CPaT Flashcards
Short field performance package loaded in FMC
FMC IDENT page
737-800W.1
W = winglets
1 or 2 = number of positions of tail skid
Flap load relief settings
Normal trailing edge flap load relief for 30 and 40 - flaps auto retract to prevent overspeed
SFP provides additional flap load relief settings for 10, 15, and 20
Engine idle thrust delay time
Normal: 5 seconds
SFP: 2 seconds
Nose to nose gear distance
13’ 2”
(Pilot seat to nose gear 5.25’)
-800 length
129’ 6” - due to increased fuselage length, 800s are equipped with a tail skid
-800 takeoff weight
174200lbs max
Landing 146300
-800 emergency exits
8 total
2 overwing each side - no slides
FA stations/control panels
Fwd: controls for cabin lights and IFE, handset and mic for PA Zane service interphone
Aft: controls for work lights and entry lights, emergency exit light switch, water quantity and waste system display, handset and mic
Galley power switch in flight deck
Fwd and aft cargo
647cu ft; 883cu ft
Pressurized, not ventilated
Retrac wing landing lights
No Boeing speed limit
Avelo 250kts
Nosegear taxi light
Turns with steering
Light control knobs
Overhead panel:
Dome lights (aft cockpit) - operate from batt bus
Circuit breaker - flood lighting on P6 and P18 panels
Panel - fwd and aft overhead integral panel lighting
Aft electronics panel:
Panel - fwd and aft elec integral panel lighting
Flood - spotlight on throttle quadrant
Front/center:
Background - fluorescent flood lighting on instruments
AFDS flood - afds control panel (MCP)
Panel - CA’s for CA, center instrument, mcp edge lighting; FO’s for FO
Magnetic compass - powered by batt bus
Side panel - map and chart spotlights
Batt bus powered lights (operating on standby power)
Fire warning & master caution
Stby compass
Dome lights
Instrument flood lights
Fasten Seatbelt sign in auto
Illuminates if either the landing gear or flaps are extended
External power connected to an otherwise cold aircraft
Entry and lavatory lights automatically illuminate
Emergency exit lights
Powered by individual Ni-Cad batteries, charged by DC bus 1 (even if switch is off, if power is available)
Aisle path lighting; overhead, ceiling, stowage bin bullnose, overwing lights; inflatable slide lighting
Emergency exit lights armed
Batteries all charged by DC bus 1. If this bus fails, or if the AC power used to generate this DC bus power is off, the lights automatically come on.
Batteries last about 20min
Flight crew oxygen
Bottle in E&E compartment
Oxygen blowout disc
Pressure indicator - batt switch on for gauge to display pressure
Oxygen mask
Right lever inflates harness
Left cover door - mask mic auto
Oxygen shut off - close doors then push and release reset/test lever
Re-initiate oxygen flow - open left stowage door
Observer mask - oxygen available when crew shutoff valve is opened
PSU doors
Auto open - 14000 cabin alt; PASS OXY ON
Oxygen generating canister (chemical) - pull mask to pull lanyard; lasts ~12 minutes
Girt bar
Down on floor to arm
FO side window
Can be opened from outside
Potable water tank
Below cabin floor, behind aft cargo.
Pneumatic system normally pressurizes tank, however AC motor driven compressor auto activates if pressure low
Waste tank - two quantity level sensors
Lavatory water and valves
Water shutoff valve - on, faucet only, toilet only, off
Combination of rinse water and differential pressure (vacuum blower below 16000’) is used to flush
Flush valve close handle - bottom of toilet assembly through shroud cutout
