Walk Around Flashcards by Brian Nicosia

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TAT Probe

An aspirated TAT Probe delivers an accurate temp measurement on the ground w/APU running.

Check for damage

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Pitot Tube and AOA

Check for damage

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Nose Radome

All covers must be removed by MX before flight

The radome is normaly closed, no servicing required.

Ensure Conductor straps are secure

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Lower Nose Compartment Access Door

Ensure closed.

Normally closed, no servicing required. Secured w/latch.

This compartment is pressurized and contains flight control cables, PSEU module, etc.

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Nose Gear Taxi Light

Nose gear strut not compressed (some chrome visible)
Tire inflation and wear
Wheels
Condition of nose gear doors

Downlock Pin removed before flight

Taxi light clean & not cracked

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Nose Wheel Well

Downlock Pin locaton

Nose wheel steering lockout pin location

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Nose Wheel Snubbers

Snubbers stop nose wheel rotation after takeoff.

Check that snubbers are in place.

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Ground Call Horn

GRD CALL switch pressed
On the ground, a battery drain condition exists
On the ground, an E&E bay over temperature condition exists

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Nose Wheel Well

Down Lock Sensor

Nose wheel strut servicing placard

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Nose Wheel Well

Lock actuator

Gas charging (Schrader valve)

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Nose Wheel Well

Rudder pedal cables to steering actuators

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Nose Wheel Well

Oil charging valve

Air/Ground system sensors (2)

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Nose Wheel Steering Bypass Mechanism

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Tow Bar Limit Stripe

Red stripe indicates the tow bar limit for the ground crew during pushback

Tire inflation valve

Over-pressure relief valve

Only Nitrogren is used for inflation

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Ground Crew Towing Instructions

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2 sliding window exterior emergency exit access handle

Emergency Exit Access Handle

Only the FO side can be opened from the outside

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External Power Receptacle

Flight Interphone

Service Interphone

Ground Power Connected Light

Nose Wheelwell Light Switch

Pilot Call Switch

Service Not in Use Light (illuminated when Ext Power is connected but not in use)

Six-pin Ext Power Receptacle

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E & E Bay Access Door

Electronics and Equipment Bay access door (ensure closed)

Inside the E&E compartment

TCAS antenna; Check antennas for damage

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Forward Fuselage

Crew Oxygen disc (Green); Check to ensure in place; If missing, the system may be been over-pressurized

Moisture drain plugs

Transponder antenna

Radio Altimeter antennas (4)

Overboard exhaust valve port; exhaust air should be felt on the ground

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Forward Fuselage

RVSM critical area markings; no fuselage deformations

Static Ports; clear & unobstructed

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Forward Cargo Door

To open from exterior, rotate handle counter-clockwise; door swings open, upward inward

Dings & dents that have been logged are noted by a sticker; if there is no sticker, make a logbook entry & contact MX

Alternate Static Port; check that it is clear & unobstructed

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Forward Cargo Compartment

Door close, soft-grip bungee lanyard

Aircraft Main Battery/Batteries

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Ram Air Inlet

Ram Air Door

Ram Air Deflector Door; ensure extended & pack inlet is clear & unobstructed

Forward gray water drain mast; check for damage

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Ground Conditioned Air Connector

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Ground Pneumatic Air Connector ## Footnote Ground Pneumatic Connector access door (3 snap latches) Right inboard landing light; clear & not cracked

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Leading Edge (Krueger) Flaps ## Footnote Fixed Landing Light and Runway Turnoff Light; clear & not cracked Leading Edge Flaps; check condition The "fin," or strake on the engine nacelle, improves airflow over the wing

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Leading Edge (Krueger) Flaps Extended ## Footnote Krueger Flaps (2 segments) Hydraulic actuator rod Hot air duct

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Type III Overwing Exits ## Footnote There are two Overwing Exit Doors (Plug Type) on each side. The Type III Overwing Exits have been _deactivated_ and are _not available_ for use.

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Number 2 Engine - Left Cowl Area ## Footnote Starter override access hole; requires pneumatic air to prevent damage Hazard area Access dooor left side of #2 engine

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Chip Detector Underside of engine Three detectors: * Forward sump * Aft sump * Accessory gear box

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Number 2 Engine ## Footnote Total Inlet Temp Sensor for EEC Check condition of exterior surfaces, spinner, fan blades Engine intake should be unobstructed. Ensure all FOD has been removed. Check all access panels are latched.

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Number 2 Engine - Right Cowl Area Engine Oil Compartment Ensure access panels are latched Engine oil access door Note engine hazard areas * 14 ft radius around inlet * 4-5 ft behind cowl * 45-degree entry/exit corridor

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Electronic Engine Control (EEC) ## Footnote The EEC is shown here for informational purposes and is not checked during the preflight

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Thrust Reverser Sleeves ## Footnote Thrust Reverser deployed The black stripes confirm sleeves aligned. WARNING: Activation of the thrust reversers on the ground w/o suitable precautions is dangerous to ground personnel.

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Engine Tail Cone ## Footnote Check for leaks or pooling fluids. A large puddle of oil can cause heavy smoke, especially if there is a tailpipe fire.

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Right Wing Leading Edge ## Footnote Check the condition of the wing surfaces. There are 4 leading edge slats, but only the _3 inboard_ slats receive wing anti-ice protection

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Wing - Dripless Measuring Fluid Sitck ## Footnote 16 total; 6 each main tank; 4 center tank Magnetic float stops, indicates graduated linear unit Use inclinometers in wheel well (pitch/roll) Determine fuel "height" at each station. Note: locked position. Check they are all in the locked position before departure. Sump Drain: Lowest part of the tank. Push up on center of valve to check for contamination.

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Right Wing Leading Edge - Outboard of Engine Wing Anti-Ice Exhaust Defueling access door; pull down to open valve Pump fuel out of any tank using X-Feed valve & boost pumps Door won't close unless handle is in proper (closed) position Refueling station access door; outboard of the engine w/4 latches Blue valve position lights, "open" position valve has power.

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Fuel Tank Vent ## Footnote Fuel Tank pressure relief Fuel Tank vent Check that the vent is not blocked

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Right Wing Flap Components ## Footnote Flight Spoliers Ground Spoilers (inboard & outboard on wing) TE flaps 1-15 increased lift; 15-40 increased lift & drag 15, 30, 40 normal landing positions Check that all wing surfaces are stowed; check the ailerons and flaps

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Right Wing Tip ## Footnote Check condition of wing and winglet. Check the position lights: illuminated & not cracked On aircraft w/2 position lights in each spot (2 green) _both_ should be illuminated Check static wicks

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Right Wing Tip ## Footnote Check condition of wing and winglet. Check the position lights: illuminated & not cracked On aircraft w/2 position lights in each spot (2 green) both should be illuminated Check static wicks

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Wing Tip - Scimitar Winglets ## Footnote Check condition of both upper & lower winglet Check the position lights: illuminated & not cracked On aircraft w/2 position lights in each spot (2 red) both should be illuminated Check static wicks

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Main Landing Gear Strut - Lower Section ## Footnote Gas Chargine Valve Brake Wear Indicators; must be more than flush w/the guide. NOTE: Check w/parking brake applied Check brake for leaks Check strut compression (ensure some chrome shows) Brake assembly retention cable

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Main Landing Gear Strut ## Footnote The Main Gear strut is shown fully compressed in this picture. Contact MX

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Main Landing Gear Downlock ## Footnote Downlock sensors and targets (2) Main gear downlock pin (normally removed); must be removed before departure Main gear door

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Main Gear Tire Shred Impact Fitting ## Footnote Tire shred impact fitting (AKA frangible fitting) loose tread should break off the impact fitting and release all uplock fluid. A fuse will stop all hydraulic fluid from draining out.

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Main Gear Retracted ## Footnote Tire shred impact fitting This open area helps w/brake cooling after gear retraction

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Hydraulic System A Reservoir ## Footnote To Engine Driven Pump (EDP) To Electronic Motor-Driven Pump (EMDP)

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Main Wheel Well - Hydraulic System B Reservoir ## Footnote STBY reservoir fill System return line Head pressure on hydraulic reservoir

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Quantity Gauge and Transmitter ## Footnote NOTE: RFL- Refill

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# Fill Selector Valve Closed Port "B" Port "A"

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Single Point Hydraulic Servicing ## Footnote Manual pump handle Suction hose Pressure fill connection

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Hydraulic Pumps ## Footnote Electric motor driven hydraulic pump A Electric motor driven hydraulic pump B Landing gear transfer unit PTU control valve Power Transfer Unit (PTU) Thrust reverser module

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Standby Hydraulic System Reservoir ## Footnote From system B fill line Servicing line To Standby Electric Motor Driven Pump (EMDP)

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Flap Components ## Footnote Flap bypass valve Flap Drive Unit Right Normal antiskid valves

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Flap Components ## Footnote Hydraulic flap drive motor Electric flap drive motor Trailing edge flap torque tube

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Main Wheel Well - APU Fire Detection ## Footnote Fire warning horn Extinguisher switch Fire handle Fire light Check that the APU Fire Control handle is up. Saftey wires are used to prevent inadvertent movement.

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Brake Accumulator ## Footnote Accumulator placard Brake accumulator servicing port

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Brake Accumulator ## Footnote Servicing port Pressure guage Fully charged 6 full brake applications / 8 hr parking brake Pre-charge: 1000 psi (gas) Pressurized by System B Pressure relief valve opens at \>3500 psi

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Right Aft Wing Body Fairing ## Footnote Brake accumulator Standby hydraulic pump

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Mid-Body Lower Fuselage and Sump Drain ## Footnote Pack ram air outlets Marker beacon antenna Anti-Collision Light; not damaged or cracked DME antenna Center tank sump drain access door

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Aft Cargo Door ## Footnote Operation is the same as the FWD cargo door

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Aft Cargo Compartment ## Footnote Fire/Smoke detector Cargo compartment light Cargo fire spray nozzle Vacuum wast disposal enclosure access door

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Aft Entry/Service Doors ## Footnote The aft entry/service doors are deactivated and not available for use.

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Outflow Valve and Pressure Relief Valves ## Footnote Negative Pressure Relief Valve; check closed & unobstructed Two (2) Positive Pressure Relief Valves; either side of outflow valve Outflow valve (full open); check that it is not blocked

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APU Door ## Footnote The strake is designed to break up the air boundary layer at higher altitudes to guarantee air flow to the APU if in operation.

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Tail ## Footnote Static Wicks; reference DDG's CDL if any are missing Elevator Pitot Probe; covers removed; supplies inputs to Elevator feel computer Tail Skid Check condition of Vertical & Horizontal Stabilizers, and Rudder

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Tail Skid ## Footnote Warning decal green / red; check for damage & compression Tail Strike Pitch Attitude 11-degrees

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APU Access Door ## Footnote Hold open rods APU fire detector Three over-center latches

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Section 48 Access and Blowout Door ## Footnote Normally closed; latch spring loaded; protects aft pressure bulkhead Access to Stabilizer jack screw & APU fire bottle

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APU ## Footnote Strobe Light Eductor inlet duct for ground operation APU exhaust duct

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Section 48 ## Footnote Stab trim actuator Behind the pressure bulkhead

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APU Shroud and Hydraulic Drain Mast ## Footnote Top Hole: exit port for fuel if APU fuel line leaks Botom Hole: hydraulic fluid overservicing exit port Unheated mast

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Left Main Gear Wheel Well ## Footnote Main gear strut servicng placard Pitch/roll inclinometers

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Left Main Gear Wheel Well ## Footnote Engine fire extinguisher bottles (2) Left normal main gear antiskid valves

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Engine Fire Bottles ## Footnote Pressure / quantity guages

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Main Deck Cargo Door Panel ## Footnote If flight crew operates MDCD, follow FCOM Supplementary Procedures. CAUTION: Do not operate the entry or cargo doors w/winds of more than 40 knots. Strong winds can cause damage to the structure of the airplane.

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Main Deck Cargo Door (MDCD) - Closed ## Footnote When closed, the MDCD should be flush w/fuselage Vent Door; prevents pressurization to unsafe level Viewing Ports; confirm MDCD locked w/veiwing ports, complete yellow circles

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Main Deck Cargo Door (MDCD) - Canopy Position Canopy Position * Approx 88 degrees * Lift actuator interna ram lock will hold the door in the canopy position WARNING: Do not leave MDCD open in canopy position unattended when using a hydraulic ground cart. The MDCD should be lowered to the close position prior to leaving the aircraft unattended.

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Main Deck Cargo Door (MDCD) - Open Position

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Oxygen Masks ## Footnote Flow indicator; yellow cross indicates flow TEST/RESET switch Inflation levers Regulator; 100% normal setting for dispatch OXY ON flag indicates oxygen is on

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Halon Fire Extinguisher Pin in place Tamper strap not broken Guage shows proper charge (green range) Bracket is secure All fire types, most effective on B, C, and D * A - Wood, Cloth, Paper * B - Flamable Liquids * C - Electrical * D - Metal * E - Radioactive

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Crash Axe ## Footnote Secured in place Cover is in place Access through interior panels and cosmetic walls. Should not be used on the aircraft skin itself.

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Under Observer's Seat & Behind Captain's Seat ## Footnote Smoke Goggles Gloves Fire Containment Bag Life Raft Protective Breathing Equipment (PBE)

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Fire Containment Bag ## Footnote Package is sealed & contains gloves & fire containment bag

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Life Raft ## Footnote The inflation lanyard cover is in place

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Protective Breathing Equipment (PBE) ## Footnote PBE w/humidity indicator; ensure white or blue; pink contact MX for replacement PBE w/o humidity indicator; package is sealed & tamper strap not broken

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Smoke Goggles ## Footnote Lens; check for dents, scratches, separation, or other damage Strap; check for elasticity Located near each pilot/observer seat. May not be installed on aircraft with full face oxygen masks

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Gloves ## Footnote Stowed next to Captain's seat Used for protection when lifting hot items _Do not pick up an item unless safe to do so!_

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Life Vests ## Footnote Stowed in pouches behind each pilot seat; 2 vests per pouch Check condition & seal Never inflate inside the aircraft. Don at first indication they may need to ditch.

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Flashlights ## Footnote Next to each pilot seat. Battery indicator light flashes every 3-4 seconds. Flashlight auto-illuminates when removed from stowage bracket & extinguishes when placed back. Batteries cannot be recharged.

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Escape Straps ## Footnote Stowed in compartments above each pilot seat. Used to egress through #2 window; ensure rope is secured to airplane prior to egress

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Left Forward Entry Door ## Footnote Girt Warning Flag Single lever easy action Slide bottle pressure guage; check pressure Slide housing w/girt bar at the bottom Girt Warning Flag Warning Position Maximum wind for operating the entry/service door is 40 knots.

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Escape Slides ## Footnote If the slide fails to auto inflate, use manual inflation handle. If it still does not inflate, the slide is not usable.

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Forward Supernumerary Seats No Smoking Light Attendant Panel: * Potable Water Level * Waste Tank Level * Ground Service Power Switch * Sumernumerary Cabin Lights Oxygen Masks near each seat Handset for Communication Compartments under each seat

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Supernumerary Oxygen ## Footnote PTT switch to communicate w/flight deck Inflation levers; squeeze to inflate mask harness Normal/100% switch set to 100% for dispatch

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Supernumerary Seat Compartment Contains: * Flashlight * Smoke Goggles * Life Vest * Fire Bane * Demo Kit

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Rigid Cargo Barrier ## Footnote Main Deck Cargo Door (MDCD) Panel Flight Crew/Supernumerary Oxygen Cylinders Main Deck Cargo Compartment Hatch

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Protective Breathing Equipment (PBE) ## Footnote Two (2) PBEs w/humidity indicators mounted to rigid cargo barrier

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Life Rafts Two (2) life rafts are installed in the supernumerary cabin: * One is located on the rigid cargo barrier * One is located in the galley area Check: * Pressure (if visible) * Lanyard cover in place

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Portable Oxygen Bottles On/Off Valve; ensure set to OFF Demand Regulator Cover Safety Strap Continuous Flow Outlets: * HI = 4 liters/min * LO = 2 liters/min Guage; ensure full Any time the main deck cargo compartment is accessed in flight, an oxygen bottle & mask must be carried.

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Protective Gloves ## Footnote One pair of protective gloves is mounted on the rigid cargo barrier. Check the condition of the gloves and that they are secure.

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Halon Fire Extinguishers ## Footnote Two (2) Halon Fire Extinguishers are mounted on the rigid cargo barrier. Preflight items are same as the fire extinguishers on the flight deck.

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First Aid Kit One is mounted on the rigid cargo barrier Ensure the tamper strap is in place and the kit is sealed If something is used, a logbook entry is required. First Aid Kit contains: * List of contents * Gauzes * Bandages * Other first aid supplies

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Flight Crew and Supernumerary Oxygen Cylinders ## Footnote Oxygen pressure is read by the crew on the gauge on the aft overhead panel in the flight deck. Use FCOM Vol 1 charts to determine if oxygen pressure is sufficient for dispatch.

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Forward Galley ## Footnote Galley Light and Power Switches Coffee Maker Storage Containers; ensure secured for taxi, takeoff, and landing Work area; loose items secured for taxi, takeoff, turbulence, and landing Waste Container Loose items cannot be stored in area between raft and vent panel Vent Panel

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Portable ELT

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9G Bulkhead

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Main Deck Cargo Compartment Alerting Horns * Activated either auto or manually * Occupants don oxygen masks & return to seats Cargo Positions Lights * Flash when alerting system is activated

Walk Around Flashcards

(112 cards)