CPaT Flashcards

1
Q

Short field performance package loaded in FMC

A

FMC IDENT page
737-800W.1
W = winglets
1 or 2 = number of positions of tail skid

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2
Q

Flap load relief settings

A

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

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3
Q

Engine idle thrust delay time

A

Normal: 5 seconds
SFP: 2 seconds

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4
Q

Nose to nose gear distance

A

13’ 2”
(Pilot seat to nose gear 5.25’)

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5
Q

-800 length

A

129’ 6” - due to increased fuselage length, 800s are equipped with a tail skid

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6
Q

-800 takeoff weight

A

174200lbs max
Landing 146300

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7
Q

-800 emergency exits

A

8 total
2 overwing each side - no slides

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8
Q

FA stations/control panels

A

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

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9
Q

Fwd and aft cargo

A

647cu ft; 883cu ft
Pressurized, not ventilated

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10
Q

Retrac wing landing lights

A

No Boeing speed limit
Avelo 250kts

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11
Q

Nosegear taxi light

A

Turns with steering

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12
Q

Light control knobs

A

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

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13
Q

Batt bus powered lights (operating on standby power)

A

Fire warning & master caution
Stby compass
Dome lights
Instrument flood lights

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14
Q

Fasten Seatbelt sign in auto

A

Illuminates if either the landing gear or flaps are extended

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15
Q

External power connected to an otherwise cold aircraft

A

Entry and lavatory lights automatically illuminate

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16
Q

Emergency exit lights

A

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

17
Q

Emergency exit lights armed

A

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

18
Q

Flight crew oxygen

A

Bottle in E&E compartment
Oxygen blowout disc
Pressure indicator - batt switch on for gauge to display pressure

19
Q

Oxygen mask

A

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

20
Q

PSU doors

A

Auto open - 14000 cabin alt; PASS OXY ON
Oxygen generating canister (chemical) - pull mask to pull lanyard; lasts ~12 minutes

21
Q

Girt bar

A

Down on floor to arm

22
Q

FO side window

A

Can be opened from outside

23
Q

Potable water tank

A

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

24
Q

Lavatory water and valves

A

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

25
Q

Water and waste service panels

A

Water - lower aft right side fuselage. When panel door is open, the compressor is disabled
Waste - lower aft slightly-left fuselage

26
Q
A