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STARTING TIT
Max for Enrichment C
Max Normal Start C
Max During Start C
Abnormal Torch _________________
720C or less _________________
720C - 750C _________________
750C - 830C _________________
830C - 850C _________________
850C - 965C _________________
Exceeds 965C- _________________
ENGINE TIT
Takeoff Max (5 Min) - C
Takeoff Range - C
Takeoff Reduced Min - C/ / C
Normal Continuous - C
Military (30 Min.) - C
Climb - C
Exceeds 1083C over 5 seconds or 1175C
Momentarily - ________________
Crossover - /
Normal Limiting - C
Max Downshift TIT - C
ENGINE RPM
Ignition by - %
Oil Press Ind by - %
LSGI - %
Normal Ground Idle - %
Max Reverse - %
Flight Idle on Ground - %
Normal (Incl. Takeoff) - % __
Starter Disengage - %
ENGINE TORQUE
Oil Temp < 0C ________________
Oil Temp 0 - 40C - lbs
Max Allow on T.O. - lbs
Max Allow in flight - lbs
NTS Action - lbs
Propulsion check - in.lbs
Torq Comparison CK - in.lbs
Max Continous - lbs
Safety Coupling - lbs
PROP DE-ICING
Load Range - AmpsTiming Cycle - / f
Max Gnd Ops - ( )
Anti Ice Amperage - __________________
WINDSHIELD ANTI-ICE
Max OAT Ops GND - C/ F
Cold Start - C
OIL QUANTITY
Capacity Range - Gal
Low Light - Gal
Allowable Burn Rate - Gal/Hour
C-130H OPS LIMITS
AC ELECTRIC
Freq Range - Hz (4 cyc/rpm)
Voltage Range - V
Max load in Flight - ________
Generator Capacity - KVA
APU Generator - KVA
APU Gen Load ________
DC ELECTRIC
Volt Range / Norm - V / V
Max DC Load - ________
Batt. Volt Norm / Min - V / V
Min INS Batt Volt - V
DC Pwr Sources - _____________________
CP Inverter Pwr - ________________
AC I & EFC Inv. Pwr - ________________
# Gens to Pwr all Buses - ________
FUEL SYSTEM
Out / Inboard Diff - lbs
Sym Tank Diff. (exc. Aux) - lbs
Wing to Wing (exc. Aux) - lbsAux Diff. -
___________________________
Main Tank Pressure - psi
Aux / Ext. / Fus. Press - psi
Low Pressure Light - psi
Tank Empty Light - psi
OXYGEN SYSTEM
Low Light - ltrs
Fully Serviced Qty - ltrs
Press. Rng No Flow - psi
Press. Range Cont. - psi
ENGINE OIL PRESSUREMax (Start & Warmup) - psi
Normal Range - psi
LSGI Min. - %
Flux - __
GEARBOX OIL PRESSURE
Max (Start & Warmup) - psi
Normal Range - psi
Min Allow for Mis. Accomp - psi
LSGI - psi
Flux - __
OIL TEMPERATUREMax GND (30 Min) - C
Max Flight (5 Min) - C
Normal Range - C
Min (Increasing) - C
Minimum for Start - C
Cooler Flaps Maintain - C
PROPELLER (HYD) OIL
Complete System - Qts
Press Sump - Qts
Prop Low Oil Light - _____________________
PROPS
Prop brake held disengaged -
Cyclic Variation -
Feather Blade Angle -
Reverse Blade Angle -
Pitch Lock Range -
Pitchlock prevents overspeed >
Pitchlocked RPM range - %
To unlock pitchlock -
Low Pitch Stop - (Flt Idle
Low Pitch Stop Torq. Ind -
Safety Coupling -
Prop Aux Pump Ops ___________
Limits - (
Static Fthr Check time ______(______
(Rev to Fthr) -
UTIL / BOOST HYD PRESSU
Normal -
Max Allowable -
ESP if Hyd Press Exceeds -
RPM for Indication - ________
RPM for Normal Press -
Min Press LSGI -
Aileron Boost Press -
Low Press Light On -
Suction Boost Press Light -
AUXILIARY HYD PRESSUR
Normal -
Max Allowable -
Time between Cycles -
NORMAL BRAKE PRESSUR
Normal - Max Allowable -
2 Brake Applications -
1 Brake Applications -
EMERGENCY BRAKE PRESS
Normal -
Max Allowable -
1 Brake Application -
BLEED AIR SYSTEM
APU Min Press Output -
Gnd Check APU - ps
Gnd Ck Engine - psNormal Temp and Press - F
PRESSURIZATION
Gauge Rate -
Safety Valve Open -
Differential Press Max -
Aux Vent Valve Open -
Windshield Window Max (1 or 2)-
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LEADING EDGE ANTI-ICING
Max Ground Ops - sec
Normal Range - F
Overheat Range - F
Control Valve Open - F
Control Valve Closed - F
AIRSPEEDS
Max Speed - Mach
T-Storm Penetration - ( PO Stall)
Windmill Taxi Start - kts until last ft
Flaps 10% - kts
Flaps 50% - kts
Flaps 100% - kts
Flap Formula - % = ____
Door Only - kts
Ramp and Door - kts
Air Deflector Door - kts
w/o elev hyd assist - ind. _____
Crew door Bailout - kts
Gear and Lights - kts
Airstart - / < C
Airstart (no NTS) - kias below ft
Max Bank Angle -
Max Bank w/Flaps -
Painted Control Surfaces (not stencil) - kias
Max Nose Tire Rotation - kts
Max Main Tire Rotation - kts
TAXI OPERATIONS
Taxi over rough/substandard kts
Terrain -
Normal X wind Limit - kts @
Max X wind Limit - kts @
Max NW turn above 155,000 lbs -
Max taxi speed above 155,000 - kts
Max taxi speed w/60 NW - kts
Max taxi speed w/20 NW - kts
Max taxi speed hard surface - kts
Stop in turn - ___________________
THROTTLE QUADRANT RANGES
LSGI Throt Range -
Ground Idle -
Flight Idle - Temp Limit Range -
Temp Control Range -
Reverse Range -
Beta Range -
Alpha Range -
C-130H OPS LIMITS
RUDDER BOOSTER PRESSURE
Norm 0 15% Flaps - psi
Caution 0 15% Flaps - psi
Max 0 15% Flaps - psi
Norm 15 100% Flaps - psi
Max 15 100% Flaps - psi
HYD ACCUMULATOR PRELOAD
Utility System - psi
Booster System - psi
Auxiliary System - psi
Normal Brakes - psi
Emergency Brakes - psi
HYD RES QUANTITY
Utility System - gal
Booster System - gal
Auxiliary System - gal
MAXIMUM WEIGHTS
Max T/O Weight - lbsMax Weight EWP - lbs
Normal Landing Wt. - lbs
Max Effort Rec Wt - lbs
No Flap rec Wt - lbs
APU
APU Starter Limit - ___________ / ________
Warmup Normal - min
Warmup Cold - mins
Min Air Pressure (Grnd) - psi
No INSTRUMENT TRANSFORMER
Engine Oil Pressure Indicators (3 & 4)Gearbox Oil Pressure
Indicators (3 & 4)
Fuel Pressure Indicator (Fuel Panel)
Hyd Pressure Indicator (EMER BRAKE)
Hyd Pressure Indicator (BOOSTER)
No. INSTRUMENT TRANSFORMER
Engine Oil Pressure Indicators (1 & 2)
Gearbox Oil Pressure Indicators (1 & 2)
Hyd Pressure Indicator (RAMP)
Hyd Pressure Indicator (NORMAL BRAKES)
Hyd Pressure Indicator (UTILITY)
Rudder Booster Hyd Press (BOOSTER)Rudder Booster Hyd Press
(UTILITY)
Anti-skid Test (Circuit Breaker)
All 26 Volt, 400 cycle, Single Phase
MISCELLANEOUS
Crew Door Jettison - < in Hg
Flap setting for Prop malf on T/O - %
Cold WX ops Temp - < F
Hot WX ops Temp - > F
Battery Min Temp - F
CG Limits - ___________________
%
ENGINE SHUTDOWN CONDIT
1.2.3.4.5.6.7.8.9.10.11.
ENGINE SHUTDOWN PROCED
1.2.3. ( __
)
MULTIPLE ENGINE POWE
LOSS/STALL/FLAMEOUT
1. _______________________________
2. _______________________________
APU EMERGENCY SHUTDO
1.2. (
SMOKE AND FUME ELIMINA
1.
RAPID DECOMPRESSION
1.
