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C-130E Limitations Last update 11 July 2007
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TABLE OF CONTENTS Click a category to jump to that slide, or spacebar to advance through every slide. Category Slide AC Electric 10 Airspeeds 26 Autopilot 29 Auxillary Hyd Pressure 20 Bleed Air System 23 DC Electric 11 Emergency Brake Pressure 22 Engine Oil Pressure 14 Engine RPM 5 Engine Shutdown Conditions 38 Engine Shutdown Procedure 39 Engine TIT 4 Engine Torque 6 Fuel System 12 Gearbox Oil Pressure 15 GTC 34 GTC Emergency Shutdown 40 Hyd Accumulator Preload 31 Hyd Res Quantity 32 Leading Edge Anti-Icing 25 Category Slide Maximum Weights 33 Miscellaneous 37 No. 1 Intrument Transformer 35 No. 2 Instrument Transformer 36 Normal Brake Pressure 21 Oil Quantity 9 Oil Temperature 16 Oxygen System 13 Pressurization 24 Prop De-Icing 7 Propeller (Hyd) Oil 17 Props 18 Rapid Decompression 42 Rudder Booster Pressure 30 Smoke and Fume Elimination 41 Starting TIT 3 Taxi Operations 27 Throttle Quadrant Ranges 28 Util / Boost Hyd Pressure 19 Windshield Anti-Ice 8
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STARTING TIT Click to return to Table Of Contents 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 …………….…………………….. 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
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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 °C 900 °C / 932 °C 200 °C °C 932 °C 781 / O/T Inspection 65° / 760 °C ± 20 850 °C
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Engine RPM Click to return to Table Of Contents Ignition By…………………………………….….. Oil Pressure Indicated By………………….….. Low Speed Ground Idle………………….…….. Normal Ground Idle…………………………..…. Max Reverse………………………………………. Flight Idle On Ground……………………………. Normal (Including Takeoff)…………………..…. Starter Disengage……………………………..…. 35 % 69 – 75.5 % 94 – 102 % 96 – 106 % 92.5 – % 98 – 102 % ± .5 60 %
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ENGINE TORQUE Click to return to Table Of Contents 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………………………………...… Min Torque 4500 lbs 19,600 lbs -1260 ± 600 lbs 8,000 in-lbs >200 in-lbs 19,600 in-lbs -6000 in-lbs
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PROP DE-ICING Click to return to Table Of Contents Load Range………………………………….…….. Timing Cycle…………………………………….… Max Ground Ops…………………………………. Anti Ice Amperage……………………………….. 65 – 90 Amps 15 Seconds On / 45 Sec. off 2 Cycles (2 minutes) 20 Amps per prop
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WINDSHIELD ANTI-ICE Click to return to Table Of Contents Max OAT Operation………………………..…….. Cold Start………………………………….………. 27 °C / 81 °F 5 Sec On / 10 sec off until -43 °C
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OIL QUANTITY Click to return to Table Of Contents Capacity Range…………………………………... Low Light………………………………………...… Allowable Burn Rate……………………………... 4 to 12 Gallons 4 Gallons .35 Gal/Hour
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AC ELECTRIC Click to return to Table Of Contents Freq Range………………………………………… Voltage Range…………………………..………… Max Load In Flight……………………………..… Generator Capacity………………………………. ATM Capacity……………………………………... ATM Load………………………………………….. AC Gen Rating……………………………………. 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
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DC ELECTRIC Click to return to Table Of Contents 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……………… 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
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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
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OXYGEN SYSTEM Click to return to Table Of Contents Low Light…………………………………………... Fully Service Qty…………………………………. Pressure Range No Flow……………………….. Pressure Range Continuous..………………….. 2.5 Liters 25 Liters 270 – 455 psi 270 – 340 psi
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ENGINE OIL PRESSURE Click to return to Table Of Contents Max (Start & Warm Up)...…………………...…… Normal Range…………………………………….. Low Speed Ground Idle Min……………………. Flux..………………………………………………... 100 psi 50 – 60 psi < 50 psi if 100 % ± 10 psi
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GEARBOX OIL PRESSURE Click to return to Table Of Contents Max (Start & Warm Up)...………………...……… Normal Range…………………………………….. Min Allow for Mission Accomplish……………. Low Speed Ground Idle..………………………... Flux…………………………………………………. < 250 psi 150 – 250 psi 130 psi 50 psi ± 20 psi
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OIL TEMPERATURE Click to return to Table Of Contents Max Ground (30 Minutes)……………………….. Max Flight (5 Minutes)…………………………… Normal Range…………………………………….. Minimum (increasing)…………………………… Minimum For Start……………………………….. Cooler Flap Maintain…………………………….. 85 – 100 °C 60 – 85 °C 40 °C -40 °C 78 – 82 °C
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PROPELLER (HYD) OIL Click to return to Table Of Contents Complete System………………………………… Pressurized Sump Qty…………………………... Prop Low Oil Light……………………………….. 26 Qts 6.5 Qts 2 Qts Low in Press. Sump
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PROPS Click to return to Table Of Contents 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)… 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
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UTIL / BOOST HYD PRESSURE
Click to return to Table Of Contents 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…………………….. 2900 – 3200 psi 3500 psi 3900 psi On Speed On Speed + 30 Seconds 2550 psi 2050 psi 1000 psi 20 psi
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AUXILLARY HYD PRESSURE
Click to return to Table Of Contents Normal…………………………………..… Max Allowable………………………..….. Time Between Cycles…………………... 2900 – 3300 psi 3500 psi 10 sec
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NORMAL BRAKE PRESSURE Click to return to Table Of Contents Normal…………………………..……… Max Allowable………………………… 2 Brake Applications………………… 1 Brake Application………………….. 2900 – 3200 psi 3500 psi 2250 psi
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EMERGENCY BRAKE PRESSURE
Click to return to Table Of Contents Normal………………………………. Max Allowable……………………… 1 Brake Application……………….. 2900 – 3300 psi 3500 psi 2900 psi
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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
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PRESSURIZATION Click to return to Table Of Contents 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…………………... -1.2 – 15.8 in. Hg -0.76 – 15.9 in. Hg 15.16 in. Hg 0.28 PSID < ∆ 10 in. Hg 0 in. Hg 30 – 200 fpm 1600 – 2900 fpm
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LEADING EDGE ANTI-ICING
Click to return to Table Of Contents Max Ground Operations…………….. Normal Range…………………………. Overheat Range………………………. Control Valve Open………………….. Control Valve Closed………………… 30 Sec 75 – 200 °F 200 °F 158 °F 180 °F
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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 170 KIAS Or less 165 Kts ≤180 / < 200 °C 130 KIAS below 5000’ 60° 45° 250 KIAS 139 Kts 174 Kts Click to return to Table Of Contents
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TAXI OPERATIONS Click to return to Table Of Contents Taxi Over Rough Terrain……………………… Crosswind Taxi Normal……………………….. Max Crosswind Taxi…………………………… Max Nosewheel Turn above 155,000 lbs or between 5 & 20 Kts…………………………….. ≤10 Kts 30 90° 60 90° 20°
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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° ° 0 - 18° 0 - 34° °
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AUTOPILOT Click to return to Table Of Contents Min Altitude……………………… Max Speed………………………. Retrim Rudder Through………. Altitude Hold, Retrim…………... 1000 AGL 250 Kts 200 Kts 20 – 30 Kts
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RUDDER BOOSTER PRESSURE
Click to return to Table Of Contents Norm 0 – 15% Flaps……………………… Caution 0 -15% Flaps……………………. Max 0 – 15% Flaps……………………...... Norm 15 – 100% Flaps…………………... Max 15 – 100% Flaps……………………... 1100 – 1400 psi 1400 – 1600 psi 1600 psi 2900 – 3200 psi 3500 psi
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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 1000 ± 100 psi
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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
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MAXIMUM WEIGHTS Click to return to Table Of Contents Max T/O Weight…………………….. Max Weight EWP………………….... Normal Landing Weight…………… Max Effort Rec Weight…………….. No Flap Rec Weight………………... 155,000 lbs 175,000 lbs 130,000 lbs 120,000 lbs
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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
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NO. 1 INTRUMENT TRANSFORMER
Click to return to Table Of Contents 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)
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NO. 2 INTRUMENT TRANSFORMER
Click to return to Table Of Contents E G H R 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
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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%
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ENGINE SHUTDOWN CONDITIONS
Click to return to Table Of Contents V E N T G C U 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
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ENGINE SHUTDOWN PROCEDURES
Click to return to Table Of Contents 1. 2. 3. CONDITION LEVER “FEATHER” (CP) FIRE HANDLE “PULLED” (CP) AGENT “DISCHARGED” (FOR FIRE OR NACELLE OVERHEAT) (CP)
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GTC EMERGENCY SHUTDOWN
Click to return to Table Of Contents 1. 2. FIRE HANDLE “PULLED” (E) AGENT “DISCHARGED” (FOR FIRE) (E)
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SMOKE AND FUME ELIMINATION
Click to return to Table Of Contents 1. OXYGEN “ON, 100%” (ALL)
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RAPID DECOMPRESSION Click to return to Table Of Contents 1. OXYGEN “ON, 100%” (ALL)
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