c-130e limitations last update 11 july 2007. categoryslide ac electric10 airspeeds26 autopilot29...

C-130E LimitationsLast update 11 July 2007

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

TABLE OF CONTENTSClick a category to jump to that slide, or spacebar to advance through every slide.

STARTING TIT

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

Click to return to Table Of Contents

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 - 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


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 %

35 %

69 – 75.5 %

94 – 102 %

96 – 106 %

92.5 – 100.5 %

98 – 102 % ± .5

60 %


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

19,600 lbs

-1260 ± 600 lbs

8,000 in-lbs

>200 in-lbs

19,600 in-lbs

-6000 in-lbs


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


WINDSHIELD ANTI-ICE

Max OAT Operation………………………..……..

Cold Start………………………………….……….

27 °C / 81 °F

5 Sec On / 10 sec off until -43 °C


OIL QUANTITY

Capacity Range…………………………………...

Low Light………………………………………...…

Allowable Burn Rate……………………………...

4 to 12 Gallons

4 Gallons

.35 Gal/Hour


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

1.05

40 Kva

20 Kva / 30 Kva below 104 °F

0.66 / 1.0 below 104 °F

115 / 200 V, 400 Cycle


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………………

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


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


OXYGEN SYSTEM

Low Light…………………………………………...

Fully Service Qty………………………………….

Pressure Range No Flow………………………..

Pressure Range Continuous..…………………..

2.5 Liters

25 Liters

270 – 455 psi

270 – 340 psi


ENGINE OIL PRESSURE

Max (Start & Warm Up)...…………………...……

Normal Range……………………………………..

Low Speed Ground Idle Min…………………….

Flux..………………………………………………...

100 psi

50 – 60 psi

< 50 psi if Normal @ 100 %

± 10 psi


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


OIL TEMPERATURE

Max Ground (30 Minutes)………………………..

Max Flight (5 Minutes)……………………………

Normal Range……………………………………..

Minimum (increasing)……………………………

Minimum For Start………………………………..

Cooler Flap Maintain……………………………..

85 – 100 °C

85 – 100 °C

60 – 85 °C

40 °C

-40 °C

78 – 82 °C


PROPELLER (HYD) OIL

Complete System…………………………………

Pressurized Sump Qty…………………………...

Prop Low Oil Light………………………………..

26 Qts

6.5 Qts

2 Qts Low in Press. Sump


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

-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


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……………………..

2900 – 3200 psi

3500 psi

3900 psi

On Speed

On Speed + 30 Seconds

2550 psi

2050 psi

1000 psi

20 psi


Normal…………………………………..…

Max Allowable………………………..…..

Time Between Cycles…………………...

AUXILLARY HYD PRESSUREClick to return

to Table Of Contents2900 – 3300 psi

3500 psi

10 sec

NORMAL BRAKE PRESSURE

Normal…………………………..………

Max Allowable…………………………

2 Brake Applications…………………

1 Brake Application…………………..

2900 – 3200 psi

3500 psi

2900 – 3200 psi

2250 psi


EMERGENCY BRAKE PRESSURE

Normal……………………………….

Max Allowable………………………

1 Brake Application………………..

2900 – 3300 psi

3500 psi

2900 psi


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


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…………………...

-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


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


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


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 Kts @ 90°

60 Kts @ 90°

20°


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………………………………………...

9 - 30°

18°

34°

0 - 65°

65 - 90°

0 - 18°

0 - 34°

34 - 90°


AUTOPILOT

Min Altitude………………………

Max Speed……………………….

Retrim Rudder Through……….

Altitude Hold, Retrim…………...

1000 AGL

250 Kts

200 Kts

20 – 30 Kts


RUDDER BOOSTER PRESSURE

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


HYD ACCUMULATOR PRELOAD

Utility System………………..……

Booster System………………….

Auxiliary System…………………

Normal Brakes……………………

Emergency Brakes………………

1500 ±100 psi

1500 ± 100 psi

300 psi

1500 ± 100 psi

1000 ± 100 psi


HYD RES QUANTITY

Utility System……………..…

Booster System……………..

Auxiliary System…………….

3.2 gal

2.0 gal

3.4 gal


MAXIMUM WEIGHTS

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

130,000 lbs

120,000 lbs


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


NO. 1 INTRUMENT TRANSFORMER

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)


NO. 2 INTRUMENT TRANSFORMER

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


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%


ENGINE SHUTDOWN CONDITIONS

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


ENGINE SHUTDOWN PROCEDURES

1.

2.

3.

CONDITION LEVER “FEATHER” (CP)

FIRE HANDLE “PULLED” (CP)

AGENT “DISCHARGED” (FOR FIRE OR NACELLE OVERHEAT) (CP)


GTC EMERGENCY SHUTDOWN

1.

2.

FIRE HANDLE “PULLED” (E)

AGENT “DISCHARGED” (FOR FIRE) (E)


SMOKE AND FUME ELIMINATION

1. OXYGEN “ON, 100%” (ALL)


RAPID DECOMPRESSION

1. OXYGEN “ON, 100%” (ALL)


c-130e limitations last update 11 july 2007. categoryslide ac electric10 airspeeds26 autopilot29...

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