A 330 Facts

TRAINING PURPOSES ONLY (www.airbusdriver.net)

1. IMMEDIATE ACTIONS  then Engine-Out Unable To Maintain Altitude ENG Tailpipe Fire Evacuation NAV IR FAULT (-300 only) Red ATT Flag on PFD (-300 only) Smoke/Avionics Vent Smoke/Fumes or SMOKE AVNCS VENT SMOKE - OXYGEN   MASKS -VERIFY ON/100%/EMERG Unreliable Speed Indication/ADR Check

2. ECAM EXCEPTIONS  then AIR BLEED LO TEMP (Wing Anti-Ice OFF) ENG ALL ENG FLAME OUT FUEL (L or R) WING TK LO LVL NAV ADR (1+2, 2+3, 1+3,1+2+3) FAULT (-300 only) SMOKE (FWD or AFT/BULK) CARGO SMOKE (With Cargo Door Open)

3. ECAM  then 4. ECAM Follow-up (QRH yellow pages) then 5. ECAM supplement supplement (blue (blue book) ALTITUDES  Max  41,000'  Max Flapand/or Slat extension  20,000'  Max gear extension  21,000' APU (25,000' with Jet B or JP4) 41,000' APU bleed operation 22,500' A/P  on (T/O) & G/A 100' AGL (with SRS) on (Enroute) 500' off (APPR) DA/DDA/MDA (non-pre c.) off (APPR) 160' AGL (CAT I ILS 80' with Cat 2, Cat 3 Single, or Cat 3 Dual on FMA) Takeoff & Landing -2,000' to 12,500'  RVSM (>FL290) PFD 1&2 + 200' (+20' ground), +75' ISIS +60' with either PFD WIND Crosswind  (Guidance) Braking “fair/medium” “poor”  Autoland  ( Headwind  Headwind 35 K ) CAT II/IIIa/IIIb Tailwind  (Guidance) Braking “less than good” WEIGHTS Taxi T/O Landing ZFW Minimum (autoland)

 29/G32 K  15 K 10 K  20 K  15 K  10 K  5K

-200 515,656 513,600 401,200 374,782 255,733 (271,200)

-300 515,656 513,600 412,200 385,805 266,757

SPEEDS - Max - Max (V  MO / M  MO  ) 330 / .86  Gear (Gravity Ext. 200) 250 / .55 Shutoff Hydraulics 280 Flaps (Max VFE) 1 240 1+F 215 2 196 ( PFD no amber =) 3 186 Full 180 Turbulence > 20,000' 260/.78 (.8 -200) < 20,000' 240 Holding < 6,000' 200 >6-14,000' 230(210 if published) >14,000' 265 [PANS table IV-1-2 IV-1-2 Holding 210/220/240] Taxi straight 30K, 90 o turn 10K Tire 204K Window/ Wiper Max 230 Max angle – green green dot. Max Rate 250/.78 Alternate descent 290/.76 high speed 320/.82

AB 330 FACT SHEET 1/6/2012  Italic print  Italic print denotes Chapter 2 memory item ELECTRICA L- GEN 90 KVA EMER GEN 5KVA ENGINES PW4168A RR TRENT 772B (-200) Thrust 68,000# 72,000# Do not reset tripped fuel boost pump /  pump / indicating indicating C/B TO/GA 5min(10-1ENG) 620 oC 900oC(920o20sec) No E&E compartment w/o dispatch/Mx direction o MCT continuous 600 C 850oC No electrical outlet use during T/O and landing o o Starting (air) 535 C(620 ) 700oC (850o) Battery OFF and 150 o and any brake is >600 o or 200o; or temp >900 o Alternate Brakes - no antiskid if on accumulators only Auto Brakes with normal normal brakes only. On when wet/slippery, wet/slippery, rollout limited, higher approach speeds, crosswind>10k, CAT II/III II/III.. DECEL at 80% rate B Alternate Brake Accumulators provide 7 full Applications or parking for 12 hours. Landing Gear red arrow- gear not locked down for landing (flaps 3 or full)

APU 3 Starter cycles then 60 minutes before 3 more ECAM LOW OIL LEVEL still allows 15 hours ops. APU bleed valve auto closes >25,000', opens40 sec 100K, 1.1 EPR, stabilize, 1.3 EPR, then TOGA or FLX After flap retract, 1+F not available until 38 oC/100oF Flaps 1on ground Thunderstorms T/O VLS+10 Contact Dispatch if not Jet A or A1 180o turn - 200’pavement width minimum Transfers (x11 factor) Inner to Engines always first Rest Audio - Level Level Adjust/Room(456 Adjust/Room(456 Enter)/-db (-200) Center to Inner Inner when Inner full full minus 4400 # (-200) (-200) Trim aft > FL255 LIGHTS Trim fwd: CG at aft target, Inner Inner 8800# (until 11000), Loss of normal electrics – Capt instrument panel, Center < FL245, < 35min to destination, emer elect (-200) i nstrument nstrument pane panell f lood, Li ghting,s ghti ng,standby tandby compa compass ss Outer to Inner at 7700# light, and right dome light, (provided the respective X Feed auto open in electrical emergence configuration control switch activated). Dispatch with any main fuel pump inop prohibited Logo on with main gear struts compressed or flaps 3/full Strobe on when shock absorber not compressed CONFIGURATION Range Width /Length/Height Cabin Emergency Lights on on DC Ess Bus. On if normal -200 20/238=258 6,700nm 60.3m/ 58.37m /17.3m electrics fail (AC Bus 1 fails) -300 30/263=293 4,900nm 60.3m/63.69m /16.83m Cabin lights on >11,300’ cabin altitude -300 (new) 28/263=291

INSTRUMENTS/NAVIGATION REJECTED TAKEOFF “PF”, PM CALLOUTS CAT II/III APPROACH “PF”, PM CALLOUTS OPEN DES prohibited inside FAF or < 1,000' AGL (>72K, spoilers auto extend, therefore autobraking) Initially – Waypoints sequenced, Activate & confirm NAV (Magnetic) 82o N to 60 o S (73 oN from 90-120 o W) Capt. - “Reject, My Aircraft”, thrust levers to idle, max approach phase, “Flaps 1”, FLAPS 1, “Flaps 2”, nd RMP only to tune VHF3 braking and max reverse until assured aircraft can stop FLAPS 2, cleared approach, select approach and 2 1 FD off, other must be off. Both off FPV recommended on runway, slight forward sidestick, “This is the A/P, “CAT 3 Dual or CAT 3 Single or CAT 2”, Auto Callouts 1000(or PM), 500( or PM), 100,50,30,10 COURSE ALIVE verify LOC *, G LIDESLOPE ALIVE, 1½ Captain, remain seated.” IRS tolerance preflight 7o), touchdown reversers, SPOILERS / NO SPOILERS, FLAPS UP, disarm spoilers, Green dot speed, select No external condition air with packs 2/1/ NO REVERSE, NO ROLLOUT, NO AUTO-BRAKES, 80, “Open Climb”, “Speed ___”(green dot), MCT, MCT Ram air inlet only with differential pressure < 1 psi idle rev, disc A/P>60 (at touchdown if no rollout) SET. G/A if no LAND GREEN