C-130E Limitations

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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
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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
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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
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Engine RPM
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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 35 69 75.5 94 102 96 106 92.5
100.5 98 102 .5 60
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ENGINE TORQUE
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Oil Temp lt 0 C ...... Oil Temp 0 C
- 40 C . Max Allow on
Takeoff. Max Allow in
Flight. NTS Action Pr
opulsion Check... Torque Comparison
Check.. Max Continuous.. Safe
ty Coupling...
Min Torque 4500 lbs 19,600 lbs 19,600 lbs -1260
600 lbs 8,000 in-lbs gt200 in-lbs 19,600
in-lbs -6000 in-lbs
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PROP DE-ICING
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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
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Max OAT Operation.... Cold
Start..
27 C / 81 F 5 Sec On / 10 sec off until -43 C
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OIL QUANTITY
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Capacity Range... Low
Light... Allowable Burn
Rate...
4 to 12 Gallons 4 Gallons .35 Gal/Hour
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AC ELECTRIC
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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
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Volt Range / Norm... Max DC
Load Battery Volt Norm /
Min. Min INS Battery Voltage D
C 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
TRs / External Iso DC Bus Essential DC Bus 2 Gens
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FUEL SYSTEM
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Out / Inboard Diff.... Sym Tank Diff
(except Aux.). Wing to Wing (except
Aux.).. Aux Diff...... Mai
n Tank Pressure Aux / Ext. / Fus.
Press Low Pressure Light. T
ank Empty Light
500 1000 lbs. lt 1000 lbs. lt 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
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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
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Max (Start Warm Up)...... Normal
Range.. Low Speed Ground Idle
Min. Flux.....
100 psi 50 60 psi lt 50 psi if Normal _at_ 100
10 psi
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GEARBOX OIL PRESSURE
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lt 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.
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OIL TEMPERATURE
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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.. M
inimum (increasing) Minimum For
Start.. Cooler Flap
Maintain..
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PROPELLER (HYD) OIL
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26 Qts 6.5 Qts 2 Qts Low in Press. Sump
Complete System Pressurized Sump
Qty... Prop Low Oil Light..
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PROPS
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23 - Goes By Oil 0.5 92.5 -5 to -8 25 to
55 103 96 98 Increase 2 23 (Flight Idle
or Above) gt200 lbs. Difference -6000 lbs 1 min on
/ 1 min off (not to exceed 2 minutes over 30
minute period 25 Seconds (if it doesnt pop out
in 6 seconds, pull it out
Prop Brake Held Disengaged Cyclic
Variations.. Feather Blade
Angle Reverse Blade Angle
Range. Pitch Lock Range. Pi
tch Lock Prevents Overspeed Above. Pitchlocked
RPM Range To Unlock
Pitchlock Low Pitch Stop
at Low Pitch Stop Torq.
Ind.. Safety Coupling Pro
p Aux Pump Operating limit.. Static
Feather Check time (reverse to feather)
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UTIL / BOOST HYD PRESSURE
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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.. RP
M For Normal Pressure. Min Pressure -
Low Speed Ground Idle. Aileron Boost
Pressure.. Low Pressure Light
On.. Suction boost Pressure
Light..
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AUXILLARY HYD PRESSURE
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Normal.. Max Allowable....
Time Between Cycles...
2900 3300 psi 3500 psi 10 sec
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NORMAL BRAKE PRESSURE
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Normal.. Max Allowable 2
Brake Applications 1 Brake
Application..
2900 3200 psi 3500 psi 2900 3200 psi 2250 psi
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EMERGENCY BRAKE PRESSURE
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Normal. Max Allowable 1
Brake Application..
2900 3300 psi 3500 psi 2900 psi
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BLEED AIR SYSTEM
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GTC Min Pressure Output... Ground Check
GTC.. Ground Check Engine. Norm
al 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
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-1.2 15.8 in. Hg -0.76 15.9 in. Hg 15.16 in.
Hg 0.28 PSID lt ? 10 in. Hg lt ? 10 in. Hg 0 in.
Hg 30 200 fpm 1600 2900 fpm
Gauge Rate Safety Valve
Open... Differential Pressure
Max.. Aux Vent Valve Open. Windshiel
d Window Cracked (1 or 2). Cargo Window Cracked
(1 Pane) Cargo Window Cracked (2
Panes).. Rate Controller at Min Rate
Controller at Max...
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LEADING EDGE ANTI-ICING
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30 Sec 75 200 F 200 F 158 F 180 F
Max Ground Operations.. Normal
Range. Overheat Range. Control
Valve Open.. Control Valve Closed
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AIRSPEEDS
Max Speed........ Thunderstorm
Penetration.......... Windmill Taxi
Start. Flaps 10......... Fl
aps 50...........................................
......... Flaps 100..............................
.................... Flap Formula. Do
or Only......... Ramp and
Door Air Deflection
Door........ Without Elevator Hydraulic
Assist......... Crew Door Bailout... Ge
ar 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 / lt 200 C 130 KIAS below
5000 60 45 250 KIAS 139 Kts 174 Kts
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TAXI OPERATIONS
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10 Kts 30 Kts _at_ 90 60 Kts _at_ 90 20
Taxi Over Rough Terrain Crosswind Taxi
Normal.. Max Crosswind
Taxi Max Nosewheel Turn above 155,000
lbs or between 5 20 Kts..
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THROTTLE QUADRANT RANGES
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Low Speed Ground Idle Throttle Range. Ground
Idle. Flight Idle
Temp Limit Range. Temp Control
Range Reverse Range.. Be
ta Range. Alpha
Range...
9 - 30 18 34 0 - 65 65 - 90 0 - 18 0 -
34 34 - 90
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AUTOPILOT
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1000 AGL 250 Kts 200 Kts 20 30 Kts
Min Altitude Max Speed. Retrim
Rudder Through. Altitude Hold, Retrim...
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RUDDER BOOSTER PRESSURE
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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...... Nor
m 15 100 Flaps... Max 15 100
Flaps...
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HYD ACCUMULATOR PRELOAD
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Utility System.. Booster
System. Auxiliary System Normal
Brakes Emergency Brakes
1500 100 psi 1500 100 psi 300 psi 1500 100
psi 1000 100 psi
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HYD RES QUANTITY
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Utility System.. Booster System.. Auxil
iary System.
3.2 gal 2.0 gal 3.4 gal
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MAXIMUM WEIGHTS
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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...
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GTC
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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
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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)
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NO. 2 INTRUMENT TRANSFORMER
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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
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MISCELLANEOUS
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Crew Door Jettison.. Flap Setting for
Prop Malfunction on T/O. Cold WX Ops
Temp.. Hot WX Ops Temp Batt
ery Min Temp. CG Limits

lt3.1 in. Hg 20 lt 32 F gt 95 F -29 F Must Be
Within MAC Max 15 30
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ENGINE SHUTDOWN CONDITIONS
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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 ncontro
llable Power ncontrollable Rise in
TIT ncontrollable Drop in Oil Pressure ncontrollab
le Rise in Oil Temp ncontrollable Vibration or
Roughness hrottle Control Failure
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ENGINE SHUTDOWN PROCEDURES
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CONDITION LEVER FEATHER (CP) FIRE HANDLE
PULLED (CP) AGENT DISCHARGED
(FOR FIRE OR NACELLE OVERHEAT)
(CP)
1. 2. 3.
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GTC EMERGENCY SHUTDOWN
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1. 2.
FIRE HANDLE PULLED
(E) AGENT DISCHARGED (FOR FIRE) (E)
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SMOKE AND FUME ELIMINATION
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1.
OXYGEN ON, 100 (ALL)
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RAPID DECOMPRESSION
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1.
OXYGEN ON, 100 (ALL)