Presentation is loading. Please wait.

Presentation is loading. Please wait.

C-130E Limitations Last update 11 July 2007. CategorySlide AC Electric10 Airspeeds26 Autopilot29 Auxillary Hyd Pressure20 Bleed Air System23 DC Electric11.

Similar presentations


Presentation on theme: "C-130E Limitations Last update 11 July 2007. CategorySlide AC Electric10 Airspeeds26 Autopilot29 Auxillary Hyd Pressure20 Bleed Air System23 DC Electric11."— Presentation transcript:

1 C-130E Limitations Last update 11 July 2007

2 CategorySlide AC Electric10 Airspeeds26 Autopilot29 Auxillary Hyd Pressure20 Bleed Air System23 DC Electric11 Emergency Brake Pressure22 Engine Oil Pressure14 Engine RPM5 Engine Shutdown Conditions38 Engine Shutdown Procedure39 Engine TIT4 Engine Torque6 Fuel System12 Gearbox Oil Pressure15 GTC34 GTC Emergency Shutdown40 Hyd Accumulator Preload31 Hyd Res Quantity32 Leading Edge Anti-Icing25 CategorySlide Maximum Weights33 Miscellaneous37 No. 1 Intrument Transformer35 No. 2 Instrument Transformer36 Normal Brake Pressure21 Oil Quantity9 Oil Temperature16 Oxygen System13 Pressurization24 Prop De-Icing7 Propeller (Hyd) Oil17 Props18 Rapid Decompression42 Rudder Booster Pressure30 Smoke and Fume Elimination41 Starting TIT3 Taxi Operations27 Throttle Quadrant Ranges28 Util / Boost Hyd Pressure19 Windshield Anti-Ice8 TABLE OF CONTENTS Click a category to jump to that slide, or spacebar to advance through every slide.

3 STARTING TIT Max for enrichment………………………………. Max Normal Start………………….……………… Max During Start………..………………………… What do you do if? Abnormal Torch………………………………… °C or less…………………………………… °C to 750 °C …………………… °C to 830 °C ………………………………… °C to 850 °C ………………………………… °C to 965 °C ………………………………….. Exceeds 965 °C …………….…………………… °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 Click to return to Table Of Contents

4 ENGINE TIT 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 977 °C 932 °C 781 / O/T Inspection 65° / 760 °C ± °C 850 °C Click to return to Table Of Contents

5 Engine RPM 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 % Click to return to Table Of Contents

6 ENGINE TORQUE 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 ± 600 lbs 8,000 in-lbs >200 in-lbs 19,600 in-lbs in-lbs Click to return to Table Of Contents

7 PROP DE-ICING 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 Click to return to Table Of Contents

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

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

10 AC ELECTRIC 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 Kva 20 Kva / 30 Kva below 104 ° F 0.66 / 1.0 below 104 °F 115 / 200 V, 400 Cycle Click to return to Table Of Contents

11 DC ELECTRIC 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……………… V / 28 V V / 21 V 21 V Batt / 4 TR’s / External Iso DC Bus Essential DC Bus 2 Gens Click to return to Table Of Contents

12 FUEL SYSTEM 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 Click to return to Table Of Contents

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

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

15 GEARBOX OIL PRESSURE 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 Click to return to Table Of Contents

16 OIL TEMPERATURE 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 Click to return to Table Of Contents

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

18 PROPS 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 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 Click to return to Table Of Contents

19 UTIL / BOOST HYD PRESSURE 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…………………… – 3200 psi 3500 psi 3900 psi On Speed On Speed + 30 Seconds 2550 psi 2050 psi 1000 psi 20 psi Click to return to Table Of Contents

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

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

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

23 BLEED AIR SYSTEM 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 Click to return to Table Of Contents

24 PRESSURIZATION 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………………… – 15.8 in. Hg – 15.9 in. Hg in. Hg 0.28 PSID < ∆ 10 in. Hg 0 in. Hg 30 – 200 fpm 1600 – 2900 fpm Click to return to Table Of Contents

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

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 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 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° Click to return to Table Of Contents

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

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

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

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

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

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

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

35 NO. 1 INTRUMENT TRANSFORMER HHFEGHHFEG 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) Click to return to Table Of Contents

36 NO. 2 INTRUMENT TRANSFORMER EGHHHRRAAEGHHHRRAA 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 Click to return to Table Of Contents

37 MISCELLANEOUS 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% Click to return to Table Of Contents

38 ENGINE SHUTDOWN CONDITIONS VENTGCUUUUUTVENTGCUUUUUT 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 Click to return to Table Of Contents

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

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

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

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


Download ppt "C-130E Limitations Last update 11 July 2007. CategorySlide AC Electric10 Airspeeds26 Autopilot29 Auxillary Hyd Pressure20 Bleed Air System23 DC Electric11."

Similar presentations


Ads by Google