. 830 °C to 850 °C………………………………….. 850 °C to 965 °C………………………………….. Exceeds 965 °C…………….……………………..

  4. ENGINE TIT Click to return to Table Of Contents Takeoff Max (5 minutes)……………………………….. Takeoff Range……………………………………........... Takeoff Reduced Min...…………………………………. Normal Continuous……………………………………... Military (30 Minutes)…………………………………….. Climb……………………………………………………… Exceeds 977 °C over 5 seconds or 1070 °C Momentarily… Crossover………………………………………………… Normal Limiting………………………………………….. Max Downshift TIT………………………………………. 977 °C 961 °C - 977 °C 900 °C / 932 °C 200 °C - 932 °C 977 °C 932 °C 781 / O/T Inspection 65° / 760 °C ± 20 977 °C 850 °C

  5. Engine RPM Click to return to Table Of Contents 35 % 35 % 69 – 75.5 % 94 – 102 % 96 – 106 % 92.5 – 100.5 % 98 – 102 % ± .5 60 % Ignition By…………………………………….….. Oil Pressure Indicated By………………….….. Low Speed Ground Idle………………….…….. Normal Ground Idle…………………………..…. Max Reverse………………………………………. Flight Idle On Ground……………………………. Normal (Including Takeoff)…………………..…. Starter Disengage……………………………..….

  6. ENGINE TORQUE Click to return to Table Of Contents Min Torque 4500 lbs 19,600 lbs 19,600 lbs -1260 ± 600 lbs 8,000 in-lbs >200 in-lbs 19,600 in-lbs -6000 in-lbs Oil Temp < 0 °C………………………..……….... Oil Temp 0 °C - 40 °C……………………………. Max Allow on Takeoff……………………………. Max Allow in Flight………………………………. NTS Action………………………………………… Propulsion Check……………………………..…. Torque Comparison Check………………….…. Max Continuous………………………………….. Safety Coupling………………………………...…

  7. PROP DE-ICING Click to return to Table Of Contents 65 – 90 Amps 15 Seconds On / 45 Sec. off 2 Cycles (2 minutes) 20 Amps per prop Load Range………………………………….…….. Timing Cycle…………………………………….… Max Ground Ops…………………………………. Anti Ice Amperage………………………………..

  8. WINDSHIELD ANTI-ICE Click to return to Table Of Contents 27 °C / 81 °F 5 Sec On / 10 sec off until -43 °C Max OAT Operation………………………..…….. Cold Start………………………………….……….

  9. OIL QUANTITY Click to return to Table Of Contents 4 to 12 Gallons 4 Gallons .35 Gal/Hour Capacity Range…………………………………... Low Light………………………………………...… Allowable Burn Rate……………………………...

  10. AC ELECTRIC Click to return to Table Of Contents 380 – 420 Hz (4 cyc/rpm 110 – 125 V 1.05 40 Kva 20 Kva / 30 Kva below 104 °F 0.66 / 1.0 below 104 °F 115 / 200 V, 400 Cycle Freq Range………………………………………… Voltage Range…………………………..………… Max Load In Flight……………………………..… Generator Capacity………………………………. ATM Capacity……………………………………... ATM Load………………………………………….. AC Gen Rating…………………………………….

  11. DC ELECTRIC Click to return to Table Of Contents 25-30 V / 28 V 1.03 24 V / 21 V 21 V Batt / 4 TR’s / External Iso DC Bus Essential DC Bus 2 Gens Volt Range / Norm...……………………………… Max DC Load……………………………………… Battery Volt Norm / Min…………………………. Min INS Battery Voltage………………………… DC Power Sources………………………………. CP Inverter Power……………………………….. AC EI & FC Inverter Power……………………… # Generators to power all buses………………

  12. FUEL SYSTEM Click to return to Table Of Contents Out / Inboard Diff...……………………….……… Sym Tank Diff (except Aux.)………………….… Wing to Wing (except Aux.)…………….………. Aux Diff..…………………………………….……... Main Tank Pressure……………………………… Aux / Ext. / Fus. Press…………………………… Low Pressure Light………………………………. Tank Empty Light………………………………… 500 – 1000 lbs. < 1000 lbs. < 1500 lbs. 1 Empty, 1 Full if others even 15 – 24 psi 28 – 40 psi 8.5 psi 23 psi

  13. OXYGEN SYSTEM Click to return to Table Of Contents 2.5 Liters 25 Liters 270 – 455 psi 270 – 340 psi Low Light…………………………………………... Fully Service Qty…………………………………. Pressure Range No Flow……………………….. Pressure Range Continuous..…………………..

  14. ENGINE OIL PRESSURE Click to return to Table Of Contents 100 psi 50 – 60 psi < 50 psi if Normal @ 100 % ± 10 psi Max (Start & Warm Up)...…………………...…… Normal Range…………………………………….. Low Speed Ground Idle Min……………………. Flux..………………………………………………...

  15. GEARBOX OIL PRESSURE Click to return to Table Of Contents < 250 psi 150 – 250 psi 130 psi 50 psi ± 20 psi Max (Start & Warm Up)...………………...……… Normal Range…………………………………….. Min Allow for Mission Accomplish……………. Low Speed Ground Idle..………………………... Flux………………………………………………….

  16. OIL TEMPERATURE Click to return to Table Of Contents 85 – 100 °C 85 – 100 °C 60 – 85 °C 40 °C -40 °C 78 – 82 °C Max Ground (30 Minutes)……………………….. Max Flight (5 Minutes)…………………………… Normal Range…………………………………….. Minimum (increasing)…………………………… Minimum For Start……………………………….. Cooler Flap Maintain……………………………..

  17. PROPELLER (HYD) OIL Click to return to Table Of Contents 26 Qts 6.5 Qts 2 Qts Low in Press. Sump Complete System………………………………… Pressurized Sump Qty…………………………... Prop Low Oil Light………………………………..

  18. PROPS Click to return to Table Of Contents 23% - Goes By Oil ± 0.5% 92.5 ° -5° to -8° 25° to 55° 103 % 96 – 98% Increase 2° 23° (Flight Idle or Above) >200 lbs. Difference -6000 lbs 1 min on / 1 min off (not to exceed 2 minutes over 30 minute period 25 Seconds (if it doesn’t pop out in 6 seconds, pull it out Prop Brake Held Disengaged……………………… Cyclic Variations…………………………………….. Feather Blade Angle………………………………… Reverse Blade Angle Range………………………. Pitch Lock Range……………………………………. Pitch Lock Prevents Overspeed Above…………. Pitchlocked RPM Range…………………………… To Unlock Pitchlock………………………………… Low Pitch Stop at…………………………………… Low Pitch Stop Torq. Ind………………………….. Safety Coupling……………………………………… Prop Aux Pump Operating limit………………….. Static Feather Check time (reverse to feather)…

  19. UTIL / BOOST HYD PRESSURE Click to return to Table Of Contents 2900 – 3200 psi 3500 psi 3900 psi On Speed On Speed + 30 Seconds 2550 psi 2050 psi 1000 psi 20 psi Normal………………………………………………… Max Allowable……………………………………….. ESP If Hydraulic Pressure Exceeds……………… RPM For Indication………………………………….. RPM For Normal Pressure…………………………. Min Pressure - Low Speed Ground Idle…………. Aileron Boost Pressure…………………………….. Low Pressure Light On…………………………….. Suction boost Pressure Light……………………..

  20. AUXILLARY HYD PRESSURE Click to return to Table Of Contents Normal…………………………………..… Max Allowable………………………..….. Time Between Cycles…………………... 2900 – 3300 psi 3500 psi 10 sec

  21. NORMAL BRAKE PRESSURE Click to return to Table Of Contents Normal…………………………..……… Max Allowable………………………… 2 Brake Applications………………… 1 Brake Application………………….. 2900 – 3200 psi 3500 psi 2900 – 3200 psi 2250 psi

  22. EMERGENCY BRAKE PRESSURE Click to return to Table Of Contents Normal………………………………. Max Allowable……………………… 1 Brake Application……………….. 2900 – 3300 psi 3500 psi 2900 psi

  23. BLEED AIR SYSTEM Click to return to Table Of Contents GTC Min Pressure Output…………………... Ground Check GTC………………………….. Ground Check Engine………………………. Normal Temp and Pressure………………… 35 psi 30  15 psi ≥ 8.5 Seconds 65  35 psi ≥10 Seconds 600 °F / 125 psi

  24. PRESSURIZATION Click to return to Table Of Contents -1.2 – 15.8 in. Hg -0.76 – 15.9 in. Hg 15.16 in. Hg 0.28 PSID < ∆ 10 in. Hg < ∆10 in. Hg 0 in. Hg 30 – 200 fpm 1600 – 2900 fpm Gauge Rate………………………………… Safety Valve Open………………………... Differential Pressure Max……………….. Aux Vent Valve Open……………………. Windshield Window Cracked (1 or 2)…. Cargo Window Cracked (1 Pane)……… Cargo Window Cracked (2 Panes)…….. Rate Controller at Min…………………… Rate Controller at Max…………………...

  25. LEADING EDGE ANTI-ICING Click to return to Table Of Contents 30 Sec 75 – 200 °F 200 °F 158 °F 180 °F Max Ground Operations…………….. Normal Range…………………………. Overheat Range………………………. Control Valve Open………………….. Control Valve Closed…………………

  26. AIRSPEEDS Max Speed………………………………........ Thunderstorm Penetration………….......... Windmill Taxi Start…………………………. Flaps 10%………………………………......... Flaps 50%.................................................... Flaps 100%.................................................. Flap Formula…………………………………. Door Only………………………………......... Ramp and Door……………………………… Air Deflection Door……………………........ Without Elevator Hydraulic Assist…......... Crew Door Bailout…………………………... Gear and Lights……………………………... Airstart………………………………………... Airstart (No NTS)………………………........ Max Bank Angle…………………………….. Max Bank with Flaps………………………. Painted Control Surfaces (not stencil)… Max Nose Tire Rotation…………………… Max Main Tire Rotation…………………… 0.64 Mach ≤180 (65 ↑PO Stall) 100 Kts until last 4000’ 220 Kts 180 Kts 145 Kts 230 – Flap % = A/S 185 Kts 150 Kts 150 Kts 170 KIAS Or less 150 Kts 165 Kts ≤180 / < 200 °C 130 KIAS below 5000’ 60° 45° 250 KIAS 139 Kts 174 Kts Click to return to Table Of Contents

  27. TAXI OPERATIONS Click to return to Table Of Contents ≤10 Kts 30 Kts @ 90° 60 Kts @ 90° 20° Taxi Over Rough Terrain……………………… Crosswind Taxi Normal……………………….. Max Crosswind Taxi…………………………… Max Nosewheel Turn above 155,000 lbs or between 5 & 20 Kts……………………………..

  28. THROTTLE QUADRANT RANGES Click to return to Table Of Contents Low Speed Ground Idle Throttle Range………. Ground Idle…………………………………………. Flight Idle…………………………………………… Temp Limit Range…………………………………. Temp Control Range……………………………… Reverse Range…………………………………….. Beta Range…………………………………………. Alpha Range………………………………………... 9 - 30° 18° 34° 0 - 65° 65 - 90° 0 - 18° 0 - 34° 34 - 90°

  29. AUTOPILOT Click to return to Table Of Contents 1000 AGL 250 Kts 200 Kts 20 – 30 Kts Min Altitude……………………… Max Speed………………………. Retrim Rudder Through………. Altitude Hold, Retrim…………...

  30. RUDDER BOOSTER PRESSURE Click to return to Table Of Contents 1100 – 1400 psi 1400 – 1600 psi 1600 psi 2900 – 3200 psi 3500 psi Norm 0 – 15% Flaps……………………… Caution 0 -15% Flaps……………………. Max 0 – 15% Flaps……………………...... Norm 15 – 100% Flaps…………………... Max 15 – 100% Flaps……………………...

  31. HYD ACCUMULATOR PRELOAD Click to return to Table Of Contents Utility System………………..…… Booster System…………………. Auxiliary System………………… Normal Brakes…………………… Emergency Brakes……………… 1500 ±100 psi 1500 ±100 psi 300 psi 1500 ±100 psi 1000 ±100 psi

  32. HYD RES QUANTITY Click to return to Table Of Contents Utility System……………..… Booster System…………….. Auxiliary System……………. 3.2 gal 2.0 gal 3.4 gal

  33. MAXIMUM WEIGHTS Click to return to Table Of Contents 155,000 lbs 175,000 lbs 130,000 lbs 130,000 lbs 120,000 lbs Max T/O Weight…………………….. Max Weight EWP………………….... Normal Landing Weight…………… Max Effort Rec Weight…………….. No Flap Rec Weight………………...

  34. GTC Click to return to Table Of Contents GTC Starter Limit………………..… Warmup Normal…………………… Warmup Cold………………………. Oil Pressure For Start……………. 1 min on / 4 min off 1 min 4 min 3.5 psi

  35. NO. 1 INTRUMENT TRANSFORMER Click to return to Table Of Contents H H F E G ydraulic Pressure Indicator (EMER BRAKE) ydraulic Pressure Indicator (BOOSTER) uel Pressure Indicator (Fuel Panel) ngine Oil Pressure Indicators (3 & 4) earbox Oil Pressure Indicators (3 & 4)

  36. NO. 2 INTRUMENT TRANSFORMER Click to return to Table Of Contents E G H H H R R A A ngine Oil Pressure Indicators (1 & 2) earbox Oil Pressure Indicators (1 & 2) ydraulic Pressure Indicator (RAMP) ydraulic Pressure Indicator (NORMAL BRAKES) ydraulic Pressure Indicator (UTILITY) udder Booster Hyd Press (BOOSTER) udder Booster Hyd Press (UTILITY) nti-Skid Test (Circuit Breaker) ll 26 Volt, 400 Cycle, Single Phase

  37. MISCELLANEOUS Click to return to Table Of Contents Crew Door Jettison…………………………….. Flap Setting for Prop Malfunction on T/O…. Cold WX Ops Temp…………………………….. Hot WX Ops Temp……………………………… Battery Min Temp………………………………. CG Limits………………………………………… <3.1 in. Hg 20% < 32 °F > 95 °F -29 °F Must Be Within MAC Max 15 – 30%

  38. ENGINE SHUTDOWN CONDITIONS Click to return to Table Of Contents V E N T G C U U U U U T isible Fluid Leak ngine Fire acelle Overheat urbine Overheat enerator Failure (no disconnects) ertain Propeller Malfunctions ncontrollable Power ncontrollable Rise in TIT ncontrollable Drop in Oil Pressure ncontrollable Rise in Oil Temp ncontrollable Vibration or Roughness hrottle Control Failure

  39. ENGINE SHUTDOWN PROCEDURES Click to return to Table Of Contents CONDITION LEVER “FEATHER” (CP) FIRE HANDLE “PULLED” (CP) AGENT “DISCHARGED” (FOR FIRE OR NACELLE OVERHEAT) (CP) 1. 2. 3.

  40. GTC EMERGENCY SHUTDOWN Click to return to Table Of Contents 1. 2. FIRE HANDLE “PULLED” (E) AGENT “DISCHARGED” (FOR FIRE) (E)

  41. SMOKE AND FUME ELIMINATION Click to return to Table Of Contents 1. OXYGEN “ON, 100%” (ALL)

  42. RAPID DECOMPRESSION Click to return to Table Of Contents 1. OXYGEN “ON, 100%” (ALL)

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