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135 Cards in this Set
- Front
- Back
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ENGINE FIRE/EMERGENCY ENGINE SHUTDOWN CHECKLIST
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THROTTLE – “IDLE” (PF)
FIRE HANDLE – “PULL” (PNF) AGENT – “DISCHARGE” (AS REQUIRED) (PNF) |
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FOUR ENGINE FLAMEOUT
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ENGINE IGNITION NORM/ORIDE SWITCH – “ORIDE” (PNF)
RAT – “EXT” (PNF) |
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LOSS OF PRESSURIZATION
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OXYGEN – “ON, 100%” (ALL)
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SMOKE/FUMES IN THE AIRCRAFT
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OXYGEN – “ON, 100%” (ALL)
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Max Taxi weight?
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586,000 LBS
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Max TO/Land weight?
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585,000 LBS
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Max ZFW?
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447,400 LBS
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Max Cargo weight?
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170,900 LBS
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Max Fuel @=>CX?
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181,000 LBS
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Max Fuel @ CY>=?
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245,000 LBS
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Aircraft OW?
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282,500 LBS
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Max Landing weight full flap?
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502,100 LBS
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Min Plan Landing fuel weight?
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16,000 LBS
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Max Airspeed?
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350/.825
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Slats extend airspeed?
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280/.62
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Slats retract airspeed?
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270/.62
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Doors/Ramp/AD speed?
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250/.62
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Flaps ½ airspeed?
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250/.62
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Flaps ¾ airspeed?
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190/.62
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Flaps Full Airspeed?
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175/.62
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Lndg gear ext/opr airspeed?
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250/.62
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Lndg gear retract airspeed?
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225/.62
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Pilot windows airspeed?
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205
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Tire placard speed?
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182 GS
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Rev thrust (flight) speed?
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350/.825
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Rev thrust (ground)?
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182
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Max EGT start?
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495°C
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Min Oil Temp TO?
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50°C
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Min Oil Pressure?
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70 psi
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Min Oil Quantity?
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4 quarts
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Min N2 for fuel on?
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18% N2
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Starter cutout?
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51% N2
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Pullout starter by?
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55% N2
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Motor engine to <?
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190°C
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AC pack off by (if disag)?
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20% N2
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Min air press start APU?
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20 psi
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Crossbleed?
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25 psi
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External Air?
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30 psi
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Donor engine for crossbleed?
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70 - 75% N2
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APU starter __ min on/__ min off
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APU starter 1 min on/5 min off
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Eng starter __ starts w/o cooling
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Eng starter 2 starts w/o cooling
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Lndg gear __ landings; __ down, __ up
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Lndg gear 4 landings; 10 down, 20 up
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Min Brake Pressure
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1,000 psi
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Brake Temp Caution
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650°C
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Max Brake Temp
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750°C
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Alt brakes in use
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<2500 psi
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Max Temp for SAAF
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150°C
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Normal quantities
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7, 11, 7, 7
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Min Hyd Temp (TO)
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7°C
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Normal Hydraulic Pressure
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4000 psi
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Max Hydraulic Pressure
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4200 psi
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Aux Hydraulic Pump Output
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3850 psi
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Prim/Sec Low (hydraulics)
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3400 psi
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Aux Pump Low (hydraulic)
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2200 psi
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Max Cabin Diff Press
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7.8 psi
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Crew Oxy Pressure
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285-430 psi
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Crew Oxy Quantity
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25 liters
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Troop quantity
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75 liters x 2
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Airevac min Oxy quantity
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100 liters
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“CREW OXY LOW”
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5 liters 60±5
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“OXY QTY LOW”
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7.5 ltrs 60±5
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Lineup dist static TO
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RWY -250 ft
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Standing/Rolling TO
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RWY -350 ft
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RCR dry runway
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23
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RCR wet runway
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11
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RCR icy runway
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5
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RSC snowy runway
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0.5
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3 eng climb schedule
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250 to 270/.66
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Bailout A/S min alt
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135/2,000 agl
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KCAS loss of all gen
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250 KCAS
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Min A/S airstart
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250/10% N2
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Min Starter Assist
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180/10% N2
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Max EGT airstart
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655° C
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Two eng approach
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Flaps ½ ind 0/8°
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Min alt for autopilot on
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200 agl
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Min alt for autopilot off
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DH/MDA
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Min runway length
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3500 ft
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Min runway width
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90 ft
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Min taxiway
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50 ft
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Min star turn width
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90 ft
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Min turn radius
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116 ft
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Norm turn radius
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143 ft
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Max Crosswind
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30 knots
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Max Headwind
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40 knots
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Max Tailwind
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10 knots
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Max Crosswind T &G
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25 knots
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Min RVR Operational TO
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1000 ft
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Min RVR Training TO
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1600 ft
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Min RVR Cat II ll.,S
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1200 ft
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Mins w/o full flight inst
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300/¾/40
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RZ speed> 3 NM
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340 kts
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RZ speed 2-3 NM
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310 kts
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RZ speed 1 NM
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AR +20
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RZ speed ½ NM
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AR +10
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AR speed KC-10
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285 kts
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AR speed KC-135
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265 kts
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Max AR speed
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310 kts
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Min AR speed
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Vmma
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Breakaway
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Idle/SB
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MINIMUM RUNWAY LENGTH
Take Off - ___ |
CFL
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MINIMUM RUNWAY LENGTH
¾ Flap Land - ___________________ |
Computed Landing Distance(IDLE REV)
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MINIMUM RUNWAY LENGTH
Full Flap Landing – _______________ |
Computed Ground Roll (MAX REV) Plus 500’
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TACTICAL
Tac Descent AS |
320/.80
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TACTICAL
Min alt Tac Descent |
5,000 ft agl
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TACTICAL
Level off initiated |
2,000 ft above
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TACTICAL
Min FOM<MSA |
5
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TACTICAL
Min ceiling/vis VR route |
3,000 ft/5 mi
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Min fuel combat offload
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1,000 ft
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Rec combat offload lngth
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1,500 ft
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Min fuel combat offload
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30,000 lbs
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FPV @ TD on SAAF
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-1.5° → 2.0°
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No DLC <300 ft
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400k/15 kt x-wind
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Cold WX procedures
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< 0° C
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Stop start if no N1 by
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30% N2
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Ground ice shedding
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50% N1/15 min
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A/PDMC
ABC ABU |
A/PDMC Aircraft/Propulsion Data Management Computer
ABC Antiskid/Brake Temperature Computer ABU Analog Backup Unit (Flaps) |
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ADC
AFCS AFCSCP |
ADC Air Data Computer
AFCS Automatic Flight Control System AFCSCP Automatic Flight Control System Control Panel |
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AGS
ANVIS API |
AGS Automatic Ground Spoilers
ANVIS Aviator’s Night Vision Imaging System API Approach Path Indicator |
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BATH
BIT BTMS |
BATH Best Available True Heading
BIT Built In Test BTMS Brake Temperature Monitor System |
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Instructions or procedures prefaced by the word ________ are mandatory.
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shall
Ref: TO 1C-17A-1 [Pg.IV] |
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The C-17A max design zero fuel weight is _________.
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447,400
Ref: TO 1C-17A-1 [Para.1-8] |
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To override the #2 and #3 hydraulic aux. pumps for an auto shutdown due to low quantity or overheat, _________.
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Press and hold appropriate Aux pump switch for 5 seconds.
Ref: TO 1C-17A-1 [Fig.1-154 S2] |
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An automatic shut down override switchlight provides a means to override all APU ECU automatic shutdown signals except _________.
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over temperature
Ref: TO 1C-17A-1 [Para.1-160] |
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When the APU alert start feature is used, there will be no _______ until the battery bus is powered.
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fire detection or protection
Ref: TO 1C-17A-1 [Para.1-178(C)] |
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When the warning horn makes the tone of a squeal it indicates what warning situation?
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APU Fire Warning
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The maximum payload weight for a C-17 is ________ pounds.
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170,900
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For specific aircraft, Maximum Payload is Zero Fuel Weight minus Operating Weight
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True
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When any engine is operating in the N2 mode, pilots should monitor N2 RPM when moving the throttle to prevent
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Possible overboost
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____ thrust is the recommended rating for engine out climbs
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INT
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Which thrust rating is recommended for normal climb?
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MCT
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DRT will be less than MAX and equal to or greater than
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MCT
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The THRUST LOSS warning will extinguish when the ______ is reset
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MASTER CAUTION
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If an ENGINE STABILITY X message on the WAP is illuminated, throttle movement should be slow and deliberate to prevent possible
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Engine surge or stall
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In the event of boost pump failure, fuel can be suction fed by the engine driven fuel pump at ____ thrust rating up to an altitude of ____ ft and at a pitch angle no greater than 21.5 degrees
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MAX; 10,000
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When the start sequence is initiated, ignition is energized when the associated
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ENG SHUT OFF selector is turned on
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