ㆍAIRCRAFT DIMENTIONS
- LENGTH 146FT, WIDTH 117.5FT, HEIGHT 38FT 7INCH
ㆍPACK FLOW CONTROL
- ON GROUND WITH BOTH ENGINES RUNNING, THE NORMAL FLOW IS LIMITED TO 90% + E/WD PACKS DISPLAYS
ㆍHYDRAULIC RESERVOIR QUANTITY
ㆍENGINE START UP WIND LIMITATION
- CROSSWIND MAX 45KTS
ㆍCABIN ALERT SIGNAL
- CAB ALERT RESET → L1, L2, R2
ㆍENGINE STARTER
- 1 CYCLE 3 ATTEMPTS → WITH 60 SECONDS BETWEEN CYCLES
- AFTER 3 CYCLES → 15 MINS COOLING PERIOD IS REQUIRED
ㆍFADEC PROTECTION
- CEO: HOT START, HUNG START, STALL, FAILED LIGHT UP, LOW START AIR PRESSURE, THRUST LEVER NOT AT IDLE
- NEO: HOT START, STALL, FAILED LIGHT UP, LOW START AIR PRESSURE, THRUST LEVER NOT AT IDLE
- NEO ONLY: EGT OVERLIMIT, FAILED BOWED ROTOR PROTECTION, START SHAFT SHEAR
ㆍRCDR
- EXT PWR ↔ APU GEN로 전환시 RCDR GND CTL이 AUTO가 되므로 RCDR GND CTL ON 확인
ㆍANTI-ICE (EDTO)
- AFTER START → ENG 1 & 2 ANTI-ICE PB ON → 20SECONDS, NO ECAM CHECK → OFF
ㆍTHRUST SETTING AND EGT LIMITS
- CEO: TOGA 635ºC (10MINS, 5MINS), MCT 610ºC, STARTING 635ºC
- NEO: TOGA 1,060ºC (10MINS, 5MINS), MCT 1,025ºC, STARTING 750ºC ON GND, 875º IN FLT
- NEO: MAX SHAFT SPEED N1 101%, N2 116.5%
ㆍBACKUP SPD/ALT
- AIRSPEED INDIACTORS를 신뢰할 수 없으면 → BUSS가 AIRSPEED를 표시, GPS ALT가 고도를 표시함
- BUSS는 NORMAL SPD/ALT INDICATOR로 전환 가능함
- CPT와 F/O 각각 BKUP SPD/ALT PB를 눌러 전환할 수 있으며 각각 독립적으로 작동됨
- BUSS는 AOA + SLAT/FLAP CONFIGURATION를 기반으로 작동됨
- BKUP SPD/ALT가 작동되면 ECAM E/WD에 표시됨
- 만약 한 쪽에서만 BUSS를 작동시키고 AP/FD를 ENGAGE하면 NAV BKUP SPD/ALT ON CAPT(F/O) PFD가 표시됨
ㆍTAXI FUEL CONSUMPTION
- 24LBS/MIN
ㆍOANS (ON-BOARD AIRPORT NAVIATION SYSTEM)
- TAXI → PF & PM DISPLAYS
- TAKEOFF → PM DISPLAY ONLY
- ROLLOUT AFTER TOUCHDOWN → ON PM DISPLAY, ON PF DISPLAY AT TAXI SPEED
ㆍTAILWIND & CROSSWIND TAKEOFF (ABV 20KTS)
- SIDESTICK FULL FORWARD
- SET N1 50% → RELEASE BRAKES → SET N1 70% → GS >15KTS → SET FLX OR TOGA
ㆍWEATHER RADAR
- TAXI → ON DURING TAXI (30SECONDS FOR 3D BUFFER)
- TAKEOFF → ALL WX
- IN FLIGHT → ALL WX (PF 80NM, PM 160NM), PATH WX & ELEVN FOR STORM CELL ANALYSIS
ㆍAUTOMATIC FLAP RETRACTION (ARS)
- CEO: CONF 1+F 215KTS → AUTO FLAP RETRACTION → 230KTS
- NEO: CONF 1+F 225KTS → AUTO FLAP RETRACTION → 243KTS
ㆍEXPEDITE CLIMB
- GREEN DOT SPEED로 CLIMB (FL250 이상에서 EXPEDITE CLIMB은 속도가 너무 낮아 효율성이 떨어짐)
- MACH 0.8 또는 340KTS로 DESCEND (MANAGED SPEED)
ㆍAP/FD TCAS
- AP ON 상태에서는 자동으로 ENGAGE, AP OFF 상태에서는 FD로 MANUAL GUIDANCE 됨
- A/THR DISCONNECTED → THR LEVER 위치에 따라 자동으로 ARM OR ACTIVE 됨
- CLEAR OF CONFLICT 이후에는 AP/FD TCAS가 V/S MODE로 전환되거나 ALTITUDE ACQUIRE 또는 ALTITUDE HOLD MODE로 전환됨
ㆍAP/FD TCAS RA
- AP ON & FD ON → VERTICAL MODE가 TCAS MODE로 바뀌고, TCAS GUIDANCE를 따라감
- AP OFF & FD ON → 새로운 FD GUIDANCE로 전환되고, FD PITCH BAR가 상승이나 하강 등을 지시함
- AP OFF & FD OFF → TCAS MODE GUIDE와 함께 FD BAR가 자동으로 다시 나타남
ㆍAUTO LANDING LIMITATION
- G/S ANGLE -2.5º ~ -3.25º, APRT ELEV 9,200FT AT OR BELOW, NOT BELOW -2,000FT PRESSURE ALT, WGT AT OR ABOVE 115,743LBS
ㆍSOFT GO-AROUND
- BOTH ENGINES OPERATIVE + SLATS/FLAPS EXTENDED + BELOW GO-AROUND THRUST REDICTION ALTITUDE + BELOW FL160
- SET TOGA THEN FLX/MCT
- SOFT GO-AROUND가 불가능한 경우 → ENG GA SOFT FAULT 경고 → TOGA로 GO-AROUND 사용
ㆍFLARE MODE
- CEO: 50FT RA 통과시 → THS FROZEN, FLARE MODE로 변경됨 → 30FT RA에서 8초 동안 PITCH를 -2º NOSE DOWN
- NEO: 100FT RA 통과시 → THS IS FROZEN, FLARE MODE로 변경됨 (WITH DAMPING FEEDBACK)
ㆍROW/ROP (RUNWAY OVERRUNPREVENTION SYSTEM)
- 왼쪽부터 400FT 미만 (NO AURAL), 400FT 미만 (200FT에서 AURAL TRIGGER, GO-AROUND), ROP (30KTS 미만까지)
- DRY 또는 WET RUNWAY에서 활주로의 OVERRUN 가능성을 경고함
- 2,000FT부터 DECTECTION 시작
- ROW (RUNWAY OVERRUN WARNING) → 400FT AGL에서 BRAKING을 시작할 때까지 자동으로 작동함
- ROP (RUNWAY OVERRUN PROTECTION) → BRAKING을 시작한 후, 항공기가 정지할 때까지 30KTS 미만으로 감속되면 INHIBIT 됨
- ROPS INHIBITED WHEN THE AIRCRAFT IS LESS THEN 15NM FROM THE AIRFIELD
ㆍAUTO BRAKE ON FMA
- AUTO BRK LOW, MED, MAX DISPLAYS ON FMA
ㆍENGINE COOLING DOWN
- 착륙 후 3분이 지난 뒤에 ENGINE SHUTDOWN 실시